ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13289 1238 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 475 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
200/12:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
8
000/00:00:00
000 0
0 0
0 221
5
202/16:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
5
000/00:00:00
000 0
0 0
0 221
6
205/14:26:22
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 221
6
205/17:47:57
000 0
0 0
0 0
0
N/A 0
0 0
0 228
4
000/00:00:00
000 0
0 0
0 221
6
206/00:32:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 221
7
Coasting Arc #1 (Orbit 3639)
---------------------------------------
Vector Time (GMT): 2020/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 968616
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4975188
31 A = 6801395
04 meter
Y = 4236013
64 meter E =
0008641
Z = -1878048
80 I = 51
47277
XDOT = -4440
018857 Wp = 137
07955
YDOT = 2738
438402 meter/sec RA = 207
18294 deg
ZDOT = -5606
962613 TA = 63
59740
MA = 63
50874
Ha = 228
853 n
mi
Hp = 221
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16322796
28 X = 4936572
61
Y = 13897682
53 feet Y = 4291434
08 meter
Z = -6161577
44 Z = -1853974
61
XDOT = -14566
991000 XDOT = -4443
075621
YDOT = 8984
377958 feet/sec YDOT = 2688
770611 meter/sec
ZDOT = -18395
546629 ZDOT = -5628
537439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6435076
87 X = 1961411
43
Y = -20482222
53 feet Y = -6242981
43 meter
Z = -6050838
01 Z = -1844295
42
XDOT = 12400
796331 XDOT = 3779
762722
YDOT = 9338
657877 feet/sec YDOT = 2846
422921 meter/sec
ZDOT = -18494
955928 ZDOT = -5637
262567
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 20197
52866404
00016717 00000-0 10270-3 0 9001
2 25544 51
6397 208
2028 0001552 115
4559 244
6752 15
49494647 36404
Satellite: ISS
Catalog Number: 25544
Epoch time: 20197
52866404 = yrday
fracday
Element set: 900
Inclination: 51
6397 deg
RA of node: 208
2028 deg
Eccentricity:
0001552
Arg of perigee: 115
4559 deg
Mean anomaly: 244
6752 deg
Mean motion: 15
49494647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3640
Checksum: 319
Coasting Arc #2 (Orbit 3655)
---------------------------------------
Vector Time (GMT): 2020/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 968616
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5205528
10 A = 6801068
48 meter
Y = -3868087
36 meter E =
0014826
Z = 2026678
46 I = 51
50198
XDOT = 4378
158515 Wp = 72
81495
YDOT = -2972
907101 meter/sec RA = 202
22289 deg
ZDOT = 5541
939292 TA = 309
58817
MA = 309
71900
Ha = 228
733 n
mi
Hp = 221
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17078504
27 X = -5171731
50
Y = -12690575
33 feet Y = -3926110
63 meter
Z = 6649207
56 Z = 2001473
68
XDOT = 14364
037122 XDOT = 4384
157645
YDOT = -9753
632220 feet/sec YDOT = -2923
914715 meter/sec
ZDOT = 18182
215525 ZDOT = 5563
220669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4670726
57 X = -1423637
46
Y = 20795171
29 feet Y = 6338368
21 meter
Z = 6533233
19 Z = 1991329
47
XDOT = -13166
440414 XDOT = -4013
131038
YDOT = -8731
161232 feet/sec YDOT = -2661
257943 meter/sec
ZDOT = 18280
292007 ZDOT = 5571
833004
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 20198
56056455
00016717 00000-0 10270-3 0 9014
2 25544 51
6392 203
0949 0001398 119
2975 240
8315 15
49527705 36568
Satellite: ISS
Catalog Number: 25544
Epoch time: 20198
56056455 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 203
0949 deg
Eccentricity:
0001398
Arg of perigee: 119
2975 deg
Mean anomaly: 240
8315 deg
Mean motion: 15
49527705 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3656
Checksum: 326
Coasting Arc #3 (Orbit 3670)
---------------------------------------
