[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 25th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24756 99 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 134 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 284 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 3807)
---------------------------------------
Vector Time (GMT): 2012/298/08:11:24
524
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5873193
38 A = 6793706
82 meter
Y = 806185
84 meter E =
0014968
Z = -3332198
29 I = 51
53202
XDOT = -3352
076062 Wp = 188
67475
YDOT = -5051
656515 meter/sec RA = 198
70931 deg
ZDOT = 4668
811901 TA = 132
58304
MA = 132
45666
Ha = 229
371 n
mi
Hp = 218
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19269007
16 X = -5865584
55
Y = 2644966
68 feet Y = 740550
42 meter
Z = -10932409
09 Z = -3360711
90
XDOT = -10997
624876 XDOT = -3318
018543
YDOT = -16573
676230 feet/sec YDOT = -5088
950748 meter/sec
ZDOT = 15317
624348 ZDOT = 4652
610587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18538091
95 X = 5650410
43
Y = 5659889
19 feet Y = 1725134
22 meter
Z = -11050468
55 Z = -3368182
82
XDOT = 3523
227498 XDOT = 1073
879741
YDOT = 18345
771423 feet/sec YDOT = 5591
791130 meter/sec
ZDOT = 15251
026904 ZDOT = 4648
513000
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 12298
34829093
00016717 00000-0 10270-3 0 9007
2 25544 51
6451 199
7666 0016525 204
7426 155
2934 15
50983925 38087
Satellite: ISS
Catalog Number: 25544
Epoch time: 12298
34829093 = yrday
fracday
Element set: 900
Inclination: 51
6451 deg
RA of node: 199
7666 deg
Eccentricity:
0016525
Arg of perigee: 204
7426 deg
Mean anomaly: 155
2934 deg
Mean motion: 15
50983925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3808
Checksum: 338
Coasting Arc #2 (Orbit 3823)
---------------------------------------
Vector Time (GMT): 2012/299/08:11:24
524
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6140604
10 A = 6794944
36 meter
Y = -767684
11 meter E =
0017591
Z = 2778100
80 I = 51
56659
XDOT = 2927
461812 Wp = 163
09961
YDOT = 4902
242352 meter/sec RA = 193
74322 deg
ZDOT = -5124
393518 TA = 345
37843
MA = 345
42925
Ha = 228
974 n
mi
Hp = 218
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20146338
90 X = 6135236
53
Y = -2518648
64 feet Y = -699045
81 meter
Z = 9114503
92 Z = 2807919
03
XDOT = 9604
533503 XDOT = 2897
319846
YDOT = 16083
472284 feet/sec YDOT = 4934
810096 meter/sec
ZDOT = -16812
314690 ZDOT = -5110
245463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19394405
70 X = -5911414
86
Y = -5814612
99 feet Y = -1772294
04 meter
Z = 9237967
69 Z = 2815732
55
XDOT = -2805
102695 XDOT = -854
995301
YDOT = -17219
214045 feet/sec YDOT = -5248
416441 meter/sec
ZDOT = -16754
193948 ZDOT = -5106
678315
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 12299
37918188
00016717 00000-0 10270-3 0 9016
2 25544 51
6458 194
6520 0016527 208
7844 151
2396 15
51047643 38242
Satellite: ISS
Catalog Number: 25544
Epoch time: 12299
37918188 = yrday
fracday
Element set: 901
Inclination: 51
6458 deg
RA of node: 194
6520 deg
Eccentricity:
0016527
Arg of perigee: 208
7844 deg
Mean anomaly: 151
2396 deg
Mean motion: 15
51047643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3824
Checksum: 332
Coasting Arc #3 (Orbit 3838)
---------------------------------------
Vector Time (GMT): 2012/300/08:11:24
524
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6409511
71 A = 6796145
89 meter
Y = 735047
61 meter E =
0010510
Z = -2150966
68 I = 51
60074
XDOT = -2394
540326 Wp = 207
09564
YDOT = -4769
251838 meter/sec RA = 188
78002 deg
ZDOT = 5485
778645 TA = 129
10200
MA = 129
00849
Ha = 228
795 n
mi
Hp = 218
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21028581
72 X = -6406805
69
Y = 2411573
52 feet Y = 663387
39 meter
