[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 3rd 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 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 2040)
---------------------------------------
Vector Time (GMT): 2012/184/13:22:35
791
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3397654
62 A = 6772428
00 meter
Y = 2484042
41 meter E =
0009630
Z = 5297457
41 I = 51
86828
XDOT = -5087
529134 Wp = 98
12070
YDOT = -5722
799797 meter/sec RA = 44
95462 deg
ZDOT = -579
951584 TA = 357
38637
MA = 357
39140
Ha = 221
028 n
mi
Hp = 209
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11147160
82 X = -3450912
84
Y = 8149745
45 feet Y = 2445748
97 meter
Z = 17380109
61 Z = 5280822
96
XDOT = -16691
368551 XDOT = -5020
340243
YDOT = -18775
589884 feet/sec YDOT = -5779
315918 meter/sec
ZDOT = -1902
728295 ZDOT = -604
504268
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12766306
38 X = 3891170
18
Y = 5485325
20 feet Y = 1671927
12 meter
Z = 17311221
33 Z = 5276460
26
XDOT = -7173
931152 XDOT = -2186
614215
YDOT = 23014
154171 feet/sec YDOT = 7014
714191 meter/sec
ZDOT = -2003
327853 ZDOT = -610
614329
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 12184
60452621
00016717 00000-0 10270-3 0 9009
2 25544 51
6385 45
3312 0007364 111
0233 249
1709 15
55859266 20410
Satellite: ISS
Catalog Number: 25544
Epoch time: 12184
60452621 = yrday
fracday
Element set: 900
Inclination: 51
6385 deg
RA of node: 45
3312 deg
Eccentricity:
0007364
Arg of perigee: 111
0233 deg
Mean anomaly: 249
1709 deg
Mean motion: 15
55859266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2041
Checksum: 283
Coasting Arc #2 (Orbit 2055)
---------------------------------------
Vector Time (GMT): 2012/185/13:22:35
791
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4951065
57 A = 6775341
19 meter
Y = -572295
32 meter E =
0017391
Z = -4606807
72 I = 51
85460
XDOT = 3530
617404 Wp = 111
74441
YDOT = 6075
016258 meter/sec RA = 39
95333 deg
ZDOT = 3042
700892 TA = 188
59075
MA = 188
62056
Ha = 220
843 n
mi
Hp = 209
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16243653
45 X = 4979475
67
Y = -1877609
30 feet Y = -516769
77 meter
Z = -15114198
56 Z = -4582687
06
XDOT = 11583
390434 XDOT = 3447
642359
YDOT = 19931
155701 feet/sec YDOT = 6114
033330 meter/sec
ZDOT = 9982
614476 ZDOT = 3059
651796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10208543
55 X = -3111564
07
Y = -12890561
49 feet Y = -3929043
14 meter
Z = -15014651
35 Z = -4576465
73
XDOT = 9922
208803 XDOT = 3024
289243
YDOT = -19554
643295 feet/sec YDOT = -5960
255276 meter/sec
ZDOT = 10051
821274 ZDOT = 3063
795124
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 12185
56796879
00016717 00000-0 10270-3 0 9012
2 25544 51
6372 40
5136 0007387 114
7097 245
4826 15
55891160 20564
Satellite: ISS
Catalog Number: 25544
Epoch time: 12185
56796879 = yrday
fracday
Element set: 901
Inclination: 51
6372 deg
RA of node: 40
5136 deg
Eccentricity:
0007387
Arg of perigee: 114
7097 deg
Mean anomaly: 245
4826 deg
Mean motion: 15
55891160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2056
Checksum: 330
Coasting Arc #3 (Orbit 2071)
---------------------------------------
Vector Time (GMT): 2012/186/13:22:35
791
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5928694
73 A = 6780297
06 meter
Y = -1251601
67 meter E =
0020007
Z = 3019661
73 I = 51
84794
XDOT = -1339
032647 Wp = 104
09385
YDOT = -5699
529272 meter/sec RA = 34
96756 deg
ZDOT = -4968
650638 TA = 41
35116
MA = 41
19987
Ha = 220
743 n
mi
Hp = 209
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19451098
21 X = -5928927
02
Y = -4106304
70 feet Y = -1317901
79 meter
Z = 9907026
66 Z = 2990860
11
XDOT = -4393
151730 XDOT = -1251
063651
YDOT = -18699
243020 feet/sec YDOT = -5714
