[list_settings.list_name] Current ISS TLEs @ 18:30 UTC

 
Date: October 5th 2020

  • spaceflight nasa gov will be taken offline by October 2020 *
  • Do you use any data hosted on this site? *
  • Please let us know how you use the data at the survey link below *
  • *
  • https://www surveymonkey com/r/KRLJMCN *
  • *

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 19920 769 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 431 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


277/01:16:14 000 0 0 0 0 0 0
N/A 0 0 0 0 229 8
000/00:00:00 000 0 0 0 0 222 7

277/05:58:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 8
000/00:00:00 000 0 0 0 0 222 5

279/10:05:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 8
000/00:00:00 000 0 0 0 0 222 6

280/09:58:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 7
000/00:00:00 000 0 0 0 0 222 6

281/08:14:31 819 -2 2 -2 4 2 4
N/A 0 8 0 2 228 3
000/00:07:03 639 0 1 -0 0 222 7

283/20:35:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 3
000/00:00:00 000 0 0 0 0 222 7

288/05:45:05 000 0 0 0 0 0 0
N/A 0 0 0 0 228 3
000/00:00:00 000 0 0 0 0 222 6

288/08:50:45 000 0 0 0 0 0 0
N/A 0 0 0 0 228 4
000/00:00:00 000 0 0 0 0 222 7

289/02:17:30 000 0 0 0 0 0 0
N/A 0 0 0 0 228 2
000/00:00:00 000 0 0 0 0 222 6

291/11:10:00 000 0 0 0 0 0 0
N/A 0 0 0 0 228 4
000/00:00:00 000 0 0 0 0 222 7

Coasting Arc #1 (Orbit 864)
---------------------------------------

Vector Time (GMT): 2020/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 922360
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2478315
35                 A    =         6794154
35  meter
 Y    =       -3828479
62  meter          E    =           
0007112
 Z    =        5031822
93                 I    =           51
64989
 XDOT =       7125
387748                 Wp   =          121
14153
 YDOT =      -2021
353075  meter/sec      RA   =          176
28421  deg
 ZDOT =       1965
848026                 TA   =          309
73316
                                          MA   =          309
79581
                                          Ha   =            229
853  n
mi
                                          Hp   =            222
583

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8130955
87                 X    =        -2459761
97
 Y    =      -12560628
66  feet           Y    =        -3856089
71  meter
 Z    =       16508605
41                 Z    =         5019829
52
 XDOT =      23377
256390                 XDOT =        7137
912465
 YDOT =      -6631
735809  feet/sec       YDOT =       -1941
601662  meter/sec
 ZDOT =       6449
632631                 ZDOT =        2000
491412

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10443809
36                 X    =         3183273
09
 Y    =       10799798
88  feet           Y    =         3291778
70  meter
 Z    =       16453178
37                 Z    =         5014928
77
 XDOT =     -20896
565503                 XDOT =       -6369
273165
 YDOT =      10109
754774  feet/sec       YDOT =        3081
453255  meter/sec
 ZDOT =       6609
677261                 ZDOT =        2014
629629


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20276
55192314  
00016717  00000-0  10270-3 0  9004
2 25544  51
6436 177
2276 0001220 106
8798 253
2485 15
48833362  8654


Satellite: ISS
Catalog Number: 25544
Epoch time:      20276
55192314   =   yrday
fracday
Element set:     900
Inclination:       51
6436  deg
RA of node:       177
2276  deg
Eccentricity:     
0001220     
Arg of perigee:   106
8798  deg
Mean anomaly:     253
2485  deg
Mean motion:   15
48833362  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             865
Checksum:              312


Coasting Arc #2 (Orbit 872)
---------------------------------------

Vector Time (GMT): 2020/277/01:16:14
000
Vector Time (MET): N/A
Weight (LBS)     : 922360
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -235944
96                 A    =         6793020
64  meter
 Y    =        4250602
83  meter          E    =           
0015710
 Z    =       -5307251
58                 I    =           51
66338
 XDOT =      -7613
573212                 Wp   =           96
89476
 YDOT =        363
024566  meter/sec      RA   =          173
52856  deg
 ZDOT =        628
989814                 TA   =          179
12505
                                          MA   =          179
12230
                                          Ha   =            229
767  n
mi
                                          Hp   =            222
667

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -774097
63                 X    =         -257678
96
 Y    =       13945547
36  feet           Y    =         4247842
33  meter
 Z    =      -17412242
70                 Z    =        -5308450
89
 XDOT =     -24978
914739                 XDOT =       -7620
122122
 YDOT =       1191
025478  feet/sec       YDOT =         277
847567  meter/sec
 ZDOT =       2063
614876                 ZDOT =         591
989570

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6483895
98                 X    =         1976291
49
 Y    =       12363018
65  feet           Y    =         3768248
09  meter
 Z    =      -17417766
13                 Z    =        -5308935
12
 XDOT =     -20060
556093                 XDOT =       -6114
457497
 YDOT =      13188
525947  feet/sec       YDOT =        4019
862709  meter/sec
 ZDOT =       1892
663809                 ZDOT =         576
883929


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20277
06810324  
00016717  00000-0  10270-3 0  9010
2 25544  51
6424 174
6735 0001171 121
3529 238
7736 15
48802735  8737


Satellite: ISS
Catalog Number: 25544
Epoch time:      20277
06810324   =   yrday
fracday
Element set:     901
Inclination:       51
6424  deg
RA of node:       174
6735  deg
Eccentricity:     
0001171     
Arg of perigee:   121
3529  deg
Mean anomaly:     238
7736  deg
Mean motion:   15
48802735  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             873
Checksum:              301


