[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 2nd 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
There are no maneuvers
Coasting Arc #1 (Orbit 2355)
---------------------------------------
Vector Time (GMT): 2011/057/23:54:14
789
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3382219
04 A = 6728194
73 meter
Y = -3821138
74 meter E =
0012499
Z = -4397822
97 I = 51
67187
XDOT = 6623
168616 Wp = 51
02873
YDOT = -2012
935297 meter/sec RA = 5
54109 deg
ZDOT = -3343
317975 TA = 185
29545
MA = 185
30868
Ha = 193
433 n
mi
Hp = 185
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11096519
15 X = -3317875
68
Y = -12536544
42 feet Y = -3858601
08 meter
Z = -14428553
04 Z = -4414097
01
XDOT = 21729
555827 XDOT = 6661
426214
YDOT = -6604
118427 feet/sec YDOT = -1938
657169 meter/sec
ZDOT = -10968
890993 ZDOT = -3311
050480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4471432
83 X = 1362892
73
Y = 16075060
15 feet Y = 4899678
33 meter
Z = -14494121
41 Z = -4417808
21
XDOT = -21327
876331 XDOT = -6500
736706
YDOT = -3844
062272 feet/sec YDOT = -1171
670180 meter/sec
ZDOT = -10838
553885 ZDOT = -3303
591224
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 11058
01778494
00016717 00000-0 10270-3 0 9002
2 25544 51
6455 5
9197 0004596 12
9535 347
1745 15
72431419 23562
Satellite: ISS
Catalog Number: 25544
Epoch time: 11058
01778494 = yrday
fracday
Element set: 900
Inclination: 51
6455 deg
RA of node: 5
9197 deg
Eccentricity:
0004596
Arg of perigee: 12
9535 deg
Mean anomaly: 347
1745 deg
Mean motion: 15
72431419 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2356
Checksum: 318
Coasting Arc #2 (Orbit 2371)
---------------------------------------
Vector Time (GMT): 2011/058/23:54:14
789
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5252716
49 A = 6731911
33 meter
Y = 2587447
95 meter E =
0014685
Z = 3313704
28 I = 51
65402
XDOT = -4819
087464 Wp = 74
06030
YDOT = -3744
465458 meter/sec RA =
37013 deg
ZDOT = -4694
048674 TA = 67
03752
MA = 66
88265
Ha = 193
540 n
mi
Hp = 185
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17233321
81 X = -5297356
34
Y = 8489002
46 feet Y = 2528459
41 meter
Z = 10871733
21 Z = 3288078
81
XDOT = -15810
654410 XDOT = -4754
055792
YDOT = -12284
991660 feet/sec YDOT = -3797
991948 meter/sec
ZDOT = -15400
422158 ZDOT = -4717
301050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19263319
11 X = 5871459
66
Y = -464440
22 feet Y = -141561
38 meter
Z = 10768191
98 Z = 3282144
91
XDOT = 9094
178591 XDOT = 2771
905635
YDOT = 16334
529599 feet/sec YDOT = 4978
764622 meter/sec
ZDOT = -15494
166712 ZDOT = -4722
622014
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 11059
03461789
00016717 00000-0 10270-3 0 9012
2 25544 51
6458
7101 0004547 18
0993 342
0330 15
72452338 23729
Satellite: ISS
Catalog Number: 25544
Epoch time: 11059
03461789 = yrday
fracday
Element set: 901
Inclination: 51
6458 deg
RA of node:
7101 deg
Eccentricity:
0004547
Arg of perigee: 18
0993 deg
Mean anomaly: 342
0330 deg
Mean motion: 15
72452338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2372
Checksum: 285
Coasting Arc #3 (Orbit 2387)
---------------------------------------
Vector Time (GMT): 2011/059/23:54:14
789
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4926718
00 A = 6730079
87 meter
Y = 2590422
64 meter E =
0013284
Z = 3769533
89 I = 51
61935
XDOT = -5222
504620 Wp = 77
92830
YDOT = 3781
315103 meter/sec RA = 355
29727 deg
ZDOT = 4217
476400 TA = 327
74019
MA = 327
82137