Vector Time (GMT): 2020/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 968616
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5383307
72 A = 6800798
07 meter
Y = 3514245
04 meter E =
0007609
Z = -2213060
85 I = 51
53245
XDOT = -4321
462957 Wp = 133
85317
YDOT = 3195
373964 meter/sec RA = 197
26387 deg
ZDOT = -5454
808717 TA = 70
71162
MA = 70
62933
Ha = 228
819 n
mi
Hp = 221
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17661770
74 X = 5354359
98
Y = 11529675
32 feet Y = 3574283
54 meter
Z = -7260698
32 Z = -2186980
78
XDOT = -14178
028074 XDOT = -4330
377289
YDOT = 10483
510382 feet/sec YDOT = 3146
999352 meter/sec
ZDOT = -17896
354060 ZDOT = -5475
821639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3012010
12 X = 918060
68
Y = -20917170
74 feet Y = -6375553
64 meter
Z = -7140662
60 Z = -2176473
96
XDOT = 13896
223157 XDOT = 4235
568818
YDOT = 8124
263869 feet/sec YDOT = 2476
275627 meter/sec
ZDOT = -17993
213559 ZDOT = -5484
331493
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 20199
52797239
00016717 00000-0 10270-3 0 9024
2 25544 51
6390 198
3052 0001491 115
5734 244
5571 15
49506309 36712
Satellite: ISS
Catalog Number: 25544
Epoch time: 20199
52797239 = yrday
fracday
Element set: 902
Inclination: 51
6390 deg
RA of node: 198
3052 deg
Eccentricity:
0001491
Arg of perigee: 115
5734 deg
Mean anomaly: 244
5571 deg
Mean motion: 15
49506309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3671
Checksum: 320
Coasting Arc #4 (Orbit 3686)
---------------------------------------
Vector Time (GMT): 2020/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 968616
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5551904
89 A = 6800425
56 meter
Y = -3126722
18 meter E =
0014683
Z = 2357985
02 I = 51
56345
XDOT = 4234
795547 Wp = 77
24061
YDOT = -3444
648172 meter/sec RA = 192
30808 deg
ZDOT = 5378
075188 TA = 309
05988
MA = 309
19044
Ha = 228
691 n
mi
Hp = 221
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18214911
05 X = -5527981
92
Y = -10258274
88 feet Y = -3188674
19 meter
Z = 7736171
34 Z = 2331073
93
XDOT = 13893
686178 XDOT = 4246
876607
YDOT = -11301
339146 feet/sec YDOT = -3397
225052 meter/sec
ZDOT = 17644
603636 ZDOT = 5398
674663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1264972
11 X = -385563
50
Y = 20912117
38 feet Y = 6374013
38 meter
Z = 7612274
79 Z = 2320221
36
XDOT = -14650
566346 XDOT = -4465
492622
YDOT = -7374
167064 feet/sec YDOT = -2247
646121 meter/sec
ZDOT = 17739
579230 ZDOT = 5407
023749
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 20200
55987065
00016717 00000-0 10270-3 0 9039
2 25544 51
6384 193
1973 0001344 123
2953 236
8326 15
49543027 36873
Satellite: ISS
Catalog Number: 25544
Epoch time: 20200
55987065 = yrday
fracday
Element set: 903
Inclination: 51
6384 deg
RA of node: 193
1973 deg
Eccentricity:
0001344
Arg of perigee: 123
2953 deg
Mean anomaly: 236
8326 deg
Mean motion: 15
49543027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3687
Checksum: 316
Coasting Arc #5 (Orbit 3686)
---------------------------------------
Vector Time (GMT): 2020/200/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 968616
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5889217
52 A = 6801313
22 meter
Y = 2813370
73 meter E =
0008389
Z = -1904104
20 I = 51
56717
XDOT = -3607
374597 Wp = 137
14676
YDOT = 3772
316236 meter/sec RA = 192
14897 deg
ZDOT = -5604
140979 TA = 63
80170
MA = 63
71547
Ha = 228
775 n
mi
Hp = 221
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19321579
80 X = 5866568
81
Y = 9230218
93 feet Y = 2879101
85 meter
Z = -6247061
02 Z = -1875551
56
XDOT = -11835
218495 XDOT = -3622
068289
YDOT = 12376
365604 feet/sec YDOT = 3731
894817 meter/sec
ZDOT = -18386