Coasting Arc #3 (Orbit 875)
---------------------------------------

Vector Time (GMT): 2020/277/05:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922360
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1755852
08                 A    =         6794201
13  meter
 Y    =        4236610
89  meter          E    =           
0014104
 Z    =       -5025857
22                 I    =           51
67198
 XDOT =      -7348
356273                 Wp   =          105
50266
 YDOT =       -649
929762  meter/sec      RA   =          172
54985  deg
 ZDOT =       2020
445547                 TA   =          184
16915
                                          MA   =          184
18091
                                          Ha   =            229
845  n
mi
                                          Hp   =            222
548

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -5760669
55                 X    =        -1778683
51
 Y    =       13899642
03  feet           Y    =         4216847
60  meter
 Z    =      -16489032
88                 Z    =        -5034442
42
 XDOT =     -24108
780423                 XDOT =       -7350
356739
 YDOT =      -2132
315491  feet/sec       YDOT =        -732
115363  meter/sec
 ZDOT =       6628
758355                 ZDOT =        1984
744750

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14727404
53                 X    =         4488912
90
 Y    =        2860029
24  feet           Y    =          871736
91  meter
 Z    =      -16528682
83                 Z    =        -5037942
53
 XDOT =       2776
710056                 XDOT =         846
341225
 YDOT =      23037
143910  feet/sec       YDOT =        7021
721464  meter/sec
 ZDOT =       6463
803429                 ZDOT =        1970
167285


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20277
26167090  
00016717  00000-0  10270-3 0  9028
2 25544  51
6405 173
7171 0001295 108
7630 251
3661 15
48800636  8768


Satellite: ISS
Catalog Number: 25544
Epoch time:      20277
26167090   =   yrday
fracday
Element set:     902
Inclination:       51
6405  deg
RA of node:       173
7171  deg
Eccentricity:     
0001295     
Arg of perigee:   108
7630  deg
Mean anomaly:     251
3661  deg
Mean motion:   15
48800636  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             876
Checksum:              300


Coasting Arc #4 (Orbit 891)
---------------------------------------

Vector Time (GMT): 2020/278/05:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922360
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1327102
95                 A    =         6794046
74  meter
 Y    =       -4360922
84  meter          E    =           
0006477
 Z    =        5033607
07                 I    =           51
70508
 XDOT =       7404
433207                 Wp   =           65
19175
 YDOT =        -30
732893  meter/sec      RA   =          167
60931  deg
 ZDOT =      -1974
144772                 TA   =           43
99619
                                          MA   =           43
94466
                                          Ha   =            229
731  n
mi
                                          Hp   =            222
603

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4354012
32                 X    =         1351318
63
 Y    =      -14307489
62  feet           Y    =        -4345946
45  meter
 Z    =       16514458
90                 Z    =         5040112
88
 XDOT =      24292
759865                 XDOT =        7413
816004
 YDOT =       -100
829700  feet/sec       YDOT =          52
121108  meter/sec
 ZDOT =      -6476
852926                 ZDOT =       -1938
153464

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14878063
03                 X    =        -4534833
61
 Y    =       -1145220
69  feet           Y    =         -349063
27  meter
 Z    =       16544508
01                 Z    =         5042766
04
 XDOT =      -5287
850106                 XDOT =       -1611
736712
 YDOT =     -22688
797701  feet/sec       YDOT =       -6915
545539  meter/sec
 ZDOT =      -6310
539641                 ZDOT =       -1923
452483


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20278
29402844  
00016717  00000-0  10270-3 0  9032
2 25544  51
6404 168
6116 0001196 110
8616 249
2662 15
48829358  8924


Satellite: ISS
Catalog Number: 25544
Epoch time:      20278
29402844   =   yrday
fracday
Element set:     903
Inclination:       51
6404  deg
RA of node:       168
6116  deg
Eccentricity:     
0001196     
Arg of perigee:   110
8616  deg
Mean anomaly:     249
2662  deg
Mean motion:   15
48829358  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             892
Checksum:              320


Coasting Arc #5 (Orbit 906)
---------------------------------------

Vector Time (GMT): 2020/279/05:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 922360
6

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -881171
74                 A    =         6794037
65  meter
 Y    =        4458257
43  meter          E    =           
0014232
 Z    =       -5063360
18                 I    =           51
73732
 XDOT =      -7370
235126                 Wp   =          104
81084
 YDOT =        717
298895  meter/sec      RA   =          162
67140  deg
 ZDOT =       1915
177917                 TA   =          183
78006
                                          MA   =          183
79082
                                          Ha   =            229
801  n
mi
                                          Hp   =            222
589

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2890983
40                 X    =         -906364
40
 Y    =       14626828
82  feet           Y    =         4448262
38  meter
 Z    =      -16612074
09                 Z    =        -5067702
10
 XDOT =     -24180
561437                 XDOT =       -7387
011438
 YDOT =       2353
342832  feet/sec       YDOT =         634
785947  meter/sec
 ZDOT =       6283
392116                 ZDOT =        1879
334667

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14874960
22                 X    =         4533887
87
 Y    =        -608823
97  feet           Y    =         -185569
55  meter
 Z    =      -16632131
67                 Z    =        -5069473
73
 XDOT =       7736
319075                 XDOT =        2358
030054
 YDOT =      21975
059387  feet/sec       YDOT =        6697
998101  meter/sec
 ZDOT =       6117
744167                 ZDOT =        1864
688422


