[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 25th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 107 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 032 ET - UTC (sec) : 67 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
027/19:42:43
043 0
7 2
1 2
1
N/A 1
6 -0
2 222
9
000/00:05:22
087 1
2 -0
1 212
6
Coasting Arc #1 (Orbit 2262)
---------------------------------------
Vector Time (GMT): 2016/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3699060
92 A = 6775948
43 meter
Y = -2010031
83 meter E =
0020417
Z = -5326646
75 I = 51
92257
XDOT = 4180
103701 Wp = 81
85766
YDOT = 6393
280556 meter/sec RA = 53
91349 deg
ZDOT = 494
750836 TA = 192
82616
MA = 192
87818
Ha = 222
473 n
mi
Hp = 211
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12136026
63 X = 3747136
62
Y = -6594592
63 feet Y = -1968397
70 meter
Z = -17475875
15 Z = -5308561
28
XDOT = 13714
250988 XDOT = 4105
898560
YDOT = 20975
329907 feet/sec YDOT = 6439
610340 meter/sec
ZDOT = 1623
198282 ZDOT = 514
875998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12248254
54 X = 3733267
99
Y = 6595600
85 feet Y = 2010339
14 meter
Z = -17397020
34 Z = -5302611
80
XDOT = -9489
722963 XDOT = -2892
467559
YDOT = 22092
577664 feet/sec YDOT = 6733
817672 meter/sec
ZDOT = 1709
219872 ZDOT = 520
970217
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 16025
51520741
00016717 00000-0 10270-3 0 9006
2 25544 51
6423 54
5209 0006720 55
2942 304
8843 15
54644189 22630
Satellite: ISS
Catalog Number: 25544
Epoch time: 16025
51520741 = yrday
fracday
Element set: 900
Inclination: 51
6423 deg
RA of node: 54
5209 deg
Eccentricity:
0006720
Arg of perigee: 55
2942 deg
Mean anomaly: 304
8843 deg
Mean motion: 15
54644189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2263
Checksum: 290
Coasting Arc #2 (Orbit 2278)
---------------------------------------
Vector Time (GMT): 2016/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4751720
82 A = 6777933
32 meter
Y = 294285
24 meter E =
0014276
Z = 4816699
58 I = 51
90873
XDOT = -3034
595285 Wp = 59
82193
YDOT = -6560
327525 meter/sec RA = 48
92787 deg
ZDOT = -2580
151541 TA = 55
53242
MA = 55
39763
Ha = 222
608 n
mi
Hp = 211
541
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15589635
24 X = -4778055
37
Y = 965502
74 feet Y = 241001
22 meter
Z = 15802820
13 Z = 4793553
45
XDOT = -9956
021277 XDOT = -2948
477562
YDOT = -21523
384270 feet/sec YDOT = -6593
780931 meter/sec
ZDOT = -8465
064110 ZDOT = -2594
683191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9657928
64 X = -2943736
65
Y = -12403967
41 feet Y = -3780729
27 meter
Z = 15702358
21 Z = 4786078
78
XDOT = 11269
013416 XDOT = 3434
795289
YDOT = -19621
455441 feet/sec YDOT = -5980
619619 meter/sec
ZDOT = -8526
782833 ZDOT = -2598
963408
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 16026
54368136
00016717 00000-0 10270-3 0 9019
2 25544 51
6409 49
3887 0006862 59
1361 301
0466 15
54697782 22797
Satellite: ISS
Catalog Number: 25544
Epoch time: 16026
54368136 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 49
3887 deg
Eccentricity:
0006862
Arg of perigee: 59
1361 deg
Mean anomaly: 301
0466 deg
Mean motion: 15
54697782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2279
Checksum: 330
Coasting Arc #3 (Orbit 2293)
---------------------------------------
Vector Time (GMT): 2016/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5525301
16 A = 6781898
85 meter
Y = 1261121
54 meter E =
0011899
Z = -3732989
33 I = 51
90124
XDOT = 1502
953548 Wp = 79
