[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 14th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 23680 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 120 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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
016/01:58:06
797 -1
3 3
6 3
6
N/A 3
2 -0
3 228
6
000/00:08:13
594 -1
1 -0
1 221
3
Coasting Arc #1 (Orbit 2734)
---------------------------------------
Vector Time (GMT): 2014/013/14:13:39
129
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6050182
17 A = 6798485
04 meter
Y = 2264127
38 meter E =
0018389
Z = 2084710
53 I = 51
86428
XDOT = -58
855333 Wp = 56
07047
YDOT = -5291
239085 meter/sec RA = 144
80622 deg
ZDOT = 5550
782895 TA = 326
91270
MA = 327
02760
Ha = 228
449 n
mi
Hp = 219
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19849679
03 X = -6085177
24
Y = 7428239
42 feet Y = 2196274
55 meter
Z = 6839601
47 Z = 2055235
05
XDOT = -193
094925 XDOT = -26
646801
YDOT = -17359
708284 feet/sec YDOT = -5291
717572 meter/sec
ZDOT = 18211
229971 ZDOT = 5550
574820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20607764
37 X = -6281246
58
Y = -5118409
32 feet Y = -1560091
16 meter
Z = 6714951
99 Z = 2046717
37
XDOT = 9187
271626 XDOT = 2800
280392
YDOT = -12988
523824 feet/sec YDOT = -3958
902061 meter/sec
ZDOT = 18211
136253 ZDOT = 5550
754330
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 14013
65323139
00016717 00000-0 10270-3 0 9008
2 25544 51
6486 145
5419 0005807 22
6848 337
4558 15
50379807 27358
Satellite: ISS
Catalog Number: 25544
Epoch time: 14013
65323139 = yrday
fracday
Element set: 900
Inclination: 51
6486 deg
RA of node: 145
5419 deg
Eccentricity:
0005807
Arg of perigee: 22
6848 deg
Mean anomaly: 337
4558 deg
Mean motion: 15
50379807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2735
Checksum: 320
Coasting Arc #2 (Orbit 2749)
---------------------------------------
Vector Time (GMT): 2014/014/14:13:39
129
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5860850
48 A = 6797565
08 meter
Y = -2344288
44 meter E =
0006779
Z = -2530650
35 I = 51
88593
XDOT = -81
501136 Wp = 75
41682
YDOT = 5514
502709 meter/sec RA = 139
86777 deg
ZDOT = -5307
389791 TA = 132
80973
MA = 132
75273
Ha = 228
422 n
mi
Hp = 219
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19228512
08 X = 5898922
17
Y = -7691235
05 feet Y = -2278535
63 meter
Z = -8302658
63 Z = -2502087
22
XDOT = -267
392178 XDOT = -117
378218
YDOT = 18092
200488 feet/sec YDOT = 5513
391083 meter/sec
ZDOT = -17412
696166 ZDOT = -5307
872463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20327059
12 X = 6195687
62
Y = 4206337
34 feet Y = 1282091
62 meter
Z = -8181827
89 Z = -2493821
14
XDOT = -9795
198247 XDOT = -2985
576426
YDOT = 13526
083578 feet/sec YDOT = 4122
750275 meter/sec
ZDOT = -17415
552740 ZDOT = -5308
260475
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 14014
62009096
00016717 00000-0 10270-3 0 9010
2 25544 51
6483 140
7501 0005814 25
6973 334
4465 15
50399058 27505
Satellite: ISS
Catalog Number: 25544
Epoch time: 14014
62009096 = yrday
fracday
Element set: 901
Inclination: 51
6483 deg
RA of node: 140
7501 deg
Eccentricity:
0005814
Arg of perigee: 25
6973 deg
Mean anomaly: 334
4465 deg
Mean motion: 15
50399058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2750
Checksum: 299
Coasting Arc #3 (Orbit 2765)
---------------------------------------
Vector Time (GMT): 2014/015/14:13:39
129
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5633556
51 A = 6796544
37 meter
Y = 2399009
