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

 
Date: November 6th 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) : 19920 769 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


311/18:30:00 000 0 0 0 0 0 0
N/A 0 0 0 0 229 2
000/00:00:00 000 0 0 0 0 221 4

317/19:37:58 974 1 8 2 1 2 1
N/A -1 1 -0 2 229 1
000/00:05:57 948 0 2 0 1 222 5

320/00:49:48 000 0 0 0 0 0 0
N/A 0 0 0 0 228 9
000/00:00:00 000 0 0 0 0 222 6

320/09:04:15 000 0 0 0 0 0 0
N/A 0 0 0 0 229 0
000/00:00:00 000 0 0 0 0 222 6

Coasting Arc #1 (Orbit 1344)
---------------------------------------

Vector Time (GMT): 2020/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2707764
62                 A    =         6791628
05  meter
 Y    =       -3346033
21  meter          E    =           
0015831
 Z    =       -5267262
16                 I    =           51
78404
 XDOT =       6596
131390                 Wp   =           95
56839
 YDOT =       3736
076838  meter/sec      RA   =           23
45371  deg
 ZDOT =       1018
698805                 TA   =          184
18444
                                          MA   =          184
19770
                                          Ha   =            229
102  n
mi
                                          Hp   =            221
644

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        8883742
19                 X    =         2770565
83
 Y    =      -10977799
24  feet           Y    =        -3315401
74  meter
 Z    =      -17281043
83                 Z    =        -5253956
07
 XDOT =      21640
851017                 XDOT =        6548
914805
 YDOT =      12257
469941  feet/sec       YDOT =        3809
575477  meter/sec
 ZDOT =       3342
187679                 ZDOT =        1050
626606

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         486862
24                 X    =          148395
61
 Y    =       14188940
92  feet           Y    =         4324789
19  meter
 Z    =      -17219301
62                 Z    =        -5248443
13
 XDOT =     -23294
481096                 XDOT =       -7100
157838
 YDOT =       5029
722196  feet/sec       YDOT =        1533
059325  meter/sec
 ZDOT =       3489
689886                 ZDOT =        1063
657477


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
51431578  
00016717  00000-0  10270-3 0  9003
2 25544  51
6449  24
0155 0001679  77
5371 282
5967 15
49368251 13457


Satellite: ISS
Catalog Number: 25544
Epoch time:      20307
51431578   =   yrday
fracday
Element set:     900
Inclination:       51
6449  deg
RA of node:        24
0155  deg
Eccentricity:     
0001679     
Arg of perigee:    77
5371  deg
Mean anomaly:     282
5967  deg
Mean motion:   15
49368251  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1345
Checksum:              314


Coasting Arc #2 (Orbit 1360)
---------------------------------------

Vector Time (GMT): 2020/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2561217
39                 A    =         6791607
64  meter
 Y    =        3489584
21  meter          E    =           
0005502
 Z    =        5229660
80                 I    =           51
75326
 XDOT =      -6836
692238                 Wp   =           62
40272
 YDOT =      -3260
958631  meter/sec      RA   =           18
51337  deg
 ZDOT =      -1168
896089                 TA   =           38
81485
                                          MA   =           38
77535
                                          Ha   =            229
088  n
mi
                                          Hp   =            221
537

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8402944
21                 X    =        -2625452
03
 Y    =       11448767
08  feet           Y    =         3460583
42  meter
 Z    =       17157679
78                 Z    =         5217063
21
 XDOT =     -22430
092643                 XDOT =       -6794
041105
 YDOT =     -10698
683172  feet/sec       YDOT =       -3337
172894  meter/sec
 ZDOT =      -3834
960921                 ZDOT =       -1202
003557

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1404050
40                 X    =         -427954
56
 Y    =      -14202660
20  feet           Y    =        -4328970
83  meter
 Z    =       17099204
66                 Z    =         5211837
58
 XDOT =      22734
904592                 XDOT =        6929
598920
 YDOT =      -7062
373760  feet/sec       YDOT =       -2152
611522  meter/sec
 ZDOT =      -3987
933372                 ZDOT =       -1215
522092


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   20308
54630826  
00016717  00000-0  10270-3 0  9015
2 25544  51
6453  18
9082 0001551  81
4773 278
6553 15
49410029 13618


Satellite: ISS
Catalog Number: 25544
Epoch time:      20308
54630826   =   yrday
fracday
Element set:     901
Inclination:       51
6453  deg
RA of node:        18
9082  deg
Eccentricity:     
0001551     
Arg of perigee:    81
4773  deg
Mean anomaly:     278
6553  deg
Mean motion:   15
49410029  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1361
Checksum:              297


