[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 20th 2012
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) : 134 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 300 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 3267)
---------------------------------------
Vector Time (GMT): 2012/263/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3475458
98 A = 6791576
79 meter
Y = 3191206
47 meter E =
0024766
Z = 4867242
69 I = 51
71137
XDOT = -6476
781543 Wp = 72
95821
YDOT = -3329
110802 meter/sec RA = 11
96418 deg
ZDOT = -2424
730765 TA = 40
86818
MA = 40
68275
Ha = 234
270 n
mi
Hp = 214
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11402424
49 X = -3534529
66
Y = 10469837
50 feet Y = 3152011
85 meter
Z = 15968643
98 Z = 4850215
11
XDOT = -21249
283279 XDOT = -6427
294425
YDOT = -10922
279534 feet/sec YDOT = -3401
261721 meter/sec
ZDOT = -7955
153427 ZDOT = -2456
074562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11860317
83 X = 3615024
87
Y = -10060842
81 feet Y = -3066544
89 meter
Z = 15897882
72 Z = 4845674
65
XDOT = 20070
185128 XDOT = 6117
392427
YDOT = 10795
141762 feet/sec YDOT = 3290
359209 meter/sec
ZDOT = -8084
391431 ZDOT = -2464
122508
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 12263
54409851
00016717 00000-0 10270-3 0 9007
2 25544 51
6491 12
2974 0017974 78
7976 281
5193 15
49941243 32685
Satellite: ISS
Catalog Number: 25544
Epoch time: 12263
54409851 = yrday
fracday
Element set: 900
Inclination: 51
6491 deg
RA of node: 12
2974 deg
Eccentricity:
0017974
Arg of perigee: 78
7976 deg
Mean anomaly: 281
5193 deg
Mean motion: 15
49941243 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3268
Checksum: 336
Coasting Arc #2 (Orbit 3282)
---------------------------------------
Vector Time (GMT): 2012/264/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3531009
35 A = 6791977
12 meter
Y = -3354365
11 meter E =
0028035
Z = -4758720
96 I = 51
68341
XDOT = 6487
751600 Wp = 91
86744
YDOT = 2972
945778 meter/sec RA = 7
01417 deg
ZDOT = 2731
438863 TA = 205
16706
MA = 205
30394
Ha = 234
087 n
mi
Hp = 214
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11584676
33 X = 3591373
16
Y = -11005134
86 feet Y = -3314541
95 meter
Z = -15612601
57 Z = -4741420
45
XDOT = 21285
274277 XDOT = 6440
756456
YDOT = 9753
759115 feet/sec YDOT = 3045
233273 meter/sec
ZDOT = 8961
413592 ZDOT = 2762
842063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11875126
28 X = -3619538
49
Y = 10795337
64 feet Y = 3290418
91 meter
Z = -15540692
01 Z = -4736802
92
XDOT = -20264
848183 XDOT = -6176
725726
YDOT = -9266
749349 feet/sec YDOT = -2824
505202 meter/sec
ZDOT = 9090
930083 ZDOT = 2770
915489
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 12264
51122661
00016717 00000-0 10270-3 0 9017
2 25544 51
6492 7
5078 0017912 82
2342 278
0841 15
49988275 32831
Satellite: ISS
Catalog Number: 25544
Epoch time: 12264
51122661 = yrday
fracday
Element set: 901
Inclination: 51
6492 deg
RA of node: 7
5078 deg
Eccentricity:
0017912
Arg of perigee: 82
2342 deg
Mean anomaly: 278
0841 deg
Mean motion: 15
49988275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3283
Checksum: 312
Coasting Arc #3 (Orbit 3298)
---------------------------------------
Vector Time (GMT): 2012/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3617448
43 A = 6792660
43 meter
Y = 3477809
22 meter E =
0026462
Z = 4558215
87 I = 51
65550
XDOT = -6495
020776 Wp = 79
06864
YDOT = -2679
474863 meter/sec RA = 2
06032 deg
ZDOT = -3090
002275 TA = 41
