[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 25th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25833 39 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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
There are no maneuvers
Coasting Arc #1 (Orbit 3384)
---------------------------------------
Vector Time (GMT): 2014/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4872447
99 A = 6793567
77 meter
Y = -2962150
32 meter E =
0012813
Z = 3686373
69 I = 51
33467
XDOT = 579
639294 Wp = 110
10167
YDOT = 6320
148263 meter/sec RA = 297
55242 deg
ZDOT = 4295
837292 TA = 293
95088
MA = 294
08502
Ha = 226
861 n
mi
Hp = 219
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15985721
75 X = 4887302
34
Y = -9718340
93 feet Y = -2907580
23 meter
Z = 12094401
87 Z = 3710079
23
XDOT = 1901
703721 XDOT = 488
055420
YDOT = 20735
394565 feet/sec YDOT = 6326
118314 meter/sec
ZDOT = 14093
954370 ZDOT = 4298
430273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18575077
90 X = 5661683
74
Y = -1585865
64 feet Y = -483371
85 meter
Z = 12194897
22 Z = 3717004
67
XDOT = -7757
325007 XDOT = -2364
432662
YDOT = 18007
771221 feet/sec YDOT = 5488
768668 meter/sec
ZDOT = 14103
869820 ZDOT = 4298
859521
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 14055
55652208
00016717 00000-0 10270-3 0 9005
2 25544 51
6498 297
9337 0003352 173
7621 186
3572 15
50670435 33852
Satellite: ISS
Catalog Number: 25544
Epoch time: 14055
55652208 = yrday
fracday
Element set: 900
Inclination: 51
6498 deg
RA of node: 297
9337 deg
Eccentricity:
0003352
Arg of perigee: 173
7621 deg
Mean anomaly: 186
3572 deg
Mean motion: 15
50670435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3385
Checksum: 321
Coasting Arc #2 (Orbit 3399)
---------------------------------------
Vector Time (GMT): 2014/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4685243
38 A = 6792119
35 meter
Y = 2733960
31 meter E =
0007001
Z = -4092797
49 I = 51
31637
XDOT = -546
392725 Wp = 97
35763
YDOT = -6622
341795 meter/sec RA = 292
57067 deg
ZDOT = -3804
691002 TA = 133
13718
MA = 133
07862
Ha = 226
656 n
mi
Hp = 219
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15371533
41 X = -4695585
81
Y = 8969686
06 feet Y = 2681508
85 meter
Z = -13427813
28 Z = -4115582
58
XDOT = -1792
627052 XDOT = -453
817996
YDOT = -21726
843158 feet/sec YDOT = -6627
934521 meter/sec
ZDOT = -12482
582026 ZDOT = -3807
119999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17660468
39 X = -5382910
76
Y = 1498100
26 feet Y = 456620
96 meter
Z = -13524386
45 Z = -4122232
99
XDOT = 7933
616516 XDOT = 2418
166314
YDOT = -19054
719294 feet/sec YDOT = -5807
878441 meter/sec
ZDOT = -12491
768804 ZDOT = -3807
491132
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 14056
52318521
00016717 00000-0 10270-3 0 9011
2 25544 51
6495 293
1400 0003360 182
2594 177
8542 15
50708675 34009
Satellite: ISS
Catalog Number: 25544
Epoch time: 14056
52318521 = yrday
fracday
Element set: 901
Inclination: 51
6495 deg
RA of node: 293
1400 deg
Eccentricity:
0003360
Arg of perigee: 182
2594 deg
Mean anomaly: 177
8542 deg
Mean motion: 15
50708675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3400
Checksum: 294
Coasting Arc #3 (Orbit 3415)
---------------------------------------
Vector Time (GMT): 2014/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4507608
55 A = 6790850
28 meter
Y = -2483014
09 meter E =
0010613
Z = 4427157
98 I = 51
30099
XDOT = 568
975491 Wp = 127
63833
YDOT = 6903
034229 meter/sec RA = 287
58656 deg
ZDOT = 3280
531972 TA = 289
04266
MA = 289
15760
Ha = 226
557 n
mi
Hp = 219
980
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14788741
97 X = 4513533
93
Y = -8146371
69 feet Y = -2432573
66 meter