289301 ZDOT = -5621
699011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4331705
53 X = -1320303
85
Y = -21009093
11 feet Y = -6403571
58 meter
Z = -6115594
24 Z = -1864033
12
XDOT = 15402
820207 XDOT = 4694
779599
YDOT = 2179
822010 feet/sec YDOT = 664
409749 meter/sec
ZDOT = -18467
262093 ZDOT = -5628
821486
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 20200
55987239
00016717 00000-0 10270-3 0 9043
2 25544 51
6383 193
1964 0001365 113
4689 246
6604 15
49512088 36873
Satellite: ISS
Catalog Number: 25544
Epoch time: 20200
55987239 = yrday
fracday
Element set: 904
Inclination: 51
6383 deg
RA of node: 193
1964 deg
Eccentricity:
0001365
Arg of perigee: 113
4689 deg
Mean anomaly: 246
6604 deg
Mean motion: 15
49512088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3687
Checksum: 330
Coasting Arc #6 (Orbit 3702)
---------------------------------------
Vector Time (GMT): 2020/201/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 968616
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6016401
69 A = 6800955
94 meter
Y = -2399431
47 meter E =
0014613
Z = 2052573
46 I = 51
59904
XDOT = 3488
322269 Wp = 73
43544
YDOT = -3984
328660 meter/sec RA = 187
19589 deg
ZDOT = 5538
486460 TA = 309
23748
MA = 309
36708
Ha = 228
640 n
mi
Hp = 221
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19738850
70 X = -5999093
44
Y = -7872150
50 feet Y = -2466614
74 meter
Z = 6734164
88 Z = 2023390
25
XDOT = 11444
626866 XDOT = 3505
714629
YDOT = -13071
944421 feet/sec YDOT = -3945
223453 meter/sec
ZDOT = 18170
887335 ZDOT = 5555
472638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6020512
66 X = 1835052
26
Y = 20423970
99 feet Y = 6225226
36 meter
Z = 6599757
07 Z = 2011605
96
XDOT = -15782
059757 XDOT = -4810
371814
YDOT = -1275
862969 feet/sec YDOT = -388
883033 meter/sec
ZDOT = 18249
241856 ZDOT = 5562
368918
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 20201
59177114
00016717 00000-0 10270-3 0 9052
2 25544 51
6378 188
0888 0001328 128
5747 231
5522 15
49554466 37033
Satellite: ISS
Catalog Number: 25544
Epoch time: 20201
59177114 = yrday
fracday
Element set: 905
Inclination: 51
6378 deg
RA of node: 188
0888 deg
Eccentricity:
0001328
Arg of perigee: 128
5747 deg
Mean anomaly: 231
5522 deg
Mean motion: 15
49554466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3703
Checksum: 319
Coasting Arc #7 (Orbit 3717)
---------------------------------------
Vector Time (GMT): 2020/202/12:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 968616
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6097036
95 A = 6800744
07 meter
Y = 2011554
80 meter E =
0007339
Z = -2237471
33 I = 51
63240
XDOT = -3375
896715 Wp = 135
15076
YDOT = 4186
668665 meter/sec RA = 182
24347 deg
ZDOT = -5451
276111 TA = 69
66686
MA = 69
58802
Ha = 228
709 n
mi
Hp = 221
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20003402
07 X = 6084958
12
Y = 6599589
24 feet Y = 2079669
04 meter
Z = -7340785
22 Z = -2207883
96
XDOT = -11075
776623 XDOT = -3395
983786
YDOT = 13735
789582 feet/sec YDOT = 4148
805538 meter/sec
ZDOT = -17884
764145 ZDOT = -5467
722662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7527918
63 X = -2294509
60
Y = -19723177
11 feet Y = -6011624
38 meter
Z = -7204479
58 Z = -2195925
38
XDOT = 16128
716982 XDOT = 4916
032936
YDOT = 385
124315 feet/sec YDOT = 117
385891 meter/sec
ZDOT = -17960
646705 ZDOT = -5474
405116
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 20202
55917991
00016717 00000-0 10270-3 0 9065
2 25544 51
6386 183
2988 0001228 121
3343 238
7928 15
49512554 37189
Satellite: ISS
Catalog Number: 25544
Epoch time: 20202
55917991 = yrday
fracday
Element set: 906
Inclination: 51
6386 deg
RA of node: 183
2988 deg
Eccentricity:
0001228
Arg of perigee: 121
3343 deg
Mean anomaly: 238
7928 deg
Mean motion: 15
49512554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3718
Checksum: 328
Coasting Arc #8 (Orbit 3720)
---------------------------------------
Vector Time (GMT): 2020/202/16:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 968616
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1007058
26 A = 6790892
11 meter
Y = -4155296
78 meter E =
0003706
Z = 5272910
75 I = 51
60859
XDOT = 7578
026940 Wp = 77
00334
YDOT = 815
901018 meter/sec RA = 181
35639 deg
ZDOT = -803
047073 TA = 20
68682
MA = 20
67183
Ha = 228
491 n
mi
Hp = 221
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3303996
93 X = 1027836
98
Y = -13632863
46 feet Y = -4143919
79 meter
Z = 17299575
94 Z = 5277852
35
XDOT = 24862
293110 XDOT = 7572
240737
YDOT = 2676
840609 feet/sec YDOT = 900
611694 meter/sec
ZDOT = -2634
668875 ZDOT = -766
250722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -275098
51 X = -83850
02
Y = 13996575
29 feet Y = 4266156
15 meter
Z = 17322438
93 Z = 5279879
39
XDOT = -23870
616350 XDOT = -7275
763863
YDOT = 2586
935174 feet/sec YDOT = 788
497841 meter/sec
ZDOT = -2465
110179 ZDOT = -751
365582
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 20202
75266036
00016717 00000-0 10270-3 0 9075
2 25544 51
6412 182
3427 0001022 126
4973 233
6271 15
49551440 37210
Satellite: ISS
Catalog Number: 25544
Epoch time: 20202
75266036 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 182
3427 deg
Eccentricity:
0001022
Arg of perigee: 126
4973 deg
Mean anomaly: 233
6271 deg
Mean motion: 15
49551440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3721
Checksum: 279
Coasting Arc #9 (Orbit 3735)
---------------------------------------
Vector Time (GMT): 2020/203/16:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 968616
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -872829
84 A = 6791087
23 meter
Y = 4224390
80 meter E =
0015354
Z = -5258639
05 I = 51
64426
XDOT = -7576
908941 Wp = 99
60105
YDOT = -318
300728 meter/sec RA = 176
40438 deg
ZDOT = 1001
921794 TA = 180
01400
MA = 180
01404
Ha = 228
588 n
mi
Hp = 221
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2863614
95 X = -894460
55
Y = 13859549
88 feet Y = 4214509
97 meter
Z = -17252752
78 Z = -5262930
76
XDOT = -24858
625135 XDOT = -7577
653120
YDOT = -1044
293728 feet/sec YDOT = -403
035429 meter/sec
ZDOT = 3287
144995 ZDOT = 965
115210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -445507
52 X = -135790
69
Y = -14121011
85 feet Y = -4304084
41 meter
Z = -17272621
08 Z = -5264694
91
XDOT = 23446
832918 XDOT = 7146
594673
YDOT = -4552
995758 feet/sec YDOT = -1387
753107 meter/sec
ZDOT = 3117
498888 ZDOT = 950
213661
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 20203
72006679
00016717 00000-0 10270-3 0 9089
2 25544 51
6427 177
5533 0001090 123
3513 236
7741 15
49527555 37363
Satellite: ISS
Catalog Number: 25544
Epoch time: 20203
72006679 = yrday
fracday
Element set: 908
Inclination: 51
6427 deg
RA of node: 177
5533 deg
Eccentricity:
0001090
Arg of perigee: 123
3513 deg
Mean anomaly: 236
7741 deg
Mean motion: 15
49527555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3736
Checksum: 306
Coasting Arc #10 (Orbit 3751)
---------------------------------------
Vector Time (GMT): 2020/204/16:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 968616
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 734459
99 A = 6791132
56 meter
Y = -4280472
62 meter E =
0004353
Z = 5217629
33 I = 51
67835
XDOT = 7566
690243 Wp = 69
31476
YDOT = -173
597417 meter/sec RA = 171
45549 deg
ZDOT = -1205
226813 TA = 32
26152
MA = 32
23490
Ha = 228
484 n
mi
Hp = 221
577
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2409645