91655
MA = 41
71428
Ha = 234
204 n
mi
Hp = 214
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11868269
12 X = -3678212
11
Y = 11410135
25 feet Y = 3437017
14 meter
Z = 14954776
49 Z = 4540494
57
XDOT = -21309
123280 XDOT = -6449
564951
YDOT = -8790
928027 feet/sec YDOT = -2751
852230 meter/sec
ZDOT = -10137
802739 ZDOT = -3121
444493
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11967521
59 X = 3647700
58
Y = -11402775
26 feet Y = -3475565
90 meter
Z = 14881111
57 Z = 4535762
81
XDOT = 20409
046351 XDOT = 6220
677328
YDOT = 7933
646321 feet/sec YDOT = 2418
175399 meter/sec
ZDOT = -10267
509801 ZDOT = -3129
536987
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 12265
54281621
00016717 00000-0 10270-3 0 9024
2 25544 51
6492 2
3970 0017998 85
6037 274
7169 15
49993411 32998
Satellite: ISS
Catalog Number: 25544
Epoch time: 12265
54281621 = yrday
fracday
Element set: 902
Inclination: 51
6492 deg
RA of node: 2
3970 deg
Eccentricity:
0017998
Arg of perigee: 85
6037 deg
Mean anomaly: 274
7169 deg
Mean motion: 15
49993411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3299
Checksum: 336
Coasting Arc #4 (Orbit 3313)
---------------------------------------
Vector Time (GMT): 2012/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3659196
52 A = 6793185
92 meter
Y = -3679744
48 meter E =
0026330
Z = -4407997
01 I = 51
62728
XDOT = 6432
657096 Wp = 95
65752
YDOT = 2359
018929 meter/sec RA = 357
10621 deg
ZDOT = 3385
589287 TA = 208
67638
MA = 208
82141
Ha = 234
036 n
mi
Hp = 214
603
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12005237
94 X = 3721485
37
Y = -12072652
50 feet Y = -3638476
99 meter
Z = -14461932
45 Z = -4390069
27
XDOT = 21104
518030 XDOT = 6389
353470
YDOT = 7739
563416 feet/sec YDOT = 2430
710940 meter/sec
ZDOT = 11107
576402 ZDOT = 3416
733674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11892608
37 X = -3624867
03
Y = 12271553
44 feet Y = 3740369
49 meter
Z = -14387390
63 Z = -4385276
66
XDOT = -20266
164214 XDOT = -6177
126852
YDOT = -6524
757039 feet/sec YDOT = -1988
745945 meter/sec
ZDOT = 11236
086684 ZDOT = 3424
759221
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 12266
50991686
00016717 00000-0 10270-3 0 9031
2 25544 51
6492 357
6069 0017933 89
1165 271
2041 15
50032724 33145
Satellite: ISS
Catalog Number: 25544
Epoch time: 12266
50991686 = yrday
fracday
Element set: 903
Inclination: 51
6492 deg
RA of node: 357
6069 deg
Eccentricity:
0017933
Arg of perigee: 89
1165 deg
Mean anomaly: 271
2041 deg
Mean motion: 15
50032724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3314
Checksum: 310
Coasting Arc #5 (Orbit 3329)
---------------------------------------
Vector Time (GMT): 2012/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3728161
41 A = 6793976
40 meter
Y = 3842365
12 meter E =
0028103
Z = 4159812
53 I = 51
59974
XDOT = -6366
014628 Wp = 85
87681
YDOT = -2109
234381 meter/sec RA = 352
14853 deg
ZDOT = -3733
413908 TA = 42
59637
MA = 42
37874
Ha = 234
097 n
mi
Hp = 214
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12231500
67 X = -3791057
87
Y = 12606184
78 feet Y = 3800323
04 meter
Z = 13647678
91 Z = 4141548
32
XDOT = -20885
874763 XDOT = -6323
819510
YDOT = -6920
060305 feet/sec YDOT = -2180
187393 meter/sec
ZDOT = -12248
733293 ZDOT = -3764
237115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11882933
96 X = 3621918
27
Y = -13014941
45 feet Y = -3966954
15 meter
Z = 13571728
80 Z = 4136662
94
XDOT = 20082
856638 XDOT = 6121
254703
YDOT = 5349
