[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 1st 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 ET - UTC (sec) : 66 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
091/21:57:25
640 -1
3 3
1 3
1
N/A -1
1 -0
4 214
2
000/00:06:51
280 2
6 -0
1 207
6
096/19:03:32
171 -0
1 6
6 6
6
N/A -4
8 -0
7 212
6
000/00:15:04
342 4
6 -0
4 212
1
Coasting Arc #1 (Orbit 574)
---------------------------------------
Vector Time (GMT): 2012/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3721964
99 A = 6768211
54 meter
Y = 4583121
55 meter E =
0013089
Z = -3318675
38 I = 51
78553
XDOT = -5898
284829 Wp = 199
70385
YDOT = -1369
747453 meter/sec RA = 155
34740 deg
ZDOT = 4705
979135 TA = 121
71355
MA = 121
58589
Ha = 214
662 n
mi
Hp = 205
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12211171
23 X = -3756816
40
Y = 15036488
03 feet Y = 4541305
18 meter
Z = -10888042
59 Z = -3336841
42
XDOT = -19351
328180 XDOT = -5905
390213
YDOT = -4493
922089 feet/sec YDOT = -1435
745168 meter/sec
ZDOT = 15439
564092 ZDOT = 4677
308402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10084609
16 X = -3073788
87
Y = 16488586
27 feet Y = 5025721
09 meter
Z = -10962906
90 Z = -3341494
02
XDOT = -18661
814665 XDOT = -5688
121110
YDOT = -1188
784068 feet/sec YDOT = -362
341384 meter/sec
ZDOT = 15321
921023 ZDOT = 4670
121528
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 12090
50695961
00016717 00000-0 10270-3 0 9000
2 25544 51
6397 156
3861 0015525 215
7505 144
2612 15
59773256 5753
Satellite: ISS
Catalog Number: 25544
Epoch time: 12090
50695961 = yrday
fracday
Element set: 900
Inclination: 51
6397 deg
RA of node: 156
3861 deg
Eccentricity:
0015525
Arg of perigee: 215
7505 deg
Mean anomaly: 144
2612 deg
Mean motion: 15
59773256 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 575
Checksum: 317
Coasting Arc #2 (Orbit 590)
---------------------------------------
Vector Time (GMT): 2012/091/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925359
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5882029
98 A = 6772907
33 meter
Y = -3329780
16 meter E =
0020344
Z = -19587
65 I = 51
82914
XDOT = 2324
387032 Wp = 183
36200
YDOT = 4143
302800 meter/sec RA = 150
35555 deg
ZDOT = -6043
349690 TA = 356
84920
MA = 356
86199
Ha = 214
351 n
mi
Hp = 205
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19297998
62 X = 5918922
24
Y = -10924475
59 feet Y = -3263797
39 meter
Z = -64263
94 Z = 9076
70
XDOT = 7625
941707 XDOT = 2307
240143
YDOT = 13593
513123 feet/sec YDOT = 4169
199264 meter/sec
ZDOT = -19827
262763 ZDOT = -6032
099889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17479974
57 X = 5327896
25
Y = -13645829
33 feet Y = -4159248
78 meter
Z = 53647
37 Z = 16351
72
XDOT = 8667
440993 XDOT = 2641
836015
YDOT = 11029
585723 feet/sec YDOT = 3361
817728 meter/sec
ZDOT = -19781
313510 ZDOT = -6029
344358
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 12091
53206383
00016717 00000-0 10270-3 0 9011
2 25544 51
6402 151
2321 0015312 219
7377 140
2658 15
59798539 5915
Satellite: ISS
Catalog Number: 25544
Epoch time: 12091
53206383 = yrday
fracday
Element set: 901
Inclination: 51
6402 deg
RA of node: 151
2321 deg
Eccentricity:
0015312
Arg of perigee: 219
7377 deg
Mean anomaly: 140
2658 deg
Mean motion: 15
59798539 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 591
Checksum: 300
Coasting Arc #3 (Orbit 597)
---------------------------------------
Vector Time (GMT): 2012/091/22:00:51
280
Vector Time (MET): N/A
Weight (LBS) : 925056
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5926468
