[list_settings.list_name] Current ISS TLEs @ 06:30 UTC

 
Date: October 25th 2020

  • spaceflight nasa gov will be taken offline in the next 30 days *
  • *
  • Current information about the International Space Station can be *
  • found at www nasa gov/station *
  • *
  • Predicted ISS and visiting vehicle sightings opportunities can be *
  • found at spotthestation nasa gov *
  • *
  • Updated ISS trajectory information will be made available as a CCSDS *
  • Orbital Ephemeris Message (OEM) in the Mean of J2000 (J2K) reference *
  • system *
  • Included in the OEM are a sequence of events with ISS maneuver *
  • details (in the comment section), predicted post-maneuver state *
  • vectors, predicted coasting state vectors at 4-minute intervals, *
  • and ISS ballistic details *
  • *
  • OEMs will be provided in xml and txt formats *
  • Links to the OEMs and more details to follow *
  • *

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 15144 822 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 453 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


296/18:14:30 000 0 0 0 0 0 0
N/A 0 0 0 0 229 1
000/00:00:00 000 0 0 0 0 221 8

303/01:06:42 218 1 5 1 9 1 9
N/A 1 1 -0 2 229 2
000/00:05:24 437 -0 0 0 1 222 8

303/17:20:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 3
000/00:00:00 000 0 0 0 0 222 6

Coasting Arc #1 (Orbit 1127)
---------------------------------------

Vector Time (GMT): 2020/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 953675
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4182782
19                 A    =         6791623
03  meter
 Y    =        -764512
38  meter          E    =           
0015696
 Z    =       -5309507
90                 I    =           52
01334
 XDOT =        327
655156                 Wp   =           80
72783
 YDOT =       7596
122470  meter/sec      RA   =           92
45161  deg
 ZDOT =       -835
285588                 TA   =          181
30586
                                          MA   =          181
30996
                                          Ha   =            229
002  n
mi
                                          Hp   =            221
970

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13723038
68                 X    =         4216811
54
 Y    =       -2508242
72  feet           Y    =         -717547
22  meter
 Z    =      -17419645
33                 Z    =        -5289106
40
 XDOT =       1074
984106                 XDOT =         246
746115
 YDOT =      24921
661648  feet/sec       YDOT =        7599
334158  meter/sec
 ZDOT =      -2740
438280                 ZDOT =        -833
890410

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11116907
31                 X    =        -3388433
35
 Y    =        8620234
21  feet           Y    =         2627447
39  meter
 Z    =      -17325214
27                 Z    =        -5280725
31
 XDOT =     -11855
226999                 XDOT =       -3613
473189
 YDOT =     -20786
407504  feet/sec       YDOT =       -6335
697007  meter/sec
 ZDOT =      -2734
175506                 ZDOT =        -833
376694


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   20293
51758046  
00016717  00000-0  10270-3 0  9009
2 25544  51
6408  93
2800 0001437  50
6290 309
4987 15
49321265 11285


Satellite: ISS
Catalog Number: 25544
Epoch time:      20293
51758046   =   yrday
fracday
Element set:     900
Inclination:       51
6408  deg
RA of node:        93
2800  deg
Eccentricity:     
0001437     
Arg of perigee:    50
6290  deg
Mean anomaly:     309
4987  deg
Mean motion:   15
49321265  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1128
Checksum:              298


Coasting Arc #2 (Orbit 1143)
---------------------------------------

Vector Time (GMT): 2020/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 953675
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4110576
05                 A    =         6791635
60  meter
 Y    =         981963
53  meter          E    =           
0003981
 Z    =        5313144
84                 I    =           52
01318
 XDOT =       -885
795273                 Wp   =           96
61212
 YDOT =      -7578
934340  meter/sec      RA   =           87
52718  deg
 ZDOT =        714
512065                 TA   =          346
58914
                                          MA   =          346
59972
                                          Ha   =            229
253  n
mi
                                          Hp   =            221
835

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13486141
90                 X    =        -4147059
94
 Y    =        3221665
13  feet           Y    =          935792
00  meter
 Z    =       17431577
57                 Z    =         5293088
25
 XDOT =      -2906
152471                 XDOT =        -804
450275
 YDOT =     -24865
270143  feet/sec       YDOT =       -7588
385125  meter/sec
 ZDOT =       2344
199687                 ZDOT =         710
406525