Coasting Arc #3 (Orbit 1375)
---------------------------------------

Vector Time (GMT): 2020/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2408083
20                 A    =         6791847
28  meter
 Y    =       -3649275
97  meter          E    =           
0015487
 Z    =       -5211101
77                 I    =           51
72056
 XDOT =       7013
191172                 Wp   =           97
71096
 YDOT =       2757
386331  meter/sec      RA   =           13
57098  deg
 ZDOT =       1311
195012                 TA   =          184
89478
                                          MA   =          184
90994
                                          Ha   =            229
106  n
mi
                                          Hp   =            221
607

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        7900535
44                 X    =         2474024
72
 Y    =      -11972690
18  feet           Y    =        -3621978
02  meter
 Z    =      -17096790
58                 Z    =        -5199244
02
 XDOT =      23009
157387                 XDOT =        6975
466812
 YDOT =       9046
543080  feet/sec       YDOT =        2835
601852  meter/sec
 ZDOT =       4301
820907                 ZDOT =        1345
171749

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        2373384
17                 X    =          723407
49
 Y    =       14213043
77  feet           Y    =         4332135
74  meter
 Z    =      -17041726
82                 Z    =        -5194318
33
 XDOT =     -21893
808118                 XDOT =       -6673
232714
 YDOT =       8996
981955  feet/sec       YDOT =        2742
280100  meter/sec
 ZDOT =       4458
832537                 ZDOT =        1359
052157


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   20309
51379895  
00016717  00000-0  10270-3 0  9020
2 25544  51
6447  14
1202 0001703  80
3078 279
8264 15
49374210 13767


Satellite: ISS
Catalog Number: 25544
Epoch time:      20309
51379895   =   yrday
fracday
Element set:     902
Inclination:       51
6447  deg
RA of node:        14
1202  deg
Eccentricity:     
0001703     
Arg of perigee:    80
3078  deg
Mean anomaly:     279
8264  deg
Mean motion:   15
49374210  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1376
Checksum:              301


Coasting Arc #4 (Orbit 1391)
---------------------------------------

Vector Time (GMT): 2020/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2251705
73                 A    =         6791860
40  meter
 Y    =        3786214
64  meter          E    =           
0006280
 Z    =        5165368
33                 I    =           51
68804
 XDOT =      -7175
079285                 Wp   =           61
65837
 YDOT =      -2260
479996  meter/sec      RA   =            8
62621  deg
 ZDOT =      -1466
584091                 TA   =           42
48093
                                          MA   =           42
43234
                                          Ha   =            229
115  n
mi
                                          Hp   =            221
475

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -7387485
99                 X    =        -2318967
91
 Y    =       12421964
03  feet           Y    =         3760657
99  meter
 Z    =       16946746
49                 Z    =         5154267
09
 XDOT =     -23540
286367                 XDOT =       -7142
144668
 YDOT =      -7416
272953  feet/sec       YDOT =       -2340
532626  meter/sec
 ZDOT =      -4811
627595                 ZDOT =       -1501
358722

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -3299217
92                 X    =        -1005601
62
 Y    =      -14132962
61  feet           Y    =        -4307727
00  meter
 Z    =       16895173
44                 Z    =         5149648
86
 XDOT =      20978
300121                 XDOT =        6394
185877
 YDOT =     -10858
171646  feet/sec       YDOT =       -3309
570718  meter/sec
 ZDOT =      -4972
350449                 ZDOT =       -1515
572417


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   20310
54578242  
00016717  00000-0  10270-3 0  9033
2 25544  51
6449   9
0128 0001689  82
8119 277
3223 15
49416673 13921


Satellite: ISS
Catalog Number: 25544
Epoch time:      20310
54578242   =   yrday
fracday
Element set:     903
Inclination:       51
6449  deg
RA of node:         9
0128  deg
Eccentricity:     
0001689     
Arg of perigee:    82
8119  deg
Mean anomaly:     277
3223  deg
Mean motion:   15
49416673  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1392
Checksum:              308


Coasting Arc #5 (Orbit 1406)
---------------------------------------

Vector Time (GMT): 2020/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        2081869
80                 A    =         6792137
15  meter
 Y    =       -3940134
32  meter          E    =           
0015185
 Z    =       -5139436
37                 I    =           51
65382
 XDOT =       7271
514604                 Wp   =           99
88569
 YDOT =       1743
908151  meter/sec      RA   =            3
67937  deg
 ZDOT =       1610
086681                 TA   =          185
67433
                                          MA   =          185
69156
                                          Ha   =            229
162  n
mi
                                          Hp   =            221
524

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        6830281
50                 X    =         2150739
71
 Y    =      -12926949
86  feet           Y    =        -3916467
92  meter
 Z    =      -16861667
87                 Z    =        -5129156
29
 XDOT =      23856
675210                 XDOT =        7243
652247
 YDOT =       5721
483434  feet/sec       YDOT =        1825
067542  meter/sec
 ZDOT =       5282
436618                 ZDOT =        1645
341905