010586 feet/sec YDOT = 1630
378427 meter/sec
ZDOT = -12375
943320 ZDOT = -3772
187524
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 12267
54147673
00016717 00000-0 10270-3 0 9046
2 25544 51
6491 352
4958 0017971 92
3726 267
9483 15
50046566 33304
Satellite: ISS
Catalog Number: 25544
Epoch time: 12267
54147673 = yrday
fracday
Element set: 904
Inclination: 51
6491 deg
RA of node: 352
4958 deg
Eccentricity:
0017971
Arg of perigee: 92
3726 deg
Mean anomaly: 267
9483 deg
Mean motion: 15
50046566 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3330
Checksum: 334
Coasting Arc #6 (Orbit 3344)
---------------------------------------
Vector Time (GMT): 2012/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3741332
36 A = 6794604
11 meter
Y = -4077620
27 meter E =
0024460
Z = -3966117
36 I = 51
57198
XDOT = 6240
959789 Wp = 98
29695
YDOT = 1843
498487 meter/sec RA = 347
19073 deg
ZDOT = 4009
746187 TA = 213
66380
MA = 213
81941
Ha = 233
969 n
mi
Hp = 214
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12274712
47 X = 3805917
54
Y = -13378019
27 feet Y = -4035421
51 meter
Z = -13012196
07 Z = -3947785
04
XDOT = 20475
589860 XDOT = 6200
403176
YDOT = 6048
223382 feet/sec YDOT = 1913
062298 meter/sec
ZDOT = 13155
335260 ZDOT = 4039
965760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11657297
91 X = -3553144
40
Y = 13990212
14 feet Y = 4264216
66 meter
Z = -12935941
47 Z = -3942874
96
XDOT = -19655
883819 XDOT = -5991
113388
YDOT = -4153
278470 feet/sec YDOT = -1265
919278 meter/sec
ZDOT = 13280
078570 ZDOT = 4047
767948
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 12268
50855020
00016717 00000-0 10270-3 0 9056
2 25544 51
6488 347
7056 0017942 95
9616 264
3580 15
50074285 33455
Satellite: ISS
Catalog Number: 25544
Epoch time: 12268
50855020 = yrday
fracday
Element set: 905
Inclination: 51
6488 deg
RA of node: 347
7056 deg
Eccentricity:
0017942
Arg of perigee: 95
9616 deg
Mean anomaly: 264
3580 deg
Mean motion: 15
50074285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3345
Checksum: 325
Coasting Arc #7 (Orbit 3360)
---------------------------------------
Vector Time (GMT): 2012/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3778047
84 A = 6795443
98 meter
Y = 4270831
89 meter E =
0029570
Z = 3669403
91 I = 51
54581
XDOT = -6112
502076 Wp = 93
28586
YDOT = -1657
073484 meter/sec RA = 342
22963 deg
ZDOT = -4336
264947 TA = 43
00214
MA = 42
77141
Ha = 233
956 n
mi
Hp = 214
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12395170
08 X = -3843349
44
Y = 14011915
66 feet Y = 4228218
61 meter
Z = 12038726
74 Z = 3650891
41
XDOT = -20054
140670 XDOT = -6072
453524
YDOT = -5436
592795 feet/sec YDOT = -1725
203753 meter/sec
ZDOT = -14226
591032 ZDOT = -4365
861662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11486015
11 X = 3500937
41
Y = -14828819
25 feet Y = -4519824
11 meter
Z = 11961711
41 Z = 3645929
64
XDOT = 19209
100950 XDOT = 5854
933970
YDOT = 3228
356851 feet/sec YDOT = 984
003168 meter/sec
ZDOT = -14348
777950 ZDOT = -4373
507519
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 12269
54008046
00016717 00000-0 10270-3 0 9060
2 25544 51
6490 342
5944 0017905 99
1166 261
2012 15
50099710 33616
Satellite: ISS
Catalog Number: 25544
Epoch time: 12269
54008046 = yrday
fracday
Element set: 906
Inclination: 51
6490 deg
RA of node: 342
5944 deg
Eccentricity:
0017905
Arg of perigee: 99
1166 deg
Mean anomaly: 261
2012 deg
Mean motion: 15
50099710 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3361