Ha = 193
320 n
mi
Hp = 185
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16163772
96 X = 4879074
08
Y = 8498761
94 feet Y = 2645249
98 meter
Z = 12367237
18 Z = 3793351
30
XDOT = -17134
201508 XDOT = -5284
886970
YDOT = 12405
889445 feet/sec YDOT = 3722
565310 meter/sec
ZDOT = 13836
864828 ZDOT = 4191
954534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11297957
86 X = -3443617
56
Y = -14264196
25 feet Y = -4347727
02 meter
Z = 12463302
93 Z = 3798814
73
XDOT = 19716
889988 XDOT = 6009
708068
YDOT = -3589
295504 feet/sec YDOT = -1094
017270 meter/sec
ZDOT = 13733
704850 ZDOT = 4186
033238
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 11060
05142834
00016717 00000-0 10270-3 0 9024
2 25544 51
6468 355
5005 0004545 21
0896 339
0453 15
72533383 23887
Satellite: ISS
Catalog Number: 25544
Epoch time: 11060
05142834 = yrday
fracday
Element set: 902
Inclination: 51
6468 deg
RA of node: 355
5005 deg
Eccentricity:
0004545
Arg of perigee: 21
0896 deg
Mean anomaly: 339
0453 deg
Mean motion: 15
72533383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2388
Checksum: 295
Coasting Arc #4 (Orbit 2402)
---------------------------------------
Vector Time (GMT): 2011/060/23:54:14
789
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3761782
07 A = 6729477
02 meter
Y = -3884232
09 meter E =
0008811
Z = -4011726
87 I = 51
58667
XDOT = 6292
219203 Wp = 76
03957
YDOT = 2057
336223 meter/sec RA = 350
12020 deg
ZDOT = 3917
499169 TA = 234
45793
MA = 234
54011
Ha = 193
527 n
mi
Hp = 185
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12341804
68 X = 3824424
36
Y = -12743543
61 feet Y = -3841815
60 meter
Z = -13161833
55 Z = -3993300
26
XDOT = 20643
763791 XDOT = 6249
716105
YDOT = 6749
790759 feet/sec YDOT = 2127
462259 meter/sec
ZDOT = 12852
687562 ZDOT = 3947
962451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16386888
39 X = -4994723
58
Y = 6938578
04 feet Y = 2114878
59 meter
Z = -13087319
53 Z = -3989014
99
XDOT = -15840
638896 XDOT = -4828
226736
YDOT = -12994
427555 feet/sec YDOT = -3960
701519 meter/sec
ZDOT = 12975
599641 ZDOT = 3954
962771
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 11061
00467274
00016717 00000-0 10270-3 0 9039
2 25544 51
6469 350
6175 0004634 23
5195 336
6179 15
72523523 24031
Satellite: ISS
Catalog Number: 25544
Epoch time: 11061
00467274 = yrday
fracday
Element set: 903
Inclination: 51
6469 deg
RA of node: 350
6175 deg
Eccentricity:
0004634
Arg of perigee: 23
5195 deg
Mean anomaly: 336
6179 deg
Mean motion: 15
72523523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2403
Checksum: 294
Coasting Arc #5 (Orbit 2418)
---------------------------------------
Vector Time (GMT): 2011/061/23:54:14
789
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5918091
02 A = 6732080
03 meter
Y = -945249
58 meter E =
0007215
Z = -3075774
58 I = 51
56642
XDOT = 3325
559883 Wp = 65
40836
YDOT = -4909
822751 meter/sec RA = 345
04178 deg
ZDOT = -4895
846192 TA = 150
24593
MA = 150
20488
Ha = 193
501 n
mi
Hp = 184
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19416309
12 X = -5892140
09
Y = -3101212
53 feet Y = -1011284
43 meter
Z = -10091123
96 Z = -3104460
72
XDOT = 10910
629537 XDOT = 3403
997741
YDOT = -16108
342358 feet/sec YDOT = -4872
196196 meter/sec
ZDOT = -16062
487507 ZDOT = -4879
500131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16819123
73 X = 5126468
91
Y = 10068651
49 feet Y = 3068924
97 meter
Z = -10206894
54 Z = -3111061
46
XDOT = -15467
983778 XDOT = -4714