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20279
26186148  
00016717  00000-0  10270-3 0  9047
2 25544  51
6401 163
8257 0001214 108
7110 251
4172 15
48810797  9075


Satellite: ISS
Catalog Number: 25544
Epoch time:      20279
26186148   =   yrday
fracday
Element set:     904
Inclination:       51
6401  deg
RA of node:       163
8257  deg
Eccentricity:     
0001214     
Arg of perigee:   108
7110  deg
Mean anomaly:     251
4172  deg
Mean motion:   15
48810797  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             907
Checksum:              296


Coasting Arc #6 (Orbit 909)
---------------------------------------

Vector Time (GMT): 2020/279/10:05:00
000
Vector Time (MET): N/A
Weight (LBS)     : 937074
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5836398
97                 A    =         6803822
04  meter
 Y    =       -3149199
07  meter          E    =           
0015024
 Z    =        1488139
97                 I    =           51
77815
 XDOT =       3455
843982                 Wp   =          117
67153
 YDOT =       3655
892684  meter/sec      RA   =          161
82835  deg
 ZDOT =      -5779
154498                 TA   =           46
14608
                                          MA   =           46
02203
                                          Ha   =            229
760  n
mi
                                          Hp   =            222
586

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19148290
58                 X    =         5863951
80
 Y    =      -10332017
94  feet           Y    =        -3083778
13  meter
 Z    =        4882348
99                 Z    =         1516558
60
 XDOT =      11338
070807                 XDOT =        3442
778261
 YDOT =      11994
398570  feet/sec       YDOT =        3694
465044  meter/sec
 ZDOT =     -18960
480636                 ZDOT =       -5762
398940

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21146896
41                 X    =        -6445574
02
 Y    =        4991664
46  feet           Y    =         1521459
33  meter
 Z    =        5013682
97                 Z    =         1528170
57
 XDOT =      -7580
433823                 XDOT =       -2310
516229
 YDOT =     -13026
203736  feet/sec       YDOT =       -3970
386899  meter/sec
 ZDOT =     -18883
036941                 ZDOT =       -5755
549660


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20279
45542885  
00016717  00000-0  10270-3 0  9053
2 25544  51
6427 162
8691 0001187 109
6530 250
4748 15
48820665  9106


Satellite: ISS
Catalog Number: 25544
Epoch time:      20279
45542885   =   yrday
fracday
Element set:     905
Inclination:       51
6427  deg
RA of node:       162
8691  deg
Eccentricity:     
0001187     
Arg of perigee:   109
6530  deg
Mean anomaly:     250
4748  deg
Mean motion:   15
48820665  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             910
Checksum:              323


Coasting Arc #7 (Orbit 924)
---------------------------------------

Vector Time (GMT): 2020/280/09:58:30
000
Vector Time (MET): N/A
Weight (LBS)     : 937074
3

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3538559
19                 A    =         6799256
15  meter
 Y    =        4574232
41  meter          E    =           
0006440
 Z    =       -3582205
85                 I    =           51
79462
 XDOT =      -6093
800110                 Wp   =          100
54963
 YDOT =      -1221
793379  meter/sec      RA   =          156
90333  deg
 ZDOT =       4465
088739                 TA   =          217
37368
                                          MA   =          217
41849
                                          Ha   =            229
695  n
mi
                                          Hp   =            222
553

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11609446
15                 X    =        -3572045
96
 Y    =       15007324
19  feet           Y    =         4534474
34  meter
 Z    =      -11752643
85                 Z    =        -3599476
64
 XDOT =     -19992
782514                 XDOT =       -6101
374050
 YDOT =      -4008
508461  feet/sec       YDOT =       -1289
980813  meter/sec
 ZDOT =      14649
241269                 ZDOT =        4435
468464

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15170305
51                 X    =         4623909
12
 Y    =      -11312740
33  feet           Y    =        -3448123
25  meter
 Z    =      -11832472
00                 Z    =        -3606537
46
 XDOT =      17424
564376                 XDOT =        5311
007222
 YDOT =       8206
534582  feet/sec       YDOT =        2501
351740  meter/sec
 ZDOT =      14512
330102                 ZDOT =        4423
358215


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20280
42325970  
00016717  00000-0  10270-3 0  9067
2 25544  51
6425 158
0831 0001129 112
7163 247
4106 15
48845256  9253


Satellite: ISS
Catalog Number: 25544
Epoch time:      20280
42325970   =   yrday
fracday
Element set:     906
Inclination:       51
6425  deg
RA of node:       158
0831  deg
Eccentricity:     
0001129     
Arg of perigee:   112
7163  deg
Mean anomaly:     247
4106  deg
Mean motion:   15
48845256  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             925
Checksum:              294


Coasting Arc #8 (Orbit 939)
---------------------------------------

Vector Time (GMT): 2020/281/08:18:03
639
Vector Time (MET): N/A
Weight (LBS)     : 936818
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =          40554
22                 A    =         6792610
64  meter
 Y    =       -4522189
09  meter          E    =           
0004558
 Z    =        5066008
38                 I    =           51
80428
 XDOT =       7133
440710                 Wp   =           51
92103
 YDOT =      -2060
216039  meter/sec      RA   =          152
32351  deg
 ZDOT =      -1892
263454                 TA   =           56
41526
                                          MA   =           56
37176
                                          Ha   =            228
278  n
mi
                                          Hp   =            222
657

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         133051
90                 X    =           66511
43
 Y    =      -14836578
39  feet           Y    =        -4521590
35  meter
 Z    =       16620762
40                 Z    =         5066268
51
 XDOT =      23403
676870                 XDOT =        7165
140208
 YDOT =      -6759
238974  feet/sec       YDOT =       -1980
267583  meter/sec
 ZDOT =      -6208
213433                 ZDOT =       -1857
534270