Checksum: 300
Coasting Arc #8 (Orbit 3375)
---------------------------------------
Vector Time (GMT): 2012/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3749760
59 A = 6796133
07 meter
Y = -4528660
35 meter E =
0022683
Z = -3431820
17 I = 51
51904
XDOT = 5940
946141 Wp = 99
48127
YDOT = 1462
009024 meter/sec RA = 337
26837 deg
ZDOT = 4584
413605 TA = 220
43140
MA = 220
60019
Ha = 233
887 n
mi
Hp = 214
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12302364
13 X = 3816793
28
Y = -14857809
54 feet Y = -4486353
75 meter
Z = -11259252
51 Z = -3413440
74
XDOT = 19491
293115 XDOT = 5901
886120
YDOT = 4796
617532 feet/sec YDOT = 1528
226488 meter/sec
ZDOT = 15040
727052 ZDOT = 4613
179335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11059942
76 X = -3371070
55
Y = 15858651
72 feet Y = 4833717
04 meter
Z = -11182766
49 Z = -3408507
23
XDOT = -18580
652491 XDOT = -5663
382879
YDOT = -2320
590317 feet/sec YDOT = -707
315928 meter/sec
ZDOT = 15159
496347 ZDOT = 4620
614487
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 12270
50712706
00016717 00000-0 10270-3 0 9074
2 25544 51
6483 337
8041 0017949 102
7476 257
5682 15
50113466 33768
Satellite: ISS
Catalog Number: 25544
Epoch time: 12270
50712706 = yrday
fracday
Element set: 907
Inclination: 51
6483 deg
RA of node: 337
8041 deg
Eccentricity:
0017949
Arg of perigee: 102
7476 deg
Mean anomaly: 257
5682 deg
Mean motion: 15
50113466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3376
Checksum: 316
Coasting Arc #9 (Orbit 3391)
---------------------------------------
Vector Time (GMT): 2012/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3742549
69 A = 6796956
16 meter
Y = 4738520
19 meter E =
0030770
Z = 3087250
27 I = 51
49484
XDOT = -5768
652881 Wp = 101
17542
YDOT = -1354
940545 meter/sec RA = 332
30418 deg
ZDOT = -4877
984952 TA = 43
25236
MA = 43
01117
Ha = 233
809 n
mi
Hp = 214
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12278706
33 X = -3810255
82
Y = 15546326
08 feet Y = 4696290
48 meter
Z = 10128773
84 Z = 3068904
09
XDOT = -18926
026512 XDOT = -5729
376757
YDOT = -4445
342995 feet/sec YDOT = -1419
230217 meter/sec
ZDOT = -16003
887637 ZDOT = -4905
913238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10684643
10 X = 3256679
22
Y = -16728251
01 feet Y = -5098770
91 meter
Z = 10052410
84 Z = 3063974
82
XDOT = 17964
010892 XDOT = 5475
430520
YDOT = 1717
071156 feet/sec YDOT = 523
363288 meter/sec
ZDOT = -16119
201537 ZDOT = -4913
132628
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 12271
53862784
00016717 00000-0 10270-3 0 9081
2 25544 51
6487 332
6927 0017861 105
8581 254
4540 15
50149699 33926
Satellite: ISS
Catalog Number: 25544
Epoch time: 12271
53862784 = yrday
fracday
Element set: 908
Inclination: 51
6487 deg
RA of node: 332
6927 deg
Eccentricity:
0017861
Arg of perigee: 105
8581 deg
Mean anomaly: 254
4540 deg
Mean motion: 15
50149699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3392
Checksum: 341
Coasting Arc #10 (Orbit 3406)
---------------------------------------
Vector Time (GMT): 2012/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3663760
96 A = 6797639
04 meter
Y = -5003485
97 meter E =
0021321
Z = -2806957
93 I = 51
46994
XDOT = 5571
332482 Wp = 99
19441
YDOT = 1241
657571 meter/sec RA = 327
33946 deg
ZDOT = 5088
527672 TA = 228
99457
MA = 229
17914
Ha = 233
794 n
mi
Hp = 214
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12020213
12 X = 3733074
31
Y = -16415636
38 feet Y = -4962128
32 meter
Z = -9209179
