[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 4th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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
093/19:42:19
675 -0
8 1
9 1
9
N/A 1
7 -0
2 228
2
000/00:04:35
351 0
2 -0
1 214
4
Coasting Arc #1 (Orbit 2310)
---------------------------------------
Vector Time (GMT): 2013/093/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3149745
96 A = 6782946
08 meter
Y = 2892200
05 meter E =
0026405
Z = -5288281
94 I = 51
93683
XDOT = -4210
622580 Wp = 98
75536
YDOT = 6311
500538 meter/sec RA = 118
11719 deg
ZDOT = 944
044134 TA = 180
26672
MA = 180
26814
Ha = 228
236 n
mi
Hp = 213
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10333812
21 X = 3142859
64
Y = 9488845
31 feet Y = 2927383
66 meter
Z = -17350006
38 Z = -5272997
71
XDOT = -13814
378542 XDOT = -4285
472083
YDOT = 20707
022761 feet/sec YDOT = 6263
996256 meter/sec
ZDOT = 3097
257657 ZDOT = 923
407173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12080702
55 X = 3682198
14
Y = 7285528
23 feet Y = 2220629
01 meter
Z = -17286592
66 Z = -5268953
44
XDOT = -9028
890216 XDOT = -2752
005738
YDOT = 22113
650407 feet/sec YDOT = 6740
240644 meter/sec
ZDOT = 3010
494108 ZDOT = 917
598604
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 13093
51456316
00016717 00000-0 10270-3 0 9004
2 25544 51
6462 118
9972 0011995 100
3394 259
9111 15
52309453 23110
Satellite: ISS
Catalog Number: 25544
Epoch time: 13093
51456316 = yrday
fracday
Element set: 900
Inclination: 51
6462 deg
RA of node: 118
9972 deg
Eccentricity:
0011995
Arg of perigee: 100
3394 deg
Mean anomaly: 259
9111 deg
Mean motion: 15
52309453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2311
Checksum: 298
Coasting Arc #2 (Orbit 2315)
---------------------------------------
Vector Time (GMT): 2013/093/19:44:37
351
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2951692
88 A = 6784241
00 meter
Y = 3222041
63 meter E =
0024257
Z = -5211072
74 I = 51
94304
XDOT = -4293
296135 Wp = 101
09299
YDOT = 6173
761489 meter/sec RA = 116
51634 deg
ZDOT = 1386
376741 TA = 182
21409
MA = 182
22484
Ha = 228
155 n
mi
Hp = 214
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9684031
76 X = 2940757
83
Y = 10571002
71 feet Y = 3254987
82 meter
Z = -17096695
35 Z = -5196760
52
XDOT = -14085
617241 XDOT = -4368
747987
YDOT = 20255
122995 feet/sec YDOT = 6125
329366 meter/sec
ZDOT = 4548
480121 ZDOT = 1365
336691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2390849
78 X = 728731
01
Y = -14206877
90 feet Y = -4330256
38 meter
Z = -17037371
25 Z = -5192990
76
XDOT = 23622
541442 XDOT = 7200
150631
YDOT = -1369
543565 feet/sec YDOT = -417
436879 meter/sec
ZDOT = 4460
046606 ZDOT = 1359
422205
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 13093
83644675
00016717 00000-0 10270-3 0 9017
2 25544 51
6466 117
3969 0010364 101
6177 258
6138 15
51979172 23165
Satellite: ISS
Catalog Number: 25544
Epoch time: 13093
83644675 = yrday
fracday
Element set: 901
Inclination: 51
6466 deg
RA of node: 117
3969 deg
Eccentricity:
0010364
Arg of perigee: 101
6177 deg
Mean anomaly: 258
6138 deg
Mean motion: 15
51979172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2316
Checksum: 326
Coasting Arc #3 (Orbit 2331)
---------------------------------------
Vector Time (GMT): 2013/094/19:44:37
351
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2520245
97 A = 6785449
09 meter
Y = -3983925
27 meter E =
0016014
Z = 4867030
77 I = 51