21305
YDOT = 6149
172510 meter/sec RA = 43
95141 deg
ZDOT = 4315
767274 TA = 236
44052
MA = 236
55420
Ha = 222
579 n
mi
Hp = 211
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18127628
47 X = 5528921
23
Y = 4137537
86 feet Y = 1322929
21 meter
Z = -12247340
33 Z = -3706140
60
XDOT = 4930
949962 XDOT = 1413
116560
YDOT = 20174
450492 feet/sec YDOT = 6165
477394 meter/sec
ZDOT = 14159
341449 ZDOT = 4322
849660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7163785
41 X = 2183521
79
Y = 17240743
29 feet Y = 5254978
56 meter
Z = -12131134
65 Z = -3697569
84
XDOT = -12394
712310 XDOT = -3777
908312
YDOT = 15101
686771 feet/sec YDOT = 4602
994128 meter/sec
ZDOT = 14188
824263 ZDOT = 4324
753635
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 16027
50786758
00016717 00000-0 10270-3 0 9021
2 25544 51
6420 44
5781 0006917 62
2858 297
8996 15
54690216 22949
Satellite: ISS
Catalog Number: 25544
Epoch time: 16027
50786758 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 44
5781 deg
Eccentricity:
0006917
Arg of perigee: 62
2858 deg
Mean anomaly: 297
8996 deg
Mean motion: 15
54690216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2294
Checksum: 344
Coasting Arc #4 (Orbit 2298)
---------------------------------------
Vector Time (GMT): 2016/027/19:45:24
087
Vector Time (MET): N/A
Weight (LBS) : 922285
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5731965
58 A = 6785062
57 meter
Y = 2033718
07 meter E =
0010889
Z = -3007458
27 I = 51
90205
XDOT = 551
471584 Wp = 55
30732
YDOT = 5793
661555 meter/sec RA = 42
34590 deg
ZDOT = 4987
706235 TA = 270
41206
MA = 270
53684
Ha = 222
898 n
mi
Hp = 212
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18805661
34 X = 5723406
69
Y = 6672303
38 feet Y = 2097768
72 meter
Z = -9866989
06 Z = -2979635
22
XDOT = 1809
289974 XDOT = 462
416776
YDOT = 19008
075967 feet/sec YDOT = 5799
330753 meter/sec
ZDOT = 16363
865600 ZDOT = 4990
168549
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14740984
09 X = 4493051
95
Y = -13536430
10 feet Y = -4125903
89 meter
Z = -9746714
96 Z = -2970798
72
XDOT = 16601
736507 XDOT = 5060
209287
YDOT = 6334
670198 feet/sec YDOT = 1930
807476 meter/sec
ZDOT = 16373
378413 ZDOT = 4990
605740
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 16027
82926117
00016717 00000-0 10270-3 0 9032
2 25544 51
6434 42
9741 0006522 47
0846 313
0853 15
54307063 22995
Satellite: ISS
Catalog Number: 25544
Epoch time: 16027
82926117 = yrday
fracday
Element set: 903
Inclination: 51
6434 deg
RA of node: 42
9741 deg
Eccentricity:
0006522
Arg of perigee: 47
0846 deg
Mean anomaly: 313
0853 deg
Mean motion: 15
54307063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2299
Checksum: 301
Coasting Arc #5 (Orbit 2314)
---------------------------------------
Vector Time (GMT): 2016/028/19:45:24
087
Vector Time (MET): N/A
Weight (LBS) : 922285
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5859941
42 A = 6788136
71 meter
Y = -3133674
93 meter E =
0017253
Z = 1361769
70 I = 51
88789
XDOT = 1213
651306 Wp = 99
48414
YDOT = -4829
689311 meter/sec RA = 37
38671 deg
ZDOT = -5831
377217 TA = 65
73340
MA = 65
55325
Ha = 222
929 n
mi
Hp = 212
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19225529
58 X = -5831079
15
Y = -10281085
74 feet Y = -3199043
24 meter
Z = 4467748
35 Z = 1333374
28
XDOT = 3981
795623 XDOT = 1295
893745
YDOT = -15845
437372 feet/sec YDOT = -4815
657891 meter/sec
ZDOT = -19131
815017 ZDOT = -5825
281715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17897154