62 X = 756927
33
Y = -14043545
36 feet Y = -4272134
33 meter
Z = 17118206
46 Z = 5221251
04
XDOT = 24825
099224 XDOT = 7573
923244
YDOT = -569
545333 feet/sec YDOT = -88
940709 meter/sec
ZDOT = -3954
156209 ZDOT = -1168
454202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1172445
92 X = 357361
52
Y = 14180203
79 feet Y = 4322126
12 meter
Z = 17134985
89 Z = 5222743
70
XDOT = -22941
487462 XDOT = -6992
565378
YDOT = 6479
265505 feet/sec YDOT = 1974
880126 meter/sec
ZDOT = -3784
630310 ZDOT = -1153
555318
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 20204
75196470
00016717 00000-0 10270-3 0 9093
2 25544 51
6427 172
4453 0000991 127
5633 232
5608 15
49555996 37520
Satellite: ISS
Catalog Number: 25544
Epoch time: 20204
75196470 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 172
4453 deg
Eccentricity:
0000991
Arg of perigee: 127
5633 deg
Mean anomaly: 232
5608 deg
Mean motion: 15
49555996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3752
Checksum: 327
Coasting Arc #11 (Orbit 3765)
---------------------------------------
Vector Time (GMT): 2020/205/14:26:22
000
Vector Time (MET): N/A
Weight (LBS) : 968616
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3806764
62 A = 6793226
06 meter
Y = -2984393
60 meter E =
0008776
Z = 4764983
14 I = 51
71318
XDOT = 6204
396130 Wp = 119
84885
YDOT = -3605
499561 meter/sec RA = 167
05394 deg
ZDOT = 2690
544581 TA = 303
54033
MA = 303
62413
Ha = 228
637 n
mi
Hp = 221
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12489385
25 X = -3796254
31
Y = -9791317
58 feet Y = -3026905
21 meter
Z = 15633146
80 Z = 4746517
09
XDOT = 20355
630348 XDOT = 6231
183983
YDOT = -11829
066802 feet/sec YDOT = -3535
968032 meter/sec
ZDOT = 8827
246001 ZDOT = 2720
747107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7884126
24 X = 2403081
68
Y = 13868965
56 feet Y = 4227260
70 meter
Z = 15548063
23 Z = 4739049
67
XDOT = -22266
736679 XDOT = -6786
901340
YDOT = 2576
364802 feet/sec YDOT = 785
275992 meter/sec
ZDOT = 8966
565089 ZDOT = 2733
009039
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 20205
65487791
00016717 00000-0 10270-3 0 9104
2 25544 51
6412 167
9753 0001068 134
3507 225
7731 15
49537786 37661
Satellite: ISS
Catalog Number: 25544
Epoch time: 20205
65487791 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 167
9753 deg
Eccentricity:
0001068
Arg of perigee: 134
3507 deg
Mean anomaly: 225
7731 deg
Mean motion: 15
49537786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3766
Checksum: 329
Coasting Arc #12 (Orbit 3767)
---------------------------------------
Vector Time (GMT): 2020/205/17:47:57
000
Vector Time (MET): N/A
Weight (LBS) : 983050
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2961803
16 A = 6794507
55 meter
Y = -4270150
68 meter E =
0009929
Z = 4370269
63 I = 51
72411
XDOT = 6750
808030 Wp = 75
46185
YDOT = 1151
299583 meter/sec RA = 166
31846 deg
ZDOT = -3441
228164 TA = 49
46719
MA = 49
38076
Ha = 228
389 n
mi
Hp = 221
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9717201
98 X = 2988105
39
Y = -14009680
71 feet Y = -4236882
99 meter
Z = 14338154
96 Z = 4384720
08
XDOT = 22148
320308 XDOT = 6754
147233
YDOT = 3777
229602 feet/sec YDOT = 1226
810900 meter/sec
ZDOT = -11290
118647 ZDOT = -3408
427970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1913965
08 X = -583376
56
Y = 16885336
03 feet Y = 5146650
42 meter
Z = 14404861
00 Z = 4390601
63
XDOT = -20164
088732 XDOT = -6146
014246
YDOT = 7241
995214 feet/sec YDOT = 2207
360141 meter/sec
ZDOT = -11138
908861 ZDOT = -3395
139421
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 20205
78386430
00016717 00000-0 10270-3 0 9117
2 25544 51
6427 167
3377 0000868 128
8990 231