Z = 14524796
52 Z = 4449069
39
XDOT = 1866
717489 XDOT = 475
806513
YDOT = 22647
750094 feet/sec YDOT = 6908
876190 meter/sec
ZDOT = 10762
900169 ZDOT = 3283
069088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16753506
61 X = 5106468
82
Y = -1297909
75 feet Y = -395602
89 meter
Z = 14617640
75 Z = 4455456
90
XDOT = -7873
562046 XDOT = -2399
861712
YDOT = 20125
133219 feet/sec YDOT = 6134
140605 meter/sec
ZDOT = 10772
513241 ZDOT = 3283
462036
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 14057
55427444
00016717 00000-0 10270-3 0 9021
2 25544 51
6492 288
0264 0003257 183
3816 176
7313 15
50726613 34164
Satellite: ISS
Catalog Number: 25544
Epoch time: 14057
55427444 = yrday
fracday
Element set: 902
Inclination: 51
6492 deg
RA of node: 288
0264 deg
Eccentricity:
0003257
Arg of perigee: 183
3816 deg
Mean anomaly: 176
7313 deg
Mean motion: 15
50726613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3416
Checksum: 309
Coasting Arc #4 (Orbit 3430)
---------------------------------------
Vector Time (GMT): 2014/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4371680
68 A = 6789511
23 meter
Y = 2149876
35 meter E =
0009881
Z = -4737809
53 I = 51
28730
XDOT = -608
219903 Wp = 87
79220
YDOT = -7143
213035 meter/sec RA = 282
59982 deg
ZDOT = -2684
658177 TA = 155
52345
MA = 155
47650
Ha = 226
366 n
mi
Hp = 219
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14342784
40 X = -4372381
96
Y = 7053400
09 feet Y = 2100985
02 meter
Z = -15543994
52 Z = -4759047
95
XDOT = -1995
472122 XDOT = -515
256788
YDOT = -23435
738304 feet/sec YDOT = -7149
495019 meter/sec
ZDOT = -8807
933652 ZDOT = -2687
386251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15876907
90 X = -4839281
53
Y = 765044
05 feet Y = 233185
43 meter
Z = -15633943
39 Z = -4765225
94
XDOT = 7652
297567 XDOT = 2332
420298
YDOT = -21098
147013 feet/sec YDOT = -6430
715209 meter/sec
ZDOT = -8818
331519 ZDOT = -2687
827447
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 14058
52089883
00016717 00000-0 10270-3 0 9031
2 25544 51
6479 283
2320 0003274 191
4489 168
6588 15
50778690 34317
Satellite: ISS
Catalog Number: 25544
Epoch time: 14058
52089883 = yrday
fracday
Element set: 903
Inclination: 51
6479 deg
RA of node: 283
2320 deg
Eccentricity:
0003274
Arg of perigee: 191
4489 deg
Mean anomaly: 168
6588 deg
Mean motion: 15
50778690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3431
Checksum: 342
Coasting Arc #5 (Orbit 3446)
---------------------------------------
Vector Time (GMT): 2014/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4259538
12 A = 6788523
06 meter
Y = -1799078
99 meter E =
0007786
Z = 4968549
89 I = 51
27792
XDOT = 687
365138 Wp = 145
93428
YDOT = 7348
944255 meter/sec RA = 277
61163 deg
ZDOT = 2063
812073 TA = 283
83147
MA = 283
91809
Ha = 226
250 n
mi
Hp = 220
112
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13974862
58 X = 4255204
16
Y = -5902490
13 feet Y = -1751469
73 meter
Z = 16301016
70 Z = 4989231
36
XDOT = 2255
134966 XDOT = 595
111393
YDOT = 24110
709498 feet/sec YDOT = 7356
115244 meter/sec
ZDOT = 6771
036984 ZDOT = 2066
926151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15075159
82 X = 4594908
71
Y = -118565
99 feet Y = -36138
91 meter
Z = 16388557
53 Z = 4995232
34
XDOT = -7228
964284 XDOT = -2203
388314
YDOT = 22011
654752 feet/sec YDOT = 6709
152368 meter/sec
ZDOT = 6783
049004 ZDOT = 2067
473336
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 14059
55194695
00016717 00000-0 10270-3 0 9044
2 25544 51
6476 278
1180 0003214 193
2670 166
8397 15
50783830 34474
Satellite: ISS
Catalog Number: 25544
Epoch time: 14059
55194695 = yrday
fracday
Element set: 904
Inclination: 51
6476 deg
RA of node: 278
1180 deg
Eccentricity:
0003214