73 A = 6774478
82 meter
Y = 3251918
59 meter E =
0000806
Z = 447121
82 I = 51
84127
XDOT = -1936
636229 Wp = 238
71030
YDOT = -4354
716862 meter/sec RA = 148
26685 deg
ZDOT = 6009
896830 TA = 126
10445
MA = 126
09699
Ha = 214
158 n
mi
Hp = 207
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19443795
05 X = -5964563
88
Y = 10669024
24 feet Y = 3185432
18 meter
Z = 1466935
11 Z = 418238
68
XDOT = -6353
793402 XDOT = -1916
991555
YDOT = -14287
128812 feet/sec YDOT = -4376
263267 meter/sec
ZDOT = 19717
509285 ZDOT = 6000
536804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21979149
72 X = 6699244
83
Y = -3023355
96 feet Y = -921518
90 meter
Z = 1348124
29 Z = 410908
28
XDOT = 727
646149 XDOT = 221
786546
YDOT = 14052
857256 feet/sec YDOT = 4283
310892 meter/sec
ZDOT = 19679
332201 ZDOT = 5998
260455
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 12091
98056348
00016717 00000-0 10270-3 0 9025
2 25544 51
6416 148
9774 0013658 230
1927 129
8027 15
59224693 5989
Satellite: ISS
Catalog Number: 25544
Epoch time: 12091
98056348 = yrday
fracday
Element set: 902
Inclination: 51
6416 deg
RA of node: 148
9774 deg
Eccentricity:
0013658
Arg of perigee: 230
1927 deg
Mean anomaly: 129
8027 deg
Mean motion: 15
59224693 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 598
Checksum: 338
Coasting Arc #4 (Orbit 612)
---------------------------------------
Vector Time (GMT): 2012/092/22:00:51
280
Vector Time (MET): N/A
Weight (LBS) : 925056
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5704108
01 A = 6769151
72 meter
Y = -777666
92 meter E =
0009668
Z = -3548438
62 I = 51
85003
XDOT = -1994
453048 Wp = 218
25940
YDOT = 5897
154682 meter/sec RA = 143
27807 deg
ZDOT = -4499
371465 TA = 3
59483
MA = 3
58789
Ha = 213
957 n
mi
Hp = 207
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18714265
13 X = 5729617
52
Y = -2551400
64 feet Y = -713737
72 meter
Z = -11641858
99 Z = -3520666
45
XDOT = -6543
481129 XDOT = -2038
391182
YDOT = 19347
620347 feet/sec YDOT = 5874
605425 meter/sec
ZDOT = -14761
717404 ZDOT = -4509
167592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18529880
28 X = -5647907
51
Y = -4002599
01 feet Y = -1219992
18 meter
Z = -11527748
41 Z = -3513657
72
XDOT = 12368
848266 XDOT = 3770
024951
YDOT = -14637
952377 feet/sec YDOT = -4461
647885 meter/sec
ZDOT = -14802
308186 ZDOT = -4511
743535
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 12092
94192088
00016717 00000-0 10270-3 0 9035
2 25544 51
6425 144
1481 0013689 234
0328 125
9558 15
59268341 6136
Satellite: ISS
Catalog Number: 25544
Epoch time: 12092
94192088 = yrday
fracday
Element set: 903
Inclination: 51
6425 deg
RA of node: 144
1481 deg
Eccentricity:
0013689
Arg of perigee: 234
0328 deg
Mean anomaly: 125
9558 deg
Mean motion: 15
59268341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 613
Checksum: 315
Coasting Arc #5 (Orbit 628)
---------------------------------------
Vector Time (GMT): 2012/093/22:00:51
280
Vector Time (MET): N/A
Weight (LBS) : 925056
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3705147
02 A = 6762766
89 meter
Y = -2192757
51 meter E =
0012586
Z = 5223927
79 I = 51
85281
XDOT = 5010
535279 Wp = 220
88580
YDOT = -5690
185308 meter/sec RA = 138
25339 deg
ZDOT = 1157
615016 TA = 218
00466
MA = 218
09353
Ha = 213
559 n
mi
Hp = 207
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12155994
18 X = -3705728
33
Y = -7194086
31 feet Y = -2234193
47 meter
Z = 17138870
71 Z = 5205927
26
XDOT = 16438
764038 XDOT = 5068
168280
YDOT = -18668