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4293137
25                 X    =         1308548
23
 Y    =       14033419
48  feet           Y    =         4277386
26  meter
 Z    =      -16813885
08                 Z    =        -5124872
17
 XDOT =     -19808
071618                 XDOT =       -6037
500229
 YDOT =      12578
044828  feet/sec       YDOT =        3833
788064  meter/sec
 ZDOT =       5445
405555                 ZDOT =        1659
759613


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   20311
51326681  
00016717  00000-0  10270-3 0  9040
2 25544  51
6439   4
2249 0001858  84
8443 275
2919 15
49377859 14079


Satellite: ISS
Catalog Number: 25544
Epoch time:      20311
51326681   =   yrday
fracday
Element set:     904
Inclination:       51
6439  deg
RA of node:         4
2249  deg
Eccentricity:     
0001858     
Arg of perigee:    84
8443  deg
Mean anomaly:     275
2919  deg
Mean motion:   15
49377859  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1407
Checksum:              323


Coasting Arc #6 (Orbit 1410)
---------------------------------------

Vector Time (GMT): 2020/311/18:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6791845
64                 A    =         6803078
96  meter
 Y    =          67136
07  meter          E    =           
0013218
 Z    =        -267648
07                 I    =           51
67983
 XDOT =        181
652576                 Wp   =           48
41967
 YDOT =       4755
848101  meter/sec      RA   =            2
35099  deg
 ZDOT =       6003
097742                 TA   =          308
70361
                                          MA   =          308
82174
                                          Ha   =            229
174  n
mi
                                          Hp   =            221
390

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22282958
15                 X    =         6791890
22
 Y    =         220262
71  feet           Y    =          143087
63  meter
 Z    =        -878110
46                 Z    =         -234655
30
 XDOT =        595
973019                 XDOT =          99
297666
 YDOT =      15603
176185  feet/sec       YDOT =        4757
418582  meter/sec
 ZDOT =      19695
202565                 ZDOT =        6003
780453

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       17673600
70                 X    =         5386913
49
 Y    =       13581873
67  feet           Y    =         4139755
10  meter
 Z    =        -725509
22                 Z    =         -221135
21
 XDOT =      -8026
711565                 XDOT =       -2446
541685
 YDOT =      11454
554318  feet/sec       YDOT =        3491
348156  meter/sec
 ZDOT =      19698
079504                 ZDOT =        6003
974633


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   20311
77126225  
00016717  00000-0  10270-3 0  9051
2 25544  51
6422   2
9486 0001944  81
5697 278
5674 15
49402683 14113


Satellite: ISS
Catalog Number: 25544
Epoch time:      20311
77126225   =   yrday
fracday
Element set:     905
Inclination:       51
6422  deg
RA of node:         2
9486  deg
Eccentricity:     
0001944     
Arg of perigee:    81
5697  deg
Mean anomaly:     278
5674  deg
Mean motion:   15
49402683  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1411
Checksum:              308


Coasting Arc #7 (Orbit 1426)
---------------------------------------

Vector Time (GMT): 2020/312/18:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6785457
23                 A    =         6803119
26  meter
 Y    =         390244
38  meter          E    =           
0013424
 Z    =         104148
36                 I    =           51
64747
 XDOT =       -372
918437                 Wp   =          127
05044
 YDOT =      -4740
495107  meter/sec      RA   =          357
40314  deg
 ZDOT =      -6006
407386                 TA   =           51
83006
                                          MA   =           51
70919
                                          Ha   =            229
118  n
mi
                                          Hp   =            221
459

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -22261998
79                 X    =        -6789822
65
 Y    =        1280329
32  feet           Y    =          314340
11  meter
 Z    =         341694
10                 Z    =           71176
26
 XDOT =      -1223
485686                 XDOT =        -290
705005
 YDOT =     -15552
805468  feet/sec       YDOT =       -4744
205314  meter/sec
 ZDOT =     -19706
060978                 ZDOT =       -6008
019494

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -18766480
05                 X    =        -5720023
12
 Y    =      -12047241
59  feet           Y    =        -3671999
24  meter
 Z    =         189169
04                 Z    =           57658
72
 XDOT =       7380
826913                 XDOT =        2249
676043
 YDOT =     -11856
021453  feet/sec       YDOT =       -3613
715339  meter/sec
 ZDOT =     -19713
239003                 ZDOT =       -6008
595248


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   20312
80323953  
00016717  00000-0  10270-3 0  9064
2 25544  51
6437 357
8406 0001875  82
1878 277
9478 15
49395986 14273


Satellite: ISS
Catalog Number: 25544
Epoch time:      20312
80323953   =   yrday
fracday
Element set:     906
Inclination:       51
6437  deg
RA of node:       357
8406  deg
Eccentricity:     
0001875     
Arg of perigee:    82
1878  deg
Mean anomaly:     277
9478  deg
Mean motion:   15
49395986  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1427
Checksum:              351