Z = -7056977
31 Z = -2182097
86
XDOT = -7856
103431 XDOT = -2367
680750
YDOT = -15647
151698 feet/sec YDOT = -4795
878430 meter/sec
ZDOT = 17997
961435 ZDOT = 5474
211520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20274659
65 X = 6179716
26
Y = 5926141
77 feet Y = 1806288
01 meter
Z = -7185880
89 Z = -2190256
50
XDOT = 1698
328190 XDOT = 517
650432
YDOT = 16033
099953 feet/sec YDOT = 4886
888866 meter/sec
ZDOT = 17950
506070 ZDOT = 5471
314250
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 12300
34561111
00016717 00000-0 10270-3 0 9027
2 25544 51
6458 189
8565 0016531 212
5327 147
4807 15
51090954 38394
Satellite: ISS
Catalog Number: 25544
Epoch time: 12300
34561111 = yrday
fracday
Element set: 902
Inclination: 51
6458 deg
RA of node: 189
8565 deg
Eccentricity:
0016531
Arg of perigee: 212
5327 deg
Mean anomaly: 147
4807 deg
Mean motion: 15
51090954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3839
Checksum: 305
Coasting Arc #4 (Orbit 3854)
---------------------------------------
Vector Time (GMT): 2012/301/08:11:24
524
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6578441
66 A = 6797067
05 meter
Y = -737139
44 meter E =
0019987
Z = 1482867
52 I = 51
63526
XDOT = 1827
216499 Wp = 173
35231
YDOT = 4706
180044 meter/sec RA = 183
82044 deg
ZDOT = -5778
220238 TA = 350
45958
MA = 350
49749
Ha = 228
449 n
mi
Hp = 218
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21582813
85 X = 6578991
98
Y = -2418436
49 feet Y = -663572
00 meter
Z = 4865050
93 Z = 1514827
39
XDOT = 5994
804786 XDOT = 1802
525115
YDOT = 15440
223241 feet/sec YDOT = 4726
474592 meter/sec
ZDOT = -18957
415478 ZDOT = -5769
403868
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20903037
62 X = -6371245
87
Y = -5781390
63 feet Y = -1762167
86 meter
Z = 4997394
31 Z = 1523205
79
XDOT = -343
937235 XDOT = -104
832069
YDOT = -15079
904364 feet/sec YDOT = -4596
354850 meter/sec
ZDOT = -18921
337837 ZDOT = -5767
223773
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 12301
37643768
00016717 00000-0 10270-3 0 9031
2 25544 51
6467 184
7415 0016546 216
3721 143
6307 15
51135821 38552
Satellite: ISS
Catalog Number: 25544
Epoch time: 12301
37643768 = yrday
fracday
Element set: 903
Inclination: 51
6467 deg
RA of node: 184
7415 deg
Eccentricity:
0016546
Arg of perigee: 216
3721 deg
Mean anomaly: 143
6307 deg
Mean motion: 15
51135821 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3855
Checksum: 307
Coasting Arc #5 (Orbit 3869)
---------------------------------------
Vector Time (GMT): 2012/302/08:11:24
524
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6718040
50 A = 6797593
77 meter
Y = 733060
72 meter E =
0006283
Z = -758395
76 I = 51
66735
XDOT = -1184
903763 Wp = 221
80220
YDOT = -4676
375119 meter/sec RA = 178
86332 deg
ZDOT = 5942
950972 TA = 130
02423
MA = 129
96908
Ha = 228
184 n
mi
Hp = 218
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22040815
30 X = -6722054
23
Y = 2405054
86 feet Y = 657912
90 meter
Z = -2488175
08 Z = -791042
32
XDOT = -3887
479539 XDOT = -1161
393734
YDOT = -15342
438056 feet/sec YDOT = -4689
493582 meter/sec
ZDOT = 19497
870642 ZDOT = 5937
252056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21436216
52 X = 6533758
79
Y = 5601730
72 feet Y = 1707407
52 meter
Z = -2623371
42 Z = -799603
61
XDOT = -1314
526583 XDOT = -400
667703
YDOT = 14198
742340 feet/sec YDOT = 4327
776665 meter/sec
ZDOT = 19474
694636 ZDOT = 5935
886925
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 12302
34280623
00016717 00000-0 10270-3 0 9047
2 25544 51
6460 179
9457 0016547 220
3177 139
6748 15
51193849 38703
Satellite: ISS
Catalog Number: 25544
Epoch time: 12302
34280623 = yrday
fracday
Element set: 904
Inclination: 51
6460 deg
RA of node: 179
9457 deg
Eccentricity:
0016547
Arg of perigee: 220