96015
XDOT = 4374
496949 Wp = 86
94562
YDOT = -5800
715925 meter/sec RA = 111
56182 deg
ZDOT = -2475
166249 TA = 27
26721
MA = 27
18323
Ha = 228
129 n
mi
Hp = 214
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8268523
52 X = -2499152
16
Y = -13070620
97 feet Y = -4011989
89 meter
Z = 15967948
71 Z = 4854839
28
XDOT = 14352
024112 XDOT = 4451
060303
YDOT = -19031
220226 feet/sec YDOT = -5751
369668 meter/sec
ZDOT = -8120
624178 ZDOT = -2453
728976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4986896
09 X = -1520005
93
Y = 14695146
83 feet Y = 4479080
75 meter
Z = 15917554
04 Z = 4851670
47
XDOT = -22786
863512 XDOT = -6945
435998
YDOT = 993
615315 feet/sec YDOT = 302
853948 meter/sec
ZDOT = -8030
564007 ZDOT = -2447
715909
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 13094
86669931
00016717 00000-0 10270-3 0 9024
2 25544 51
6463 112
2777 0010274 105
0346 255
1943 15
52027519 23323
Satellite: ISS
Catalog Number: 25544
Epoch time: 13094
86669931 = yrday
fracday
Element set: 902
Inclination: 51
6463 deg
RA of node: 112
2777 deg
Eccentricity:
0010274
Arg of perigee: 105
0346 deg
Mean anomaly: 255
1943 deg
Mean motion: 15
52027519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2332
Checksum: 301
Coasting Arc #4 (Orbit 2346)
---------------------------------------
Vector Time (GMT): 2013/095/19:44:37
351
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2175853
98 A = 6787397
60 meter
Y = 4714828
29 meter E =
0019076
Z = -4390268
24 I = 51
97742
XDOT = -4380
340352 Wp = 109
61596
YDOT = 5233
156703 meter/sec RA = 106
61028 deg
ZDOT = 3455
085990 TA = 195
34128
MA = 195
39919
Ha = 228
028 n
mi
Hp = 214
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7138628
55 X = 2144296
70
Y = 15468596
77 feet Y = 4738983
16 meter
Z = -14403767
18 Z = -4379775
32
XDOT = -14371
195381 XDOT = -4455
316883
YDOT = 17169
149288 feet/sec YDOT = 5183
754121 meter/sec
ZDOT = 11335
583956 ZDOT = 3433
624114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7307341
87 X = 2227277
80
Y = -15429958
42 feet Y = -4703051
33 meter
Z = -14360541
43 Z = -4377093
03
XDOT = 21309
498939 XDOT = 6495
135277
YDOT = -355
946213 feet/sec YDOT = -108
492406 meter/sec
ZDOT = 11245
475700 ZDOT = 3427
620993
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 13095
83254991
00016717 00000-0 10270-3 0 9039
2 25544 51
6468 107
4782 0010276 108
6303 251
5965 15
52018601 23476
Satellite: ISS
Catalog Number: 25544
Epoch time: 13095
83254991 = yrday
fracday
Element set: 903
Inclination: 51
6468 deg
RA of node: 107
4782 deg
Eccentricity:
0010276
Arg of perigee: 108
6303 deg
Mean anomaly: 251
5965 deg
Mean motion: 15
52018601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2347
Checksum: 309
Coasting Arc #5 (Orbit 2362)
---------------------------------------
Vector Time (GMT): 2013/096/19:44:37
351
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1845316
74 A = 6789617
49 meter
Y = -5370030
28 meter E =
0021461
Z = 3701568
54 I = 51
99254
XDOT = 4408
938887 Wp = 97
62019
YDOT = -4528
984915 meter/sec RA = 101
66257 deg
ZDOT = -4353
695792 TA = 38
50540
MA = 38
35248
Ha = 228
035 n
mi
Hp = 214
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6054188
79 X = -1803111
97
Y = -17618209
56 feet Y = -5390429
35 meter
Z = 12144253
74 Z = 3692707
31
XDOT = 14465
022594 XDOT = 4480
404342
YDOT = -14858
874392 feet/sec YDOT = -4479
282308 meter/sec
ZDOT = -14283
778844 ZDOT = -4332