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10418440
39                 X    =         3175540
63
 Y    =       -9324143
79  feet           Y    =        -2841999
03  meter
 Z    =       17338727
99                 Z    =         5284844
29
 XDOT =      13753
458425                 XDOT =        4192
054128
 YDOT =      19697
363721  feet/sec       YDOT =        6003
756462  meter/sec
 ZDOT =       2325
417098                 ZDOT =         708
787131


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   20294
54961435  
00016717  00000-0  10270-3 0  9012
2 25544  51
6406  88
1714 0001530  52
6861 307
4428 15
49290274 11441


Satellite: ISS
Catalog Number: 25544
Epoch time:      20294
54961435   =   yrday
fracday
Element set:     901
Inclination:       51
6406  deg
RA of node:        88
1714  deg
Eccentricity:     
0001530     
Arg of perigee:    52
6861  deg
Mean anomaly:     307
4428  deg
Mean motion:   15
49290274  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1144
Checksum:              297


Coasting Arc #3 (Orbit 1158)
---------------------------------------

Vector Time (GMT): 2020/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 953675
7

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4046567
39                 A    =         6791486
72  meter
 Y    =       -1196063
05  meter          E    =           
0016021
 Z    =       -5335436
28                 I    =           52
01100
 XDOT =       1436
151171                 Wp   =           83
00488
 YDOT =       7489
569055  meter/sec      RA   =           82
60535  deg
 ZDOT =       -589
361417                 TA   =          181
38228
                                          MA   =          181
38672
                                          Ha   =            229
052  n
mi
                                          Hp   =            221
892

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13276139
73                 X    =         4085558
32
 Y    =       -3924091
36  feet           Y    =        -1150593
26  meter
 Z    =      -17504712
20                 Z    =        -5315684
63
 XDOT =       4711
782058                 XDOT =        1355
156641
 YDOT =      24572
076953  feet/sec       YDOT =        7505
176275  meter/sec
 ZDOT =      -1933
600448                 ZDOT =        -582
581545

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9728396
61                 X    =        -2965215
29
 Y    =       10010296
97  feet           Y    =         3051138
52  meter
 Z    =      -17413258
81                 Z    =        -5307561
28
 XDOT =     -15478
115288                 XDOT =       -4717
729540
 YDOT =     -18353
792662  feet/sec       YDOT =       -5594
236003  meter/sec
 ZDOT =      -1902
457930                 ZDOT =        -579
869177


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   20295
51714333  
00016717  00000-0  10270-3 0  9024
2 25544  51
6413  83
3849 0001510  58
7564 301
3734 15
49327278 11594


Satellite: ISS
Catalog Number: 25544
Epoch time:      20295
51714333   =   yrday
fracday
Element set:     902
Inclination:       51
6413  deg
RA of node:        83
3849  deg
Eccentricity:     
0001510     
Arg of perigee:    58
7564  deg
Mean anomaly:     301
3734  deg
Mean motion:   15
49327278  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1159
Checksum:              302


Coasting Arc #4 (Orbit 1174)
---------------------------------------

Vector Time (GMT): 2020/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938567
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3958900
50                 A    =         6791483
33  meter
 Y    =        1401202
88  meter          E    =           
0003775
 Z    =        5334171
01                 I    =           52
00540
 XDOT =      -1986
028841                 Wp   =           91
95443
 YDOT =      -7387
400724  meter/sec      RA   =           77
68075  deg
 ZDOT =        466
159327                 TA   =          353
61651
                                          MA   =          353
62132
                                          Ha   =            229
216  n
mi
                                          Hp   =            221
804

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -12988518
70                 X    =        -4000185
62
 Y    =        4597122
30  feet           Y    =         1356700
65  meter
 Z    =       17500561
06                 Z    =         5314839
74
 XDOT =      -6515
842655                 XDOT =       -1905
537455
 YDOT =     -24236
879015  feet/sec       YDOT =       -7409
159878  meter/sec
 ZDOT =       1529
394118                 ZDOT =         456
707177

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8965545
25                 X    =         2732698
19
 Y    =      -10610349
22  feet           Y    =        -3234034
44  meter
 Z    =       17411038
93                 Z    =         5306884
67
 XDOT =      17142
329479                 XDOT =        5224
982025
 YDOT =      16925
439398  feet/sec       YDOT =        5158
873929  meter/sec
 ZDOT =       1485
896073                 ZDOT =         452
901123


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   20296
54917464  
00016717  00000-0  10270-3 0  9039
2 25544  51
6414  78
2766 0001446  58
1779 301
9511 15
49308533 11756