641455
YDOT = 9642
274566 feet/sec YDOT = 2938
965288 meter/sec
ZDOT = -15996
346405 ZDOT = -4875
686384
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 11062
02144602
00016717 00000-0 10270-3 0 9040
2 25544 51
6472 345
4077 0004596 28
5161 331
6252 15
72559572 24190
Satellite: ISS
Catalog Number: 25544
Epoch time: 11062
02144602 = yrday
fracday
Element set: 904
Inclination: 51
6472 deg
RA of node: 345
4077 deg
Eccentricity:
0004596
Arg of perigee: 28
5161 deg
Mean anomaly: 331
6252 deg
Mean motion: 15
72559572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2419
Checksum: 294
Coasting Arc #6 (Orbit 2434)
---------------------------------------
Vector Time (GMT): 2011/062/23:54:14
789
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1996589
83 A = 6727340
64 meter
Y = 4559215
72 meter E =
0013007
Z = 4520730
23 I = 51
52142
XDOT = -7057
861478 Wp = 54
43468
YDOT = -21
258248 meter/sec RA = 339
86351 deg
ZDOT = -3082
036747 TA = 66
37730
MA = 66
24080
Ha = 193
608 n
mi
Hp = 184
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6550491
57 X = -2069383
78
Y = 14958056
82 feet Y = 4536482
10 meter
Z = 14831792
08 Z = 4510853
76
XDOT = -23155
713510 XDOT = -7042
127619
YDOT = -69
744908 feet/sec YDOT = -100
095879 meter/sec
ZDOT = -10111
669117 ZDOT = -3116
284723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11521724
71 X = 3511821
69
Y = -11622711
28 feet Y = -3542602
40 meter
Z = 14791784
96 Z = 4508536
06
XDOT = 20714
744970 XDOT = 6313
854267
YDOT = 7432
962655 feet/sec YDOT = 2265
567017 meter/sec
ZDOT = -10249
914174 ZDOT = -3124
173840
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 11063
03819910
00016717 00000-0 10270-3 0 9054
2 25544 51
6474 340
1983 0004756 32
4204 327
7249 15
72596000 24357
Satellite: ISS
Catalog Number: 25544
Epoch time: 11063
03819910 = yrday
fracday
Element set: 905
Inclination: 51
6474 deg
RA of node: 340
1983 deg
Eccentricity:
0004756
Arg of perigee: 32
4204 deg
Mean anomaly: 327
7249 deg
Mean motion: 15
72596000 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2435
Checksum: 295
Coasting Arc #7 (Orbit 2450)
---------------------------------------
Vector Time (GMT): 2011/063/23:54:14
789
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6252594
86 A = 6733726
61 meter
Y = -931927
41 meter E =
0017928
Z = 2291500
61 I = 51
51513
XDOT = -1202
613964 Wp = 63
50146
YDOT = 5335
580487 meter/sec RA = 334
77386 deg
ZDOT = 5426
627868 TA = 322
30658
MA = 322
43206
Ha = 193
473 n
mi
Hp = 184
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20513762
67 X = 6251419
70
Y = -3057504
64 feet Y = -862013
42 meter
Z = 7518046
63 Z = 2321872
29
XDOT = -3945
583873 XDOT = -1288
549054
YDOT = 17505
185326 feet/sec YDOT = 5321
652259 meter/sec
ZDOT = 17803
897204 ZDOT = 5420
576359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20291734
21 X = -6184920
59
Y = -4068115
27 feet Y = -1239961
53 meter
Z = 7640666
17 Z = 2328875
05
XDOT = 9453
941616 XDOT = 2881
561404
YDOT = -13613
344702 feet/sec YDOT = -4149
347465 meter/sec
ZDOT = 17779
312010 ZDOT = 5419
134301
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 11064
05493112
00016717 00000-0 10270-3 0 9060
2 25544 51
6474 334
9886 0004707 35
8617 324
2861 15
72630686 24510
Satellite: ISS
Catalog Number: 25544
Epoch time: 11064
05493112 = yrday
fracday
Element set: 906
Inclination: 51
6474 deg
RA of node: 334
9886 deg
Eccentricity:
0004707
Arg of perigee: 35
8617 deg
Mean anomaly: 324
2861 deg
Mean motion: 15