586967 feet/sec YDOT = -5633
832042 meter/sec
ZDOT = 3797
949527 ZDOT = 1182
096421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9261420
31 X = 2822880
91
Y = 10783019
03 feet Y = 3286664
20 meter
Z = 17065068
30 Z = 5201432
82
XDOT = -20799
694943 XDOT = -6339
747019
YDOT = 11654
158242 feet/sec YDOT = 3552
187432 meter/sec
ZDOT = 3898
852195 ZDOT = 1188
370149
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 12093
96734623
00016717 00000-0 10270-3 0 9046
2 25544 51
6423 138
9961 0013633 237
7518 122
2316 15
59314883 6290
Satellite: ISS
Catalog Number: 25544
Epoch time: 12093
96734623 = yrday
fracday
Element set: 904
Inclination: 51
6423 deg
RA of node: 138
9961 deg
Eccentricity:
0013633
Arg of perigee: 237
7518 deg
Mean anomaly: 122
2316 deg
Mean motion: 15
59314883 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 629
Checksum: 320
Coasting Arc #6 (Orbit 643)
---------------------------------------
Vector Time (GMT): 2012/094/22:00:51
280
Vector Time (MET): N/A
Weight (LBS) : 925056
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 672787
51 A = 6764502
15 meter
Y = 4751016
36 meter E =
0010114
Z = -4771088
60 I = 51
88121
XDOT = -6239
975773 Wp = 187
63497
YDOT = 3578
408485 meter/sec RA = 133
21532 deg
ZDOT = 2673
003597 TA = 108
69962
MA = 108
58981
Ha = 213
149 n
mi
Hp = 207
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2207308
11 X = 642787
51
Y = 15587324
02 feet Y = 4758371
58 meter
Z = -15653177
81 Z = -4767893
67
XDOT = -20472
361461 XDOT = -6292
511315
YDOT = 11740
185318 feet/sec YDOT = 3508
335792 meter/sec
ZDOT = 8769
696841 ZDOT = 2642
562106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2614427
15 X = 796877
39
Y = -15537154
95 feet Y = -4735724
83 meter
Z = -15640346
59 Z = -4767177
64
XDOT = 22011
958448 XDOT = 6709
244935
YDOT = -5032
381829 feet/sec YDOT = -1533
869981 meter/sec
ZDOT = 8644
432403 ZDOT = 2634
822996
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 12094
92866098
00016717 00000-0 10270-3 0 9056
2 25544 51
6424 134
1659 0013624 241
8360 118
1420 15
59348180 6448
Satellite: ISS
Catalog Number: 25544
Epoch time: 12094
92866098 = yrday
fracday
Element set: 905
Inclination: 51
6424 deg
RA of node: 134
1659 deg
Eccentricity:
0013624
Arg of perigee: 241
8360 deg
Mean anomaly: 118
1420 deg
Mean motion: 15
59348180 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 644
Checksum: 308
Coasting Arc #7 (Orbit 659)
---------------------------------------
Vector Time (GMT): 2012/095/22:00:51
280
Vector Time (MET): N/A
Weight (LBS) : 925056
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2289025
89 A = 6771746
83 meter
Y = -5909220
07 meter E =
0009605
Z = 2369735
56 I = 51
92531
XDOT = 5444
887529 Wp = 174
26550
YDOT = -59
241391 meter/sec RA = 128
20904 deg
ZDOT = -5414
600029 TA = 339
31506
MA = 339
35391
Ha = 212
859 n
mi
Hp = 207
945
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7509927
45 X = 2343422
18
Y = -19387204
95 feet Y = -5883318
31 meter
Z = 7774722
98 Z = 2380988
46
XDOT = 17863
804228 XDOT = 5471
448282
YDOT = -194
361520 feet/sec YDOT = 1
794523 meter/sec
ZDOT = -17764
435792 ZDOT = -5388
084419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12795726
80 X = -3900137
53
Y = 16364760
99 feet Y = 4987979
15 meter
Z = 7821318
11 Z = 2383937
76
XDOT = -16052
712547 XDOT = -4892
866784
YDOT = -4125
103672 feet/sec YDOT = -1257
331599 meter/sec
ZDOT = -17655
509373 ZDOT = -5381
399257
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 12095
95404138
00016717 00000-0 10270-3 0 9064
2 25544 51