103467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9387895
57 X = -2861430
57
Y = 16118413
91 feet Y = 4912892
56 meter
Z = 12107913
07 Z = 3690491
90
XDOT = -19577
936397 XDOT = -5967
355014
YDOT = -694
773908 feet/sec YDOT = -211
767087 meter/sec
ZDOT = -14193
198894 ZDOT = -4326
087023
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 13096
86277684
00016717 00000-0 10270-3 0 9048
2 25544 51
6464 102
3585 0010320 112
0846 248
1402 15
52045940 23630
Satellite: ISS
Catalog Number: 25544
Epoch time: 13096
86277684 = yrday
fracday
Element set: 904
Inclination: 51
6464 deg
RA of node: 102
3585 deg
Eccentricity:
0010320
Arg of perigee: 112
0846 deg
Mean anomaly: 248
1402 deg
Mean motion: 15
52045940 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2363
Checksum: 292
Coasting Arc #6 (Orbit 2377)
---------------------------------------
Vector Time (GMT): 2013/097/19:44:37
351
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1603564
47 A = 6791749
11 meter
Y = 5923033
51 meter E =
0013555
Z = -2925848
35 I = 52
00523
XDOT = -4410
519148 Wp = 100
67764
YDOT = 3682
973174 meter/sec RA = 96
71847 deg
ZDOT = 5055
898526 TA = 226
22007
MA = 226
33230
Ha = 227
873 n
mi
Hp = 214
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5261038
29 X = 1551425
69
Y = 19432524
65 feet Y = 5940673
70 meter
Z = -9599239
98 Z = -2918185
72
XDOT = -14470
207178 XDOT = -4475
935410
YDOT = 12083
245323 feet/sec YDOT = 3633
286829 meter/sec
ZDOT = 16587
593588 ZDOT = 5034
313209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11003289
68 X = 3353802
70
Y = -16876863
15 feet Y = -5144067
89 meter
Z = -9567970
15 Z = -2916317
30
XDOT = 17480
194832 XDOT = 5327
963385
YDOT = 2076
464465 feet/sec YDOT = 632
906369 meter/sec
ZDOT = 16497
133805 ZDOT = 5028
326384
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 13097
82860107
00016717 00000-0 10270-3 0 9054
2 25544 51
6466 97
5584 0010173 115
8095 244
4107 15
52060826 23786
Satellite: ISS
Catalog Number: 25544
Epoch time: 13097
82860107 = yrday
fracday
Element set: 905
Inclination: 51
6466 deg
RA of node: 97
5584 deg
Eccentricity:
0010173
Arg of perigee: 115
8095 deg
Mean anomaly: 244
4107 deg
Mean motion: 15
52060826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2378
Checksum: 314
Coasting Arc #7 (Orbit 2393)
---------------------------------------
Vector Time (GMT): 2013/098/19:44:37
351
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1346399
05 A = 6793724
90 meter
Y = -6346293
70 meter E =
0024202
Z = 1975562
08 I = 52
01419
XDOT = 4471
658791 Wp = 115
35620
YDOT = -2710
383843 meter/sec RA = 91
77830 deg
ZDOT = -5615
916453 TA = 42
95255
MA = 42
76383
Ha = 227
920 n
mi
Hp = 214
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4417319
71 X = -1284930
18
Y = -20821173
56 feet Y = -6361006
05 meter
Z = 6481502
88 Z = 1969171
42
XDOT = 14670
796558 XDOT = 4528
915347
YDOT = -8892
335442 feet/sec YDOT = -2660
059478 meter/sec
ZDOT = -18424
922745 ZDOT = -5594
053975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12317958
77 X = -3754513
83
Y = 17367699
93 feet Y = 5293674
94 meter
Z = 6455598
51 Z = 1967666
43
XDOT = -15284
693060 XDOT = -4658
774445
YDOT = -3972
948627 feet/sec YDOT = -1210
954741 meter/sec
ZDOT = -18333
415287 ZDOT = -5588
024979
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 13098
85880157
00016717 00000-0 10270-3 0 9066
2 25544 51
6464 92
4384 0010323 119
8049 240
4131 15
52057629 23944
Satellite: ISS
Catalog Number: 25544