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9540720
95                 X    =        -2908011
75
 Y    =       11361172
25  feet           Y    =         3462885
30  meter
 Z    =       16621970
78                 Z    =         5066376
69
 XDOT =     -21485
866716                 XDOT =       -6548
892175
 YDOT =      -9176
333917  feet/sec       YDOT =       -2796
946578  meter/sec
 ZDOT =      -6047
664715                 ZDOT =       -1843
328205


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20281
39107118  
00016717  00000-0  10270-3 0  9077
2 25544  51
6416 153
2964 0001025 254
7550 105
3487 15
49285966  9407


Satellite: ISS
Catalog Number: 25544
Epoch time:      20281
39107118   =   yrday
fracday
Element set:     907
Inclination:       51
6416  deg
RA of node:       153
2964  deg
Eccentricity:     
0001025     
Arg of perigee:   254
7550  deg
Mean anomaly:     105
3487  deg
Mean motion:   15
49285966  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             940
Checksum:              308


Coasting Arc #9 (Orbit 954)
---------------------------------------

Vector Time (GMT): 2020/282/08:18:03
639
Vector Time (MET): N/A
Weight (LBS)     : 936818
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         234264
59                 A    =         6792733
99  meter
 Y    =        4556125
90  meter          E    =           
0011965
 Z    =       -5043652
31                 I    =           51
83483
 XDOT =      -6925
248414                 Wp   =          106
70441
 YDOT =       2567
071697  meter/sec      RA   =          147
38646  deg
 ZDOT =       1997
855028                 TA   =          182
68942
                                          MA   =          182
69586
                                          Ha   =            228
262  n
mi
                                          Hp   =            222
646

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         768584
60                 X    =          207798
80
 Y    =       14947919
61  feet           Y    =         4558597
60  meter
 Z    =      -16547415
72                 Z    =        -5042578
64
 XDOT =     -22720
631279                 XDOT =       -6963
144086
 YDOT =       8422
151237  feet/sec       YDOT =        2489
416729  meter/sec
 ZDOT =       6554
642479                 ZDOT =        1964
122245

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8713218
36                 X    =         2655788
96
 Y    =      -12176808
91  feet           Y    =        -3711491
35  meter
 Z    =      -16542464
76                 Z    =        -5042143
26
 XDOT =      22109
304498                 XDOT =        6738
916011
 YDOT =       7130
346160  feet/sec       YDOT =        2173
329510  meter/sec
 ZDOT =       6398
672652                 ZDOT =        1950
315424


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20282
35861715  
00016717  00000-0  10270-3 0  9085
2 25544  51
6423 148
5075 0000974 262
1100  97
9940 15
49292243  9553


Satellite: ISS
Catalog Number: 25544
Epoch time:      20282
35861715   =   yrday
fracday
Element set:     908
Inclination:       51
6423  deg
RA of node:       148
5075  deg
Eccentricity:     
0000974     
Arg of perigee:   262
1100  deg
Mean anomaly:      97
9940  deg
Mean motion:   15
49292243  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             955
Checksum:              312


Coasting Arc #10 (Orbit 970)
---------------------------------------

Vector Time (GMT): 2020/283/08:18:03
639
Vector Time (MET): N/A
Weight (LBS)     : 936818
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -501335
82                 A    =         6792852
48  meter
 Y    =       -4566943
80  meter          E    =           
0005294
 Z    =        5000938
76                 I    =           51
86301
 XDOT =       6700
680400                 Wp   =           51
51603
 YDOT =      -3056
273964  meter/sec      RA   =          142
45335  deg
 ZDOT =      -2114
587017                 TA   =           59
05047
                                          MA   =           58
99845
                                          Ha   =            228
276  n
mi
                                          Hp   =            222
620

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1644802
56                 X    =         -474521
65
 Y    =      -14983411
42  feet           Y    =        -4572400
16  meter
 Z    =       16407279
41                 Z    =         4998568
57
 XDOT =      21983
859581                 XDOT =        6744
630160
 YDOT =     -10027
145550  feet/sec       YDOT =       -2981
096415  meter/sec
 ZDOT =      -6937
621447                 ZDOT =       -2081
930542

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -7834391
02                 X    =        -2387922
38
 Y    =       12891438
38  feet           Y    =         3929310
42  meter
 Z    =       16396339
37                 Z    =         4997604
24
 XDOT =     -22596
304481                 XDOT =       -6887
353606
 YDOT =      -5080
786324  feet/sec       YDOT =       -1548
623671  meter/sec
 ZDOT =      -6786
599949                 ZDOT =       -2068
555665


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20283
39066419  
00016717  00000-0  10270-3 0  9099
2 25544  51
6421 143
4013 0000960 270
3844  89
7196 15
49303279  9710


Satellite: ISS
Catalog Number: 25544
Epoch time:      20283
39066419   =   yrday
fracday
Element set:     909
Inclination:       51
6421  deg
RA of node:       143
4013  deg
Eccentricity:     
0000960     
Arg of perigee:   270
3844  deg
Mean anomaly:      89
7196  deg
Mean motion:   15
49303279  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             971
Checksum:              313


Coasting Arc #11 (Orbit 978)
---------------------------------------

Vector Time (GMT): 2020/283/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936818
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2989718
20                 A    =         6791413
26  meter
 Y    =       -2954888
01  meter          E    =           
0001841
 Z    =        5333081
53                 I    =           51
87321
 XDOT =       5682
255105                 Wp   =          132
90806
 YDOT =      -5128
488472  meter/sec      RA   =          139
94574  deg
 ZDOT =        342
639549                 TA   =          313
82544
                                          MA   =          313
84065
                                          Ha   =            228
265  n
mi
                                          Hp   =            222
653