53 X = -5455052
70
Y = 12493734
18 feet Y = 3808090
18 meter
Z = 4345221
88 Z = 1324423
63
XDOT = -11349
018276 XDOT = -3459
180770
YDOT = -9542
562714 feet/sec YDOT = -2908
573115 meter/sec
ZDOT = -19104
399846 ZDOT = -5823
021073
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 16028
85797892
00016717 00000-0 10270-3 0 9043
2 25544 51
6434 37
8440 0006487 51
8118 308
3618 15
54283704 23159
Satellite: ISS
Catalog Number: 25544
Epoch time: 16028
85797892 = yrday
fracday
Element set: 904
Inclination: 51
6434 deg
RA of node: 37
8440 deg
Eccentricity:
0006487
Arg of perigee: 51
8118 deg
Mean anomaly: 308
3618 deg
Mean motion: 15
54283704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2315
Checksum: 326
Coasting Arc #6 (Orbit 2330)
---------------------------------------
Vector Time (GMT): 2016/029/19:45:24
087
Vector Time (MET): N/A
Weight (LBS) : 922285
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5545555
23 A = 6788667
62 meter
Y = 3880972
00 meter E =
0019345
Z = 384306
63 I = 51
86469
XDOT = -3009
874372 Wp = 50
47704
YDOT = 3686
097581 meter/sec RA = 32
43083 deg
ZDOT = 6018
820307 TA = 313
65577
MA = 313
81600
Ha = 222
882 n
mi
Hp = 212
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18194078
85 X = 5499878
32
Y = 12732847
77 feet Y = 3942730
70 meter
Z = 1260848
51 Z = 411134
06
XDOT = -9874
915919 XDOT = -3080
105970
YDOT = 12093
496000 feet/sec YDOT = 3652
046766 meter/sec
ZDOT = 19746
785784 ZDOT = 6004
028534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19415585
31 X = 5917870
40
Y = -10764766
14 feet Y = -3281100
72 meter
Z = 1376413
26 Z = 419530
76
XDOT = 5702
915553 XDOT = 1738
248660
YDOT = 12875
198347 feet/sec YDOT = 3924
360456 meter/sec
ZDOT = 19681
883852 ZDOT = 5999
038198
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 16029
88668433
00016717 00000-0 10270-3 0 9056
2 25544 51
6439 32
7139 0006515 53
6439 306
5315 15
54332532 23317
Satellite: ISS
Catalog Number: 25544
Epoch time: 16029
88668433 = yrday
fracday
Element set: 905
Inclination: 51
6439 deg
RA of node: 32
7139 deg
Eccentricity:
0006515
Arg of perigee: 53
6439 deg
Mean anomaly: 306
5315 deg
Mean motion: 15
54332532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2331
Checksum: 307
Coasting Arc #7 (Orbit 2345)
---------------------------------------
Vector Time (GMT): 2016/030/19:45:24
087
Vector Time (MET): N/A
Weight (LBS) : 922285
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4736562
61 A = 6786775
47 meter
Y = -4364108
03 meter E =
0009612
Z = -2146109
25 I = 51
83095
XDOT = 4728
247458 Wp = 96
63267
YDOT = -2429
560344 meter/sec RA = 27
47203 deg
ZDOT = -5517
230082 TA = 107
07709
MA = 106
97178
Ha = 222
862 n
mi
Hp = 212
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15539903
57 X = -4676985
29
Y = -14317939
72 feet Y = -4416742
38 meter
Z = -7041040
84 Z = -2168973
13
XDOT = 15512
622894 XDOT = 4781
864015
YDOT = -7970
998503 feet/sec YDOT = -2376
386394 meter/sec
ZDOT = -18101
148562 ZDOT = -5494
131370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19526696
36 X = -5951737
05
Y = 7987907
70 feet Y = 2434714
27 meter
Z = -7139307
85 Z = -2176061
03
XDOT = -35
194254 XDOT = -10
727209
YDOT = -16109
805410 feet/sec YDOT = -4910
268689 meter/sec
ZDOT = -18000
477421 ZDOT = -5486
545518
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 16030
85108777
00016717 00000-0 10270-3 0 9066
2 25544 51
6440 27
9047 0006352 57
5897 302
5870 15
54314443 23462
Satellite: ISS
Catalog Number: 25544
Epoch time: 16030