3177 deg
Mean anomaly: 139
6748 deg
Mean motion: 15
51193849 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3870
Checksum: 324
Coasting Arc #6 (Orbit 3885)
---------------------------------------
Vector Time (GMT): 2012/303/08:11:24
524
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6744291
77 A = 6797782
71 meter
Y = -732262
98 meter E =
0020564
Z = 15827
32 I = 51
69931
XDOT = 525
062654 Wp = 188
04753
YDOT = 4726
635253 meter/sec RA = 173
90894 deg
ZDOT = -6021
567408 TA = 351
78214
MA = 351
81577
Ha = 227
894 n
mi
Hp = 218
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22126941
51 X = 6751901
94
Y = -2402437
59 feet Y = -656801
54 meter
Z = 51926
91 Z = 48610
20
XDOT = 1722
646503 XDOT = 501
421617
YDOT = 15507
333506 feet/sec YDOT = 4732
374313 meter/sec
ZDOT = -19755
798584 ZDOT = -6019
074296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21623593
70 X = -6590871
36
Y = -5268862
07 feet Y = -1605949
16 meter
Z = 187700
08 Z = 57210
98
XDOT = 3157
671649 XDOT = 962
458319
YDOT = -13631
435899 feet/sec YDOT = -4154
861662 meter/sec
ZDOT = -19745
900284 ZDOT = -6018
550407
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 12303
37356839
00016717 00000-0 10270-3 0 9055
2 25544 51
6468 174
8302 0016574 224
0903 135
8928 15
51227659 38864
Satellite: ISS
Catalog Number: 25544
Epoch time: 12303
37356839 = yrday
fracday
Element set: 905
Inclination: 51
6468 deg
RA of node: 174
8302 deg
Eccentricity:
0016574
Arg of perigee: 224
0903 deg
Mean anomaly: 135
8928 deg
Mean motion: 15
51227659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3886
Checksum: 333
Coasting Arc #7 (Orbit 3901)
---------------------------------------
Vector Time (GMT): 2012/304/08:11:24
524
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6720634
18 A = 6797369
43 meter
Y = 703839
37 meter E =
0003520
Z = 756221
94 I = 51
72785
XDOT = 164
168184 Wp = 211
09636
YDOT = -4814
511972 meter/sec RA = 168
95589 deg
ZDOT = 5949
449677 TA = 157
04770
MA = 157
03197
Ha = 227
531 n
mi
Hp = 219
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22049324
74 X = -6731678
82
Y = 2309184
27 feet Y = 628623
31 meter
Z = 2481043
11 Z = 723545
64
XDOT = 538
609529 XDOT = 189
090970
YDOT = -15795
642952 feet/sec YDOT = -4812
536562 meter/sec
ZDOT = 19519
191853 ZDOT = 5950
307943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21622125
19 X = 6590423
76
Y = 4964073
37 feet Y = 1513049
56 meter
Z = 2345699
58 Z = 714969
23
XDOT = -5151
790446 XDOT = -1570
265728
YDOT = 13229
875183 feet/sec YDOT = 4032
465956 meter/sec
ZDOT = 19523
180692 ZDOT = 5950
665475
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 12304
40429657
00016717 00000-0 10270-3 0 9060
2 25544 51
6459 169
7138 0016528 228
3263 131
6474 15
51289982 39025
Satellite: ISS
Catalog Number: 25544
Epoch time: 12304
40429657 = yrday
fracday
Element set: 906
Inclination: 51
6459 deg
RA of node: 169
7138 deg
Eccentricity:
0016528
Arg of perigee: 228
3263 deg
Mean anomaly: 131
6474 deg
Mean motion: 15
51289982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3902
Checksum: 329
Coasting Arc #8 (Orbit 3916)
---------------------------------------
Vector Time (GMT): 2012/305/08:11:24
524
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6581130
16 A = 6796566
04 meter
Y = -643589
82 meter E =
0018617
Z = -1515965
02 I = 51
75573
XDOT = -845
990581 Wp = 205
64192
YDOT = 4978
422866 meter/sec RA = 164
00443 deg
ZDOT = -5776
069873 TA = 350
88850
MA = 350
92223
Ha = 227
277 n
mi
Hp = 219
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21591634
37 X = 6595202
20
Y = -2111515
17 feet Y = -569916
87 meter
Z = -4973638
51 Z = -1483959
12
XDOT = -2775
559650 XDOT = -873
537856
YDOT = 16333
408353 feet/sec YDOT = 4968
808323 meter/sec
ZDOT = -18950
360475 ZDOT = -5780