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -9808786
74                 X    =        -2982358
91
 Y    =       -9694514
45  feet           Y    =        -2988280
02  meter
 Z    =       17496986
63                 Z    =         5318576
36
 XDOT =      18642
569242                 XDOT =        5737
516725
 YDOT =     -16825
749579  feet/sec       YDOT =       -5064
636432  meter/sec
 ZDOT =       1124
145501                 ZDOT =         370
376275

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -2990907
61                 X    =         -911628
64
 Y    =      -13549638
62  feet           Y    =        -4129929
85  meter
 Z    =       17429922
95                 Z    =         5312640
51
 XDOT =      23820
219770                 XDOT =        7260
402986
 YDOT =      -3641
410668  feet/sec       YDOT =       -1109
901972  meter/sec
 ZDOT =       1252
439458                 ZDOT =         381
743547


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20283
90668532  
00016717  00000-0  10270-3 0  9102
2 25544  51
6434 140
8445 0001248 247
5311 112
5707 15
49326281  9798


Satellite: ISS
Catalog Number: 25544
Epoch time:      20283
90668532   =   yrday
fracday
Element set:     910
Inclination:       51
6434  deg
RA of node:       140
8445  deg
Eccentricity:     
0001248     
Arg of perigee:   247
5311  deg
Mean anomaly:     112
5707  deg
Mean motion:   15
49326281  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             979
Checksum:              304


Coasting Arc #12 (Orbit 993)
---------------------------------------

Vector Time (GMT): 2020/284/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936818
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3142943
70                 A    =         6791517
39  meter
 Y    =        2787837
26  meter          E    =           
0013572
 Z    =       -5347878
01                 I    =           51
89762
 XDOT =      -5283
572761                 Wp   =           89
68429
 YDOT =       5528
638741  meter/sec      RA   =          135
01480  deg
 ZDOT =       -223
501603                 TA   =          178
19061
                                          MA   =          178
18569
                                          Ha   =            228
184  n
mi
                                          Hp   =            222
848

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10311495
08                 X    =         3137512
82
 Y    =        9146447
69  feet           Y    =         2822953
49  meter
 Z    =      -17545531
53                 Z    =        -5332623
91
 XDOT =     -17334
556303                 XDOT =       -5343
917328
 YDOT =      18138
578546  feet/sec       YDOT =        5469
216631  meter/sec
 ZDOT =       -733
272977                 ZDOT =        -249
313970

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        3941429
45                 X    =         1201347
70
 Y    =       13301116
67  feet           Y    =         4054180
36  meter
 Z    =      -17474997
63                 Z    =        -5326379
28
 XDOT =     -23364
950847                 XDOT =       -7121
637018
 YDOT =       5805
116135  feet/sec       YDOT =        1769
399398  meter/sec
 ZDOT =       -852
693129                 ZDOT =        -259
900866


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20284
87422859  
00016717  00000-0  10270-3 0  9110
2 25544  51
6428 136
0574 0001272 253
5128 106
5882 15
49285487  9947


Satellite: ISS
Catalog Number: 25544
Epoch time:      20284
87422859   =   yrday
fracday
Element set:     911
Inclination:       51
6428  deg
RA of node:       136
0574  deg
Eccentricity:     
0001272     
Arg of perigee:   253
5128  deg
Mean anomaly:     106
5882  deg
Mean motion:   15
49285487  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:             994
Checksum:              331


Coasting Arc #13 (Orbit 1009)
---------------------------------------

Vector Time (GMT): 2020/285/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936818
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3280212
12                 A    =         6791359
45  meter
 Y    =       -2605460
92  meter          E    =           
0001273
 Z    =        5344505
25                 I    =           51
92160
 XDOT =       4869
900504                 Wp   =          114
38434
 YDOT =      -5914
290558  meter/sec      RA   =          130
08464  deg
 ZDOT =        105
157441                 TA   =          334
61350
                                          MA   =          334
61976
                                          Ha   =            228
223  n
mi
                                          Hp   =            222
688

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -10761850
78                 X    =        -3276793
99
 Y    =       -8548100
12  feet           Y    =        -2642123
35  meter
 Z    =       17534466
06                 Z    =         5328579
54
 XDOT =      15977
363859                 XDOT =        4935
163145
 YDOT =     -19403
840413  feet/sec       YDOT =       -5859
466928  meter/sec
 ZDOT =        345
004727                 ZDOT =         128
972324

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -4865070
73                 X    =        -1482873
56
 Y    =      -12953603
40  feet           Y    =        -3948258
32  meter
 Z    =       17460818
81                 Z    =         5322057
57
 XDOT =      22780
800050                 XDOT =        6943
587855
 YDOT =      -7939
977506  feet/sec       YDOT =       -2420
105144  meter/sec
 ZDOT =        455
209031                 ZDOT =         138
747713


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20285
90626974  
00016717  00000-0  10270-3 0  9120
2 25544  51
6437 130
9500 0001285 259
4381 100
6625 15
49330272 10102


Satellite: ISS
Catalog Number: 25544
Epoch time:      20285
90626974   =   yrday
fracday
Element set:     912
Inclination:       51
6437  deg
RA of node:       130
9500  deg
Eccentricity:     
0001285     
Arg of perigee:   259
4381  deg
Mean anomaly:     100
6625  deg
Mean motion:   15
49330272  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1010
Checksum:              286