Epoch time: 13098
85880157 = yrday
fracday
Element set: 906
Inclination: 51
6464 deg
RA of node: 92
4384 deg
Eccentricity:
0010323
Arg of perigee: 119
8049 deg
Mean anomaly: 240
4131 deg
Mean motion: 15
52057629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2394
Checksum: 314
Coasting Arc #8 (Orbit 2408)
---------------------------------------
Vector Time (GMT): 2013/099/19:44:37
351
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1154411
60 A = 6794767
78 meter
Y = 6620024
65 meter E =
0014673
Z = -1008907
39 I = 52
01811
XDOT = -4544
185204 Wp = 81
94114
YDOT = 1684
673720 meter/sec RA = 86
84000 deg
ZDOT = 5930
175471 TA = 267
20131
MA = 267
36926
Ha = 227
697 n
mi
Hp = 214
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3787439
62 X = 1085200
32
Y = 21719240
97 feet Y = 6632546
91 meter
Z = -3310063
60 Z = -1003468
16
XDOT = -14908
744106 XDOT = -4591
493364
YDOT = 5527
144752 feet/sec YDOT = 1633
593936 meter/sec
ZDOT = 19455
956269 ZDOT = 5907
984882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13115884
25 X = 3997721
52
Y = -17725353
17 feet Y = -5402687
65 meter
Z = -3288173
26 Z = -1002235
21
XDOT = 13069
607625 XDOT = 3983
616404
YDOT = 6125
177938 feet/sec YDOT = 1866
954236 meter/sec
ZDOT = 19363
198243 ZDOT = 5901
902824
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 13099
82459929
00016717 00000-0 10270-3 0 9074
2 25544 51
6463 87
6380 0010101 123
2892 236
9228 15
52110403 24098
Satellite: ISS
Catalog Number: 25544
Epoch time: 13099
82459929 = yrday
fracday
Element set: 907
Inclination: 51
6463 deg
RA of node: 87
6380 deg
Eccentricity:
0010101
Arg of perigee: 123
2892 deg
Mean anomaly: 236
9228 deg
Mean motion: 15
52110403 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2409
Checksum: 306
Coasting Arc #9 (Orbit 2424)
---------------------------------------
Vector Time (GMT): 2013/100/19:44:37
351
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -900266
74 A = 6795288
58 meter
Y = -6725068
37 meter E =
0022102
Z = -71484
17 I = 52
01691
XDOT = 4685
603660 Wp = 131
66824
YDOT = -575
903023 meter/sec RA = 81
90396 deg
ZDOT = -6045
013814 TA = 49
09760
MA = 48
90637
Ha = 227
731 n
mi
Hp = 214
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2953631
03 X = -824651
42
Y = -22063872
60 feet Y = -6734712
94 meter
Z = -234528
12 Z = -75673
31
XDOT = 15372
715419 XDOT = 4721
060739
YDOT = -1889
445612 feet/sec YDOT = -523
308003 meter/sec
ZDOT = -19832
722488 ZDOT = -6022
165076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13655044
94 X = -4162057
70
Y = 17580388
84 feet Y = 5358502
52 meter
Z = -251176
91 Z = -76558
72
XDOT = -10934
233888 XDOT = -3332
754489
YDOT = -8721
680408 feet/sec YDOT = -2658
368188 meter/sec
ZDOT = -19737
351378 ZDOT = -6015
944700
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 13100
85477204
00016717 00000-0 10270-3 0 9087
2 25544 51
6464 82
5180 0010199 127
9306 232
2769 15
52081366 24251
Satellite: ISS
Catalog Number: 25544
Epoch time: 13100
85477204 = yrday
fracday
Element set: 908
Inclination: 51
6464 deg
RA of node: 82
5180 deg
Eccentricity:
0010199
Arg of perigee: 127
9306 deg
Mean anomaly: 232
2769 deg
Mean motion: 15
52081366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2425
Checksum: 302
Coasting Arc #10 (Orbit 2440)
---------------------------------------
Vector Time (GMT): 2013/101/19:44:37
351
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 673509
90 A = 6794539
20 meter