69 meter E =
0017536
Z = 2926571
55 I = 51
90662
XDOT = 171
686607 Wp = 66
13946
YDOT = -5773
128132 meter/sec RA = 134
92928 deg
ZDOT = 5045
997916 TA = 327
08634
MA = 327
19541
Ha = 228
546 n
mi
Hp = 219
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18482796
95 X = -5674180
20
Y = 7870766
72 feet Y = 2335784
36 meter
Z = 9601612
70 Z = 2899106
43
XDOT = 563
276270 XDOT = 211
718803
YDOT = -18940
709096 feet/sec YDOT = -5770
984692 meter/sec
ZDOT = 16555
111273 ZDOT = 5046
928822
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19870427
80 X = -6056506
39
Y = -3308654
92 feet Y = -1008478
02 meter
Z = 9485389
81 Z = 2891146
81
XDOT = 10310
565667 XDOT = 3142
660415
YDOT = -14285
315489 feet/sec YDOT = -4354
164161 meter/sec
ZDOT = 16559
900793 ZDOT = 5047
457762
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 14015
65138947
00016717 00000-0 10270-3 0 9023
2 25544 51
6490 135
6380 0005927 29
2867 330
8615 15
50439832 27667
Satellite: ISS
Catalog Number: 25544
Epoch time: 14015
65138947 = yrday
fracday
Element set: 902
Inclination: 51
6490 deg
RA of node: 135
6380 deg
Eccentricity:
0005927
Arg of perigee: 29
2867 deg
Mean anomaly: 330
8615 deg
Mean motion: 15
50439832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2766
Checksum: 324
Coasting Arc #4 (Orbit 2772)
---------------------------------------
Vector Time (GMT): 2014/016/02:02:13
594
Vector Time (MET): N/A
Weight (LBS) : 911270
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3735650
29 A = 6790339
57 meter
Y = 2068518
92 meter E =
0016085
Z = -5293308
77 I = 51
89013
XDOT = -4601
532715 Wp = 67
94188
YDOT = 6047
177180 meter/sec RA = 132
48420 deg
ZDOT = -880
597516 TA = 193
62365
MA = 193
66711
Ha = 228
630 n
mi
Hp = 221
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12256070
51 X = 3737954
77
Y = 6786479
41 feet Y = 2110306
51 meter
Z = -17366498
60 Z = -5275156
11
XDOT = -15096
892108 XDOT = -4664
534015
YDOT = 19839
820144 feet/sec YDOT = 5995
367691 meter/sec
ZDOT = -2889
099462 ZDOT = -903
103443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6274591
87 X = -1912495
60
Y = -12630932
59 feet Y = -3849908
25 meter
Z = -17290224
98 Z = -5270060
57
XDOT = 22787
040815 XDOT = 6945
490040
YDOT = -7216
914859 feet/sec YDOT = -2199
715649 meter/sec
ZDOT = -2984
953313 ZDOT = -909
813770
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 14016
10258226
00016717 00000-0 10270-3 0 9038
2 25544 51
6490 133
4028 0004396 7
5580 352
5636 15
49774569 27731
Satellite: ISS
Catalog Number: 25544
Epoch time: 14016
10258226 = yrday
fracday
Element set: 903
Inclination: 51
6490 deg
RA of node: 133
4028 deg
Eccentricity:
0004396
Arg of perigee: 7
5580 deg
Mean anomaly: 352
5636 deg
Mean motion: 15
49774569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2773
Checksum: 313
Coasting Arc #5 (Orbit 2788)
---------------------------------------
Vector Time (GMT): 2014/017/02:02:13
594
Vector Time (MET): N/A
Weight (LBS) : 911270
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3703045
26 A = 6790071
69 meter
Y = -2021292
89 meter E =
0004611
Z = 5317227
72 I = 51
90987
XDOT = 4286
840241 Wp = 47
54435
YDOT = -6326
911288 meter/sec RA = 127
54814 deg
ZDOT = 583
053851 TA = 36
92500
MA = 36
89326
Ha = 228
725 n
mi
Hp = 221
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12149098
63 X = -3705996
41
Y = -6631538
35 feet Y = -2062719
40 meter
Z = 17444972
84 Z = 5299231
93
XDOT = 14064
436487 XDOT = 4354
438331
YDOT = -20757
582966 feet/sec YDOT = -6278
595163 meter/sec
ZDOT = 1912