72630686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2451
Checksum: 314
Coasting Arc #8 (Orbit 2465)
---------------------------------------
Vector Time (GMT): 2011/064/23:54:14
789
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 117493
94 A = 6725500
01 meter
Y = -4605707
46 meter E =
0014976
Z = -4912363
90 I = 51
45994
XDOT = 7058
721345 Wp = 88
76701
YDOT = -2132
837999 meter/sec RA = 329
60121 deg
ZDOT = 2174
548733 TA = 202
40040
MA = 202
46587
Ha = 193
529 n
mi
Hp = 184
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 385478
81 X = 192850
06
Y = -15110588
77 feet Y = -4603972
81 meter
Z = -16116679
45 Z = -4911609
54
XDOT = 23158
534595 XDOT = 7071
483146
YDOT = -6997
499997 feet/sec YDOT = -2053
831489 meter/sec
ZDOT = 7134
346238 ZDOT = 2208
870634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5337262
07 X = -1626797
48
Y = 14145478
70 feet Y = 4311541
91 meter
Z = -16113500
84 Z = -4911395
05
XDOT = -23105
033221 XDOT = -7042
414126
YDOT = -455
527176 feet/sec YDOT = -138
844683 meter/sec
ZDOT = 7272
936579 ZDOT = 2216
791069
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 11065
00809959
00016717 00000-0 10270-3 0 9077
2 25544 51
6468 330
1052 0004767 38
9101 321
2404 15
72675741 24661
Satellite: ISS
Catalog Number: 25544
Epoch time: 11065
00809959 = yrday
fracday
Element set: 907
Inclination: 51
6468 deg
RA of node: 330
1052 deg
Eccentricity:
0004767
Arg of perigee: 38
9101 deg
Mean anomaly: 321
2404 deg
Mean motion: 15
72675741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2466
Checksum: 302
Coasting Arc #9 (Orbit 2481)
---------------------------------------
Vector Time (GMT): 2011/065/23:54:14
789
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5952758
92 A = 6734882
09 meter
Y = 2756660
77 meter E =
0008673
Z = -1523086
64 I = 51
46495
XDOT = -859
824464 Wp = 109
90810
YDOT = -5024
316254 meter/sec RA = 324
49560 deg
ZDOT = -5762
559798 TA = 86
89735
MA = 86
79811
Ha = 193
546 n
mi
Hp = 184
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19530048
94 X = -5975743
22
Y = 9044162
64 feet Y = 2689964
73 meter
Z = -4997003
40 Z = -1552060
89
XDOT = -2820
946404 XDOT = -775
584605
YDOT = -16483
977210 feet/sec YDOT = -5033
460986 meter/sec
ZDOT = -18906
036084 ZDOT = -5766
531572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21333829
81 X = 6502551
33
Y = -2627591
26 feet Y = -800889
82 meter
Z = -5114020
13 Z = -1558753
33
XDOT = -2670
031856 XDOT = -813
825710
YDOT = 14965
078509 feet/sec YDOT = 4561
355930 meter/sec
ZDOT = -18921
922377 ZDOT = -5767
401940
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 11066
02479341
00016717 00000-0 10270-3 0 9089
2 25544 51
6458 324
8949 0004721 42
6143 317
5385 15
72677606 24829
Satellite: ISS
Catalog Number: 25544
Epoch time: 11066
02479341 = yrday
fracday
Element set: 908
Inclination: 51
6458 deg
RA of node: 324
8949 deg
Eccentricity:
0004721
Arg of perigee: 42
6143 deg
Mean anomaly: 317
5385 deg
Mean motion: 15
72677606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2482
Checksum: 322
Coasting Arc #10 (Orbit 2497)
---------------------------------------
Vector Time (GMT): 2011/066/23:54:14
789
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1580778
41 A = 6724227
33 meter
Y = 4041626
47 meter E =
0008916
Z = 5131643
68 I = 51
40592
XDOT = -6375
384188 Wp = 48
71268
YDOT = 4129
626454 meter/sec RA = 319
32993 deg
ZDOT = -1281
304302 TA = 53
61568
MA = 53
53347
Ha = 193
404 n
mi
Hp = 184