Satellite: ISS
Catalog Number: 25544
Epoch time:      20296
54917464   =   yrday
fracday
Element set:     903
Inclination:       51
6414  deg
RA of node:        78
2766  deg
Eccentricity:     
0001446     
Arg of perigee:    58
1779  deg
Mean anomaly:     301
9511  deg
Mean motion:   15
49308533  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1175
Checksum:              319


Coasting Arc #5 (Orbit 1178)
---------------------------------------

Vector Time (GMT): 2020/296/18:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 938567
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4228349
95                 A    =         6791516
35  meter
 Y    =         159607
95  meter          E    =           
0004571
 Z    =        5309185
40                 I    =           52
00503
 XDOT =      -1223
307932                 Wp   =           58
22262
 YDOT =      -7528
682535  meter/sec      RA   =           76
39436  deg
 ZDOT =       -745
126240                 TA   =           38
88075
                                          MA   =           38
84788
                                          Ha   =            229
138  n
mi
                                          Hp   =            221
800

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13872539
22                 X    =        -4255609
76
 Y    =         523648
14  feet           Y    =          112170
98  meter
 Z    =       17418587
26                 Z    =         5288579
28
 XDOT =      -4013
477468                 XDOT =       -1135
409573
 YDOT =     -24700
402019  feet/sec       YDOT =       -7541
870955  meter/sec
 ZDOT =      -2444
639896                 ZDOT =        -750
855332

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -8328526
20                 X    =        -2538534
79
 Y    =      -11254818
09  feet           Y    =        -3430468
55  meter
 Z    =       17323205
68                 Z    =         5280113
09
 XDOT =      17315
696700                 XDOT =        5277
824354
 YDOT =     -16630
985963  feet/sec       YDOT =       -5069
124521  meter/sec
 ZDOT =      -2470
897015                 ZDOT =        -753
129410


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   20296
80717985  
00016717  00000-0  10270-3 0  9045
2 25544  51
6426  77
0038 0001444  50
3135 309
8142 15
49338451 11799


Satellite: ISS
Catalog Number: 25544
Epoch time:      20296
80717985   =   yrday
fracday
Element set:     904
Inclination:       51
6426  deg
RA of node:        77
0038  deg
Eccentricity:     
0001444     
Arg of perigee:    50
3135  deg
Mean anomaly:     309
8142  deg
Mean motion:   15
49338451  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1179
Checksum:              308


Coasting Arc #6 (Orbit 1193)
---------------------------------------

Vector Time (GMT): 2020/297/18:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 938567
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4240260
46                 A    =         6791703
38  meter
 Y    =        -391240
96  meter          E    =           
0015621
 Z    =       -5304510
42                 I    =           51
99714
 XDOT =       1763
865008                 Wp   =           92
42842
 YDOT =       7392
260166  meter/sec      RA   =           71
46956  deg
 ZDOT =        866
310973                 TA   =          185
82634
                                          MA   =          185
84454
                                          Ha   =            229
100  n
mi
                                          Hp   =            221
940

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13911615
68                 X    =         4270086
80
 Y    =       -1283598
95  feet           Y    =         -343656
51  meter
 Z    =      -17403249
40                 Z    =        -5283840
27
 XDOT =       5786
958689                 XDOT =        1676
863349
 YDOT =      24252
822068  feet/sec       YDOT =        7411
498505  meter/sec
 ZDOT =       2842
227602                 ZDOT =         874
667968

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        9163351
19                 X    =         2792989
44
 Y    =       10702108
38  feet           Y    =         3262002
64  meter
 Z    =      -17307560
14                 Z    =        -5275344
33
 XDOT =     -15667
468753                 XDOT =       -4775
444476
 YDOT =      18065
076483  feet/sec       YDOT =        5506
235312  meter/sec
 ZDOT =       2880
639165                 ZDOT =         878
018817


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   20297
77470696  
00016717  00000-0  10270-3 0  9058
2 25544  51
6436  72
2152 0001615  51
9319 308
1977 15
49301761 11944


Satellite: ISS
Catalog Number: 25544
Epoch time:      20297
77470696   =   yrday
fracday
Element set:     905
Inclination:       51
6436  deg
RA of node:        72
2152  deg
Eccentricity:     
0001615     
Arg of perigee:    51
9319  deg
Mean anomaly:     308
1977  deg
Mean motion:   15
49301761  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1194
Checksum:              316