246788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21222605
35 X = -6468650
11
Y = -4643210
60 feet Y = -1415250
59 meter
Z = -4841060
74 Z = -1475555
31
XDOT = 7216
856910 XDOT = 2199
697986
YDOT = -13174
043961 feet/sec YDOT = -4015
448599 meter/sec
ZDOT = -18968
111445 ZDOT = -5781
480368
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 12305
37057442
00016717 00000-0 10270-3 0 9077
2 25544 51
6466 164
9176 0016569 231
9507 128
0149 15
51328520 39175
Satellite: ISS
Catalog Number: 25544
Epoch time: 12305
37057442 = yrday
fracday
Element set: 907
Inclination: 51
6466 deg
RA of node: 164
9176 deg
Eccentricity:
0016569
Arg of perigee: 231
9507 deg
Mean anomaly: 128
0149 deg
Mean motion: 15
51328520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3917
Checksum: 316
Coasting Arc #9 (Orbit 3932)
---------------------------------------
Vector Time (GMT): 2012/306/08:11:24
524
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6386124
79 A = 6795216
59 meter
Y = 530416
19 meter E =
0004867
Z = 2270163
20 I = 51
78016
XDOT = 1507
237721 Wp = 186
52830
YDOT = -5167
150313 meter/sec RA = 159
05290 deg
ZDOT = 5443
685499 TA = 198
62482
MA = 198
64263
Ha = 226
837 n
mi
Hp = 219
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20951853
00 X = -6402609
61
Y = 1740210
61 feet Y = 458910
40 meter
Z = 7448041
98 Z = 2239098
85
XDOT = 4945
005647 XDOT = 1538
460977
YDOT = -16952
592889 feet/sec YDOT = -5150
120823 meter/sec
ZDOT = 17859
860562 ZDOT = 5451
083658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20593715
37 X = 6276964
45
Y = 4450584
29 feet Y = 1356538
09 meter
Z = 7319357
41 Z = 2230940
14
XDOT = -9238
654748 XDOT = -2815
941967
YDOT = 13306
265114 feet/sec YDOT = 4055
749607 meter/sec
ZDOT = 17890
976263 ZDOT = 5453
169565
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 12306
40123883
00016717 00000-0 10270-3 0 9086
2 25544 51
6460 159
8006 0016483 236
0904 123
8680 15
51383528 39336
Satellite: ISS
Catalog Number: 25544
Epoch time: 12306
40123883 = yrday
fracday
Element set: 908
Inclination: 51
6460 deg
RA of node: 159
8006 deg
Eccentricity:
0016483
Arg of perigee: 236
0904 deg
Mean anomaly: 123
8680 deg
Mean motion: 15
51383528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3933
Checksum: 306
Coasting Arc #10 (Orbit 3947)
---------------------------------------
Vector Time (GMT): 2012/307/08:11:24
524
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6086673
99 A = 6793518
40 meter
Y = -353291
75 meter E =
0014331
Z = -2974879
35 I = 51
80375
XDOT = -2132
976301 Wp = 225
35827
YDOT = 5410
389693 meter/sec RA = 154
10183 deg
ZDOT = -5001
683210 TA = 348
55800
MA = 348
59055
Ha = 226
596 n
mi
Hp = 219
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19969402
84 X = 6104623
82
Y = -1159093
67 feet Y = -285126
39 meter
Z = -9760102
86 Z = -2945266
27
XDOT = -6997
953742 XDOT = -2169
020265
YDOT = 17750
622353 feet/sec YDOT = 5386
335903 meter/sec
ZDOT = -16409
721818 ZDOT = -5012
132889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19576605
94 X = -5966949
49
Y = -4388236
13 feet Y = -1337534
37 meter
Z = -9637429
09 Z = -2937488
39
XDOT = 11188
804150 XDOT = 3410
347505
YDOT = -13743
625817 feet/sec YDOT = -4189
057149 meter/sec
ZDOT = -16453
507919 ZDOT = -5015
029214
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 12307
36745592
00016717 00000-0 10270-3 0 9090
2 25544 51
6467 155
0039 0016552 239
9324 120
0186 15
51435307 39481
Satellite: ISS
Catalog Number: 25544
Epoch time: 12307
36745592 = yrday
fracday
Element set: 909
Inclination: 51
6467 deg
RA of node: 155
0039 deg
Eccentricity:
0016552
Arg of perigee: 239
9324 deg
Mean anomaly: 120
0186 deg
Mean motion: 15
51435307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3948
Checksum: 315
Coasting Arc #11 (Orbit 3963)