Coasting Arc #14 (Orbit 1024)
---------------------------------------

Vector Time (GMT): 2020/286/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936818
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3417290
87                 A    =         6791484
83  meter
 Y    =        2428742
25  meter          E    =           
0013636
 Z    =       -5354762
28                 I    =           51
94147
 XDOT =      -4415
451293                 Wp   =           90
22166
 YDOT =       6247
793523  meter/sec      RA   =          125
15626  deg
 ZDOT =         15
931963                 TA   =          179
92997
                                          MA   =          179
92978
                                          Ha   =            228
181  n
mi
                                          Hp   =            222
846

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       11211584
22                 X    =         3415888
49
 Y    =        7968314
47  feet           Y    =         2466948
76  meter
 Z    =      -17568117
71                 Z    =        -5338165
83
 XDOT =     -14486
388757                 XDOT =       -4485
065228
 YDOT =      20498
010247  feet/sec       YDOT =        6198
027543  meter/sec
 ZDOT =         52
270221                 ZDOT =          -5
686067

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        5768084
03                 X    =         1758112
01
 Y    =       12594200
73  feet           Y    =         3838712
38  meter
 Z    =      -17491361
60                 Z    =        -5331367
02
 XDOT =     -21927
359211                 XDOT =       -6683
459087
 YDOT =       9976
324892  feet/sec       YDOT =        3040
783827  meter/sec
 ZDOT =        -47
791987                 ZDOT =         -14
566998


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20286
87380778  
00016717  00000-0  10270-3 0  9137
2 25544  51
6428 126
1624 0001198 269
4238  90
6775 15
49289019 10253


Satellite: ISS
Catalog Number: 25544
Epoch time:      20286
87380778   =   yrday
fracday
Element set:     913
Inclination:       51
6428  deg
RA of node:       126
1624  deg
Eccentricity:     
0001198     
Arg of perigee:   269
4238  deg
Mean anomaly:      90
6775  deg
Mean motion:   15
49289019  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1025
Checksum:              334


Coasting Arc #15 (Orbit 1040)
---------------------------------------

Vector Time (GMT): 2020/287/20:35:00
000
Vector Time (MET): N/A
Weight (LBS)     : 936818
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3536464
98                 A    =         6791356
01  meter
 Y    =       -2240022
95  meter          E    =           
0001256
 Z    =        5346676
55                 I    =           51
95975
 XDOT =       3949
498724                 Wp   =           78
10799
 YDOT =      -6564
240396  meter/sec      RA   =          120
22923  deg
 ZDOT =       -137
523422                 TA   =           13
19952
                                          MA   =           13
19623
                                          Ha   =            228
255  n
mi
                                          Hp   =            222
661

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11602575
40                 X    =        -3537124
84
 Y    =       -7349156
67  feet           Y    =        -2279573
57  meter
 Z    =       17541589
72                 Z    =         5329496
20
 XDOT =      12957
672980                 XDOT =        4023
276521
 YDOT =     -21536
221772  feet/sec       YDOT =       -6519
661758  meter/sec
 ZDOT =       -451
192330                 ZDOT =        -118
158517

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6627645
39                 X    =        -2020106
31
 Y    =      -12144367
08  feet           Y    =        -3701603
09  meter
 Z    =       17462127
43                 Z    =         5322456
44
 XDOT =      20955
145117                 XDOT =        6387
128232
 YDOT =     -11957
189855  feet/sec       YDOT =       -3644
551468  meter/sec
 ZDOT =       -361
535140                 ZDOT =        -110
195911


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20287
90584490  
00016717  00000-0  10270-3 0  9140
2 25544  51
6426 121
0555 0001194 272
2496  87
8517 15
49330739 10418


Satellite: ISS
Catalog Number: 25544
Epoch time:      20287
90584490   =   yrday
fracday
Element set:     914
Inclination:       51
6426  deg
RA of node:       121
0555  deg
Eccentricity:     
0001194     
Arg of perigee:   272
2496  deg
Mean anomaly:      87
8517  deg
Mean motion:   15
49330739  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1041
Checksum:              312


Coasting Arc #16 (Orbit 1046)
---------------------------------------

Vector Time (GMT): 2020/288/05:45:05
000
Vector Time (MET): N/A
Weight (LBS)     : 936818
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4739269
36                 A    =         6793804
43  meter
 Y    =         912324
77  meter          E    =           
0006606
 Z    =        4777948
97                 I    =           51
97321
 XDOT =       1386
642366                 Wp   =          119
44022
 YDOT =      -7031
122929  meter/sec      RA   =          118
37049  deg
 ZDOT =       2711
998855                 TA   =          303
82908
                                          MA   =          303
89195
                                          Ha   =            228
315  n
mi
                                          Hp   =            222
627

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15548784
00                 X    =        -4772327
78
 Y    =        2993191
49  feet           Y    =          859142
37  meter
 Z    =       15675685
60                 Z    =         4754846
88
 XDOT =       4549
351595                 XDOT =        1451
989981
 YDOT =     -23067
988611  feet/sec       YDOT =       -7015
250916  meter/sec
 ZDOT =       8897
634040                 ZDOT =        2718
893921

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        7831686
95                 X    =         2387098
18
 Y    =       13882665
37  feet           Y    =         4231436
41  meter
 Z    =       15568791
85                 Z    =         4745367
76
 XDOT =     -22281
847448                 XDOT =       -6791
507102
 YDOT =       2533
659754  feet/sec       YDOT =         772
259493  meter/sec
 ZDOT =       8929
609048                 ZDOT =        2721
744838