2238 15
49558873 37680
Satellite: ISS
Catalog Number: 25544
Epoch time: 20205
78386430 = yrday
fracday
Element set: 911
Inclination: 51
6427 deg
RA of node: 167
3377 deg
Eccentricity:
0000868
Arg of perigee: 128
8990 deg
Mean anomaly: 231
2238 deg
Mean motion: 15
49558873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3768
Checksum: 341
Coasting Arc #13 (Orbit 3771)
---------------------------------------
Vector Time (GMT): 2020/206/00:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 983050
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3157799
48 A = 6792125
55 meter
Y = 3279841
98 meter E =
0013317
Z = -5052209
60 I = 51
72302
XDOT = -6593
558823 Wp = 81
56756
YDOT = 3358
722216 meter/sec RA = 164
96571 deg
ZDOT = -1943
233098 TA = 169
56841
MA = 169
54075
Ha = 228
603 n
mi
Hp = 221
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10360234
52 X = 3145428
78
Y = 10760636
40 feet Y = 3315085
97 meter
Z = -16575490
80 Z = -5036900
39
XDOT = -21632
410836 XDOT = -6621
188123
YDOT = 11019
429841 feet/sec YDOT = 3284
834000 meter/sec
ZDOT = -6375
436673 ZDOT = -1975
328118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1693589
64 X = -516206
12
Y = 14919470
32 feet Y = 4547454
55 meter
Z = -16504963
19 Z = -5030712
78
XDOT = -21112
290522 XDOT = -6435
026151
YDOT = -9604
241616 feet/sec YDOT = -2927
372845 meter/sec
ZDOT = -6523
483903 ZDOT = -1988
357894
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 20206
04184122
00016717 00000-0 10270-3 0 9122
2 25544 51
6410 166
0557 0001432 146
3884 213
7357 15
49517035 37720
Satellite: ISS
Catalog Number: 25544
Epoch time: 20206
04184122 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 166
0557 deg
Eccentricity:
0001432
Arg of perigee: 146
3884 deg
Mean anomaly: 213
7357 deg
Mean motion: 15
49517035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3772
Checksum: 286
Coasting Arc #14 (Orbit 3787)
---------------------------------------
Vector Time (GMT): 2020/207/00:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 983050
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3241853
33 A = 6791795
81 meter
Y = -3097173
74 meter E =
0006642
Z = 5098403
67 I = 51
75576
XDOT = 6413
844454 Wp = 130
77301
YDOT = -3807
423406 meter/sec RA = 160
02144 deg
ZDOT = 1759
620827 TA = 302
19586
MA = 302
26025
Ha = 228
589 n
mi
Hp = 221
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10636001
75 X = -3231743
52
Y = -10161331
18 feet Y = -3133370
24 meter
Z = 16727046
15 Z = 5082680
68
XDOT = 21042
796766 XDOT = 6447
396448
YDOT = -12491
546606 feet/sec YDOT = -3735
511720 meter/sec
ZDOT = 5773
034208 ZDOT = 1790
857437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 800547
85 X = 244006
98
Y = -14770062
22 feet Y = -4501914
97 meter
Z = 16654598
24 Z = 5076321
54
XDOT = 22031
721113 XDOT = 6715
268595
YDOT = 7887
566321 feet/sec YDOT = 2404
130215 meter/sec
ZDOT = 5917
148242 ZDOT = 1803
546784
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 20207
07373928
00016717 00000-0 10270-3 0 9131
2 25544 51
6422 160
9468 0001363 154
2147 205
9071 15
49548216 37888
Satellite: ISS
Catalog Number: 25544
Epoch time: 20207
07373928 = yrday
fracday
Element set: 913
Inclination: 51
6422 deg
RA of node: 160
9468 deg
Eccentricity:
0001363
Arg of perigee: 154
2147 deg
Mean anomaly: 205
9071 deg
Mean motion: 15
49548216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3788
Checksum: 313
Coasting Arc #15 (Orbit 3802)
---------------------------------------
Vector Time (GMT): 2020/208/00:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 983050
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3310020
00 A = 6791666
31 meter
Y = 2942759
26 meter E =
0013981
Z = -5161227
29 I = 51
78654