85108777 = yrday
fracday
Element set: 906
Inclination: 51
6440 deg
RA of node: 27
9047 deg
Eccentricity:
0006352
Arg of perigee: 57
5897 deg
Mean anomaly: 302
5870 deg
Mean motion: 15
54314443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2346
Checksum: 312
Coasting Arc #8 (Orbit 2361)
---------------------------------------
Vector Time (GMT): 2016/031/19:45:24
087
Vector Time (MET): N/A
Weight (LBS) : 922285
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3498484
33 A = 6783088
21 meter
Y = 4532904
43 meter E =
0017745
Z = 3618917
47 I = 51
78987
XDOT = -6158
990226 Wp = 81
73909
YDOT = 1213
316714 meter/sec RA = 22
50233 deg
ZDOT = 4418
287830 TA = 321
09966
MA = 321
22722
Ha = 222
907 n
mi
Hp = 212
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11477966
95 X = 3429957
29
Y = 14871733
71 feet Y = 4571643
77 meter
Z = 11873088
80 Z = 3635745
46
XDOT = -20206
660846 XDOT = -6193
562012
YDOT = 3980
697881 feet/sec YDOT = 1144
249657 meter/sec
ZDOT = 14495
694979 ZDOT = 4388
285282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18226305
78 X = 5555378
00
Y = -4358659
12 feet Y = -1328519
30 meter
Z = 11945136
87 Z = 3640877
72
XDOT = -4945
194361 XDOT = -1507
295241
YDOT = 18832
884538 feet/sec YDOT = 5740
263207 meter/sec
ZDOT = 14365
336928 ZDOT = 4378
554696
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 16031
87977475
00016717 00000-0 10270-3 0 9079
2 25544 51
6438 22
7743 0006606 60
2997 299
8812 15
54338414 23625
Satellite: ISS
Catalog Number: 25544
Epoch time: 16031
87977475 = yrday
fracday
Element set: 907
Inclination: 51
6438 deg
RA of node: 22
7743 deg
Eccentricity:
0006606
Arg of perigee: 60
2997 deg
Mean anomaly: 299
8812 deg
Mean motion: 15
54338414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2362
Checksum: 338
Coasting Arc #9 (Orbit 2376)
---------------------------------------
Vector Time (GMT): 2016/032/19:45:24
087
Vector Time (MET): N/A
Weight (LBS) : 922285
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1878961
45 A = 6779128
18 meter
Y = -4500291
37 meter E =
0017341
Z = -4725707
46 I = 51
74644
XDOT = 7129
542784 Wp = 67
65555
YDOT = -52
917774 meter/sec RA = 17
51940 deg
ZDOT = -2786
094406 TA = 174
74105
MA = 174
72282
Ha = 222
847 n
mi
Hp = 212
075
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6164571
68 X = -1805543
20
Y = -14764735
46 feet Y = -4520892
77 meter
Z = -15504289
58 Z = -4734656
47
XDOT = 23390
888400 XDOT = 7143
138160
YDOT = -173
614743 feet/sec YDOT = 26
885444 meter/sec
ZDOT = -9140
729679 ZDOT = -2751
428182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15961961
23 X = -4865205
78
Y = -197666
69 feet Y = -60248
81 meter
Z = -15542170
84 Z = -4737253
67
XDOT = 9002
022608 XDOT = 2743
816491
YDOT = -20483
055189 feet/sec YDOT = -6243
235222 meter/sec
ZDOT = -8990
391830 ZDOT = -2740
271430
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 16032
84415731
00016717 00000-0 10270-3 0 9080
2 25544 51
6432 17
9645 0006404 63
2471 296
9336 15
54375161 23777
Satellite: ISS
Catalog Number: 25544
Epoch time: 16032
84415731 = yrday
fracday
Element set: 908
Inclination: 51
6432 deg
RA of node: 17
9645 deg
Eccentricity:
0006404
Arg of perigee: 63
2471 deg
Mean anomaly: 296
9336 deg
Mean motion: 15
54375161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2377
Checksum: 311
Coasting Arc #10 (Orbit 2392)
---------------------------------------
Vector Time (GMT): 2016/033/19:45:24
087
Vector Time (MET): N/A
Weight (LBS) : 922285
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 37739