010508 meter/sec
ZDOT = -16301
347237 ZDOT = -4974
942730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7119112
49 X = 2169905
49
Y = 18624230
32 feet Y = 5676665
40 meter
Z = 9788381
85 Z = 2983498
79
XDOT = -12034
294250 XDOT = -3668
052887
YDOT = 13220
593503 feet/sec YDOT = 4029
636900 meter/sec
ZDOT = -16326
636289 ZDOT = -4976
358741
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 12186
59562934
00016717 00000-0 10270-3 0 9020
2 25544 51
6376 35
3761 0007141 118
2210 241
9665 15
55935654 20725
Satellite: ISS
Catalog Number: 25544
Epoch time: 12186
59562934 = yrday
fracday
Element set: 902
Inclination: 51
6376 deg
RA of node: 35
3761 deg
Eccentricity:
0007141
Arg of perigee: 118
2210 deg
Mean anomaly: 241
9665 deg
Mean motion: 15
55935654 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2072
Checksum: 309
Coasting Arc #4 (Orbit 2086)
---------------------------------------
Vector Time (GMT): 2012/187/13:22:35
791
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6146155
08 A = 6783801
66 meter
Y = 2719411
43 meter E =
0013193
Z = -912872
86 I = 51
83302
XDOT = -1205
998402 Wp = 72
54686
YDOT = 4694
677251 meter/sec RA = 29
99580 deg
ZDOT = 5940
032030 TA = 277
59624
MA = 277
74607
Ha = 220
748 n
mi
Hp = 209
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20164550
79 X = 6119723
71
Y = 8921953
53 feet Y = 2787993
89 meter
Z = -2994989
69 Z = -883079
50
XDOT = -3956
687670 XDOT = -1287
260402
YDOT = 15402
484419 feet/sec YDOT = 4680
735856 meter/sec
ZDOT = 19488
294063 ZDOT = 5933
976716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3809057
26 X = -1161000
65
Y = -21735238
44 feet Y = -6624900
68 meter
Z = -2872423
87 Z = -875514
80
XDOT = 13483
621466 XDOT = 4109
807823
YDOT = -4901
414014 feet/sec YDOT = -1493
950992 meter/sec
ZDOT = 19462
773472 ZDOT = 5932
253354
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 12187
55905409
00016717 00000-0 10270-3 0 9036
2 25544 51
6366 30
5587 0007378 122
3834 237
8035 15
55917192 20875
Satellite: ISS
Catalog Number: 25544
Epoch time: 12187
55905409 = yrday
fracday
Element set: 903
Inclination: 51
6366 deg
RA of node: 30
5587 deg
Eccentricity:
0007378
Arg of perigee: 122
3834 deg
Mean anomaly: 237
8035 deg
Mean motion: 15
55917192 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2087
Checksum: 325
Coasting Arc #5 (Orbit 2102)
---------------------------------------
Vector Time (GMT): 2012/188/13:22:35
791
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5443322
21 A = 6783095
84 meter
Y = -3779140
96 meter E =
0015552
Z = -1425130
79 I = 51
80461
XDOT = 3784
933308 Wp = 133
69571
YDOT = -3278
991524 meter/sec RA = 25
02926 deg
ZDOT = -5811
446831 TA = 61
82174
MA = 61
66474
Ha = 220
581 n
mi
Hp = 209
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17858668
66 X = -5393735
68
Y = -12398756
43 feet Y = -3839734
15 meter
Z = -4675625
94 Z = -1451453
70
XDOT = 12417
760196 XDOT = 3849
548535
YDOT = -10757
846206 feet/sec YDOT = -3236
304114 meter/sec
ZDOT = -19066
426612 ZDOT = -5792
903554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15735
90 X = -4796
30
Y = 21717231
31 feet Y = 6619412
10 meter
Z = -4783753
95 Z = -1458088
20
XDOT = -14402
540147 XDOT = -4389
894237
YDOT = -4158
049226 feet/sec YDOT = -1267
373404 meter/sec
ZDOT = -18989
565498 ZDOT = -5788
019564
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 12188
58669465
00016717 00000-0 10270-3 0 9040
2 25544 51
6369 25
4208 0007323 124
6340 235
5505 15
55962682 21038
Satellite: ISS
Catalog Number: 25544
Epoch time: 12188
58669465 = yrday
fracday
Element set: 904
Inclination: 51
6369 deg
RA of node: 25
4208 deg
Eccentricity:
0007323
Arg of perigee: 124
6340 deg
Mean anomaly: 235
5505 deg
Mean motion: 15