Coasting Arc #7 (Orbit 1209)
---------------------------------------

Vector Time (GMT): 2020/298/18:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 938567
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4230157
52                 A    =         6791651
60  meter
 Y    =         609875
81  meter          E    =           
0005359
 Z    =        5274843
11                 I    =           51
98502
 XDOT =      -2293
052059                 Wp   =           56
90523
 YDOT =      -7244
484952  meter/sec      RA   =           66
54499  deg
 ZDOT =       -997
728252                 TA   =           42
62675
                                          MA   =           42
58518
                                          Ha   =            229
243  n
mi
                                          Hp   =            221
676

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13878469
55                 X    =        -4262285
31
 Y    =        2000904
88  feet           Y    =          562391
55  meter
 Z    =       17305915
71                 Z    =         5254216
46
 XDOT =      -7523
136675                 XDOT =       -2207
025184
 YDOT =     -23767
995248  feet/sec       YDOT =       -7269
646504  meter/sec
 ZDOT =      -3273
386655                 ZDOT =       -1008
658099

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9903959
59                 X    =        -3018726
88
 Y    =      -10090755
18  feet           Y    =        -3075662
18  meter
 Z    =       17210418
36                 Z    =         5245735
52
 XDOT =      13970
090052                 XDOT =        4258
083448
 YDOT =     -19400
395898  feet/sec       YDOT =       -5913
240670  meter/sec
 ZDOT =      -3323
699905                 ZDOT =       -1013
063731


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   20298
80673179  
00016717  00000-0  10270-3 0  9065
2 25544  51
6431  67
1083 0001722  55
8089 304
3224 15
49344252 12105


Satellite: ISS
Catalog Number: 25544
Epoch time:      20298
80673179   =   yrday
fracday
Element set:     906
Inclination:       51
6431  deg
RA of node:        67
1083  deg
Eccentricity:     
0001722     
Arg of perigee:    55
8089  deg
Mean anomaly:     304
3224  deg
Mean motion:   15
49344252  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1210
Checksum:              294


Coasting Arc #8 (Orbit 1224)
---------------------------------------

Vector Time (GMT): 2020/299/18:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 938567
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4222773
84                 A    =         6791862
35  meter
 Y    =        -847060
73  meter          E    =           
0015490
 Z    =       -5265188
37                 I    =           51
97134
 XDOT =       2802
759119                 Wp   =           94
37767
 YDOT =       7028
539970  meter/sec      RA   =           61
61903  deg
 ZDOT =       1118
800357                 TA   =          186
31382
                                          MA   =          186
33336
                                          Ha   =            229
150  n
mi
                                          Hp   =            221
869

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13854244
88                 X    =         4257507
58
 Y    =       -2779070
63  feet           Y    =         -799644
55  meter
 Z    =      -17274240
05                 Z    =        -5244591
23
 XDOT =       9195
403935                 XDOT =        2718
521016
 YDOT =      23059
514338  feet/sec       YDOT =        7059
411453  meter/sec
 ZDOT =       3670
604846                 ZDOT =        1132
210430

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10680168
76                 X    =         3255315
44
 Y    =        9427783
69  feet           Y    =         2873588
47  meter
 Z    =      -17178870
57                 Z    =        -5236119
75
 XDOT =     -12094
677771                 XDOT =       -3686
457785
 YDOT =      20492
192390  feet/sec       YDOT =        6246
020240  meter/sec
 ZDOT =       3732
393677                 ZDOT =        1137
633593


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   20299
77425593  
00016717  00000-0  10270-3 0  9078
2 25544  51
6437  62
3201 0001700  57
9628 302
1687 15
49306544 12255


Satellite: ISS
Catalog Number: 25544
Epoch time:      20299
77425593   =   yrday
fracday
Element set:     907
Inclination:       51
6437  deg
RA of node:        62
3201  deg
Eccentricity:     
0001700     
Arg of perigee:    57
9628  deg
Mean anomaly:     302
1687  deg
Mean motion:   15
49306544  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1225
Checksum:              307


Coasting Arc #9 (Orbit 1240)
---------------------------------------

Vector Time (GMT): 2020/300/18:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 938567
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4194957
34                 A    =         6791849
88  meter
 Y    =        1068688
92  meter          E    =           
0006002
 Z    =        5229704
60                 I    =           51
95361
 XDOT =      -3298
672052                 Wp   =           57
70710
 YDOT =      -6803
757135  meter/sec      RA   =           56
69208  deg
 ZDOT =      -1251
484065                 TA   =           44
28407
                                          MA   =           44
23606
                                          Ha   =            229
308  n
mi
                                          Hp   =            221
602