6420 129
0141 0013511 245
2861 114
6888 15
59356663 6604
Satellite: ISS
Catalog Number: 25544
Epoch time: 12095
95404138 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 129
0141 deg
Eccentricity:
0013511
Arg of perigee: 245
2861 deg
Mean anomaly: 114
6888 deg
Mean motion: 15
59356663 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 660
Checksum: 302
Coasting Arc #8 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2012/096/19:11:04
342
Vector Time (MET): N/A
Weight (LBS) : 924391
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4598509
21 A = 6767460
53 meter
Y = -132139
76 meter E =
0005600
Z = 4968023
43 I = 51
91416
XDOT = 2559
957735 Wp = 223
75399
YDOT = -6893
316744 meter/sec RA = 123
83165 deg
ZDOT = 2183
725070 TA = 205
02827
MA = 205
05543
Ha = 212
631 n
mi
Hp = 212
115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15086972
47 X = -4620823
55
Y = -433529
41 feet Y = -183687
28 meter
Z = 16299289
47 Z = 4945629
73
XDOT = 8398
811466 XDOT = 2626
241808
YDOT = -22615
868583 feet/sec YDOT = -6864
318823 meter/sec
ZDOT = 7164
452331 ZDOT = 2196
323196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7555299
72 X = 2302855
36
Y = 13179994
16 feet Y = 4017262
22 meter
Z = 16207304
63 Z = 4939986
45
XDOT = -22690
970506 XDOT = -6916
207810
YDOT = 4123
082373 feet/sec YDOT = 1256
715507 meter/sec
ZDOT = 7216
645430 ZDOT = 2199
633527
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 12096
85128423
00016717 00000-0 10270-3 0 9075
2 25544 51
6416 124
5064 0009286 266
3434 93
6658 15
58084704 6746
Satellite: ISS
Catalog Number: 25544
Epoch time: 12096
85128423 = yrday
fracday
Element set: 907
Inclination: 51
6416 deg
RA of node: 124
5064 deg
Eccentricity:
0009286
Arg of perigee: 266
3434 deg
Mean anomaly: 93
6658 deg
Mean motion: 15
58084704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 325
Coasting Arc #9 (Orbit 688)
---------------------------------------
Vector Time (GMT): 2012/097/19:11:04
342
Vector Time (MET): N/A
Weight (LBS) : 924391
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2927247
77 A = 6766266
98 meter
Y = 3163481
19 meter E =
0005255
Z = -5220431
18 I = 51
92678
XDOT = -4454
416412 Wp = 114
41714
YDOT = 6126
561508 meter/sec RA = 118
80912 deg
ZDOT = 1213
697653 TA = 167
18348
MA = 167
17012
Ha = 211
950 n
mi
Hp = 211
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9603831
26 X = 2917015
52
Y = 10378875
31 feet Y = 3196157
71 meter
Z = -17127398
88 Z = -5206235
76
XDOT = -14614
227073 XDOT = -4528
489743
YDOT = 20100
267416 feet/sec YDOT = 6076
335435 meter/sec
ZDOT = 3981
947680 ZDOT = 1191
877430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3550955
92 X = 1082331
36
Y = -13759813
57 feet Y = -4193991
18 meter
Z = -17069290
04 Z = -5202719
60
XDOT = 23812
657468 XDOT = 7258
097996
YDOT = 1312
551494 feet/sec YDOT = 400
065695 meter/sec
ZDOT = 3891
904165 ZDOT = 1186
252389
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 12097
81336492
00016717 00000-0 10270-3 0 9080
2 25544 51
6419 119
6809 0009213 270
5891 89
4208 15
58103083 6897
Satellite: ISS
Catalog Number: 25544
Epoch time: 12097
81336492 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 119
6809 deg
Eccentricity:
0009213
Arg of perigee: 270
5891 deg
Mean anomaly: 89
4208 deg
Mean motion: 15
58103083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 689
Checksum: 331
Coasting Arc #10 (Orbit 704)
---------------------------------------
Vector Time (GMT): 2012/098/19:11:04
342
Vector Time (MET): N/A
Weight (LBS) : 924391