XDOT = -6183
855402 Wp = 83
61779
YDOT = 4225
960842 meter/sec RA = 155
08048 deg
ZDOT = -1558
472982 TA = 171
36738
MA = 171
34331
Ha = 228
558 n
mi
Hp = 221
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10859645
68 X = 3301937
12
Y = 9654721
99 feet Y = 2979729
35 meter
Z = -16933160
40 Z = -5145168
21
XDOT = -20288
239507 XDOT = -6223
081703
YDOT = 13864
700924 feet/sec YDOT = 4156
589310 meter/sec
ZDOT = -5113
100336 ZDOT = -1588
606349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17138
66 X = -5223
86
Y = 14616639
54 feet Y = 4455151
73 meter
Z = -16859152
92 Z = -5138669
81
XDOT = -22713
580652 XDOT = -6923
099383
YDOT = -6076
528369 feet/sec YDOT = -1852
125847 meter/sec
ZDOT = -5252
151964 ZDOT = -1600
855919
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 20208
04114518
00016717 00000-0 10270-3 0 9148
2 25544 51
6425 156
1587 0001349 150
0254 210
0974 15
49516713 38031
Satellite: ISS
Catalog Number: 25544
Epoch time: 20208
04114518 = yrday
fracday
Element set: 914
Inclination: 51
6425 deg
RA of node: 156
1587 deg
Eccentricity:
0001349
Arg of perigee: 150
0254 deg
Mean anomaly: 210
0974 deg
Mean motion: 15
49516713 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3803
Checksum: 283
Coasting Arc #16 (Orbit 3818)
---------------------------------------
Vector Time (GMT): 2020/209/00:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 983050
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3376228
61 A = 6791378
50 meter
Y = -2773929
44 meter E =
0005709
Z = 5196089
61 I = 51
81564
XDOT = 5935
731118 Wp = 132
29111
YDOT = -4649
829650 meter/sec RA = 150
14062 deg
ZDOT = 1369
804603 TA = 304
53789
MA = 304
59176
Ha = 228
589 n
mi
Hp = 221
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11076865
52 X = -3370198
16
Y = -9100818
36 feet Y = -2811651
44 meter
Z = 17047538
10 Z = 5179703
85
XDOT = 19474
183457 XDOT = 5980
632088
YDOT = -15255
346622 feet/sec YDOT = -4583
201094 meter/sec
ZDOT = 4494
109590 ZDOT = 1398
746543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -790862
41 X = -241054
86
Y = -14403667
33 feet Y = -4390237
80 meter
Z = 16972015
31 Z = 5173070
27
XDOT = 23314
941238 XDOT = 7106
394089
YDOT = 4190
992195 feet/sec YDOT = 1277
414421 meter/sec
ZDOT = 4627
694366 ZDOT = 1410
521243
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 20209
07304276
00016717 00000-0 10270-3 0 9155
2 25544 51
6421 151
0502 0001359 155
7564 204
3650 15
49547422 38190
Satellite: ISS
Catalog Number: 25544
Epoch time: 20209
07304276 = yrday
fracday
Element set: 915
Inclination: 51
6421 deg
RA of node: 151
0502 deg
Eccentricity:
0001359
Arg of perigee: 155
7564 deg
Mean anomaly: 204
3650 deg
Mean motion: 15
49547422 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3819
Checksum: 289
Coasting Arc #17 (Orbit 3833)
---------------------------------------
Vector Time (GMT): 2020/210/00:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 983050
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3434959
44 A = 6791313
06 meter
Y = 2632514
07 meter E =
0014406
Z = -5246397
90 I = 51
84406
XDOT = -5639
438070 Wp = 86
34222
YDOT = 5035
813695 meter/sec RA = 145
20371 deg
ZDOT = -1167
317997 TA = 172
47943
MA = 172
45780
Ha = 228
496 n
mi
Hp = 221
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11269551
97 X = 3430750
40
Y = 8636857
20 feet Y = 2670903
13 meter
Z = -17212591
53 Z = -5229722
34
XDOT = -18502
093406 XDOT = -5689
660791
YDOT = 16521
698475 feet/sec YDOT = 4972
468753 meter/sec
ZDOT = -3829
783455 ZDOT = -1194
833550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1509278
74 X = 460028
16
Y = 14211278
82 feet Y = 4331597
78 meter
Z = -17135724
18 Z = -5222968
73
XDOT = -23656
206459 XDOT = -7210