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13762983
41                 X    =        -4231999
16
 Y    =        3506197
25  feet           Y    =         1021570
96  meter
 Z    =       17157823
50                 Z    =         5209236
91
 XDOT =     -10822
414870                 XDOT =       -3216
266159
 YDOT =     -22322
037844  feet/sec       YDOT =       -6840
184535  meter/sec
 ZDOT =      -4105
918848                 ZDOT =       -1267
307516

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -11354358
66                 X    =        -3460808
52
 Y    =       -8719806
83  feet           Y    =        -2657797
12  meter
 Z    =       17063046
25                 Z    =         5200816
50
 XDOT =      10193
310546                 XDOT =        3106
921054
 YDOT =     -21477
244607  feet/sec       YDOT =       -6546
264156  meter/sec
 ZDOT =      -4178
872964                 ZDOT =       -1273
720479


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   20300
80627884  
00016717  00000-0  10270-3 0  9083
2 25544  51
6428  57
2127 0001825  63
5632 296
5705 15
49344131 12410


Satellite: ISS
Catalog Number: 25544
Epoch time:      20300
80627884   =   yrday
fracday
Element set:     908
Inclination:       51
6428  deg
RA of node:        57
2127  deg
Eccentricity:     
0001825     
Arg of perigee:    63
5632  deg
Mean anomaly:     296
5705  deg
Mean motion:   15
49344131  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1241
Checksum:              297


Coasting Arc #10 (Orbit 1255)
---------------------------------------

Vector Time (GMT): 2020/301/18:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 938567
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        4166814
95                 A    =         6792051
54  meter
 Y    =       -1309814
33  meter          E    =           
0015211
 Z    =       -5214730
08                 I    =           51
93623
 XDOT =       3764
572734                 Wp   =           96
21083
 YDOT =       6515
458211  meter/sec      RA   =           51
76405  deg
 ZDOT =       1373
387144                 TA   =          186
96076
                                          MA   =          186
98191
                                          Ha   =            229
164  n
mi
                                          Hp   =            221
815

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       13670652
73                 X    =         4206482
55
 Y    =       -4297291
12  feet           Y    =        -1262996
44  meter
 Z    =      -17108694
50                 Z    =        -5194392
63
 XDOT =      12350
960415                 XDOT =        3684
763893
 YDOT =      21376
175232  feet/sec       YDOT =        6557
110183  meter/sec
 ZDOT =       4505
863334                 ZDOT =        1391
480116

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12056330
56                 X    =         3674769
55
 Y    =        7950605
52  feet           Y    =         2423344
56  meter
 Z    =      -17014512
92                 Z    =        -5186023
54
 XDOT =      -8165
969187                 XDOT =       -2488
987408
 YDOT =      22191
169054  feet/sec       YDOT =        6763
868328  meter/sec
 ZDOT =       4589
317602                 ZDOT =        1398
824005


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   20301
77379813  
00016717  00000-0  10270-3 0  9097
2 25544  51
6447  52
4248 0001740  61
6393 298
4932 15
49316620 12562


Satellite: ISS
Catalog Number: 25544
Epoch time:      20301
77379813   =   yrday
fracday
Element set:     909
Inclination:       51
6447  deg
RA of node:        52
4248  deg
Eccentricity:     
0001740     
Arg of perigee:    61
6393  deg
Mean anomaly:     298
4932  deg
Mean motion:   15
49316620  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1256
Checksum:              313


Coasting Arc #11 (Orbit 1271)
---------------------------------------

Vector Time (GMT): 2020/302/18:14:30
000
Vector Time (MET): N/A
Weight (LBS)     : 938567
4

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -4120824
65                 A    =         6792087
91  meter
 Y    =        1532699
65  meter          E    =           
0006688
 Z    =        5172980
58                 I    =           51
91343
 XDOT =      -4214
073416                 Wp   =           57
85459
 YDOT =      -6221
353452  meter/sec      RA   =           46
83435  deg
 ZDOT =      -1508
742277                 TA   =           46
65724
                                          MA   =           46
60152
                                          Ha   =            229
343  n
mi
                                          Hp   =            221
551