906335 ZDOT = 604
042295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6488785
22 X = 1977781
74
Y = 12333143
19 feet Y = 3759142
04 meter
Z = 17369347
17 Z = 5294177
02
XDOT = -22331
923621 XDOT = -6806
770320
YDOT = 8941
884481 feet/sec YDOT = 2725
486390 meter/sec
ZDOT = 2002
412320 ZDOT = 610
335275
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 14017
13431062
00016717 00000-0 10270-3 0 9044
2 25544 51
6490 128
2936 0004396 9
8339 350
2897 15
49808694 27896
Satellite: ISS
Catalog Number: 25544
Epoch time: 14017
13431062 = yrday
fracday
Element set: 904
Inclination: 51
6490 deg
RA of node: 128
2936 deg
Eccentricity:
0004396
Arg of perigee: 9
8339 deg
Mean anomaly: 350
2897 deg
Mean motion: 15
49808694 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2789
Checksum: 334
Coasting Arc #6 (Orbit 2803)
---------------------------------------
Vector Time (GMT): 2014/018/02:02:13
594
Vector Time (MET): N/A
Weight (LBS) : 911270
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3700721
90 A = 6789939
79 meter
Y = 1988791
14 meter E =
0016626
Z = -5347996
63 I = 51
92823
XDOT = -3933
484030 Wp = 72
65589
YDOT = 6554
786867 meter/sec RA = 122
61318 deg
ZDOT = -280
238342 TA = 194
65273
MA = 194
70098
Ha = 228
709 n
mi
Hp = 220
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12141476
05 X = 3704186
12
Y = 6524905
32 feet Y = 2030194
45 meter
Z = -17545920
71 Z = -5330010
93
XDOT = -12905
131331 XDOT = -4005
127491
YDOT = 21505
206258 feet/sec YDOT = 6510
399561 meter/sec
ZDOT = -919
417133 ZDOT = -299
520193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6751956
12 X = -2057996
23
Y = -12126331
83 feet Y = -3696105
94 meter
Z = -17470327
09 Z = -5324955
70
XDOT = 21618
637813 XDOT = 6589
360805
YDOT = -10574
591160 feet/sec YDOT = -3223
135386 meter/sec
ZDOT = -1001
767412 ZDOT = -305
338707
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 14018
10154133
00016717 00000-0 10270-3 0 9054
2 25544 51
6496 123
5038 0004537 13
6627 346
4646 15
49827665 28049
Satellite: ISS
Catalog Number: 25544
Epoch time: 14018
10154133 = yrday
fracday
Element set: 905
Inclination: 51
6496 deg
RA of node: 123
5038 deg
Eccentricity:
0004537
Arg of perigee: 13
6627 deg
Mean anomaly: 346
4646 deg
Mean motion: 15
49827665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2804
Checksum: 307
Coasting Arc #7 (Orbit 2819)
---------------------------------------
Vector Time (GMT): 2014/019/02:02:13
594
Vector Time (MET): N/A
Weight (LBS) : 911270
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3682122
41 A = 6789799
53 meter
Y = -1987109
64 meter E =
0005738
Z = 5344243
31 I = 51
94398
XDOT = 3588
878404 Wp = 40
11887
YDOT = -6772
528203 meter/sec RA = 117
67886 deg
ZDOT = -41
185748 TA = 50
29741
MA = 50
24683
Ha = 228
814 n
mi
Hp = 220
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12080454
10 X = -3685588
61
Y = -6519388
60 feet Y = -2028304
88 meter
Z = 17533606
65 Z = 5326347
96
XDOT = 11774
535446 XDOT = 3664
543656
YDOT = -22219
580717 feet/sec YDOT = -6731
972004 meter/sec
ZDOT = -135
123844 ZDOT = -23
568015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6910573
10 X = 2106342
68
Y = 11971456
14 feet Y = 3648899
83 meter
Z = 17458389
91 Z = 5321317
24
XDOT = -20858
928063 XDOT = -6357
801273
YDOT = 12148
687168 feet/sec YDOT = 3702
919849 meter/sec
ZDOT = -59
752967 ZDOT = -18
212704
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 14019
13323574
00016717 00000-0 10270-3 0 9066
2 25544 51
6495 118
3943 0004544 16
4401 343
6896 15
49859872 28203