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20288
29285995  
00016717  00000-0  10270-3 0  9152
2 25544  51
6415 119
1417 0001133 287
5452  72
5574 15
49332728 10475


Satellite: ISS
Catalog Number: 25544
Epoch time:      20288
29285995   =   yrday
fracday
Element set:     915
Inclination:       51
6415  deg
RA of node:       119
1417  deg
Eccentricity:     
0001133     
Arg of perigee:   287
5452  deg
Mean anomaly:      72
5574  deg
Mean motion:   15
49332728  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1047
Checksum:              321


Coasting Arc #17 (Orbit 1048)
---------------------------------------

Vector Time (GMT): 2020/288/08:50:45
000
Vector Time (MET): N/A
Weight (LBS)     : 951926
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4736358
60                 A    =         6793981
52  meter
 Y    =        1007158
29  meter          E    =           
0006731
 Z    =        4761818
06                 I    =           51
97703
 XDOT =       1272
739827                 Wp   =          117
70822
 YDOT =      -7038
497865  meter/sec      RA   =          117
73624  deg
 ZDOT =       2748
617106                 TA   =          305
17298
                                          MA   =          305
23600
                                          Ha   =            228
416  n
mi
                                          Hp   =            222
650

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -15539234
26                 X    =        -4770399
36
 Y    =        3304325
09  feet           Y    =          954002
95  meter
 Z    =       15622762
66                 Z    =         4738727
70
 XDOT =       4175
655599                 XDOT =        1338
000496
 YDOT =     -23092
184596  feet/sec       YDOT =       -7023
900070  meter/sec
 ZDOT =       9017
772659                 ZDOT =        2754
958680

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       15585836
87                 X    =         4750563
08
 Y    =        3577003
99  feet           Y    =         1090270
82  meter
 Z    =       15515921
20                 Z    =         4729252
78
 XDOT =     -13177
517599                 XDOT =       -4016
507364
 YDOT =      18087
516924  feet/sec       YDOT =        5513
075159  meter/sec
 ZDOT =       9047
188633                 ZDOT =        2757
583095


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20288
42186533  
00016717  00000-0  10270-3 0  9166
2 25544  51
6431 118
5039 0001080 294
9168  65
1870 15
49294238 10495


Satellite: ISS
Catalog Number: 25544
Epoch time:      20288
42186533   =   yrday
fracday
Element set:     916
Inclination:       51
6431  deg
RA of node:       118
5039  deg
Eccentricity:     
0001080     
Arg of perigee:   294
9168  deg
Mean anomaly:      65
1870  deg
Mean motion:   15
49294238  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1049
Checksum:              315


Coasting Arc #18 (Orbit 1059)
---------------------------------------

Vector Time (GMT): 2020/289/02:17:30
000
Vector Time (MET): N/A
Weight (LBS)     : 951926
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1305270
72                 A    =         6801911
82  meter
 Y    =       -6413357
28  meter          E    =           
0012812
 Z    =        1830045
57                 I    =           52
01124
 XDOT =       5116
333540                 Wp   =          113
78974
 YDOT =       -585
076095  meter/sec      RA   =          114
11738  deg
 ZDOT =      -5673
284091                 TA   =           46
23109
                                          MA   =           46
12514
                                          Ha   =            228
225  n
mi
                                          Hp   =            222
593

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        4282384
26                 X    =         1368000
37
 Y    =      -21041198
42  feet           Y    =        -6398409
91  meter
 Z    =        6004086
51                 Z    =         1836539
05
 XDOT =      16785
871195                 XDOT =        5150
053729
 YDOT =      -1919
540993  feet/sec       YDOT =        -527
673514  meter/sec
 ZDOT =     -18613
136781                 ZDOT =       -5648
348657

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -15480002
76                 X    =        -4718304
84
 Y    =      -14868683
41  feet           Y    =        -4531974
70  meter
 Z    =        6034208
23                 Z    =         1839226
67
 XDOT =       6369
945396                 XDOT =        1941
559357
 YDOT =     -14173
696625  feet/sec       YDOT =       -4320
142731  meter/sec
 ZDOT =     -18497
758354                 ZDOT =       -5638
116746


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20289
13138885  
00016717  00000-0  10270-3 0  9173
2 25544  51
6395 114
9907 0001102 297
3799  62
7238 15
49322680 10607


Satellite: ISS
Catalog Number: 25544
Epoch time:      20289
13138885   =   yrday
fracday
Element set:     917
Inclination:       51
6395  deg
RA of node:       114
9907  deg
Eccentricity:     
0001102     
Arg of perigee:   297
3799  deg
Mean anomaly:      62
7238  deg
Mean motion:   15
49322680  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1060
Checksum:              324


Coasting Arc #19 (Orbit 1074)
---------------------------------------

Vector Time (GMT): 2020/290/02:17:30
000
Vector Time (MET): N/A
Weight (LBS)     : 951926
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -829648
59                 A    =         6802047
90  meter
 Y    =        6519242
70  meter          E    =           
0007465
 Z    =       -1741971
27                 I    =           52
02486
 XDOT =      -5026
840526                 Wp   =           30
89359
 YDOT =        881
601692  meter/sec      RA   =          109
19376  deg
 ZDOT =       5710
535045                 TA   =          310
13867
                                          MA   =          310
20404
                                          Ha   =            228
273  n
mi
                                          Hp   =            222
558