Arg of perigee: 193
2670 deg
Mean anomaly: 166
8397 deg
Mean motion: 15
50783830 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3447
Checksum: 332
Coasting Arc #6 (Orbit 3461)
---------------------------------------
Vector Time (GMT): 2014/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4203523
58 A = 6787568
09 meter
Y = 1385477
98 meter E =
0012525
Z = -5156849
34 I = 51
27047
XDOT = -770
729385 Wp = 92
26363
YDOT = -7487
735757 meter/sec RA = 272
62057 deg
ZDOT = -1386
881188 TA = 164
32493
MA = 164
28612
Ha = 226
100 n
mi
Hp = 220
014
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13791087
86 X = -4193654
03
Y = 4545531
45 feet Y = 1338525
95 meter
Z = -16918797
03 Z = -5177245
30
XDOT = -2528
639714 XDOT = -680
205661
YDOT = -24566
062196 feet/sec YDOT = -7495
848594 meter/sec
ZDOT = -4550
135131 ZDOT = -1390
404294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14396723
26 X = -4388121
25
Y = -814687
02 feet Y = -248316
60 meter
Z = -17005066
83 Z = -5183144
37
XDOT = 6662
729731 XDOT = 2030
800022
YDOT = -22710
922143 feet/sec YDOT = -6922
289069 meter/sec
ZDOT = -4563
867957 ZDOT = -1391
066953
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 14060
51853245
00016717 00000-0 10270-3 0 9056
2 25544 51
6460 273
3224 0003238 199
8789 160
2236 15
50845840 34629
Satellite: ISS
Catalog Number: 25544
Epoch time: 14060
51853245 = yrday
fracday
Element set: 905
Inclination: 51
6460 deg
RA of node: 273
3224 deg
Eccentricity:
0003238
Arg of perigee: 199
8789 deg
Mean anomaly: 160
2236 deg
Mean motion: 15
50845840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3462
Checksum: 309
Coasting Arc #7 (Orbit 3477)
---------------------------------------
Vector Time (GMT): 2014/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4180838
29 A = 6787084
04 meter
Y = -964519
18 meter E =
0004597
Z = 5257940
47 I = 51
26850
XDOT = 870
991277 Wp = 161
25129
YDOT = 7582
897815 meter/sec RA = 267
62961 deg
ZDOT = 693
996873 TA = 282
05721
MA = 282
10873
Ha = 225
940 n
mi
Hp = 220
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13716661
06 X = 4165772
00
Y = -3164433
02 feet Y = -917849
83 meter
Z = 17250460
87 Z = 5278213
66
XDOT = 2857
582931 XDOT = 782
761709
YDOT = 24878
273672 feet/sec YDOT = 7592
144581 meter/sec
ZDOT = 2276
892628 ZDOT = 698
012540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13850573
39 X = 4221654
77
Y = 1832607
00 feet Y = 558578
61 meter
Z = 17336147
08 Z = 5284057
63
XDOT = -5967
524738 XDOT = -1818
901540
YDOT = 23275
754762 feet/sec YDOT = 7094
450052 meter/sec
ZDOT = 2292
703284 ZDOT = 698
815961
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 14061
54953856
00016717 00000-0 10270-3 0 9060
2 25544 51
6461 268
2079 0003228 202
9841 157
1166 15
50845603 34786
Satellite: ISS
Catalog Number: 25544
Epoch time: 14061
54953856 = yrday
fracday
Element set: 906
Inclination: 51
6461 deg
RA of node: 268
2079 deg
Eccentricity:
0003228
Arg of perigee: 202
9841 deg
Mean anomaly: 157
1166 deg
Mean motion: 15
50845603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3478
Checksum: 320
Coasting Arc #8 (Orbit 3492)
---------------------------------------
Vector Time (GMT): 2014/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4221611
43 A = 6786743
85 meter
Y = 507646
18 meter E =
0013673
Z = -5301266
43 I = 51
26880
XDOT = -955
986247 Wp = 102
39988
YDOT = -7593
451811 meter/sec RA = 262
63629 deg
ZDOT = 31
333896 TA = 167
91724
MA = 167
88441
Ha = 225
853 n
mi
Hp = 220
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13850431
21 X = -4201222
67
Y = 1665505
86 feet Y = 460550
64 meter
Z = -17392606
40 Z = -5321724
78
XDOT = -3136
437818 XDOT = -871
155721
YDOT = -24912
899642 feet/sec YDOT = -7603