02 A = 6776816
98 meter
Y = 4262790
40 meter E =
0008876
Z = 5260323
03 I = 51
70806
XDOT = -7563
976060 Wp = 83
76407
YDOT = -988
735527 meter/sec RA = 12
52536 deg
ZDOT = 855
209825 TA = 358
07349
MA = 358
07690
Ha = 222
924 n
mi
Hp = 212
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 123815
70 X = -35483
47
Y = 13985532
80 feet Y = 4262803
08 meter
Z = 17258277
66 Z = 5260328
45
XDOT = -24816
194421 XDOT = -7556
511804
YDOT = -3243
882961 feet/sec YDOT = -1073
279171 meter/sec
ZDOT = 2805
806511 ZDOT = 818
484452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12968649
80 X = 3952844
46
Y = 5239667
13 feet Y = 1597050
54 meter
Z = 17257422
07 Z = 5260062
25
XDOT = -11948
543651 XDOT = -3641
916105
YDOT = 20853
144774 feet/sec YDOT = 6356
038527 meter/sec
ZDOT = 2646
760493 ZDOT = 806
732598
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 16033
87282369
00016717 00000-0 10270-3 0 9094
2 25544 51
6433 12
8343 0006494 67
8282 292
3560 15
54381807 23937
Satellite: ISS
Catalog Number: 25544
Epoch time: 16033
87282369 = yrday
fracday
Element set: 909
Inclination: 51
6433 deg
RA of node: 12
8343 deg
Eccentricity:
0006494
Arg of perigee: 67
8282 deg
Mean anomaly: 292
3560 deg
Mean motion: 15
54381807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2393
Checksum: 325
Coasting Arc #11 (Orbit 2407)
---------------------------------------
Vector Time (GMT): 2016/034/19:45:24
087
Vector Time (MET): N/A
Weight (LBS) : 922285
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1861809
29 A = 6777019
16 meter
Y = -3918740
88 meter E =
0019964
Z = -5223520
54 I = 51
67626
XDOT = 7317
913903 Wp = 90
10178
YDOT = 1908
027092 meter/sec RA = 7
52460 deg
ZDOT = 1180
758958 TA = 191
21611
MA = 191
26067
Ha = 222
839 n
mi
Hp = 212
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6108298
20 X = 1930864
54
Y = -12856761
41 feet Y = -3897534
80 meter
Z = -17137534
59 Z = -5214308
72
XDOT = 24008
903882 XDOT = 7290
298447
YDOT = 6259
931403 feet/sec YDOT = 1989
706449 meter/sec
ZDOT = 3873
881096 ZDOT = 1216
240021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9763580
18 X = -2975939
24
Y = -10424743
31 feet Y = -3177461
76 meter
Z = -17096781
62 Z = -5211099
04
XDOT = 13703
063625 XDOT = 4176
693793
YDOT = -19418
010711 feet/sec YDOT = -5918
609665 meter/sec
ZDOT = 4027
336245 ZDOT = 1227
532087
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 16034
83718735
00016717 00000-0 10270-3 0 9104
2 25544 51
6421 8
0235 0006411 70
8948 289
2899 15
54416524 24085
Satellite: ISS
Catalog Number: 25544
Epoch time: 16034
83718735 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 8
0235 deg
Eccentricity:
0006411
Arg of perigee: 70
8948 deg
Mean anomaly: 289
2899 deg
Mean motion: 15
54416524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2408
Checksum: 313
Coasting Arc #12 (Orbit 2423)
---------------------------------------
Vector Time (GMT): 2016/035/19:45:24
087
Vector Time (MET): N/A
Weight (LBS) : 922285
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3652269
27 A = 6779690
36 meter
Y = 3441145
78 meter E =
0015091
Z = 4549401
92 I = 51
65400
XDOT = -6462
984733 Wp = 69
65930
YDOT = -2741
184531 meter/sec RA = 2
52712 deg
ZDOT = -3101
610662 TA = 51
42443
MA = 51
28934
Ha = 222
859 n
mi
Hp = 211
933
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11982510
73 X = -3712576
25
Y = 11289848
37 feet Y = 3399966
48 meter
Z = 14925859
30 Z = 4531513
92
XDOT = -21204
018153 XDOT = -6416
785741
YDOT = -8993