Coasting Arc #8 (Orbit 1442)
---------------------------------------

Vector Time (GMT): 2020/313/18:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6739982
33                 A    =         6803076
63  meter
 Y    =        -879262
32  meter          E    =           
0013745
 Z    =          17118
17                 I    =           51
61355
 XDOT =        592
361784                 Wp   =           50
62613
 YDOT =       4720
365238  meter/sec      RA   =          352
45316  deg
 ZDOT =       6005
105274                 TA   =          309
55796
                                          MA   =          309
67931
                                          Ha   =            229
143  n
mi
                                          Hp   =            221
380

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       22112802
93                 X    =         6749230
43
 Y    =       -2884718
90  feet           Y    =         -803839
29  meter
 Z    =          56161
97                 Z    =           49881
17
 XDOT =       1943
444172                 XDOT =         510
363505
 YDOT =      15486
762593  feet/sec       YDOT =        4726
530719  meter/sec
 ZDOT =      19701
788957                 ZDOT =        6007
783807

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       19766824
66                 X    =         6024928
16
 Y    =       10321351
57  feet           Y    =         3145947
96  meter
 Z    =         207738
98                 Z    =           63318
84
 XDOT =      -6650
364603                 XDOT =       -2027
031131
 YDOT =      12282
090816  feet/sec       YDOT =        3743
581281  meter/sec
 ZDOT =      19713
903509                 ZDOT =        6008
797790


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   20313
83521233  
00016717  00000-0  10270-3 0  9070
2 25544  51
6435 352
7333 0001907  84
6017 275
5351 15
49410973 14438


Satellite: ISS
Catalog Number: 25544
Epoch time:      20313
83521233   =   yrday
fracday
Element set:     907
Inclination:       51
6435  deg
RA of node:       352
7333  deg
Eccentricity:     
0001907     
Arg of perigee:    84
6017  deg
Mean anomaly:     275
5351  deg
Mean motion:   15
49410973  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1443
Checksum:              292


Coasting Arc #9 (Orbit 1457)
---------------------------------------

Vector Time (GMT): 2020/314/18:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6664376
60                 A    =         6803084
45  meter
 Y    =        1327270
59  meter          E    =           
0012929
 Z    =        -184701
24                 I    =           51
58029
 XDOT =       -777
988588                 Wp   =          129
10131
 YDOT =      -4700
684014  meter/sec      RA   =          347
50110  deg
 ZDOT =      -5998
423132                 TA   =           52
88609
                                          MA   =           52
76802
                                          Ha   =            229
136  n
mi
                                          Hp   =            221
410

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21864752
62                 X    =        -6677826
04
 Y    =        4354562
31  feet           Y    =         1252669
55  meter
 Z    =        -605975
20                 Z    =         -217107
20
 XDOT =      -2552
455999                 XDOT =        -696
229035
 YDOT =     -15422
191648  feet/sec       YDOT =       -4708
926752  meter/sec
 ZDOT =     -19679
865920                 ZDOT =       -6002
003873

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -20555037
19                 X    =        -6265175
33
 Y    =       -8620664
99  feet           Y    =        -2627578
69  meter
 Z    =        -755914
84                 Z    =         -230402
84
 XDOT =       5996
204494                 XDOT =        1827
643130
 YDOT =     -12637
194882  feet/sec       YDOT =       -3851
817000  meter/sec
 ZDOT =     -19696
158000                 ZDOT =       -6003
388958


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   20314
80268498  
00016717  00000-0  10270-3 0  9080
2 25544  51
6437 347
9451 0001955  85
4965 274
6409 15
49400431 14589


Satellite: ISS
Catalog Number: 25544
Epoch time:      20314
80268498   =   yrday
fracday
Element set:     908
Inclination:       51
6437  deg
RA of node:       347
9451  deg
Eccentricity:     
0001955     
Arg of perigee:    85
4965  deg
Mean anomaly:     274
6409  deg
Mean motion:   15
49400431  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1458
Checksum:              333


Coasting Arc #10 (Orbit 1473)
---------------------------------------

Vector Time (GMT): 2020/315/18:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6546502
41                 A    =         6803025
42  meter
 Y    =       -1801409
93  meter          E    =           
0014188
 Z    =         308481
10                 I    =           51
54678
 XDOT =        994
961869                 Wp   =           53
47178
 YDOT =       4672
893131  meter/sec      RA   =          342
54703  deg
 ZDOT =       5989
370991                 TA   =          309
85070
                                          MA   =          309
97543
                                          Ha   =            229
131  n
mi
                                          Hp   =            221
373

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21478026
27                 X    =         6564661
32
 Y    =       -5910137
57  feet           Y    =        -1728100
71  meter
 Z    =        1012077
12                 Z    =          340326
01
 XDOT =       3264
310593                 XDOT =         913
540849
 YDOT =      15331
014209  feet/sec       YDOT =        4683
564208  meter/sec
 ZDOT =      19650
167292                 ZDOT =        5994
006475