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -805509
71 A = 6771597
09 meter
Y = -5545310
57 meter E =
0003106
Z = 3801827
86 I = 51
95824
XDOT = 5240
582106 Wp = 47
16161
YDOT = -3668
390614 meter/sec RA = 113
79983 deg
ZDOT = -4236
095902 TA = 87
36779
MA = 87
33224
Ha = 212
572 n
mi
Hp = 212
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2642748
39 X = -761909
76
Y = -18193276
14 feet Y = -5554074
18 meter
Z = 12473188
52 Z = 3798021
04
XDOT = 17193
510848 XDOT = 5301
791615
YDOT = -12035
402277 feet/sec YDOT = -3609
445294 meter/sec
ZDOT = -13897
952433 ZDOT = -4210
488017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13685935
36 X = -4171473
10
Y = 12290447
40 feet Y = 3746128
37 meter
Z = 12457926
14 Z = 3797175
89
XDOT = -18666
728819 XDOT = -5689
618944
YDOT = -6791
635757 feet/sec YDOT = -2070
090579 meter/sec
ZDOT = -13792
496985 ZDOT = -4203
953081
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 12098
83956225
00016717 00000-0 10270-3 0 9096
2 25544 51
6415 114
5344 0009157 274
3685 85
6423 15
58123957 7059
Satellite: ISS
Catalog Number: 25544
Epoch time: 12098
83956225 = yrday
fracday
Element set: 909
Inclination: 51
6415 deg
RA of node: 114
5344 deg
Eccentricity:
0009157
Arg of perigee: 274
3685 deg
Mean anomaly: 85
6423 deg
Mean motion: 15
58123957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 705
Checksum: 329
Coasting Arc #11 (Orbit 719)
---------------------------------------
Vector Time (GMT): 2012/099/19:11:04
342
Vector Time (MET): N/A
Weight (LBS) : 924391
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1283181
71 A = 6777034
76 meter
Y = 6548100
72 meter E =
0009311
Z = -1148727
63 I = 51
98896
XDOT = -4902
881369 Wp = 338
61215
YDOT = 76
449159 meter/sec RA = 108
82024 deg
ZDOT = 5905
978429 TA = 8
95280
MA = 8
93621
Ha = 212
986 n
mi
Hp = 211
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4209913
75 X = -1350728
18
Y = 21483270
07 feet Y = 6533373
65 meter
Z = -3768791
43 Z = -1155125
78
XDOT = -16085
568796 XDOT = -4932
062189
YDOT = 250
817450 feet/sec YDOT = 21
459260 meter/sec
ZDOT = 19376
569650 ZDOT = 5882
089209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20089656
01 X = 6123327
15
Y = -8686636
28 feet Y = -2647686
74 meter
Z = -3795540
41 Z = -1156880
72
XDOT = 8731
321577 XDOT = 2661
306817
YDOT = 11760
163595 feet/sec YDOT = 3584
497864 meter/sec
ZDOT = 19278
413247 ZDOT = 5876
060358
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 12099
80160054
00016717 00000-0 10270-3 0 9103
2 25544 51
6423 109
7083 0009245 278
1918 81
8188 15
58170437 7201
Satellite: ISS
Catalog Number: 25544
Epoch time: 12099
80160054 = yrday
fracday
Element set: 910
Inclination: 51
6423 deg
RA of node: 109
7083 deg
Eccentricity:
0009245
Arg of perigee: 278
1918 deg
Mean anomaly: 81
8188 deg
Mean motion: 15
58170437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 720
Checksum: 308
Coasting Arc #12 (Orbit 735)
---------------------------------------
Vector Time (GMT): 2012/100/19:11:04
342
Vector Time (MET): N/A
Weight (LBS) : 924391
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2948276
26 A = 6776103
13 meter
Y = -5798065
06 meter E =
0005964
Z = -1886377
45 I = 51
99538
XDOT = 3640
672139 Wp = 231
05041
YDOT = 3693
965734 meter/sec RA = 103
85513 deg
ZDOT = -5655
544633 TA = 329
65004
MA = 329
68456
Ha = 213
176 n
mi
Hp = 211
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9672822
38 X = 3022055
98
Y = -19022523
15 feet Y = -5764683
13 meter
Z = -6188902
39 Z = -1871875
31
XDOT = 11944
462398 XDOT = 3626
568576