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -13519765
92                 X    =        -4162785
35
 Y    =        5028542
15  feet           Y    =         1486383
23  meter
 Z    =       16971721
06                 Z    =         5152860
87
 XDOT =     -13825
700184                 XDOT =       -4136
862417
 YDOT =     -20411
264605  feet/sec       YDOT =       -6268
046595  meter/sec
 ZDOT =      -4949
941853                 ZDOT =       -1529
025182

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12651135
21                 X    =        -3856066
01
 Y    =       -7153548
52  feet           Y    =        -2180401
59  meter
 Z    =       16878540
93                 Z    =         5144579
28
 XDOT =       6138
484493                 XDOT =        1871
010073
 YDOT =     -22794
065421  feet/sec       YDOT =       -6947
631140  meter/sec
 ZDOT =      -5043
526143                 ZDOT =       -1537
266768


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   20302
80581631  
00016717  00000-0  10270-3 0  9107
2 25544  51
6433  47
3173 0001927  66
3444 293
7908 15
49346802 12727


Satellite: ISS
Catalog Number: 25544
Epoch time:      20302
80581631   =   yrday
fracday
Element set:     910
Inclination:       51
6433  deg
RA of node:        47
3173  deg
Eccentricity:     
0001927     
Arg of perigee:    66
3444  deg
Mean anomaly:     293
7908  deg
Mean motion:   15
49346802  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1272
Checksum:              298


Coasting Arc #12 (Orbit 1275)
---------------------------------------

Vector Time (GMT): 2020/303/01:09:24
437
Vector Time (MET): N/A
Weight (LBS)     : 938366
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3200941
79                 A    =         6792362
26  meter
 Y    =       -2724926
65  meter          E    =           
0014937
 Z    =       -5348138
99                 I    =           51
90581
 XDOT =       5211
779813                 Wp   =           89
01182
 YDOT =       5592
216621  meter/sec      RA   =           45
42447  deg
 ZDOT =        270
946645                 TA   =          183
56255
                                          MA   =          183
57320
                                          Ha   =            229
159  n
mi
                                          Hp   =            222
791

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10501777
53                 X    =         3257153
56
 Y    =       -8940048
05  feet           Y    =        -2688817
33  meter
 Z    =      -17546387
75                 Z    =        -5332453
11
 XDOT =      17099
015136                 XDOT =        5147
542475
 YDOT =      18347
167392  feet/sec       YDOT =        5650
139322  meter/sec
 ZDOT =        888
932563                 ZDOT =         296
107684

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1057506
05                 X    =         -322327
84
 Y    =      -13843408
48  feet           Y    =        -4219470
90  meter
 Z    =      -17473672
66                 Z    =        -5325975
43
 XDOT =      23865
343964                 XDOT =        7274
156840
 YDOT =      -3088
020934  feet/sec       YDOT =        -941
228781  meter/sec
 ZDOT =       1005
114971                 ZDOT =         306
359043


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   20303
06382309  
00016717  00000-0  10270-3 0  9118
2 25544  51
6449  46
0410 0000796  11
9017 348
2151 15
48999933 12767


Satellite: ISS
Catalog Number: 25544
Epoch time:      20303
06382309   =   yrday
fracday
Element set:     911
Inclination:       51
6449  deg
RA of node:        46
0410  deg
Eccentricity:     
0000796     
Arg of perigee:    11
9017  deg
Mean anomaly:     348
2151  deg
Mean motion:   15
48999933  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1276
Checksum:              299


Coasting Arc #13 (Orbit 1286)
---------------------------------------

Vector Time (GMT): 2020/303/17:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938366
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1276142
17                 A    =         6793244
04  meter
 Y    =        4266895
05  meter          E    =           
0005078
 Z    =        5126321
89                 I    =           51
89077
 XDOT =      -6347
265113                 Wp   =          117
02540
 YDOT =      -3943
000317  meter/sec      RA   =           42
11824  deg
 ZDOT =       1698
333536                 TA   =          316
59441
                                          MA   =          316
63439
                                          Ha   =            229
290  n
mi
                                          Hp   =            222
623

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4186818
13                 X    =        -1348662
34
 Y    =       13998999
52  feet           Y    =         4252219
01  meter
 Z    =       16818641
36                 Z    =         5119946
45
 XDOT =     -20824
360608                 XDOT =       -6310
951268
 YDOT =     -12936
352745  feet/sec       YDOT =       -4013
776888  meter/sec
 ZDOT =       5571
960419                 ZDOT =        1667
588649