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21221715
37                 X    =         6468378
84
 Y    =        6749381
17  feet           Y    =         2057211
38  meter
 Z    =        1159434
84                 Z    =          353395
74
 XDOT =      -5241
874909                 XDOT =       -1597
723472
 YDOT =      13012
151130  feet/sec       YDOT =        3966
103664  meter/sec
 ZDOT =      19671
342237                 ZDOT =        5995
825114


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   20315
83465310  
00016717  00000-0  10270-3 0  9097
2 25544  51
6431 342
8382 0001896  89
7959 270
3408 15
49411313 14745


Satellite: ISS
Catalog Number: 25544
Epoch time:      20315
83465310   =   yrday
fracday
Element set:     909
Inclination:       51
6431  deg
RA of node:       342
8382  deg
Eccentricity:     
0001896     
Arg of perigee:    89
7959  deg
Mean anomaly:     270
3408  deg
Mean motion:   15
49411313  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1474
Checksum:              316


Coasting Arc #11 (Orbit 1488)
---------------------------------------

Vector Time (GMT): 2020/316/18:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6404169
32                 A    =         6802961
52  meter
 Y    =        2229271
62  meter          E    =           
0012312
 Z    =        -478673
01                 I    =           51
51583
 XDOT =      -1180
016815                 Wp   =          131
82849
 YDOT =      -4649
274972  meter/sec      RA   =          337
59016  deg
 ZDOT =      -5972
467179                 TA   =           53
33248
                                          MA   =           53
21937
                                          Ha   =            229
081  n
mi
                                          Hp   =            221
417

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21011054
21                 X    =        -6426296
58
 Y    =        7313883
26  feet           Y    =         2157531
88  meter
 Z    =       -1570449
52                 Z    =         -509836
30
 XDOT =      -3871
446244                 XDOT =       -1098
928132
 YDOT =     -15253
526810  feet/sec       YDOT =       -4662
017372  meter/sec
 ZDOT =     -19594
708594                 ZDOT =       -5978
002396

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21680477
17                 X    =        -6608209
44
 Y    =       -4943726
99  feet           Y    =        -1506847
99  meter
 Z    =       -1714663
90                 Z    =         -522629
56
 XDOT =       4566
211761                 XDOT =        1391
781345
 YDOT =     -13331
847662  feet/sec       YDOT =       -4063
547167  meter/sec
 ZDOT =     -19620
047852                 ZDOT =       -5980
190585


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   20316
80212009  
00016717  00000-0  10270-3 0  9102
2 25544  51
6443 338
0497 0001861  92
5544 267
5820 15
49410513 14899


Satellite: ISS
Catalog Number: 25544
Epoch time:      20316
80212009   =   yrday
fracday
Element set:     910
Inclination:       51
6443  deg
RA of node:       338
0497  deg
Eccentricity:     
0001861     
Arg of perigee:    92
5544  deg
Mean anomaly:     267
5820  deg
Mean motion:   15
49410513  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1489
Checksum:              295


Coasting Arc #12 (Orbit 1504)
---------------------------------------

Vector Time (GMT): 2020/317/18:30:00
000
Vector Time (MET): N/A
Weight (LBS)     : 938443
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6218146
19                 A    =         6802894
87  meter
 Y    =       -2675648
66  meter          E    =           
0014632
 Z    =         606199
05                 I    =           51
48423
 XDOT =       1395
677740                 Wp   =           56
35985
 YDOT =       4614
443794  meter/sec      RA   =          332
63091  deg
 ZDOT =       5955
055106                 TA   =          310
18577
                                          MA   =          310
31377
                                          Ha   =            229
123  n
mi
                                          Hp   =            221
360

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20400742
09                 X    =         6244659
31
 Y    =       -8778374
86  feet           Y    =        -2605964
64  meter
 Z    =        1988842
02                 Z    =          636469
48
 XDOT =       4578
995211                 XDOT =        1315
046953
 YDOT =      15139
251292  feet/sec       YDOT =        4629
600400  meter/sec
 ZDOT =      19537
582369                 ZDOT =        5961
639107

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21992680
50                 X    =         6703369
02
 Y    =        2999210
37  feet           Y    =          914159
32  meter
 Z    =        2128938
04                 Z    =          648900
31
 XDOT =      -3785
383416                 XDOT =       -1153
784865
 YDOT =      13658
992644  feet/sec       YDOT =        4163
260958  meter/sec
 ZDOT =      19567
773755                 ZDOT =        5964
257440


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   20317
83408123  
00016717  00000-0  10270-3 0  9111
2 25544  51
6437 332
9420 0001908  92
2711 267
8658 15
49413528 15056


Satellite: ISS
Catalog Number: 25544
Epoch time:      20317
83408123   =   yrday
fracday
Element set:     911
Inclination:       51
6437  deg
RA of node:       332
9420  deg
Eccentricity:     
0001908     
Arg of perigee:    92
2711  deg
Mean anomaly:     267
8658  deg
Mean motion:   15
49413528  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1505
Checksum:              301