667943 meter/sec
ZDOT = 102
801495 ZDOT = 26
897052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13501477
19 X = -4115250
25
Y = -3050507
74 feet Y = -929794
76 meter
Z = -17479005
35 Z = -5327600
83
XDOT = 5194
988536 XDOT = 1583
432506
YDOT = -23533
705378 feet/sec YDOT = -7173
073399 meter/sec
ZDOT = 85
204000 ZDOT = 25
970179
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 14062
51608497
00016717 00000-0 10270-3 0 9077
2 25544 51
6447 263
4114 0003235 207
5499 152
5481 15
50909880 34939
Satellite: ISS
Catalog Number: 25544
Epoch time: 14062
51608497 = yrday
fracday
Element set: 907
Inclination: 51
6447 deg
RA of node: 263
4114 deg
Eccentricity:
0003235
Arg of perigee: 207
5499 deg
Mean anomaly: 152
5481 deg
Mean motion: 15
50909880 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3493
Checksum: 320
Coasting Arc #9 (Orbit 3508)
---------------------------------------
Vector Time (GMT): 2014/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4298042
99 A = 6786912
90 meter
Y = -57300
03 meter E =
0001670
Z = 5251147
76 I = 51
27477
XDOT = 1029
981762 Wp = 140
70508
YDOT = 7556
715989 meter/sec RA = 257
64478 deg
ZDOT = -761
713631 TA = 316
60698
MA = 316
62012
Ha = 225
630 n
mi
Hp = 220
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14101190
91 X = 4272856
06
Y = -187992
24 feet Y = -9376
68 meter
Z = 17228175
06 Z = 5271965
74
XDOT = 3379
205255 XDOT = 949
104453
YDOT = 24792
375293 feet/sec YDOT = 7567
781591 meter/sec
ZDOT = -2499
060470 ZDOT = -756
907627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13318005
45 X = 4059328
06
Y = 4298243
86 feet Y = 1310104
73 meter
Z = 17316026
46 Z = 5277924
87
XDOT = -4398
637681 XDOT = -1340
704765
YDOT = 23604
692512 feet/sec YDOT = 7194
710278 meter/sec
ZDOT = -2479
890579 ZDOT = -755
870648
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 14063
54704809
00016717 00000-0 10270-3 0 9086
2 25544 51
6451 258
2969 0003260 212
0369 148
0584 15
50912864 35097
Satellite: ISS
Catalog Number: 25544
Epoch time: 14063
54704809 = yrday
fracday
Element set: 908
Inclination: 51
6451 deg
RA of node: 258
2969 deg
Eccentricity:
0003260
Arg of perigee: 212
0369 deg
Mean anomaly: 148
0584 deg
Mean motion: 15
50912864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3509
Checksum: 317
Coasting Arc #10 (Orbit 3523)
---------------------------------------
Vector Time (GMT): 2014/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4435468
99 A = 6787295
20 meter
Y = -397950
21 meter E =
0012769
Z = -5133363
83 I = 51
28337
XDOT = -1065
869682 Wp = 114
85971
YDOT = -7430
347247 meter/sec RA = 252
65202 deg
ZDOT = 1494
651579 TA = 169
64772
MA = 169
62140
Ha = 225
614 n
mi
Hp = 220
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14552063
62 X = -4405753
26
Y = -1305610
92 feet Y = -447384
93 meter
Z = -16841744
86 Z = -5154838
38
XDOT = -3496
947775 XDOT = -989
963154
YDOT = -24377
779682 feet/sec YDOT = -7441
841888 meter/sec
ZDOT = 4903
712529 ZDOT = 1489
659019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13368641
19 X = -4074761
83
Y = -5629215
99 feet Y = -1715785
03 meter
Z = -16932303
61 Z = -5160966
14
XDOT = 3625
760607 XDOT = 1105
131833
YDOT = -23323
477945 feet/sec YDOT = -7108
996078 meter/sec
ZDOT = 4883
728636 ZDOT = 1488
560488
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 14064
51355474
00016717 00000-0 10270-3 0 9095
2 25544 51
6443 253
5003 0003227 214
6648 145
4293 15
50972783 35247
Satellite: ISS
Catalog Number: 25544
Epoch time: 14064
51355474 = yrday
fracday
Element set: 909
Inclination: 51
6443 deg
RA of node: 253
5003 deg
Eccentricity:
0003227
Arg of perigee: 214
6648 deg
Mean anomaly: 145
4293 deg
Mean motion: 15
50972783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3524