YDOT = 12119
310151 feet/sec YDOT = 3734
598968 meter/sec
ZDOT = -18554
936459 ZDOT = -5637
892556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21131194
14 X = -6440787
97
Y = 3103499
27 feet Y = 945946
58 meter
Z = -6128892
14 Z = -1868086
32
XDOT = 3120
599839 XDOT = 951
158831
YDOT = -15306
858673 feet/sec YDOT = -4665
530524 meter/sec
ZDOT = -18482
674992 ZDOT = -5633
519338
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 12100
82775352
00016717 00000-0 10270-3 0 9112
2 25544 51
6429 104
5615 0009297 281
3264 78
6846 15
58175477 7369
Satellite: ISS
Catalog Number: 25544
Epoch time: 12100
82775352 = yrday
fracday
Element set: 911
Inclination: 51
6429 deg
RA of node: 104
5615 deg
Eccentricity:
0009297
Arg of perigee: 281
3264 deg
Mean anomaly: 78
6846 deg
Mean motion: 15
58175477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 736
Checksum: 325
Coasting Arc #13 (Orbit 751)
---------------------------------------
Vector Time (GMT): 2012/101/19:11:04
342
Vector Time (MET): N/A
Weight (LBS) : 924391
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3946862
67 A = 6769593
40 meter
Y = 3409422
26 meter E =
0000677
Z = 4315504
69 I = 51
98071
XDOT = -1785
924754 Wp = 125
92061
YDOT = -6563
649723 meter/sec RA = 98
86956 deg
ZDOT = 3551
406020 TA = 288
09804
MA = 288
10541
Ha = 213
529 n
mi
Hp = 211
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12949024
51 X = -4005658
09
Y = 11185768
58 feet Y = 3364957
32 meter
Z = 14158479
96 Z = 4296188
00
XDOT = -5859
333182 XDOT = -1729
648023
YDOT = -21534
283868 feet/sec YDOT = -6583
306330 meter/sec
ZDOT = 11651
594554 ZDOT = 3542
866793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16737995
44 X = 5101741
01
Y = 3858337
30 feet Y = 1176021
21 meter
Z = 14078847
64 Z = 4291232
76
XDOT = -13537
131765 XDOT = -4126
117762
YDOT = 16326
857583 feet/sec YDOT = 4976
426191 meter/sec
ZDOT = 11616
996732 ZDOT = 3540
860604
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 12101
85388335
00016717 00000-0 10270-3 0 9128
2 25544 51
6433 99
4139 0009197 286
3104 73
7039 15
58226495 7529
Satellite: ISS
Catalog Number: 25544
Epoch time: 12101
85388335 = yrday
fracday
Element set: 912
Inclination: 51
6433 deg
RA of node: 99
4139 deg
Eccentricity:
0009197
Arg of perigee: 286
3104 deg
Mean anomaly: 73
7039 deg
Mean motion: 15
58226495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 752
Checksum: 321
Coasting Arc #14 (Orbit 766)
---------------------------------------
Vector Time (GMT): 2012/102/19:11:04
342
Vector Time (MET): N/A
Weight (LBS) : 924391
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4177481
00 A = 6765273
81 meter
Y = -29061
43 meter E =
0007147
Z = -5326740
12 I = 51
97083
XDOT = -301
010968 Wp = 58
73795
YDOT = 7660
209377 meter/sec RA = 93
85517 deg
ZDOT = -274
518007 TA = 208
63848
MA = 208
67775
Ha = 213
605 n
mi
Hp = 211
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13705646
32 X = 4203371
68
Y = -95345
89 feet Y = 17798
45 meter
Z = -17476181
48 Z = -5306383
15
XDOT = -987
568793 XDOT = -385
313057
YDOT = 25131
920527 feet/sec YDOT = 7656
371924 meter/sec
ZDOT = -900
649630 ZDOT = -276
185168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8459413
27 X = -2578429
17
Y = -10918300
68 feet Y = -3327898
05 meter
Z = -17392521
05 Z = -5301240
42
XDOT = 19773
383063 XDOT = 6026
927158
YDOT = -13856
158066 feet/sec YDOT = -4223
356979 meter/sec
ZDOT = -908
088113 ZDOT = -276
785257
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 12102
81585781
00016717 00000-0 10270-3 0 9130