Coasting Arc #13 (Orbit 1504)
---------------------------------------

Vector Time (GMT): 2020/317/19:40:57
948
Vector Time (MET): N/A
Weight (LBS)     : 938222
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -700502
01                 A    =         6792718
40  meter
 Y    =       -4318725
16  meter          E    =           
0014245
 Z    =       -5208682
03                 I    =           51
44673
 XDOT =       7085
016625                 Wp   =           99
34475
 YDOT =      -2614
940285  meter/sec      RA   =          332
36998  deg
 ZDOT =       1215
897141                 TA   =          182
37932
                                          MA   =          182
38610
                                          Ha   =            229
086  n
mi
                                          Hp   =            222
538

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -2298234
95                 X    =         -626855
24
 Y    =      -14169045
79  feet           Y    =        -4326146
86  meter
 Z    =      -17088851
80                 Z    =        -5211906
02
 XDOT =      23244
805200                 XDOT =        7107
824825
 YDOT =      -8579
200409  feet/sec       YDOT =       -2535
583019  meter/sec
 ZDOT =       3989
163849                 ZDOT =        1250
369602

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        1130121
94                 X    =          344461
17
 Y    =      -14292125
90  feet           Y    =        -4356239
97  meter
 Z    =      -17103524
78                 Z    =        -5213154
35
 XDOT =      23524
153360                 XDOT =        7170
161944
 YDOT =      -3102
322045  feet/sec       YDOT =        -945
587759  meter/sec
 ZDOT =       4148
683390                 ZDOT =        1264
518697


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   20317
83408092  
00016717  00000-0  10270-3 0  9127
2 25544  51
6453 332
9421 0000243 106
7194 253
3983 15
49048324 15051


Satellite: ISS
Catalog Number: 25544
Epoch time:      20317
83408092   =   yrday
fracday
Element set:     912
Inclination:       51
6453  deg
RA of node:       332
9421  deg
Eccentricity:     
0000243     
Arg of perigee:   106
7194  deg
Mean anomaly:     253
3983  deg
Mean motion:   15
49048324  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1505
Checksum:              292


Coasting Arc #14 (Orbit 1520)
---------------------------------------

Vector Time (GMT): 2020/318/19:40:57
948
Vector Time (MET): N/A
Weight (LBS)     : 938222
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1040148
07                 A    =         6792631
72  meter
 Y    =        4251343
60  meter          E    =           
0004317
 Z    =        5191923
75                 I    =           51
41654
 XDOT =      -6850
197240                 Wp   =           56
55303
 YDOT =       3200
245406  meter/sec      RA   =          327
41011  deg
 ZDOT =      -1245
033439                 TA   =           45
46124
                                          MA   =           45
42599
                                          Ha   =            228
954  n
mi
                                          Hp   =            222
566

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3412559
27                 X    =          967310
83
 Y    =       13947977
68  feet           Y    =         4262567
89  meter
 Z    =       17033870
56                 Z    =         5196799
72
 XDOT =     -22474
400395                 XDOT =       -6879
426394
 YDOT =      10499
492802  feet/sec       YDOT =        3123
478184  meter/sec
 ZDOT =      -4084
755376                 ZDOT =       -1278
380880

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         252073
42                 X    =           76831
98
 Y    =       14330645
24  feet           Y    =         4367980
67  meter
 Z    =       17056185
23                 Z    =         5198725
26
 XDOT =     -23121
010599                 XDOT =       -7047
284031
 YDOT =       5464
038953  feet/sec       YDOT =        1665
439073  meter/sec
 ZDOT =      -4239
091990                 ZDOT =       -1292
075239


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   20318
86629564  
00016717  00000-0  10270-3 0  9131
2 25544  51
6445 327
8363 0000139 107
3370 252
7796 15
49082296 15216


Satellite: ISS
Catalog Number: 25544
Epoch time:      20318
86629564   =   yrday
fracday
Element set:     913
Inclination:       51
6445  deg
RA of node:       327
8363  deg
Eccentricity:     
0000139     
Arg of perigee:   107
3370  deg
Mean anomaly:     252
7796  deg
Mean motion:   15
49082296  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1521
Checksum:              321


Coasting Arc #15 (Orbit 1535)
---------------------------------------

Vector Time (GMT): 2020/319/19:40:57
948
Vector Time (MET): N/A
Weight (LBS)     : 938222
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -1385571
17                 A    =         6792729
14  meter
 Y    =       -4167451
02  meter          E    =           
0014056
 Z    =       -5194555
27                 I    =           51
38873
 XDOT =       6543
475689                 Wp   =           99
81899
 YDOT =      -3754
119623  meter/sec      RA   =          322
44784  deg
 ZDOT =       1267
046983                 TA   =          182
41570
                                          MA   =          182
42250
                                          Ha   =            229
023  n
mi
                                          Hp   =            222
544