Satellite: ISS
Catalog Number: 25544
Epoch time: 14019
13323574 = yrday
fracday
Element set: 906
Inclination: 51
6495 deg
RA of node: 118
3943 deg
Eccentricity:
0004544
Arg of perigee: 16
4401 deg
Mean anomaly: 343
6896 deg
Mean motion: 15
49859872 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2820
Checksum: 323
Coasting Arc #8 (Orbit 2834)
---------------------------------------
Vector Time (GMT): 2014/020/02:02:13
594
Vector Time (MET): N/A
Weight (LBS) : 911270
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3701617
54 A = 6789797
22 meter
Y = 1990851
56 meter E =
0016737
Z = -5346427
55 I = 51
95745
XDOT = -3213
106675 Wp = 77
36572
YDOT = 6932
719863 meter/sec RA = 112
74511 deg
ZDOT = 361
443532 TA = 196
04729
MA = 196
10037
Ha = 228
776 n
mi
Hp = 220
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12144414
51 X = 3705051
11
Y = 6531665
22 feet Y = 2032264
55 meter
Z = -17540772
79 Z = -5328437
57
XDOT = -10541
688565 XDOT = -3292
146840
YDOT = 22745
143908 feet/sec YDOT = 6896
346917 meter/sec
ZDOT = 1185
838360 ZDOT = 345
642894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7164103
61 X = -2183618
78
Y = -11894207
01 feet Y = -3625354
30 meter
Z = -17465154
55 Z = -5323379
11
XDOT = 19861
146378 XDOT = 6053
677416
YDOT = -13582
716059 feet/sec YDOT = -4140
011855 meter/sec
ZDOT = 1118
101612 ZDOT = 340
797371
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 14020
10043436
00016717 00000-0 10270-3 0 9072
2 25544 51
6493 113
6039 0004657 19
5114 340
6214 15
49878491 28350
Satellite: ISS
Catalog Number: 25544
Epoch time: 14020
10043436 = yrday
fracday
Element set: 907
Inclination: 51
6493 deg
RA of node: 113
6039 deg
Eccentricity:
0004657
Arg of perigee: 19
5114 deg
Mean anomaly: 340
6214 deg
Mean motion: 15
49878491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2835
Checksum: 296
Coasting Arc #9 (Orbit 2850)
---------------------------------------
Vector Time (GMT): 2014/021/02:02:13
594
Vector Time (MET): N/A
Weight (LBS) : 911270
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3710527
97 A = 6789811
95 meter
Y = -2027106
89 meter E =
0007237
Z = 5309334
15 I = 51
96892
XDOT = 2852
496490 Wp = 38
67383
YDOT = -7079
490615 meter/sec RA = 107
81199 deg
ZDOT = -703
418088 TA = 58
05200
MA = 57
98165
Ha = 228
886 n
mi
Hp = 220
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12173648
21 X = -3713375
35
Y = -6650613
16 feet Y = -2068616
20 meter
Z = 17419075
29 Z = 5291302
28
XDOT = 9358
584284 XDOT = 2934
865866
YDOT = -23226
675247 feet/sec YDOT = -7047
131637 meter/sec
ZDOT = -2307
802125 ZDOT = -689
361036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7333027
16 X = 2235106
68
Y = 11886536
38 feet Y = 3623016
29 meter
Z = 17343284
45 Z = 5286233
10
XDOT = -18836
543942 XDOT = -5741
378594
YDOT = 14928
635427 feet/sec YDOT = 4550
248078 meter/sec
ZDOT = -2247
390896 ZDOT = -685
004745
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 14021
13209498
00016717 00000-0 10270-3 0 9089
2 25544 51
6493 108
4942 0004668 22
7378 337
3979 15
49909390 28517
Satellite: ISS
Catalog Number: 25544
Epoch time: 14021
13209498 = yrday
fracday
Element set: 908
Inclination: 51
6493 deg
RA of node: 108
4942 deg
Eccentricity:
0004668
Arg of perigee: 22
7378 deg
Mean anomaly: 337
3979 deg
Mean motion: 15
49909390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2851
Checksum: 340
Coasting Arc #10 (Orbit 2865)
---------------------------------------
Vector Time (GMT): 2014/022/02:02:13
594
Vector Time (MET): N/A
Weight (LBS) : 911270