57 Z = -2788990
46
XDOT = 18278
649875 XDOT = 5532
314909
YDOT = 4073
679694 feet/sec YDOT = 1303
742200 meter/sec
ZDOT = 16694
644593 ZDOT = 5115
498122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10029266
05 X = -3056920
29
Y = 17741050
79 feet Y = 5407472
28 meter
Z = -9134361
99 Z = -2784153
53
XDOT = -17238
940944 XDOT = -5254
429200
YDOT = -1143
367812 feet/sec YDOT = -348
498509 meter/sec
ZDOT = 16806
005307 ZDOT = 5122
470418
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 12272
50564750
00016717 00000-0 10270-3 0 9092
2 25544 51
6477 327
9020 0017968 109
4724 250
8369 15
50152403 34076
Satellite: ISS
Catalog Number: 25544
Epoch time: 12272
50564750 = yrday
fracday
Element set: 909
Inclination: 51
6477 deg
RA of node: 327
9020 deg
Eccentricity:
0017968
Arg of perigee: 109
4724 deg
Mean anomaly: 250
8369 deg
Mean motion: 15
50152403 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3407
Checksum: 312
Coasting Arc #11 (Orbit 3422)
---------------------------------------
Vector Time (GMT): 2012/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3605819
02 A = 6798381
68 meter
Y = 5211707
68 meter E =
0031593
Z = 2417049
29 I = 51
44801
XDOT = -5377
968893 Wp = 109
39569
YDOT = -1224
155994 meter/sec RA = 322
37231 deg
ZDOT = -5336
713084 TA = 43
49644
MA = 43
24767
Ha = 233
682 n
mi
Hp = 214
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11830114
90 X = -3675571
01
Y = 17098778
48 feet Y = 5170995
48 meter
Z = 7929951
73 Z = 2399362
11
XDOT = -17644
254897 XDOT = -5337
955652
YDOT = -4016
259824 feet/sec YDOT = -1284
072789 meter/sec
ZDOT = -17508
901195 ZDOT = -5362
741872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9433301
86 X = 2875270
41
Y = -18560594
98 feet Y = -5657269
35 meter
Z = 7856278
28 Z = 2394593
62
XDOT = 16567
468775 XDOT = 5049
764483
YDOT = 898
202979 feet/sec YDOT = 273
772268 meter/sec
ZDOT = -17616
365292 ZDOT = -5369
468141
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 12273
53711896
00016717 00000-0 10270-3 0 9103
2 25544 51
6480 322
7903 0017892 112
6416 247
6629 15
50192388 34230
Satellite: ISS
Catalog Number: 25544
Epoch time: 12273
53711896 = yrday
fracday
Element set: 910
Inclination: 51
6480 deg
RA of node: 322
7903 deg
Eccentricity:
0017892
Arg of perigee: 112
6416 deg
Mean anomaly: 247
6629 deg
Mean motion: 15
50192388 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3423
Checksum: 317
Coasting Arc #12 (Orbit 3437)
---------------------------------------
Vector Time (GMT): 2012/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3472981
64 A = 6798962
13 meter
Y = -5464964
87 meter E =
0020652
Z = -2096992
41 I = 51
42607
XDOT = 5178
615381 Wp = 98
08316
YDOT = 1197
414987 meter/sec RA = 317
40438 deg
ZDOT = 5499
959671 TA = 238
70780
MA = 238
91019
Ha = 233
684 n
mi
Hp = 214
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11394296
71 X = 3544020
73
Y = -17929674
76 feet Y = -5425730
89 meter
Z = -6879896
36 Z = -2079947
35
XDOT = 16990
207944 XDOT = 5138
122852
YDOT = 3928
526859 feet/sec YDOT = 1255
099803 meter/sec
ZDOT = 18044
487110 ZDOT = 5525
018945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8548095
71 X = -2605459
57
Y = 19473205
69 feet Y = 5935433
10 meter
Z = -6808856
59 Z = -2075339
49
XDOT = -15862
565762 XDOT = -4834
910044
YDOT = -668
505265 feet/sec YDOT = -203
760405 meter/sec
ZDOT = 18147
941260 ZDOT = 5531
492496
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 12274
50411122
00016717 00000-0 10270-3 0 9111