2 25544 51
6436 94
5885 0009311 289
8437 70
1714 15
58293727 7670
Satellite: ISS
Catalog Number: 25544
Epoch time: 12102
81585781 = yrday
fracday
Element set: 913
Inclination: 51
6436 deg
RA of node: 94
5885 deg
Eccentricity:
0009311
Arg of perigee: 289
8437 deg
Mean anomaly: 70
1714 deg
Mean motion: 15
58293727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 767
Checksum: 334
Coasting Arc #15 (Orbit 782)
---------------------------------------
Vector Time (GMT): 2012/103/19:11:04
342
Vector Time (MET): N/A
Weight (LBS) : 924391
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3644892
81 A = 6768270
04 meter
Y = -3413588
45 meter E =
0007256
Z = 4572833
15 I = 51
98267
XDOT = 2296
595551 Wp = 354
88732
YDOT = -6625
881103 meter/sec RA = 88
83797 deg
ZDOT = -3108
953040 TA = 126
10674
MA = 126
03954
Ha = 213
706 n
mi
Hp = 211
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11958309
76 X = -3628664
27
Y = -11199437
17 feet Y = -3454257
06 meter
Z = 15002733
43 Z = 4555165
92
XDOT = 7534
762305 XDOT = 2385
619396
YDOT = -21738
455062 feet/sec YDOT = -6599
701457 meter/sec
ZDOT = -10199
977165 ZDOT = -3097
579909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1304964
03 X = -397753
04
Y = 16397898
94 feet Y = 4998079
60 meter
Z = 14930390
31 Z = 4550782
97
XDOT = -20565
661595 XDOT = -6268
413654
YDOT = 7627
471186 feet/sec YDOT = 2324
853218 meter/sec
ZDOT = -10152
718431 ZDOT = -3094
548578
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 12103
84194121
00016717 00000-0 10270-3 0 9149
2 25544 51
6438 89
4413 0009431 293
8260 66
1906 15
58348314 7833
Satellite: ISS
Catalog Number: 25544
Epoch time: 12103
84194121 = yrday
fracday
Element set: 914
Inclination: 51
6438 deg
RA of node: 89
4413 deg
Eccentricity:
0009431
Arg of perigee: 293
8260 deg
Mean anomaly: 66
1906 deg
Mean motion: 15
58348314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 783
Checksum: 306
Coasting Arc #16 (Orbit 797)
---------------------------------------
Vector Time (GMT): 2012/104/19:11:04
342
Vector Time (MET): N/A
Weight (LBS) : 924391
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2432561
79 A = 6774916
04 meter
Y = 5887119
79 meter E =
0009595
Z = -2288216
23 I = 52
00279
XDOT = -3891
871681 Wp = 333
39967
YDOT = 3732
550754 meter/sec RA = 83
84725 deg
ZDOT = 5465
268203 TA = 1
19597
MA = 1
19368
Ha = 213
958 n
mi
Hp = 210
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7980845
77 X = 2377665
64
Y = 19314697
49 feet Y = 5914015
18 meter
Z = -7507271
09 Z = -2276532
54
XDOT = -12768
607876 XDOT = -3959
869547
YDOT = 12245
901423 feet/sec YDOT = 3688
649443 meter/sec
ZDOT = 17930
669956 ZDOT = 5446
196406
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9849613
11 X = 3002162
08
Y = -18451241
33 feet Y = -5623938
36 meter
Z = -7459716
64 Z = -2273721
63
XDOT = 16289
512692 XDOT = 4965
043468
YDOT = 1477
593281 feet/sec YDOT = 450
370432 meter/sec
ZDOT = 17851
988600 ZDOT = 5441
286125
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 12104
80387422
00016717 00000-0 10270-3 0 9155
2 25544 51
6435 84
6150 0009449 297
2480 62
7712 15
58337598 7981
Satellite: ISS
Catalog Number: 25544
Epoch time: 12104
80387422 = yrday
fracday
Element set: 915
Inclination: 51
6435 deg
RA of node: 84
6150 deg
Eccentricity:
0009449
Arg of perigee: 297
2480 deg
Mean anomaly: 62
7712 deg
Mean motion: 15
58337598 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 798
Checksum: 330
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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