Checksum: 306
Coasting Arc #11 (Orbit 3539)
---------------------------------------
Vector Time (GMT): 2014/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4601817
74 A = 6788141
87 meter
Y = 831763
36 meter E =
0003477
Z = 4917800
41 I = 51
29667
XDOT = 1061
157325 Wp = 74
67228
YDOT = 7259
776812 meter/sec RA = 247
66224 deg
ZDOT = -2218
626062 TA = 37
11083
MA = 37
08680
Ha = 225
341 n
mi
Hp = 220
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15097827
23 X = 4568285
78
Y = 2728882
41 feet Y = 883036
85 meter
Z = 16134515
78 Z = 4940073
74
XDOT = 3481
487286 XDOT = 990
675320
YDOT = 23818
165395 feet/sec YDOT = 7271
249037 meter/sec
ZDOT = -7278
956895 ZDOT = -2213
643080
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13582024
49 X = 4139801
06
Y = 6919669
34 feet Y = 2109115
21 meter
Z = 16228387
87 Z = 4946412
62
XDOT = -2953
002982 XDOT = -900
075309
YDOT = 22837
323755 feet/sec YDOT = 6960
816281 meter/sec
ZDOT = -7258
980364 ZDOT = -2212
537215
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 14065
54447377
00016717 00000-0 10270-3 0 9105
2 25544 51
6445 248
3856 0003254 220
0437 140
0475 15
50982753 35403
Satellite: ISS
Catalog Number: 25544
Epoch time: 14065
54447377 = yrday
fracday
Element set: 910
Inclination: 51
6445 deg
RA of node: 248
3856 deg
Eccentricity:
0003254
Arg of perigee: 220
0437 deg
Mean anomaly: 140
0475 deg
Mean motion: 15
50982753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3540
Checksum: 302
Coasting Arc #12 (Orbit 3554)
---------------------------------------
Vector Time (GMT): 2014/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4815679
65 A = 6789166
67 meter
Y = -1239962
91 meter E =
0009743
Z = -4631782
64 I = 51
31318
XDOT = -997
326765 Wp = 127
50488
YDOT = -7008
965850 meter/sec RA = 242
67269 deg
ZDOT = 2911
689050 TA = 171
66593
MA = 171
64973
Ha = 225
370 n
mi
Hp = 220
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15799473
92 X = -4778956
63
Y = -4068119
79 feet Y = -1293610
02 meter
Z = -15196137
27 Z = -4655087
06
XDOT = -3272
069438 XDOT = -933
020767
YDOT = -22995
294785 feet/sec YDOT = -7019
758777 meter/sec
ZDOT = 9552
785598 ZDOT = 2907
001042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14017920
00 X = -4272662
02
Y = -8165633
82 feet Y = -2488885
19 meter
Z = -15294309
59 Z = -4661705
56
XDOT = 2417
044315 XDOT = 736
715107
YDOT = -22016
314913 feet/sec YDOT = -6710
572786 meter/sec
ZDOT = 9534
008882 ZDOT = 2905
965907
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 14066
51093922
00016717 00000-0 10270-3 0 9117
2 25544 51
6444 243
5892 0003183 221
6085 138
4824 15
51037988 35553
Satellite: ISS
Catalog Number: 25544
Epoch time: 14066
51093922 = yrday
fracday
Element set: 911
Inclination: 51
6444 deg
RA of node: 243
5892 deg
Eccentricity:
0003183
Arg of perigee: 221
6085 deg
Mean anomaly: 138
4824 deg
Mean motion: 15
51037988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3555
Checksum: 314
Coasting Arc #13 (Orbit 3570)
---------------------------------------
Vector Time (GMT): 2014/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5041977
00 A = 6790547
34 meter
Y = 1613880
20 meter E =
0007161
Z = 4246920
63 I = 51
33263
XDOT = 865
855664 Wp = 84
69543
YDOT = 6724
187316 meter/sec RA = 237
68653 deg
ZDOT = -3577
350492 TA = 42
03722
MA = 41
98229
Ha = 225
092 n
mi
Hp = 220
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16541919
30 X = 5002925
51
Y = 5294882
55 feet Y = 1670044
83 meter
Z = 13933466
63 Z = 4271318
63
XDOT = 2840
733805 XDOT = 807
977403
YDOT = 22060
982007 feet/sec YDOT = 6733
545945 meter/sec
ZDOT = -11736
714212 ZDOT = -3573
285484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14570591