Y = 6670049
75 meter E =
0018958
Z = 1085884
24 I = 52
00962
XDOT = -4851
660205 Wp = 87
43822
YDOT = -486
804951 meter/sec RA = 76
96635 deg
ZDOT = 5911
387795 TA = 284
26719
MA = 284
47766
Ha = 227
485 n
mi
Hp = 214
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2209678
14 X = 593598
90
Y = 21883365
32 feet Y = 6677134
64 meter
Z = 3562612
34 Z = 1088961
49
XDOT = -15917
520356 XDOT = -4874
572427
YDOT = -1597
129105 feet/sec YDOT = -541
186893 meter/sec
ZDOT = 19394
316912 ZDOT = 5887
762891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13769847
68 X = 4197049
57
Y = -17148468
88 feet Y = -5226853
31 meter
Z = 3574614
90 Z = 1089542
62
XDOT = 9075
309238 XDOT = 2766
154256
YDOT = 11369
501583 feet/sec YDOT = 3465
424083 meter/sec
ZDOT = 19295
839275 ZDOT = 5881
371811
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 13101
88492725
00016717 00000-0 10270-3 0 9097
2 25544 51
6460 77
3973 0010035 131
5446 228
6568 15
52166112 24411
Satellite: ISS
Catalog Number: 25544
Epoch time: 13101
88492725 = yrday
fracday
Element set: 909
Inclination: 51
6460 deg
RA of node: 77
3973 deg
Eccentricity:
0010035
Arg of perigee: 131
5446 deg
Mean anomaly: 228
6568 deg
Mean motion: 15
52166112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2441
Checksum: 302
Coasting Arc #11 (Orbit 2455)
---------------------------------------
Vector Time (GMT): 2013/102/19:44:37
351
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -335163
02 A = 6793177
58 meter
Y = -6436175
43 meter E =
0016338
Z = -2133549
43 I = 51
99672
XDOT = 5059
272252 Wp = 136
27065
YDOT = 1561
580143 meter/sec RA = 72
02780 deg
ZDOT = -5542
233122 TA = 67
23468
MA = 67
06213
Ha = 227
464 n
mi
Hp = 214
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1099616
20 X = -252803
05
Y = -21116061
13 feet Y = -6439463
07 meter
Z = -6999834
08 Z = -2134977
18
XDOT = 16598
662245 XDOT = 5068
357398
YDOT = 5123
294434 feet/sec YDOT = 1618
206555 meter/sec
ZDOT = -18183
179535 ZDOT = -5517
633286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13765714
43 X = -4195789
76
Y = 16047752
36 feet Y = 4891354
92 meter
Z = -7004971
17 Z = -2135115
21
XDOT = -7428
929262 XDOT = -2264
337639
YDOT = -14212
365566 feet/sec YDOT = -4331
929025 meter/sec
ZDOT = -18080
772166 ZDOT = -5511
019356
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 13102
85068775
00016717 00000-0 10270-3 0 9101
2 25544 51
6457 72
5972 0010012 135
3697 224
8262 15
52141522 24561
Satellite: ISS
Catalog Number: 25544
Epoch time: 13102
85068775 = yrday
fracday
Element set: 910
Inclination: 51
6457 deg
RA of node: 72
5972 deg
Eccentricity:
0010012
Arg of perigee: 135
3697 deg
Mean anomaly: 224
8262 deg
Mean motion: 15
52141522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2456
Checksum: 296
Coasting Arc #12 (Orbit 2471)
---------------------------------------
Vector Time (GMT): 2013/103/19:44:37
351
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -11220
02 A = 6791056
90 meter
Y = 6069887
99 meter E =
0020431
Z = 3036058
62 I = 51
97957
XDOT = -5274
902508 Wp = 107
05681
YDOT = -2509
550309 meter/sec RA = 67
08464 deg
ZDOT = 4964
401234 TA = 287
54337
MA = 287
76650
Ha = 227
285 n
mi
Hp = 214
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -36811
09 X = -93842
54
Y = 19914330
68 feet Y = 6069300
70 meter
Z = 9960822
23 Z = 3035803
13
XDOT = -17306
110589 XDOT = -5270
564198
YDOT = -8233
432772 feet/sec YDOT = -2568
513095 meter/sec
ZDOT = 16287