55962682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2103
Checksum: 312
Coasting Arc #6 (Orbit 2118)
---------------------------------------
Vector Time (GMT): 2012/189/13:22:35
791
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3924639
93 A = 6778889
42 meter
Y = 4317902
43 meter E =
0018663
Z = 3439935
52 I = 51
76217
XDOT = -5911
005918 Wp = 105
14214
YDOT = 1694
299984 meter/sec RA = 20
05050 deg
ZDOT = 4591
655260 TA = 295
14182
MA = 295
33530
Ha = 220
534 n
mi
Hp = 209
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12876115
27 X = 3859354
42
Y = 14166346
54 feet Y = 4361424
84 meter
Z = 11285877
69 Z = 3458842
76
XDOT = -19393
064035 XDOT = -5951
817471
YDOT = 5558
726983 feet/sec YDOT = 1627
970836 meter/sec
ZDOT = 15064
485761 ZDOT = 4562
841349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4012119
44 X = 1222894
00
Y = -18671577
32 feet Y = -5691096
77 meter
Z = 11363355
66 Z = 3463550
81
XDOT = 14536
513135 XDOT = 4430
729204
YDOT = 12269
838779 feet/sec YDOT = 3739
846860 meter/sec
ZDOT = 14945
451883 ZDOT = 4555
373734
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 12189
61432484
00016717 00000-0 10270-3 0 9055
2 25544 51
6365 20
2824 0007422 130
4201 229
7601 15
55968336 21193
Satellite: ISS
Catalog Number: 25544
Epoch time: 12189
61432484 = yrday
fracday
Element set: 905
Inclination: 51
6365 deg
RA of node: 20
2824 deg
Eccentricity:
0007422
Arg of perigee: 130
4201 deg
Mean anomaly: 229
7601 deg
Mean motion: 15
55968336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2119
Checksum: 292
Coasting Arc #7 (Orbit 2133)
---------------------------------------
Vector Time (GMT): 2012/190/13:22:35
791
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1697405
01 A = 6773920
98 meter
Y = -4424156
48 meter E =
0016918
Z = -4854638
06 I = 51
71766
XDOT = 7248
139317 Wp = 94
71703
YDOT = -74
038431 meter/sec RA = 15
05251 deg
ZDOT = -2475
597684 TA = 151
01590
MA = 150
92185
Ha = 220
561 n
mi
Hp = 209
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5568914
09 X = -1624224
61
Y = -14514949
08 feet Y = -4442728
35 meter
Z = -15927290
24 Z = -4862706
48
XDOT = 23779
984637 XDOT = 7260
454269
YDOT = -242
908238 feet/sec YDOT = 7
083813 meter/sec
ZDOT = -8122
039645 ZDOT = -2440
357100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8358359
97 X = -2547628
12
Y = 13068653
27 feet Y = 3983325
52 meter
Z = -15960051
55 Z = -4864623
71
XDOT = -13497
949387 XDOT = -4114
174973
YDOT = -18339
302209 feet/sec YDOT = -5589
819313 meter/sec
ZDOT = -7976
694411 ZDOT = -2431
296457
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 12190
57771942
00016717 00000-0 10270-3 0 9068
2 25544 51
6375 15
4661 0007529 132
3566 227
8226 15
55980448 21349
Satellite: ISS
Catalog Number: 25544
Epoch time: 12190
57771942 = yrday
fracday
Element set: 906
Inclination: 51
6375 deg
RA of node: 15
4661 deg
Eccentricity:
0007529
Arg of perigee: 132
3566 deg
Mean anomaly: 227
8226 deg
Mean motion: 15
55980448 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2134
Checksum: 321
Coasting Arc #8 (Orbit 2149)
---------------------------------------
Vector Time (GMT): 2012/191/13:22:35
791
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -823495
76 A = 6772072
05 meter
Y = 4114754
76 meter E =
0009208
Z = 5308528
19 I = 51
68086
XDOT = -7547
743725 Wp = 123
40134
YDOT = -1405
341553 meter/sec RA = 10
03775 deg
ZDOT = -86
400288 TA = 327
39208
MA = 327
44890
Ha = 220
597 n
mi
Hp = 209
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2701757
74 X = -895233
97
Y = 13499851
56 feet Y = 4105144
40 meter
Z = 17416431
06 Z = 5304353
78
XDOT = -24762
938730 XDOT = -7531
048232
YDOT = -4610
700633 feet/sec YDOT = -1489
651749 meter/sec
ZDOT = -283
465511 ZDOT = -123
026087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12396261