387569 feet/sec YDOT = -2813
199589 meter/sec
ZDOT = -10175
887999 ZDOT = -3132
893521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6457515
19 X = 1968250
63
Y = 15220781
78 feet Y = 4639294
29 meter
Z = 14847586
16 Z = 4525544
26
XDOT = -14595
762883 XDOT = -4448
788527
YDOT = 16293
828074 feet/sec YDOT = 4966
358797 meter/sec
ZDOT = -10310
963603 ZDOT = -3142
781706
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 16035
86583112
00016717 00000-0 10270-3 0 9118
2 25544 51
6425 2
8930 0006306 74
1473 286
0375 15
54449396 24241
Satellite: ISS
Catalog Number: 25544
Epoch time: 16035
86583112 = yrday
fracday
Element set: 911
Inclination: 51
6425 deg
RA of node: 2
8930 deg
Eccentricity:
0006306
Arg of perigee: 74
1473 deg
Mean anomaly: 286
0375 deg
Mean motion: 15
54449396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2424
Checksum: 303
Coasting Arc #13 (Orbit 2438)
---------------------------------------
Vector Time (GMT): 2016/036/19:45:24
087
Vector Time (MET): N/A
Weight (LBS) : 922285
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5117133
98 A = 6783653
90 meter
Y = -2902606
07 meter E =
0011079
Z = -3385386
45 I = 51
63386
XDOT = 5021
129770 Wp = 81
89876
YDOT = 3459
167988 meter/sec RA = 357
53643 deg
ZDOT = 4638
286798 TA = 238
59751
MA = 238
70592
Ha = 222
845 n
mi
Hp = 211
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16788497
32 X = 5165655
76
Y = -9522985
79 feet Y = -2845111
60 meter
Z = -11106910
93 Z = -3360411
32
XDOT = 16473
522867 XDOT = 4959
544961
YDOT = 11348
976338 feet/sec YDOT = 3514
973259 meter/sec
ZDOT = 15217
476371 ZDOT = 4662
528125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3484131
00 X = -1061963
13
Y = -19047537
73 feet Y = -5805689
50 meter
Z = -10998022
93 Z = -3352197
39
XDOT = 14694
215555 XDOT = 4478
796901
YDOT = -11506
855025 feet/sec YDOT = -3507
289412 meter/sec
ZDOT = 15321
870573 ZDOT = 4670
106150
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 16036
83017646
00016717 00000-0 10270-3 0 9121
2 25544 51
6412 358
0821 0006355 78
7921 281
3946 15
54441411 24392
Satellite: ISS
Catalog Number: 25544
Epoch time: 16036
83017646 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 358
0821 deg
Eccentricity:
0006355
Arg of perigee: 78
7921 deg
Mean anomaly: 281
3946 deg
Mean motion: 15
54441411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2439
Checksum: 307
Coasting Arc #14 (Orbit 2454)
---------------------------------------
Vector Time (GMT): 2016/037/19:45:24
087
Vector Time (MET): N/A
Weight (LBS) : 922285
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6155769
75 A = 6786998
21 meter
Y = 2220193
50 meter E =
0019502
Z = 1772249
32 I = 51
61418
XDOT = -3130
101667 Wp = 104
15785
YDOT = -4117
743310 meter/sec RA = 352
55596 deg
ZDOT = -5666
042011 TA = 56
36125
MA = 56
17534
Ha = 222
755 n
mi
Hp = 211
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20196094
99 X = -6188747
63
Y = 7284099
42 feet Y = 2151171
25 meter
Z = 5814466
27 Z = 1742266
68
XDOT = -10269
362423 XDOT = -3056
300847
YDOT = -13509
656528 feet/sec YDOT = -4152
333626 meter/sec
ZDOT = -18589
376676 ZDOT = -5681
067599
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 634131
78 X = 193283
37
Y = 21495075
25 feet Y = 6551698
94 meter
Z = 5684012
00 Z = 1732486
86
XDOT = -14429
674734 XDOT = -4398
164859
YDOT = 5400
589668 feet/sec YDOT = 1646
099731 meter/sec
ZDOT = -18653
678405 ZDOT = -5685
641178
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 16037
85879871