405623 ZDOT = 4938
786525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13527185
90 X = 4123086
26
Y = -14616224
57 feet Y = -4455025
25 meter
Z = 9958971
93 Z = 3035494
64
XDOT = 6205
409310 XDOT = 1891
408758
YDOT = 16842
724565 feet/sec YDOT = 5133
662447 meter/sec
ZDOT = 16180
889596 ZDOT = 4931
935149
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 13103
88081599
00016717 00000-0 10270-3 0 9115
2 25544 51
6455 67
4764 0009936 139
2725 220
9172 15
52197367 24722
Satellite: ISS
Catalog Number: 25544
Epoch time: 13103
88081599 = yrday
fracday
Element set: 911
Inclination: 51
6455 deg
RA of node: 67
4764 deg
Eccentricity:
0009936
Arg of perigee: 139
2725 deg
Mean anomaly: 220
9172 deg
Mean motion: 15
52197367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2472
Checksum: 331
Coasting Arc #13 (Orbit 2486)
---------------------------------------
Vector Time (GMT): 2013/104/19:44:37
351
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 502384
55 A = 6788563
94 meter
Y = -5549908
30 meter E =
0013759
Z = -3882460
52 I = 51
95774
XDOT = 5469
134291 Wp = 116
75856
YDOT = 3389
436052 meter/sec RA = 62
13720 deg
ZDOT = -4154
795402 TA = 109
78093
MA = 109
63252
Ha = 227
253 n
mi
Hp = 214
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1648243
26 X = 583267
65
Y = -18208360
55 feet Y = -5543838
22 meter
Z = -12737731
36 Z = -3879823
28
XDOT = 17943
353972 XDOT = 5451
009532
YDOT = 11120
197022 feet/sec YDOT = 3450
493859 meter/sec
ZDOT = -13631
218511 ZDOT = -4128
270665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13362552
54 X = -4072906
01
Y = 12490073
72 feet Y = 3806974
47 meter
Z = -12726002
84 Z = -3878885
66
XDOT = -5217
389202 XDOT = -1590
260229
YDOT = -19300
205407 feet/sec YDOT = -5882
702608 meter/sec
ZDOT = -13521
025272 ZDOT = -4121
208503
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 13104
84654916
00016717 00000-0 10270-3 0 9122
2 25544 51
6447 62
6759 0010009 142
4035 217
7818 15
52204785 24877
Satellite: ISS
Catalog Number: 25544
Epoch time: 13104
84654916 = yrday
fracday
Element set: 912
Inclination: 51
6447 deg
RA of node: 62
6759 deg
Eccentricity:
0010009
Arg of perigee: 142
4035 deg
Mean anomaly: 217
7818 deg
Mean motion: 15
52204785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2487
Checksum: 313
Coasting Arc #14 (Orbit 2502)
---------------------------------------
Vector Time (GMT): 2013/105/19:44:37
351
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1018459
85 A = 6786297
85 meter
Y = 4952825
80 meter E =
0018029
Z = 4520467
58 I = 51
93500
XDOT = -5631
120506 Wp = 129
87460
YDOT = -4101
206791 meter/sec RA = 57
18457 deg
ZDOT = 3205
054772 TA = 287
96250
MA = 288
15895
Ha = 227
171 n
mi
Hp = 215
121
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3341403
71 X = -1095727
15
Y = 16249428
47 feet Y = 4941004
86 meter
Z = 14830930
37 Z = 4515332
10
XDOT = -18474
804809 XDOT = -5600
410859
YDOT = -13455
402856 feet/sec YDOT = -4164
005713 meter/sec
ZDOT = 10515
271562 ZDOT = 3177
773751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13169534
41 X = 4014074
09
Y = -10120607
37 feet Y = -3084761
12 meter
Z = 14808851
07 Z = 4513737
81
XDOT = 4609
663290 XDOT = 1405
025371
YDOT = 21313
808245 feet/sec YDOT = 6496
448753 meter/sec
ZDOT = 10402
022425 ZDOT = 3170
536435
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 13105
87665029
00016717 00000-0 10270-3 0 9134
2 25544 51
6447 57
5552 0009956 146
2553 213
9234 15