---------------------------------------
Vector Time (GMT): 2012/308/08:11:24
524
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5742629
36 A = 6791576
97 meter
Y = 101749
36 meter E =
0008427
Z = 3634390
77 I = 51
82443
XDOT = 2693
848413 Wp = 199
57611
YDOT = -5647
669575 meter/sec RA = 149
14940 deg
ZDOT = 4409
838391 TA = 203
28307
MA = 203
32126
Ha = 226
116 n
mi
Hp = 219
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18840647
52 X = -5760995
75
Y = 333823
35 feet Y = 37428
97 meter
Z = 11923854
24 Z = 3606448
15
XDOT = 8838
085343 XDOT = 2735
379179
YDOT = -18529
099657 feet/sec YDOT = -5617
313102 meter/sec
ZDOT = 14467
973723 ZDOT = 4423
026091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18358508
93 X = 5595673
52
Y = 4559986
02 feet Y = 1389883
74 meter
Z = 11808108
00 Z = 3599111
32
XDOT = -12903
842520 XDOT = -3933
091200
YDOT = 14302
211283 feet/sec YDOT = 4359
313999 meter/sec
ZDOT = 14523
134244 ZDOT = 4426
651318
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 12308
39805624
00016717 00000-0 10270-3 0 9109
2 25544 51
6465 149
8864 0016451 243
9461 115
9997 15
51479671 39644
Satellite: ISS
Catalog Number: 25544
Epoch time: 12308
39805624 = yrday
fracday
Element set: 910
Inclination: 51
6465 deg
RA of node: 149
8864 deg
Eccentricity:
0016451
Arg of perigee: 243
9461 deg
Mean anomaly: 115
9997 deg
Mean motion: 15
51479671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3964
Checksum: 347
Coasting Arc #12 (Orbit 3978)
---------------------------------------
Vector Time (GMT): 2012/309/08:11:24
524
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5319511
42 A = 6789477
11 meter
Y = 234652
02 meter E =
0008798
Z = -4203106
12 I = 51
84439
XDOT = -3195
368856 Wp = 246
11289
YDOT = 5900
796362 meter/sec RA = 144
19668 deg
ZDOT = -3712
019513 TA = 345
88113
MA = 345
90571
Ha = 225
867 n
mi
Hp = 219
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17452465
30 X = 5336910
24
Y = 769855
70 feet Y = 294235
42 meter
Z = -13789718
24 Z = -4177221
45
XDOT = -10483
493623 XDOT = -3243
082830
YDOT = 19359
568118 feet/sec YDOT = 5864
796990 meter/sec
ZDOT = -12178
541708 ZDOT = -3727
658612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16831733
30 X = -5130312
31
Y = -4981874
85 feet Y = -1518475
46 meter
Z = -13682515
45 Z = -4170430
71
XDOT = 14412
975076 XDOT = 4393
074803
YDOT = -15044
139124 feet/sec YDOT = -4585
453605 meter/sec
ZDOT = -12243
893212 ZDOT = -3731
938651
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 12309
36421225
00016717 00000-0 10270-3 0 9119
2 25544 51
6472 145
0893 0016543 248
0391 111
9002 15
51547591 39798
Satellite: ISS
Catalog Number: 25544
Epoch time: 12309
36421225 = yrday
fracday
Element set: 911
Inclination: 51
6472 deg
RA of node: 145
0893 deg
Eccentricity:
0016543
Arg of perigee: 248
0391 deg
Mean anomaly: 111
9002 deg
Mean motion: 15
51547591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3979
Checksum: 301
Coasting Arc #13 (Orbit 3994)
---------------------------------------
Vector Time (GMT): 2012/310/08:11:24
524
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4876619
08 A = 6787608
91 meter
Y = -654924
68 meter E =
0011934
Z = 4686806
70 I = 51
86267
XDOT = 3602
913563 Wp = 223
66330
YDOT = -6103
006337 meter/sec RA = 139
24208 deg
ZDOT = 2891
996547 TA = 197
60726
MA = 197
64867
Ha = 225
412 n
mi
Hp = 219
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15999406
44 X = -4891700
94
Y = -2148703
01 feet Y = -709542
40 meter
Z = 15376662
41 Z = 4663079
30
XDOT = 11820
582555 XDOT = 3656
841989
YDOT = -20022
986669 feet/sec YDOT = -6062
414772 meter/sec
ZDOT = 9488
177646 ZDOT = 2909
630615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15198634
16 X = 4632543
69
Y = 5710594
84 feet Y = 1740589
31 meter