2 25544 51
6474 317
9990 0017999 116
1992 244
1012 15
50194263 34389
Satellite: ISS
Catalog Number: 25544
Epoch time: 12274
50411122 = yrday
fracday
Element set: 911
Inclination: 51
6474 deg
RA of node: 317
9990 deg
Eccentricity:
0017999
Arg of perigee: 116
1992 deg
Mean anomaly: 244
1012 deg
Mean motion: 15
50194263 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3438
Checksum: 304
Coasting Arc #13 (Orbit 3453)
---------------------------------------
Vector Time (GMT): 2012/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3363768
21 A = 6799565
03 meter
Y = 5650592
41 meter E =
0031872
Z = 1666568
01 I = 51
40666
XDOT = -4989
915280 Wp = 117
76457
YDOT = -1271
997231 meter/sec RA = 312
43444 deg
ZDOT = -5689
871030 TA = 43
91611
MA = 43
66323
Ha = 233
575 n
mi
Hp = 214
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11035984
95 X = -3434800
24
Y = 18538689
00 feet Y = 5612579
69 meter
Z = 5467742
83 Z = 1650053
52
XDOT = -16371
113123 XDOT = -4947
680136
YDOT = -4173
219261 feet/sec YDOT = -1327
562106 meter/sec
ZDOT = -18667
555872 ZDOT = -5714
009443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7746469
99 X = 2361124
05
Y = -20154812
04 feet Y = -6143186
71 meter
Z = 5398881
35 Z = 1645579
04
XDOT = 15260
471825 XDOT = 4651
391812
YDOT = 776
836643 feet/sec YDOT = 236
779809 meter/sec
ZDOT = -18767
191700 ZDOT = -5720
240030
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 12275
53555351
00016717 00000-0 10270-3 0 9129
2 25544 51
6474 312
8868 0017982 119
5375 240
7571 15
50226204 34542
Satellite: ISS
Catalog Number: 25544
Epoch time: 12275
53555351 = yrday
fracday
Element set: 912
Inclination: 51
6474 deg
RA of node: 312
8868 deg
Eccentricity:
0017982
Arg of perigee: 119
5375 deg
Mean anomaly: 240
7571 deg
Mean motion: 15
50226204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3454
Checksum: 315
Coasting Arc #14 (Orbit 3468)
---------------------------------------
Vector Time (GMT): 2012/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907764
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3179992
97 A = 6799932
68 meter
Y = -5871736
22 meter E =
0020764
Z = -1311605
76 I = 51
38843
XDOT = 4813
224746 Wp = 97
47981
YDOT = 1329
127451 meter/sec RA = 307
46391 deg
ZDOT = 5796
108443 TA = 248
24033
MA = 248
46143
Ha = 233
542 n
mi
Hp = 214
683
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10433047
79 X = 3251787
19
Y = -19264226
44 feet Y = -5835774
27 meter
Z = -4303168
52 Z = -1295982
23
XDOT = 15791
419769 XDOT = 4769
847753
YDOT = 4360
654368 feet/sec YDOT = 1382
710007 meter/sec
ZDOT = 19016
103815 ZDOT = 5819
385772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6663424
27 X = -2031011
72
Y = 20883355
91 feet Y = 6365246
88 meter
Z = -4237969
89 Z = -1291733
22
XDOT = -14691
573202 XDOT = -4477
991512
YDOT = -861
014469 feet/sec YDOT = -262
437210 meter/sec
ZDOT = 19112
171932 ZDOT = 5825
390005
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 12276
50251783
00016717 00000-0 10270-3 0 9130
2 25544 51
6474 308
0954 0018025 123
0558 237
2327 15
50241911 34695
Satellite: ISS
Catalog Number: 25544
Epoch time: 12276
50251783 = yrday
fracday
Element set: 913
Inclination: 51
6474 deg
RA of node: 308
0954 deg
Eccentricity:
0018025
Arg of perigee: 123
0558 deg
Mean anomaly: 237
2327 deg
Mean motion: 15
50241911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3469
Checksum: 299
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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