52206018 25037
Satellite: ISS
Catalog Number: 25544
Epoch time: 13105
87665029 = yrday
fracday
Element set: 913
Inclination: 51
6447 deg
RA of node: 57
5552 deg
Eccentricity:
0009956
Arg of perigee: 146
2553 deg
Mean anomaly: 213
9234 deg
Mean motion: 15
52206018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2503
Checksum: 305
Coasting Arc #15 (Orbit 2517)
---------------------------------------
Vector Time (GMT): 2013/106/19:44:37
351
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1679146
11 A = 6784208
58 meter
Y = -4257940
13 meter E =
0018207
Z = -5020886
91 I = 51
91021
XDOT = 5688
249525 Wp = 107
12111
YDOT = 4680
605913 meter/sec RA = 52
22633 deg
ZDOT = -2078
460918 TA = 142
75872
MA = 142
63233
Ha = 227
092 n
mi
Hp = 215
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5509009
55 X = 1751024
81
Y = -13969619
85 feet Y = -4238761
13 meter
Z = -16472726
07 Z = -5012554
96
XDOT = 18662
235973 XDOT = 5645
583901
YDOT = 15356
318611 feet/sec YDOT = 4743
976874 meter/sec
ZDOT = -6819
097499 ZDOT = -2050
931492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13221369
00 X = -4029873
27
Y = 7201212
29 feet Y = 2194929
50 meter
Z = -16437399
80 Z = -5010119
46
XDOT = -4121
407461 XDOT = -1256
204994
YDOT = -22785
615734 feet/sec YDOT = -6945
055676 meter/sec
ZDOT = -6704
894722 ZDOT = -2043
651911
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 13106
84235522
00016717 00000-0 10270-3 0 9144
2 25544 51
6440 52
7541 0010134 149
7909 210
3829 15
52248718 25188
Satellite: ISS
Catalog Number: 25544
Epoch time: 13106
84235522 = yrday
fracday
Element set: 914
Inclination: 51
6440 deg
RA of node: 52
7541 deg
Eccentricity:
0010134
Arg of perigee: 149
7909 deg
Mean anomaly: 210
3829 deg
Mean motion: 15
52248718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2518
Checksum: 296
Coasting Arc #16 (Orbit 2533)
---------------------------------------
Vector Time (GMT): 2013/107/19:44:37
351
Vector Time (MET): N/A
Weight (LBS) : 904028
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2352507
19 A = 6783133
02 meter
Y = 3550578
67 meter E =
0013063
Z = 5274097
68 I = 51
88685
XDOT = -5662
544072 Wp = 144
84443
YDOT = -5096
053256 meter/sec RA = 47
26467 deg
ZDOT = 893
432140 TA = 296
57505
MA = 296
70887
Ha = 227
096 n
mi
Hp = 215
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7718199
43 X = -2417655
97
Y = 11648880
15 feet Y = 3523907
39 meter
Z = 17303470
07 Z = 5262510
96
XDOT = -18577
900498 XDOT = -5609
478135
YDOT = -16719
334828 feet/sec YDOT = -5159
078648 meter/sec
ZDOT = 2931
207807 ZDOT = 866
052942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13380520
71 X = 4078382
71
Y = -4232672
77 feet Y = -1290118
66 meter
Z = 17254658
34 Z = 5259219
86
XDOT = 3811
239387 XDOT = 1161
665765
YDOT = 23689
102759 feet/sec YDOT = 7220
438521 meter/sec
ZDOT = 2817
693156 ZDOT = 858
832874
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 13107
87242781
00016717 00000-0 10270-3 0 9154
2 25544 51
6440 47
6333 0010134 153
3602 206
8073 15
52227066 25343
Satellite: ISS
Catalog Number: 25544
Epoch time: 13107
87242781 = yrday
fracday
Element set: 915
Inclination: 51
6440 deg
RA of node: 47
6333 deg
Eccentricity:
0010134
Arg of perigee: 153
3602 deg
Mean anomaly: 206
8073 deg
Mean motion: 15
52227066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2534
Checksum: 281
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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