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -4545837
18                 X    =        -1313633
56
 Y    =      -13672739
57  feet           Y    =        -4182542
95  meter
 Z    =      -17042504
16                 Z    =        -5201111
54
 XDOT =      21468
096093                 XDOT =        6578
814286
 YDOT =     -12316
665431  feet/sec       YDOT =       -3680
748262  meter/sec
 ZDOT =       4156
978291                 ZDOT =        1298
919211

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -1663694
18                 X    =         -507093
98
 Y    =      -14276349
09  feet           Y    =        -4351431
20  meter
 Z    =      -17072591
18                 Z    =        -5203725
79
 XDOT =      22395
919629                 XDOT =        6826
276303
 YDOT =      -7755
201584  feet/sec       YDOT =       -2363
785443  meter/sec
 ZDOT =       4304
515564                 ZDOT =        1312
016344


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   20319
83399727  
00016717  00000-0  10270-3 0  9145
2 25544  51
6445 323
0493 0000127 122
6812 237
4350 15
49058548 15361


Satellite: ISS
Catalog Number: 25544
Epoch time:      20319
83399727   =   yrday
fracday
Element set:     914
Inclination:       51
6445  deg
RA of node:       323
0493  deg
Eccentricity:     
0000127     
Arg of perigee:   122
6812  deg
Mean anomaly:     237
4350  deg
Mean motion:   15
49058548  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1536
Checksum:              310


Coasting Arc #16 (Orbit 1539)
---------------------------------------

Vector Time (GMT): 2020/320/00:49:48
000
Vector Time (MET): N/A
Weight (LBS)     : 938222
2

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        5791929
08                 A    =         6799289
07  meter
 Y    =       -1212321
28  meter          E    =           
0012585
 Z    =        3338054
36                 I    =           51
40045
 XDOT =      -1453
363275                 Wp   =           91
04334
 YDOT =       5911
763245  meter/sec      RA   =          321
41433  deg
 ZDOT =       4653
333176                 TA   =          307
90877
                                          MA   =          308
02249
                                          Ha   =            228
935  n
mi
                                          Hp   =            222
567

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       19002391
99                 X    =         5788840
31
 Y    =       -3977432
03  feet           Y    =        -1147569
26  meter
 Z    =       10951621
93                 Z    =         3366182
56
 XDOT =      -4768
252215                 XDOT =       -1541
966292
 YDOT =      19395
548703  feet/sec       YDOT =        5895
014987  meter/sec
 ZDOT =      15266
841129                 ZDOT =        4646
058262

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4025823
06                 X    =         1227070
87
 Y    =      -18916585
88  feet           Y    =        -5765775
38  meter
 Z    =       11081715
44                 Z    =         3377706
87
 XDOT =      14383
703716                 XDOT =        4384
152893
 YDOT =      12014
265570  feet/sec       YDOT =        3661
948146  meter/sec
 ZDOT =      15232
897730                 ZDOT =        4642
987228


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   20320
09204948  
00016717  00000-0  10270-3 0  9156
2 25544  51
6399 321
7678 0000480 166
0935 194
0228 15
49062300 15407


Satellite: ISS
Catalog Number: 25544
Epoch time:      20320
09204948   =   yrday
fracday
Element set:     915
Inclination:       51
6399  deg
RA of node:       321
7678  deg
Eccentricity:     
0000480     
Arg of perigee:   166
0935  deg
Mean anomaly:     194
0228  deg
Mean motion:   15
49062300  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1540
Checksum:              297


Coasting Arc #17 (Orbit 1544)
---------------------------------------

Vector Time (GMT): 2020/320/09:04:15
000
Vector Time (MET): N/A
Weight (LBS)     : 965317
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -3554408
34                 A    =         6802012
23  meter
 Y    =        5347273
26  meter          E    =           
0014058
 Z    =        2224828
70                 I    =           51
40372
 XDOT =      -5260
230069                 Wp   =          109
19724
 YDOT =      -1225
198331  meter/sec      RA   =          319
66824  deg
 ZDOT =      -5435
428249                 TA   =           46
03697
                                          MA   =           45
92109
                                          Ha   =            229
030  n
mi
                                          Hp   =            222
582

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -11661444
70                 X    =        -3624746
26
 Y    =       17543547
45  feet           Y    =         5307131
87  meter
 Z    =        7299306
77                 Z    =         2207391
82
 XDOT =     -17257
972667                 XDOT =       -5219
735595
 YDOT =      -4019
679563  feet/sec       YDOT =       -1283
795174  meter/sec
 ZDOT =     -17832
769847                 ZDOT =       -5460
882882

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        8463118
95                 X    =         2579558
66
 Y    =      -19321368
38  feet           Y    =        -5889153
08  meter
 Z    =        7218418
84                 Z    =         2200174
06
 XDOT =      16165
505497                 XDOT =        4927
246076
 YDOT =        345
248938  feet/sec       YDOT =         105
231876  meter/sec
 ZDOT =     -17950
373883                 ZDOT =       -5471
273959