81 X = 3778380
60
Y = -6041042
49 feet Y = -1841309
75 meter
Z = 17398737
22 Z = 5303135
10
XDOT = 11065
184887 XDOT = 3372
668354
YDOT = 21500
785370 feet/sec YDOT = 6553
439381 meter/sec
ZDOT = -434
344235 ZDOT = -132
388123
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 12191
60533015
00016717 00000-0 10270-3 0 9071
2 25544 51
6371 10
3276 0007513 136
0140 224
1613 15
55941905 21506
Satellite: ISS
Catalog Number: 25544
Epoch time: 12191
60533015 = yrday
fracday
Element set: 907
Inclination: 51
6371 deg
RA of node: 10
3276 deg
Eccentricity:
0007513
Arg of perigee: 136
0140 deg
Mean anomaly: 224
1613 deg
Mean motion: 15
55941905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2150
Checksum: 261
Coasting Arc #9 (Orbit 2164)
---------------------------------------
Vector Time (GMT): 2012/192/13:22:35
791
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3309215
56 A = 6774323
79 meter
Y = -3503006
67 meter E =
0017967
Z = -4778491
24 I = 51
65984
XDOT = 6664
831880 Wp = 120
89618
YDOT = 2685
749229 meter/sec RA = 5
02245 deg
ZDOT = 2645
063397 TA = 175
24340
MA = 175
22630
Ha = 220
425 n
mi
Hp = 209
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10857006
45 X = 3371353
63
Y = -11492804
04 feet Y = -3465653
15 meter
Z = -15677464
69 Z = -4762264
68
XDOT = 21866
246325 XDOT = 6621
454902
YDOT = 8811
513218 feet/sec YDOT = 2760
036763 meter/sec
ZDOT = 8678
029519 ZDOT = 2677
335490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15818490
41 X = -4821475
88
Y = -1356788
32 feet Y = -413549
08 meter
Z = -15610141
55 Z = -4757971
15
XDOT = -6866
412095 XDOT = -2092
882407
YDOT = -21377
694427 feet/sec YDOT = -6515
921261 meter/sec
ZDOT = 8810
797658 ZDOT = 2685
531126
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 12192
56870262
00016717 00000-0 10270-3 0 9086
2 25544 51
6384 5
5114 0007503 140
2087 219
9618 15
55995045 21650
Satellite: ISS
Catalog Number: 25544
Epoch time: 12192
56870262 = yrday
fracday
Element set: 908
Inclination: 51
6384 deg
RA of node: 5
5114 deg
Eccentricity:
0007503
Arg of perigee: 140
2087 deg
Mean anomaly: 219
9618 deg
Mean motion: 15
55995045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2165
Checksum: 310
Coasting Arc #10 (Orbit 2180)
---------------------------------------
Vector Time (GMT): 2012/193/13:22:35
791
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5303892
14 A = 6779366
15 meter
Y = 2608381
38 meter E =
0018310
Z = 3298571
29 I = 51
64562
XDOT = -4777
031368 Wp = 110
62778
YDOT = -3732
441097 meter/sec RA =
01901 deg
ZDOT = -4714
875853 TA = 30
95081
MA = 30
84303
Ha = 220
432 n
mi
Hp = 209
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17401220
92 X = -5348689
03
Y = 8557681
68 feet Y = 2548819
18 meter
Z = 10822084
29 Z = 3272696
78
XDOT = -15672
675093 XDOT = -4712
035716
YDOT = -12245
541657 feet/sec YDOT = -3785
496976 meter/sec
ZDOT = -15468
752799 ZDOT = -4737
924821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17742400
61 X = 5407883
71
Y = 7971708
06 feet Y = 2429776
62 meter
Z = 10715083
05 Z = 3265957
31
XDOT = 1110
120156 XDOT = 338
364624
YDOT = 18514
549089 feet/sec YDOT = 5643
234562 meter/sec
ZDOT = -15563
359456 ZDOT = -4743
711962
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 12193
59629095
00016717 00000-0 10270-3 0 9097
2 25544 51
6378
3731 0007475 144
1603 216
0053 15
55996042 21813
Satellite: ISS
Catalog Number: 25544
Epoch time: 12193
59629095 = yrday
fracday
Element set: 909
Inclination: 51
6378 deg
RA of node:
3731 deg
Eccentricity:
0007475
Arg of perigee: 144
1603 deg
Mean anomaly: 216
0053 deg
Mean motion: 15
55996042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2181
Checksum: 304
Coasting Arc #11 (Orbit 2195)
---------------------------------------