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -14400075
74                 X    =        -4389143
09
 Y    =        2671615
04  feet           Y    =          814308
26  meter
 Z    =       16788937
50                 Z    =         5117268
15
 XDOT =       1997
131577                 XDOT =         608
725705
 YDOT =     -23430
903904  feet/sec       YDOT =       -7141
739510  meter/sec
 ZDOT =       5429
874277                 ZDOT =        1655
025680


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   20303
77349445  
00016717  00000-0  10270-3 0  9121
2 25544  51
6432  42
5298 0000665  32
6096 327
5094 15
48994420 12870


Satellite: ISS
Catalog Number: 25544
Epoch time:      20303
77349445   =   yrday
fracday
Element set:     912
Inclination:       51
6432  deg
RA of node:        42
5298  deg
Eccentricity:     
0000665     
Arg of perigee:    32
6096  deg
Mean anomaly:     327
5094  deg
Mean motion:   15
48994420  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1287
Checksum:              315


Coasting Arc #14 (Orbit 1301)
---------------------------------------

Vector Time (GMT): 2020/304/17:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938366
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         914533
97                 A    =         6793278
21  meter
 Y    =       -4366743
21  meter          E    =           
0013744
 Z    =       -5135241
77                 I    =           51
86573
 XDOT =       6650
597426                 Wp   =           75
19772
 YDOT =       3380
343036  meter/sec      RA   =           37
18987  deg
 ZDOT =      -1690
433207                 TA   =          178
48740
                                          MA   =          178
48324
                                          Ha   =            229
188  n
mi
                                          Hp   =            222
730

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3000439
53                 X    =          988240
97
 Y    =      -14326585
33  feet           Y    =        -4356104
23  meter
 Z    =      -16847906
08                 Z    =        -5130620
09
 XDOT =      21819
545361                 XDOT =        6620
514493
 YDOT =      11090
364292  feet/sec       YDOT =        3454
546548  meter/sec
 ZDOT =      -5546
040705                 ZDOT =       -1658
199503

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       14072284
90                 X    =         4289232
44
 Y    =       -4117264
87  feet           Y    =        -1254942
33  meter
 Z    =      -16826305
34                 Z    =        -5128657
87
 XDOT =        415
862610                 XDOT =         126
754924
 YDOT =      23472
940687  feet/sec       YDOT =        7154
552321  meter/sec
 ZDOT =      -5397
056830                 ZDOT =       -1645
022922


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   20304
74122779  
00016717  00000-0  10270-3 0  9139
2 25544  51
6441  37
7440 0000568  20
5940 339
5233 15
48982529 13024


Satellite: ISS
Catalog Number: 25544
Epoch time:      20304
74122779   =   yrday
fracday
Element set:     913
Inclination:       51
6441  deg
RA of node:        37
7440  deg
Eccentricity:     
0000568     
Arg of perigee:    20
5940  deg
Mean anomaly:     339
5233  deg
Mean motion:   15
48982529  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1302
Checksum:              297


Coasting Arc #15 (Orbit 1317)
---------------------------------------

Vector Time (GMT): 2020/305/17:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938366
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -536222
35                 A    =         6793229
63  meter
 Y    =        4423575
18  meter          E    =           
0005001
 Z    =        5124278
77                 I    =           51
83742
 XDOT =      -6928
879737                 Wp   =          115
90798
 YDOT =      -2802
199641  meter/sec      RA   =           32
25850  deg
 ZDOT =       1690
548099                 TA   =          317
77746
                                          MA   =          317
81596
                                          Ha   =            229
267  n
mi
                                          Hp   =            222
622

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -1759259
68                 X    =         -610539
78
 Y    =       14513041
94  feet           Y    =         4417163
25  meter
 Z    =       16811938
22                 Z    =         5121493
41
 XDOT =     -22732
545068                 XDOT =       -6905
241673
 YDOT =      -9193
568376  feet/sec       YDOT =       -2879
551169  meter/sec
 ZDOT =       5546
417648                 ZDOT =        1656
946774

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13549088
57                 X    =        -4129762
20
 Y    =        5530496
26  feet           Y    =         1685695
26  meter
 Z    =       16798823
11                 Z    =         5120281
28
 XDOT =      -2834
426847                 XDOT =        -863
933303
 YDOT =     -23353
438075  feet/sec       YDOT =       -7118
127925  meter/sec
 ZDOT =       5391
094275                 ZDOT =        1643
205535


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   20305
77347352  
00016717  00000-0  10270-3 0  9140
2 25544  51
6435  32
6377 0000753  28
2039 331
9151 15
48994852 13184