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3762997
90 A = 6789961
70 meter
Y = 2057147
60 meter E =
0016387
Z = -5277822
92 I = 51
97734
XDOT = -2470
003969 Wp = 81
94359
YDOT = 7165
589838 meter/sec RA = 102
87873 deg
ZDOT = 1036
857162 TA = 197
93467
MA = 197
99256
Ha = 228
837 n
mi
Hp = 220
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12345793
64 X = 3765352
46
Y = 6749171
91 feet Y = 2099240
90 meter
Z = -17315691
99 Z = -5259537
30
XDOT = -8103
687563 XDOT = -2554
984288
YDOT = 23509
153013 feet/sec YDOT = 7137
493545 meter/sec
ZDOT = 3401
762344 ZDOT = 1024
651792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7638871
52 X = -2328328
04
Y = -11927839
31 feet Y = -3635605
42 meter
Z = -17238834
71 Z = -5254396
82
XDOT = 17608
771303 XDOT = 5367
153493
YDOT = -16093
729703 feet/sec YDOT = -4905
368814 meter/sec
ZDOT = 3349
141024 ZDOT = 1020
818184
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 14022
09926190
00016717 00000-0 10270-3 0 9091
2 25544 51
6485 103
7030 0004744 25
6455 334
4930 15
49926478 28664
Satellite: ISS
Catalog Number: 25544
Epoch time: 14022
09926190 = yrday
fracday
Element set: 909
Inclination: 51
6485 deg
RA of node: 103
7030 deg
Eccentricity:
0004744
Arg of perigee: 25
6455 deg
Mean anomaly: 334
4930 deg
Mean motion: 15
49926478 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2866
Checksum: 319
Coasting Arc #11 (Orbit 2881)
---------------------------------------
Vector Time (GMT): 2014/023/02:02:13
594
Vector Time (MET): N/A
Weight (LBS) : 911270
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3809969
46 A = 6790154
06 meter
Y = -2119479
37 meter E =
0008936
Z = 5201840
46 I = 51
98446
XDOT = 2110
588432 Wp = 41
59622
YDOT = -7235
571326 meter/sec RA = 97
94640 deg
ZDOT = -1394
393770 TA = 61
79921
MA = 61
70900
Ha = 228
940 n
mi
Hp = 220
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12499899
80 X = -3811254
49
Y = -6953672
47 feet Y = -2162091
99 meter
Z = 17066405
72 Z = 5183329
21
XDOT = 6924
502729 XDOT = 2198
114811
YDOT = -23738
751069 feet/sec YDOT = -7211
480012 meter/sec
ZDOT = -4574
782710 ZDOT = -1383
928194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7881909
63 X = 2402406
06
Y = 12046825
77 feet Y = 3671872
50 meter
Z = 16988606
46 Z = 5178127
25
XDOT = -16383
163399 XDOT = -4993
588204
YDOT = 17143
186486 feet/sec YDOT = 5225
243241 meter/sec
ZDOT = -4529
480148 ZDOT = -1380
585549
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 14023
13088909
00016717 00000-0 10270-3 0 9106
2 25544 51
6487 98
5930 0004748 28
9817 331
1596 15
49956129 28824
Satellite: ISS
Catalog Number: 25544
Epoch time: 14023
13088909 = yrday
fracday
Element set: 910
Inclination: 51
6487 deg
RA of node: 98
5930 deg
Eccentricity:
0004748
Arg of perigee: 28
9817 deg
Mean anomaly: 331
1596 deg
Mean motion: 15
49956129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2882
Checksum: 344
Coasting Arc #12 (Orbit 2896)
---------------------------------------
Vector Time (GMT): 2014/024/02:02:13
594
Vector Time (MET): N/A
Weight (LBS) : 911270
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3902903
99 A = 6790465
87 meter
Y = 2162477
88 meter E =
0015566
Z = -5131851
06 I = 51
98792
XDOT = -1739
710762 Wp = 86
09689
YDOT = 7245
067111 meter/sec RA = 93
01331 deg
ZDOT = 1735
419471 TA = 200
60457
MA = 200
66741
Ha = 228
892 n
mi
Hp = 220
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12804803
12 X = 3903361
36
Y = 7094743
69 feet Y = 2206125
17 meter
Z = -16836781
71 Z = -5112890
31
XDOT = -5707