Vector Time (GMT): 2012/194/13:22:35
791
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6496118
57 A = 6783203
13 meter
Y = -1531012
82 meter E =
0009764
Z = -1215995
77 I = 51
62989
XDOT = 2139
744535 Wp = 83
45838
YDOT = 4464
384842 meter/sec RA = 355
03246 deg
ZDOT = 5851
532142 TA = 263
32552
MA = 263
43666
Ha = 220
234 n
mi
Hp = 209
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21312724
97 X = 6518662
87
Y = -5023007
93 feet Y = -1458243
01 meter
Z = -3989487
43 Z = -1184383
45
XDOT = 7020
159237 XDOT = 2061
238533
YDOT = 14646
931897 feet/sec YDOT = 4487
873217 meter/sec
ZDOT = 19197
940097 ZDOT = 5861
736671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17719088
63 X = -5400778
21
Y = -12904310
33 feet Y = -3933233
79 meter
Z = -3858955
51 Z = -1176209
64
XDOT = 5666
231936 XDOT = 1727
067494
YDOT = -13491
766335 feet/sec YDOT = -4112
290379 meter/sec
ZDOT = 19239
492755 ZDOT = 5864
197392
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 12194
55964433
00016717 00000-0 10270-3 0 9104
2 25544 51
6392 355
5568 0007434 147
3532 212
8082 15
56032708 21966
Satellite: ISS
Catalog Number: 25544
Epoch time: 12194
55964433 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 355
5568 deg
Eccentricity:
0007434
Arg of perigee: 147
3532 deg
Mean anomaly: 212
8082 deg
Mean motion: 15
56032708 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2196
Checksum: 314
Coasting Arc #12 (Orbit 2211)
---------------------------------------
Vector Time (GMT): 2012/195/13:22:35
791
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6672440
59 A = 6783115
36 meter
Y = 243539
99 meter E =
0016466
Z = -1151732
37 I = 51
59913
XDOT = 826
525494 Wp = 145
51644
YDOT = -4870
794019 meter/sec RA = 350
05143 deg
ZDOT = -5872
660939 TA = 47
01088
MA = 46
87298
Ha = 220
012 n
mi
Hp = 209
974
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21891209
28 X = -6669073
16
Y = 799015
71 feet Y = 168943
59 meter
Z = -3778649
52 Z = -1184138
44
XDOT = 2711
697815 XDOT = 909
458212
YDOT = -15980
295339 feet/sec YDOT = -4861
086893 meter/sec
ZDOT = -19267
260300 ZDOT = -5868
444876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15136021
96 X = 4613459
49
Y = 15803050
54 feet Y = 4816769
80 meter
Z = -3912300
46 Z = -1192469
18
XDOT = -12666
201743 XDOT = -3860
658291
YDOT = 7408
710684 feet/sec YDOT = 2258
175017 meter/sec
ZDOT = -19249
301389 ZDOT = -5867
187063
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 12195
58721063
00016717 00000-0 10270-3 0 9119
2 25544 51
6387 350
4185 0007306 150
9712 209
1850 15
56060141 22120
Satellite: ISS
Catalog Number: 25544
Epoch time: 12195
58721063 = yrday
fracday
Element set: 911
Inclination: 51
6387 deg
RA of node: 350
4185 deg
Eccentricity:
0007306
Arg of perigee: 150
9712 deg
Mean anomaly: 209
1850 deg
Mean motion: 15
56060141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2212
Checksum: 283
Coasting Arc #13 (Orbit 2227)
---------------------------------------
Vector Time (GMT): 2012/196/13:22:35
791
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5841147
62 A = 6779030
20 meter
Y = 1110955
57 meter E =
0016908
Z = 3249193
47 I = 51
55723
XDOT = -3576
784924 Wp = 111
10005
YDOT = 4852
675078 meter/sec RA = 345
06066 deg
ZDOT = 4744
948569 TA = 286
65250
MA = 286
83806
Ha = 219
886 n
mi
Hp = 210
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19163870
14 X = 5812506
81
Y = 3644867
37 feet Y = 1176114
34 meter
Z = 10660083
56 Z = 3277499
91
XDOT = -11734
858674 XDOT = -3653
832442
YDOT = 15920
849992 feet/sec YDOT = 4812
245834 meter/sec
ZDOT = 15567
416565 ZDOT = 4727
386301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10260671
59 X = -3127452
70
Y = -16515398
04 feet Y = -5033893
32 meter
Z = 10776669
46 Z = 3284728