411729
YDOT = -2251
269448 feet/sec YDOT = -686
186928 meter/sec
ZDOT = -3956
819804 ZDOT = -1206
038676
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 20210
04044904
00016717 00000-0 10270-3 0 9164
2 25544 51
6424 146
2621 0001325 159
2423 200
8781 15
49512225 38343
Satellite: ISS
Catalog Number: 25544
Epoch time: 20210
04044904 = yrday
fracday
Element set: 916
Inclination: 51
6424 deg
RA of node: 146
2621 deg
Eccentricity:
0001325
Arg of perigee: 159
2423 deg
Mean anomaly: 200
8781 deg
Mean motion: 15
49512225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3834
Checksum: 271
Coasting Arc #18 (Orbit 3849)
---------------------------------------
Vector Time (GMT): 2020/211/00:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 983050
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3489823
95 A = 6791048
13 meter
Y = -2478035
28 meter E =
0004693
Z = 5269934
56 I = 51
87132
XDOT = 5327
121033 Wp = 132
78214
YDOT = -5422
294203 meter/sec RA = 140
26717 deg
ZDOT = 974
360679 TA = 307
89505
MA = 307
93748
Ha = 228
532 n
mi
Hp = 221
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11449553
65 X = -3487452
58
Y = -8130037
00 feet Y = -2517048
27 meter
Z = 17289811
56 Z = 5252987
99
XDOT = 17477
431212 XDOT = 5382
625976
YDOT = -17789
679144 feet/sec YDOT = -5362
412285 meter/sec
ZDOT = 3196
721388 ZDOT = 1000
371805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2242616
98 X = -683549
66
Y = -13959080
54 feet Y = -4254727
75 meter
Z = 17211685
10 Z = 5246121
62
XDOT = 23904
782114 XDOT = 7286
177588
YDOT = 264
105098 feet/sec YDOT = 80
499234 meter/sec
ZDOT = 3316
851789 ZDOT = 1010
976425
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 20211
07234581
00016717 00000-0 10270-3 0 9171
2 25544 51
6431 141
1532 0001288 162
5720 197
5475 15
49550345 38506
Satellite: ISS
Catalog Number: 25544
Epoch time: 20211
07234581 = yrday
fracday
Element set: 917
Inclination: 51
6431 deg
RA of node: 141
1532 deg
Eccentricity:
0001288
Arg of perigee: 162
5720 deg
Mean anomaly: 197
5475 deg
Mean motion: 15
49550345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3850
Checksum: 291
Coasting Arc #19 (Orbit 3864)
---------------------------------------
Vector Time (GMT): 2020/212/00:32:00
000
Vector Time (MET): N/A
Weight (LBS) : 983050
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3544064
28 A = 6791051
91 meter
Y = 2349570
28 meter E =
0014753
Z = -5307820
76 I = 51
89615
XDOT = -4971
627943 Wp = 88
58972
YDOT = 5763
072441 meter/sec RA = 135
33368 deg
ZDOT = -769
989607 TA = 174
07017
MA = 174
05268
Ha = 228
437 n
mi
Hp = 221
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11627507
49 X = 3543309
38
Y = 7708563
91 feet Y = 2389198
96 meter
Z = -17414110
09 Z = -5290606
80
XDOT = -16311
115297 XDOT = -5031
962710
YDOT = 18907
717981 feet/sec YDOT = 5707
138889 meter/sec
ZDOT = -2526
212621 ZDOT = -794
285429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2906231
25 X = 885819
29
Y = 13745279
67 feet Y = 4189561
24 meter
Z = -17334740
41 Z = -5283628
88
XDOT = -23881
621885 XDOT = -7279
118351
YDOT = 1728
150236 feet/sec YDOT = 526
740192 meter/sec
ZDOT = -2638
464051 ZDOT = -804
203843
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 20212
03975017
00016717 00000-0 10270-3 0 9185
2 25544 51
6432 136
3651 0001162 163
5532 196
5656 15
49510182 38659
Satellite: ISS
Catalog Number: 25544
Epoch time: 20212
03975017 = yrday
fracday
Element set: 918
Inclination: 51
6432 deg
RA of node: 136
3651 deg
Eccentricity:
0001162
Arg of perigee: 163
5532 deg
Mean anomaly: 196
5656 deg
Mean motion: 15
49510182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3865
Checksum: 298
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