712475 XDOT = -1829
027485
YDOT = 23769
905221 feet/sec YDOT = 7225
113165 meter/sec
ZDOT = 5693
633434 ZDOT = 1726
751264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8294568
14 X = -2528184
37
Y = -12172738
55 feet Y = -3710250
71 meter
Z = -16757092
97 Z = -5107561
94
XDOT = 15002
339593 XDOT = 4572
713108
YDOT = -17983
395493 feet/sec YDOT = -5481
338946 meter/sec
ZDOT = 5655
900844 ZDOT = 1723
918577
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 14024
09802489
00016717 00000-0 10270-3 0 9110
2 25544 51
6476 93
8012 0004794 32
3782 327
7662 15
49971868 28970
Satellite: ISS
Catalog Number: 25544
Epoch time: 14024
09802489 = yrday
fracday
Element set: 911
Inclination: 51
6476 deg
RA of node: 93
8012 deg
Eccentricity:
0004794
Arg of perigee: 32
3782 deg
Mean anomaly: 327
7662 deg
Mean motion: 15
49971868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2897
Checksum: 344
Coasting Arc #13 (Orbit 2912)
---------------------------------------
Vector Time (GMT): 2014/025/02:02:13
594
Vector Time (MET): N/A
Weight (LBS) : 911270
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3994111
33 A = 6790847
93 meter
Y = -2235800
22 meter E =
0010719
Z = 5011864
94 I = 51
99063
XDOT = 1401
193523 Wp = 47
51400
YDOT = -7236
924796 meter/sec RA = 88
08141 deg
ZDOT = -2101
846768 TA = 62
90695
MA = 62
79764
Ha = 228
976 n
mi
Hp = 220
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13104039
81 X = -3993159
16
Y = -7335302
55 feet Y = -2280459
64 meter
Z = 16443126
45 Z = 4992464
51
XDOT = 4597
091612 XDOT = 1492
224334
YDOT = -23743
191589 feet/sec YDOT = -7220
746754 meter/sec
ZDOT = -6895
822729 ZDOT = -2094
818961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8664264
00 X = 2640867
67
Y = 12374477
35 feet Y = 3771740
70 meter
Z = 16361594
36 Z = 4987013
96
XDOT = -13662
070012 XDOT = -4164
198940
YDOT = 18685
901179 feet/sec YDOT = 5695
462679 meter/sec
ZDOT = -6864
999813 ZDOT = -2092
451943
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 14025
12961912
00016717 00000-0 10270-3 0 9123
2 25544 51
6480 88
6911 0004778 35
5045 324
6423 15
50000066 29139
Satellite: ISS
Catalog Number: 25544
Epoch time: 14025
12961912 = yrday
fracday
Element set: 912
Inclination: 51
6480 deg
RA of node: 88
6911 deg
Eccentricity:
0004778
Arg of perigee: 35
5045 deg
Mean anomaly: 324
6423 deg
Mean motion: 15
50000066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2913
Checksum: 286
Coasting Arc #14 (Orbit 2927)
---------------------------------------
Vector Time (GMT): 2014/026/02:02:13
594
Vector Time (MET): N/A
Weight (LBS) : 911270
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4130208
43 A = 6791316
05 meter
Y = 2276277
06 meter E =
0014316
Z = -4899186
28 I = 51
98918
XDOT = -1061
820116 Wp = 89
27640
YDOT = 7172
276682 meter/sec RA = 83
14834 deg
ZDOT = 2443
589491 TA = 204
60265
MA = 204
67101
Ha = 228
941 n
mi
Hp = 220
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13550552
58 X = 4128246
13
Y = 7468100
58 feet Y = 2322452
84 meter
Z = -16073445
81 Z = -4879127
16
XDOT = -3483
661799 XDOT = -1153
813288
YDOT = 23531
091478 feet/sec YDOT = 7159
888308 meter/sec
ZDOT = 8017
025890 ZDOT = 2438
208089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9222442
94 X = -2811000
61
Y = -12531544
65 feet Y = -3819614
81 meter
Z = -15989139
96 Z = -4873489
86
XDOT = 12223
692167 XDOT = 3725
781372
YDOT = -19167
760367 feet/sec YDOT = -5842
333360 meter/sec
ZDOT = 7993
147679 ZDOT = 2436
311413
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 14026