85
XDOT = 18520
826887 XDOT = 5645
148035
YDOT = -1341
283335 feet/sec YDOT = -408
823160 meter/sec
ZDOT = 15494
428501 ZDOT = 4722
701807
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 12196
61476507
00016717 00000-0 10270-3 0 9125
2 25544 51
6399 345
2810 0007346 155
6266 204
5236 15
56097470 22289
Satellite: ISS
Catalog Number: 25544
Epoch time: 12196
61476507 = yrday
fracday
Element set: 912
Inclination: 51
6399 deg
RA of node: 345
2810 deg
Eccentricity:
0007346
Arg of perigee: 155
6266 deg
Mean anomaly: 204
5236 deg
Mean motion: 15
56097470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2228
Checksum: 318
Coasting Arc #14 (Orbit 2242)
---------------------------------------
Vector Time (GMT): 2012/197/13:22:35
791
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4121167
49 A = 6773984
42 meter
Y = -2526731
89 meter E =
0013675
Z = -4755616
60 I = 51
51104
XDOT = 5726
821069 Wp = 102
70065
YDOT = -4336
026017 meter/sec RA = 340
04913 deg
ZDOT = -2668
433034 TA = 140
93205
MA = 140
83321
Ha = 219
808 n
mi
Hp = 210
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13520890
71 X = -4069505
25
Y = -8289802
79 feet Y = -2572527
82 meter
Z = -15602416
66 Z = -4775511
74
XDOT = 18788
783036 XDOT = 5787
844302
YDOT = -14225
807141 feet/sec YDOT = -4271
643584 meter/sec
ZDOT = -8754
701555 ZDOT = -2640
465009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3266326
05 X = 995576
18
Y = 15437265
54 feet Y = 4705278
54 meter
Z = -15684153
42 Z = -4780529
96
XDOT = -22173
328519 XDOT = -6758
430533
YDOT = -4054
180685 feet/sec YDOT = -1235
714273 meter/sec
ZDOT = -8638
868521 ZDOT = -2633
127125
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 12197
57808938
00016717 00000-0 10270-3 0 9139
2 25544 51
6400 340
4644 0007180 158
8399 201
3053 15
56073203 22439
Satellite: ISS
Catalog Number: 25544
Epoch time: 12197
57808938 = yrday
fracday
Element set: 913
Inclination: 51
6400 deg
RA of node: 340
4644 deg
Eccentricity:
0007180
Arg of perigee: 158
8399 deg
Mean anomaly: 201
3053 deg
Mean motion: 15
56073203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2243
Checksum: 302
Coasting Arc #15 (Orbit 2258)
---------------------------------------
Vector Time (GMT): 2012/198/13:22:35
791
Vector Time (MET): N/A
Weight (LBS) : 908732
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1876625
35 A = 6771540
38 meter
Y = 3775937
46 meter E =
0008217
Z = 5294621
95 I = 51
47556
XDOT = -6926
563352 Wp = 145
88496
YDOT = 3306
315922 meter/sec RA = 335
02009 deg
ZDOT = 90
360059 TA = 303
21349
MA = 303
29224
Ha = 219
590 n
mi
Hp = 210
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6156907
32 X = 1808542
80
Y = 12388246
28 feet Y = 3796541
64 meter
Z = 17370806
93 Z = 5303573
57
XDOT = -22724
945382 XDOT = -6963
459401
YDOT = 10847
493184 feet/sec YDOT = 3228
652485 meter/sec
ZDOT = 296
456886 ZDOT = 56
622369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4566264
96 X = 1391797
56
Y = -13009884
58 feet Y = -3965412
82 meter
Z = 17407274
75 Z = 5305737
35
XDOT = 22736
832693 XDOT = 6930
186605
YDOT = 8219
814318 feet/sec YDOT = 2505
399404 meter/sec
ZDOT = 156
955237 ZDOT = 47
839956
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 12198
60562267
00016717 00000-0 10270-3 0 9147
2 25544 51
6407 335
3262 0007070 162
4159 197
7240 15
56123801 22591
Satellite: ISS
Catalog Number: 25544
Epoch time: 12198
60562267 = yrday
fracday
Element set: 914
Inclination: 51
6407 deg
RA of node: 335
3262 deg
Eccentricity:
0007070
Arg of perigee: 162
4159 deg
Mean anomaly: 197
7240 deg
Mean motion: 15
56123801 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2259
Checksum: 302
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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