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5186280
88 X = 1510538
34
Y = 13259929
35 feet Y = 4058911
50 meter
Z = 16836101
30 Z = 5139151
97
XDOT = -20916
614791 XDOT = -6414
864338
YDOT = 13548
643221 feet/sec YDOT = 4058
112163 meter/sec
ZDOT = -4203
754271 ZDOT = -1312
371941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1017304
15 X = -310074
31
Y = -14165836
65 feet Y = -4317747
01 meter
Z = 16866289
06 Z = 5140844
91
XDOT = 22891
425908 XDOT = 6977
306617
YDOT = -6826
686817 feet/sec YDOT = -2080
774142 meter/sec
ZDOT = -4329
251537 ZDOT = -1319
555868
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 11067
04146463
00016717 00000-0 10270-3 0 9099
2 25544 51
6463 319
6841 0004666 43
9598 316
1935 15
72752437 24983
Satellite: ISS
Catalog Number: 25544
Epoch time: 11067
04146463 = yrday
fracday
Element set: 909
Inclination: 51
6463 deg
RA of node: 319
6841 deg
Eccentricity:
0004666
Arg of perigee: 43
9598 deg
Mean anomaly: 316
1935 deg
Mean motion: 15
72752437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2498
Checksum: 336
Coasting Arc #11 (Orbit 2513)
---------------------------------------
Vector Time (GMT): 2011/067/23:54:14
789
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5054525
51 A = 6735604
13 meter
Y = -4380708
41 meter E =
0018356
Z = 713049
65 I = 51
42067
XDOT = 2675
964611 Wp = 51
18920
YDOT = 4073
412942 meter/sec RA = 314
20659 deg
ZDOT = 5965
143908 TA = 316
60409
MA = 316
74846
Ha = 193
619 n
mi
Hp = 184
315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16583088
95 X = 5099671
92
Y = -14372402
93 feet Y = -4323933
15 meter
Z = 2339401
75 Z = 737714
42
XDOT = 8779
411454 XDOT = 2601
238673
YDOT = 13364
215689 feet/sec YDOT = 4102
919944 meter/sec
ZDOT = 19570
682113 ZDOT = 5977
961755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19870551
44 X = -6056544
08
Y = 9287075
54 feet Y = 2830700
62 meter
Z = 2439061
15 Z = 743425
84
XDOT = -3995
083432 XDOT = -1217
701430
YDOT = -13776
881085 feet/sec YDOT = -4199
193355 meter/sec
ZDOT = 19622
296342 ZDOT = 5980
875925
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 11068
05811994
00016717 00000-0 10270-3 0 9101
2 25544 51
6455 314
4738 0004927 47
9890 312
1692 15
72714914 25144
Satellite: ISS
Catalog Number: 25544
Epoch time: 11068
05811994 = yrday
fracday
Element set: 910
Inclination: 51
6455 deg
RA of node: 314
4738 deg
Eccentricity:
0004927
Arg of perigee: 47
9890 deg
Mean anomaly: 312
1692 deg
Mean motion: 15
72714914 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2514
Checksum: 319
Coasting Arc #12 (Orbit 2528)
---------------------------------------
Vector Time (GMT): 2011/068/23:54:14
789
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2987684
97 A = 6723721
11 meter
Y = -2979916
11 meter E =
0018789
Z = -5250653
89 I = 51
35976
XDOT = 5072
080477 Wp = 83
02108
YDOT = -5760
950168 meter/sec RA = 309
05210 deg
ZDOT = 386
882597 TA = 190
65423
MA = 190
69410
Ha = 193
563 n
mi
Hp = 184
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9802116
03 X = -2928634
36
Y = -9776627
65 feet Y = -3012996
45 meter
Z = -17226554
77 Z = -5265024
31
XDOT = 16640
683980 XDOT = 5134
244152
YDOT = -18900
755144 feet/sec YDOT = -5703
883485 meter/sec
ZDOT = 1269
299858 ZDOT = 411
674052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6858060
47 X = 2090336
83
Y = 11942880
45 feet Y = 3640189
96 meter
Z = -17284464
97 Z = -5268304
92
XDOT = -20063
469653 XDOT = -6115
345550
YDOT = 13487
008170 feet/sec YDOT = 4110
840090 meter/sec