41 X = 4441116
26
Y = 9300270
05 feet Y = 2834722
31 meter
Z = 14036210
68 Z = 4278237
02
XDOT = -2104
279055 XDOT = -641
384256
YDOT = 21014
509389 feet/sec YDOT = 6405
222462 meter/sec
ZDOT = -11720
516566 ZDOT = -3572
413449
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 14067
54181289
00016717 00000-0 10270-3 0 9126
2 25544 51
6440 238
4742 0003198 227
2291 132
8591 15
51052166 35715
Satellite: ISS
Catalog Number: 25544
Epoch time: 14067
54181289 = yrday
fracday
Element set: 912
Inclination: 51
6440 deg
RA of node: 238
4742 deg
Eccentricity:
0003198
Arg of perigee: 227
2291 deg
Mean anomaly: 132
8591 deg
Mean motion: 15
51052166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3571
Checksum: 305
Coasting Arc #14 (Orbit 3585)
---------------------------------------
Vector Time (GMT): 2014/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5292112
08 A = 6791935
68 meter
Y = -1937288
33 meter E =
0005066
Z = -3797051
62 I = 51
35581
XDOT = -661
722368 Wp = 134
64900
YDOT = -6382
072558 meter/sec RA = 232
70221 deg
ZDOT = 4178
419183 TA = 179
67349
MA = 179
67316
Ha = 225
111 n
mi
Hp = 220
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17362572
45 X = -5251610
92
Y = -6355932
83 feet Y = -1996241
99 meter
Z = -12457518
43 Z = -3822661
11
XDOT = -2171
005144 XDOT = -610
604606
YDOT = -20938
558262 feet/sec YDOT = -6389
186179 meter/sec
ZDOT = 13708
724355 ZDOT = 4175
329387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15282908
32 X = -4658230
46
Y = -10275770
92 feet Y = -3132054
98 meter
Z = -12565341
81 Z = -3829916
18
XDOT = 2025
287774 XDOT = 617
307713
YDOT = -19760
675009 feet/sec YDOT = -6023
053743 meter/sec
ZDOT = 13696
584410 ZDOT = 4174
718928
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 14068
50823528
00016717 00000-0 10270-3 0 9133
2 25544 51
6446 233
6781 0003109 229
0733 131
0149 15
51107455 35862
Satellite: ISS
Catalog Number: 25544
Epoch time: 14068
50823528 = yrday
fracday
Element set: 913
Inclination: 51
6446 deg
RA of node: 233
6781 deg
Eccentricity:
0003109
Arg of perigee: 229
0733 deg
Mean anomaly: 131
0149 deg
Mean motion: 15
51107455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3586
Checksum: 299
Coasting Arc #15 (Orbit 3601)
---------------------------------------
Vector Time (GMT): 2014/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5529440
94 A = 6793510
52 meter
Y = 2218952
20 meter E =
0010350
Z = 3252554
26 I = 51
37997
XDOT = 370
674743 Wp = 103
13049
YDOT = 6022
638277 meter/sec RA = 227
72114 deg
ZDOT = -4728
490532 TA = 39
04227
MA = 38
96760
Ha = 224
867 n
mi
Hp = 220
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18141210
43 X = 5488417
50
Y = 7280026
90 feet Y = 2280556
88 meter
Z = 10671109
78 Z = 3279315
29
XDOT = 1216
124486 XDOT = 326
269882
YDOT = 19759
311931 feet/sec YDOT = 6026
534667 meter/sec
ZDOT = -15513
420381 ZDOT = -4726
798299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16024048
68 X = 4884130
04
Y = 11086708
77 feet Y = 3379228
83 meter
Z = 10783767
62 Z = 3286892
37
XDOT = -2266
982166 XDOT = -690
976164
YDOT = 18392
860315 feet/sec YDOT = 5606
143824 meter/sec
ZDOT = -15507
119457 ZDOT = -4726
570011
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 14069
53906218
00016717 00000-0 10270-3 0 9146
2 25544 51
6438 228
5624 0003126 234
7373 125
3486 15
51124313 36025
Satellite: ISS
Catalog Number: 25544
Epoch time: 14069
53906218 = yrday
fracday
Element set: 914
Inclination: 51
6438 deg
RA of node: 228
5624 deg
Eccentricity:
0003126
Arg of perigee: 234
7373 deg
Mean anomaly: 125
3486 deg
Mean motion: 15
51124313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3602
Checksum: 295
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