00016717 00000-0 10270-3 0 9131
2 25544 51
6417 352
9514 0006334 80
8225 279
3644 15
54494154 24559
Satellite: ISS
Catalog Number: 25544
Epoch time: 16037
85879871 = yrday
fracday
Element set: 913
Inclination: 51
6417 deg
RA of node: 352
9514 deg
Eccentricity:
0006334
Arg of perigee: 80
8225 deg
Mean anomaly: 279
3644 deg
Mean motion: 15
54494154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2455
Checksum: 334
Coasting Arc #15 (Orbit 2470)
---------------------------------------
Vector Time (GMT): 2016/038/19:45:24
087
Vector Time (MET): N/A
Weight (LBS) : 922285
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6622816
72 A = 6788371
76 meter
Y = -1461936
07 meter E =
0017524
Z = -4068
24 I = 51
58576
XDOT = 1019
481739 Wp = 59
09597
YDOT = 4655
178261 meter/sec RA = 347
57927 deg
ZDOT = 6009
496398 TA = 300
86017
MA = 301
03244
Ha = 222
822 n
mi
Hp = 211
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21728401
30 X = 6638691
99
Y = -4796378
17 feet Y = -1387786
58 meter
Z = -13347
24 Z = 28141
55
XDOT = 3344
756360 XDOT = 938
159803
YDOT = 15272
894556 feet/sec YDOT = 4666
124295 meter/sec
ZDOT = 19716
195532 ZDOT = 6014
250981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1814384
04 X = 553024
26
Y = -22177033
78 feet Y = -6759559
90 meter
Z = 126601
55 Z = 38588
15
XDOT = 13927
910736 XDOT = 4245
227192
YDOT = 1290
104712 feet/sec YDOT = 393
223916 meter/sec
ZDOT = 19735
858961 ZDOT = 6015
489811
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 16038
88741258
00016717 00000-0 10270-3 0 9143
2 25544 51
6405 347
8198 0006363 86
6308 273
5573 15
54458388 24719
Satellite: ISS
Catalog Number: 25544
Epoch time: 16038
88741258 = yrday
fracday
Element set: 914
Inclination: 51
6405 deg
RA of node: 347
8198 deg
Eccentricity:
0006363
Arg of perigee: 86
6308 deg
Mean anomaly: 273
5573 deg
Mean motion: 15
54458388 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2471
Checksum: 346
Coasting Arc #16 (Orbit 2485)
---------------------------------------
Vector Time (GMT): 2016/039/19:45:24
087
Vector Time (MET): N/A
Weight (LBS) : 922285
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6514141
16 A = 6786764
21 meter
Y = 519672
11 meter E =
0012252
Z = -1828587
92 I = 51
55002
XDOT = 1169
565428 Wp = 116
33355
YDOT = -5058
259247 meter/sec RA = 342
60163 deg
ZDOT = -5638
610505 TA = 83
79240
MA = 83
65283
Ha = 222
735 n
mi
Hp = 211
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21371854
20 X = -6510585
86
Y = 1704961
00 feet Y = 446846
44 meter
Z = -5999304
20 Z = -1860222
57
XDOT = 3837
156916 XDOT = 1253
430452
YDOT = -16595
338738 feet/sec YDOT = -5044
711795 meter/sec
ZDOT = -18499
378297 ZDOT = -5632
725214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4292902
37 X = -1308476
64
Y = 20965884
47 feet Y = 6390401
59 meter
Z = -6136560
34 Z = -1870423
59
XDOT = -13314
383487 XDOT = -4058
224087
YDOT = -8100
549943 feet/sec YDOT = -2469
047623 meter/sec
ZDOT = -18472
837202 ZDOT = -5630
520779
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 16039
85172590
00016717 00000-0 10270-3 0 9159
2 25544 51
6407 343
0098 0006444 89
8164 270
3727 15
54498465 24865
Satellite: ISS
Catalog Number: 25544
Epoch time: 16039
85172590 = yrday
fracday
Element set: 915
Inclination: 51
6407 deg
RA of node: 343
0098 deg
Eccentricity:
0006444
Arg of perigee: 89
8164 deg
Mean anomaly: 270
3727 deg
Mean motion: 15
54498465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2486
Checksum: 338
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