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   20320
41461535  
00016717  00000-0  10270-3 0  9160
2 25544  51
6431 320
1748 0000261 143
4756 216
6412 15
49078331 15454


Satellite: ISS
Catalog Number: 25544
Epoch time:      20320
41461535   =   yrday
fracday
Element set:     916
Inclination:       51
6431  deg
RA of node:       320
1748  deg
Eccentricity:     
0000261     
Arg of perigee:   143
4756  deg
Mean anomaly:     216
6412  deg
Mean motion:   15
49078331  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1545
Checksum:              278


Coasting Arc #18 (Orbit 1559)
---------------------------------------

Vector Time (GMT): 2020/321/09:04:15
000
Vector Time (MET): N/A
Weight (LBS)     : 965317
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        3089226
14                 A    =         6802030
95  meter
 Y    =       -5638528
90  meter          E    =           
0006177
 Z    =       -2216388
55                 I    =           51
37933
 XDOT =       5331
737767                 Wp   =           46
04542
 YDOT =        788
864317  meter/sec      RA   =          314
70314  deg
 ZDOT =       5438
241972                 TA   =          289
30048
                                          MA   =          289
36727
                                          Ha   =            229
089  n
mi
                                          Hp   =            222
532

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       10135256
35                 X    =         3162814
50
 Y    =      -18499110
58  feet           Y    =        -5603571
27  meter
 Z    =       -7271615
97                 Z    =        -2201203
75
 XDOT =      17492
577977                 XDOT =        5296
103629
 YDOT =       2588
137523  feet/sec       YDOT =         848
287830  meter/sec
 ZDOT =      17842
001221                 ZDOT =        5464
055672

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6448258
14                 X    =        -1965429
08
 Y    =       20109217
81  feet           Y    =         6129289
59  meter
 Z    =       -7201127
57                 Z    =        -2194903
68
 XDOT =     -16077
665923                 XDOT =       -4900
472573
 YDOT =       1260
214128  feet/sec       YDOT =         384
113266  meter/sec
 ZDOT =      17961
287371                 ZDOT =        5474
600391


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   20321
38231219  
00016717  00000-0  10270-3 0  9172
2 25544  51
6437 315
3877 0000400 131
4161 228
7024 15
49072947 15608


Satellite: ISS
Catalog Number: 25544
Epoch time:      20321
38231219   =   yrday
fracday
Element set:     917
Inclination:       51
6437  deg
RA of node:       315
3877  deg
Eccentricity:     
0000400     
Arg of perigee:   131
4161  deg
Mean anomaly:     228
7024  deg
Mean motion:   15
49072947  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1560
Checksum:              284


Coasting Arc #19 (Orbit 1575)
---------------------------------------

Vector Time (GMT): 2020/322/09:04:15
000
Vector Time (MET): N/A
Weight (LBS)     : 965317
1

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2628214
38                 A    =         6802111
44  meter
 Y    =        5878167
98  meter          E    =           
0014182
 Z    =        2172056
83                 I    =           51
35647
 XDOT =      -5365
045708                 Wp   =          109
41976
 YDOT =       -372
834677  meter/sec      RA   =          309
73692  deg
 ZDOT =      -5458
171528                 TA   =           46
42326
                                          MA   =           46
30561
                                          Ha   =            229
077  n
mi
                                          Hp   =            222
533

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8622750
58                 X    =        -2704301
31
 Y    =       19285328
02  feet           Y    =         5848351
71  meter
 Z    =        7126170
71                 Z    =         2159105
63
 XDOT =     -17601
855998                 XDOT =       -5333
964608
 YDOT =      -1223
210883  feet/sec       YDOT =        -432
656030  meter/sec
 ZDOT =     -17907
386904                 ZDOT =       -5484
157902

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        4457217
83                 X    =         1358559
99
 Y    =      -20670337
57  feet           Y    =        -6300318
89  meter
 Z    =        7066000
80                 Z    =         2153717
05
 XDOT =      15842
239384                 XDOT =        4828
714564
 YDOT =      -2774
278552  feet/sec       YDOT =        -845
600103  meter/sec
 ZDOT =     -18027
494570                 ZDOT =       -5494
780345


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   20322
41451797  
00016717  00000-0  10270-3 0  9183
2 25544  51
6435 310
2816 0000325 114
8706 245
2478 15
49073582 15769


Satellite: ISS
Catalog Number: 25544
Epoch time:      20322
41451797   =   yrday
fracday
Element set:     918
Inclination:       51
6435  deg
RA of node:       310
2816  deg
Eccentricity:     
0000325     
Arg of perigee:   114
8706  deg
Mean anomaly:     245
2478  deg
Mean motion:   15
49073582  rev/day
Decay rate:    1
67170E-04  rev/day^2
Epoch rev:            1576
Checksum:              306
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