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2721944
18                 X    =         -894025
40
 Y    =       21388591
52  feet           Y    =         6509604
87  meter
 Z    =       -5715128
84                 Z    =        -1746158
36
 XDOT =     -16492
258945                 XDOT =       -5064
064319
 YDOT =       2892
394002  feet/sec       YDOT =         825
180291  meter/sec
 ZDOT =      18735
351196                 ZDOT =        5686
025658

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       16843242
40                 X    =         5133820
28
 Y    =       13452253
13  feet           Y    =         4100246
75  meter
 Z    =       -5734596
45                 Z    =        -1747905
00
 XDOT =      -5226
274701                 XDOT =       -1592
968529
 YDOT =      14458
320320  feet/sec       YDOT =        4406
896034  meter/sec
 ZDOT =      18621
934087                 ZDOT =        5675
965510


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20290
09891931  
00016717  00000-0  10270-3 0  9189
2 25544  51
6400 110
2025 0000998 301
7560  58
3492 15
49321201 10759


Satellite: ISS
Catalog Number: 25544
Epoch time:      20290
09891931   =   yrday
fracday
Element set:     918
Inclination:       51
6400  deg
RA of node:       110
2025  deg
Eccentricity:     
0000998     
Arg of perigee:   301
7560  deg
Mean anomaly:      58
3492  deg
Mean motion:   15
49321201  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1075
Checksum:              282


Coasting Arc #20 (Orbit 1090)
---------------------------------------

Vector Time (GMT): 2020/291/02:17:30
000
Vector Time (MET): N/A
Weight (LBS)     : 951926
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         371431
02                 A    =         6802231
74  meter
 Y    =       -6589831
87  meter          E    =           
0012739
 Z    =        1620455
50                 I    =           52
03561
 XDOT =       4925
438052                 Wp   =          115
52241
 YDOT =      -1145
094314  meter/sec      RA   =          104
27044  deg
 ZDOT =      -5755
830248                 TA   =           46
87412
                                          MA   =           46
76764
                                          Ha   =            228
275  n
mi
                                          Hp   =            222
571

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        1218605
70                 X    =          437221
46
 Y    =      -21620183
31  feet           Y    =        -6585310
30  meter
 Z    =        5316455
05                 Z    =         1622420
04
 XDOT =      16159
573662                 XDOT =        4965
836004
 YDOT =      -3756
871110  feet/sec       YDOT =       -1089
789026  meter/sec
 ZDOT =     -18883
957508                 ZDOT =       -5731
805606

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18032866
39                 X    =        -5496417
68
 Y    =      -11984786
30  feet           Y    =        -3652962
86  meter
 Z    =        5325659
35                 Z    =         1623260
97
 XDOT =       4149
281763                 XDOT =        1264
701081
 YDOT =     -14628
672480  feet/sec       YDOT =       -4458
819372  meter/sec
 ZDOT =     -18772
772317                 ZDOT =       -5721
941002


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20291
13094928  
00016717  00000-0  10270-3 0  9197
2 25544  51
6402 105
0942 0001180 310
5665  49
5383 15
49320994 10916


Satellite: ISS
Catalog Number: 25544
Epoch time:      20291
13094928   =   yrday
fracday
Element set:     919
Inclination:       51
6402  deg
RA of node:       105
0942  deg
Eccentricity:     
0001180     
Arg of perigee:   310
5665  deg
Mean anomaly:      49
5383  deg
Mean motion:   15
49320994  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1091
Checksum:              297


Coasting Arc #21 (Orbit 1095)
---------------------------------------

Vector Time (GMT): 2020/291/11:10:00
000
Vector Time (MET): N/A
Weight (LBS)     : 951926
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4326427
52                 A    =         6793447
31  meter
 Y    =        1854601
66  meter          E    =           
0005778
 Z    =        4895036
85                 I    =           52
00781
 XDOT =       -345
096617                 Wp   =          119
27801
 YDOT =      -7255
801385  meter/sec      RA   =          102
48159  deg
 ZDOT =       2439
111278                 TA   =          306
87302
                                          MA   =          306
92598
                                          Ha   =            228
432  n
mi
                                          Hp   =            222
659

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -14194316
03                 X    =        -4370622
61
 Y    =        6084651
11  feet           Y    =         1805973
60  meter
 Z    =       16059832
17                 Z    =         4873912
75
 XDOT =      -1132
206750                 XDOT =        -275
782529
 YDOT =     -23805
122653  feet/sec       YDOT =       -7259
272808  meter/sec
 ZDOT =       8002
333590                 ZDOT =        2437
603646

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12566593
18                 X    =         3830297
60
 Y    =       -9149503
33  feet           Y    =        -2788768
61  meter
 Z    =       15962052
52                 Z    =         4865233
61
 XDOT =       5848
635686                 XDOT =        1782
664157
 YDOT =      22010
016043  feet/sec       YDOT =        6708
652890  meter/sec
 ZDOT =       7995
491702                 ZDOT =        2437
025871


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   20291
51796025  
00016717  00000-0  10270-3 0  9208
2 25544  51
6391 103
1772 0001221 305
7774  54
3262 15
49288341 10960


Satellite: ISS
Catalog Number: 25544
Epoch time:      20291
51796025   =   yrday
fracday
Element set:     920
Inclination:       51
6391  deg
RA of node:       103
1772  deg
Eccentricity:     
0001221     
Arg of perigee:   305
7774  deg
Mean anomaly:      54
3262  deg
Mean motion:   15
49288341  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1096
Checksum:              292
Forward to a Friend
 
  • This mailing list is a public mailing list - anyone may join or leave, at any time.
  • This mailing list is announce-only.

ISS TLE list

Privacy Policy:

Private list