Z = 15278426
10 Z = 4656864
28
XDOT = -15545
847547 XDOT = -4738
374332
YDOT = 15757
316392 feet/sec YDOT = 4802
830036 meter/sec
ZDOT = 9561
825966 ZDOT = 2914
444555
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 12310
39474774
00016717 00000-0 10270-3 0 9122
2 25544 51
6473 139
9716 0016454 251
9181 108
0178 15
51578729 39952
Satellite: ISS
Catalog Number: 25544
Epoch time: 12310
39474774 = yrday
fracday
Element set: 912
Inclination: 51
6473 deg
RA of node: 139
9716 deg
Eccentricity:
0016454
Arg of perigee: 251
9181 deg
Mean anomaly: 108
0178 deg
Mean motion: 15
51578729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3995
Checksum: 338
Coasting Arc #14 (Orbit 4009)
---------------------------------------
Vector Time (GMT): 2012/311/08:11:24
524
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4390014
49 A = 6785874
46 meter
Y = 1161861
30 meter E =
0003794
Z = -5038989
22 I = 51
88023
XDOT = -3939
630372 Wp = 259
45580
YDOT = 6270
537070 meter/sec RA = 134
28671 deg
ZDOT = -1985
827511 TA = 351
31925
MA = 351
32581
Ha = 225
175 n
mi
Hp = 218
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14402934
67 X = 4401174
66
Y = 3811880
89 feet Y = 1211015
52 meter
Z = -16532116
86 Z = -5017635
32
XDOT = -12925
296497 XDOT = -3999
809181
YDOT = 20572
628181 feet/sec YDOT = 6226
145158 meter/sec
ZDOT = -6515
182123 ZDOT = -2005
112591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13394082
27 X = -4082516
28
Y = -6744429
30 feet Y = -2055702
05 meter
Z = -16443755
18 Z = -5012056
58
XDOT = 16390
716670 XDOT = 4995
890441
YDOT = -16465
217583 feet/sec YDOT = -5018
598319 meter/sec
ZDOT = -6595
699708 ZDOT = -2010
369271
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 12311
36084209
00016717 00000-0 10270-3 0 9131
2 25544 51
6474 135
1739 0016555 256
1157 103
8153 15
51660765 40105
Satellite: ISS
Catalog Number: 25544
Epoch time: 12311
36084209 = yrday
fracday
Element set: 913
Inclination: 51
6474 deg
RA of node: 135
1739 deg
Eccentricity:
0016555
Arg of perigee: 256
1157 deg
Mean anomaly: 103
8153 deg
Mean motion: 15
51660765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4010
Checksum: 290
Coasting Arc #15 (Orbit 4025)
---------------------------------------
Vector Time (GMT): 2012/312/08:11:24
524
Vector Time (MET): N/A
Weight (LBS) : 891886
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3915763
08 A = 6784829
05 meter
Y = -1743286
30 meter E =
0014050
Z = 5271517
17 I = 51
89773
XDOT = 4174
928017 Wp = 249
80764
YDOT = -6336
429522 meter/sec RA = 129
33056 deg
ZDOT = 1003
197253 TA = 190
58988
MA = 190
61950
Ha = 224
817 n
mi
Hp = 218
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12846991
75 X = -3921586
48
Y = -5719443
26 feet Y = -1787107
24 meter
Z = 17295003
84 Z = 5252480
19
XDOT = 13697
270396 XDOT = 4240
599626
YDOT = -20788
810769 feet/sec YDOT = -6289
375652 meter/sec
ZDOT = 3291
329571 ZDOT = 1023
638849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11620853
78 X = 3542036
23
Y = 8088842
68 feet Y = 2465479
25 meter
Z = 17216293
67 Z = 5247526
31
XDOT = -16808
649876 XDOT = -5123
276482
YDOT = 16943
411313 feet/sec YDOT = 5164
351768 meter/sec
ZDOT = 3376
657981 ZDOT = 1029
205353
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 12312
39131124
00016717 00000-0 10270-3 0 9145
2 25544 51
6477 130
0561 0016529 259
9299 99
9988 15
51686235 40262
Satellite: ISS
Catalog Number: 25544
Epoch time: 12312
39131124 = yrday
fracday
Element set: 914
Inclination: 51
6477 deg
RA of node: 130
0561 deg
Eccentricity:
0016529
Arg of perigee: 259
9299 deg
Mean anomaly: 99
9988 deg
Mean motion: 15
51686235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4026
Checksum: 331
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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