Satellite: ISS
Catalog Number: 25544
Epoch time:      20305
77347352   =   yrday
fracday
Element set:     914
Inclination:       51
6435  deg
RA of node:        32
6377  deg
Eccentricity:     
0000753     
Arg of perigee:    28
2039  deg
Mean anomaly:     331
9151  deg
Mean motion:   15
48994852  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1318
Checksum:              308


Coasting Arc #16 (Orbit 1332)
---------------------------------------

Vector Time (GMT): 2020/306/17:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938366
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         166321
74                 A    =         6793242
23  meter
 Y    =       -4460217
43  meter          E    =           
0014015
 Z    =       -5133844
14                 I    =           51
80763
 XDOT =       7131
641943                 Wp   =           74
86808
 YDOT =       2198
259000  meter/sec      RA   =           27
32653  deg
 ZDOT =      -1679
043551                 TA   =          178
91577
                                          MA   =          178
91273
                                          Ha   =            229
261  n
mi
                                          Hp   =            222
612

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         545675
00                 X    =          241122
90
 Y    =      -14633259
28  feet           Y    =        -4457939
19  meter
 Z    =      -16843320
68                 Z    =        -5132854
57
 XDOT =      23397
775404                 XDOT =        7114
686380
 YDOT =       7212
135828  feet/sec       YDOT =        2277
915358  meter/sec
 ZDOT =      -5508
673067                 ZDOT =       -1644
440944

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       12938788
83                 X    =         3943742
84
 Y    =       -6868772
11  feet           Y    =        -2093601
74  meter
 Z    =      -16838503
59                 Z    =        -5132375
89
 XDOT =       5199
448839                 XDOT =        1584
792006
 YDOT =      22904
212600  feet/sec       YDOT =        6981
204000  meter/sec
 ZDOT =      -5348
700975                 ZDOT =       -1630
284057


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   20306
74120192  
00016717  00000-0  10270-3 0  9150
2 25544  51
6430  27
8520 0000801  31
2865 328
8333 15
48989584 13330


Satellite: ISS
Catalog Number: 25544
Epoch time:      20306
74120192   =   yrday
fracday
Element set:     915
Inclination:       51
6430  deg
RA of node:        27
8520  deg
Eccentricity:     
0000801     
Arg of perigee:    31
2865  deg
Mean anomaly:     328
8333  deg
Mean motion:   15
48989584  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1333
Checksum:              294


Coasting Arc #17 (Orbit 1348)
---------------------------------------

Vector Time (GMT): 2020/307/17:20:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938366
5

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         213489
02                 A    =         6793231
02  meter
 Y    =        4452101
35  meter          E    =           
0004925
 Z    =        5123170
73                 I    =           51
77544
 XDOT =      -7307
816260                 Wp   =          114
78148
 YDOT =      -1582
634094  meter/sec      RA   =           22
39163  deg
 ZDOT =       1676
576547                 TA   =          319
02898
                                          MA   =          319
06598
                                          Ha   =            229
257  n
mi
                                          Hp   =            222
629

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         700423
28                 X    =          138802
25
 Y    =       14606631
72  feet           Y    =         4454070
96  meter
 Z    =       16808302
91                 Z    =         5124026
55
 XDOT =     -23975
775130                 XDOT =       -7297
719719
 YDOT =      -5192
369076  feet/sec       YDOT =       -1664
298944  meter/sec
 ZDOT =       5500
579222                 ZDOT =        1641
101463

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12144205
59                 X    =        -3701553
86
 Y    =        8138657
03  feet           Y    =         2480662
66  meter
 Z    =       16812015
40                 Z    =         5124302
29
 XDOT =      -7539
985414                 XDOT =       -2298
187554
 YDOT =     -22296
812434  feet/sec       YDOT =       -6796
068430  meter/sec
 ZDOT =       5336
550184                 ZDOT =        1626
580496


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   20307
77344441  
00016717  00000-0  10270-3 0  9160
2 25544  51
6415  22
7461 0000842  25
4494 334
6697 15
48988408 13498


Satellite: ISS
Catalog Number: 25544
Epoch time:      20307
77344441   =   yrday
fracday
Element set:     916
Inclination:       51
6415  deg
RA of node:        22
7461  deg
Eccentricity:     
0000842     
Arg of perigee:    25
4494  deg
Mean anomaly:     334
6697  deg
Mean motion:   15
48988408  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1349
Checksum:              322
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