09672436
00016717 00000-0 10270-3 0 9131
2 25544 51
6468 83
8990 0004821 39
8855 320
2650 15
50015921 29280
Satellite: ISS
Catalog Number: 25544
Epoch time: 14026
09672436 = yrday
fracday
Element set: 913
Inclination: 51
6468 deg
RA of node: 83
8990 deg
Eccentricity:
0004821
Arg of perigee: 39
8855 deg
Mean anomaly: 320
2650 deg
Mean motion: 15
50015921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2928
Checksum: 315
Coasting Arc #15 (Orbit 2943)
---------------------------------------
Vector Time (GMT): 2014/027/02:02:13
594
Vector Time (MET): N/A
Weight (LBS) : 911270
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4266353
26 A = 6791885
42 meter
Y = -2343901
66 meter E =
0012521
Z = 4730768
34 I = 51
98721
XDOT = 765
153033 Wp = 55
55457
YDOT = -7090
203257 meter/sec RA = 78
21641 deg
ZDOT = -2810
686432 TA = 62
24514
MA = 62
11822
Ha = 229
005 n
mi
Hp = 219
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13997222
00 X = -4262806
46
Y = -7689966
06 feet Y = -2391591
09 meter
Z = 15520893
49 Z = 4710051
74
XDOT = 2510
344598 XDOT = 858
033669
YDOT = -23261
821709 feet/sec YDOT = -7081
127396 meter/sec
ZDOT = -9221
412177 ZDOT = -2806
744133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9751374
39 X = 2972218
92
Y = 12753970
60 feet Y = 3887410
24 meter
Z = 15433822
21 Z = 4704229
01
XDOT = -10872
453977 XDOT = -3313
923972
YDOT = 19498
903316 feet/sec YDOT = 5943
265731 meter/sec
ZDOT = -9203
608524 ZDOT = -2805
259878
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 14027
12828593
00016717 00000-0 10270-3 0 9144
2 25544 51
6473 78
7888 0004782 42
7840 317
3682 15
50041932 29449
Satellite: ISS
Catalog Number: 25544
Epoch time: 14027
12828593 = yrday
fracday
Element set: 914
Inclination: 51
6473 deg
RA of node: 78
7888 deg
Eccentricity:
0004782
Arg of perigee: 42
7840 deg
Mean anomaly: 317
3682 deg
Mean motion: 15
50041932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2944
Checksum: 327
Coasting Arc #16 (Orbit 2958)
---------------------------------------
Vector Time (GMT): 2014/028/02:02:13
594
Vector Time (MET): N/A
Weight (LBS) : 911270
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4442786
08 A = 6792485
67 meter
Y = 2365928
83 meter E =
0012762
Z = -4571979
06 I = 51
98093
XDOT = -477
239428 Wp = 90
54706
YDOT = 6959
495009 meter/sec RA = 73
28296 deg
ZDOT = 3145
136609 TA = 210
86339
MA = 210
93847
Ha = 228
986 n
mi
Hp = 219
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14576069
82 X = 4438208
40
Y = 7762233
71 feet Y = 2415585
50 meter
Z = -14999931
30 Z = -4550407
98
XDOT = -1565
746156 XDOT = -570
304412
YDOT = 22832
988875 feet/sec YDOT = 6953
637725 meter/sec
ZDOT = 10318
689661 ZDOT = 3142
592530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10470896
88 X = -3191529
37
Y = -12875809
90 feet Y = -3924546
86 meter
Z = -14909254
20 Z = -4544340
68
XDOT = 9483
483888 XDOT = 2890
565889
YDOT = -19618
199498 feet/sec YDOT = -5979
627207 meter/sec
ZDOT = 10306
799309 ZDOT = 3141
512429
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 14028
09536074
00016717 00000-0 10270-3 0 9152
2 25544 51
6461 73
9966 0004853 48
2236 311
9329 15
50060537 29595
Satellite: ISS
Catalog Number: 25544
Epoch time: 14028
09536074 = yrday
fracday
Element set: 915
Inclination: 51
6461 deg
RA of node: 73
9966 deg
Eccentricity:
0004853
Arg of perigee: 48
2236 deg
Mean anomaly: 311
9329 deg
Mean motion: 15
50060537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2959
Checksum: 321
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