ZDOT = 1369
505589 ZDOT = 417
425304
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 11069
01121232
00016717 00000-0 10270-3 0 9118
2 25544 51
6448 309
5885 0004808 50
9148 309
2441 15
72752134 25293
Satellite: ISS
Catalog Number: 25544
Epoch time: 11069
01121232 = yrday
fracday
Element set: 911
Inclination: 51
6448 deg
RA of node: 309
5885 deg
Eccentricity:
0004808
Arg of perigee: 50
9148 deg
Mean anomaly: 309
2441 deg
Mean motion: 15
72752134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2529
Checksum: 295
Coasting Arc #13 (Orbit 2544)
---------------------------------------
Vector Time (GMT): 2011/069/23:54:14
789
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3741259
94 A = 6735522
21 meter
Y = 5596226
50 meter E =
0014009
Z = 21445
90 I = 51
38231
XDOT = -4009
842512 Wp = 113
85975
YDOT = -2645
829857 meter/sec RA = 303
90983 deg
ZDOT = -6013
945717 TA = 65
90663
MA = 65
76015
Ha = 193
551 n
mi
Hp = 184
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12274474
87 X = -3803664
13
Y = 18360323
15 feet Y = 5554040
54 meter
Z = 70360
58 Z = 3119
05
XDOT = -13155
651287 XDOT = -3950
743853
YDOT = -8680
544150 feet/sec YDOT = -2690
340290 meter/sec
ZDOT = -19730
793035 ZDOT = -6033
281680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16330511
66 X = 4977539
95
Y = -14868877
74 feet Y = -4532033
94 meter
Z = -3750
38 Z = -1143
12
XDOT = 9482
326343 XDOT = 2890
213069
YDOT = 10371
508094 feet/sec YDOT = 3161
235667 meter/sec
ZDOT = -19808
752074 ZDOT = -6037
707632
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 11070
02782549
00016717 00000-0 10270-3 0 9126
2 25544 51
6453 304
3771 0004994 54
7443 305
4186 15
72824489 25457
Satellite: ISS
Catalog Number: 25544
Epoch time: 11070
02782549 = yrday
fracday
Element set: 912
Inclination: 51
6453 deg
RA of node: 304
3771 deg
Eccentricity:
0004994
Arg of perigee: 54
7443 deg
Mean anomaly: 305
4186 deg
Mean motion: 15
72824489 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2545
Checksum: 317
Coasting Arc #14 (Orbit 2560)
---------------------------------------
Vector Time (GMT): 2011/070/23:54:14
789
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3914819
57 A = 6723420
22 meter
Y = 1568559
76 meter E =
0006883
Z = 5230388
32 I = 51
32534
XDOT = -3377
034146 Wp = 75
45926
YDOT = 6910
358835 meter/sec RA = 298
76711 deg
ZDOT = 456
461613 TA = 10
19572
MA = 10
18177
Ha = 193
395 n
mi
Hp = 183
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12843896
24 X = 3871580
62
Y = 5146193
45 feet Y = 1612096
16 meter
Z = 17160066
67 Z = 5249301
24
XDOT = -11079
508352 XDOT = -3456
273489
YDOT = 22671
780954 feet/sec YDOT = 6872
151766 meter/sec
ZDOT = 1497
577472 ZDOT = 439
863296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11266040
12 X = -3433889
03
Y = -7867746
79 feet Y = -2398089
22 meter
Z = 17236350
15 Z = 5253639
52
XDOT = 15307
192603 XDOT = 4665
632305
YDOT = -18793
723594 feet/sec YDOT = -5728
326951 meter/sec
ZDOT = 1430
409077 ZDOT = 435
988687
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 11071
04441776
00016717 00000-0 10270-3 0 9134
2 25544 51
6448 299
1661 0004909 58
4150 301
7491 15
72853357 25614
Satellite: ISS
Catalog Number: 25544
Epoch time: 11071
04441776 = yrday
fracday
Element set: 913
Inclination: 51
6448 deg
RA of node: 299
1661 deg
Eccentricity:
0004909
Arg of perigee: 58
4150 deg
Mean anomaly: 301
7491 deg
Mean motion: 15
72853357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2561
Checksum: 312
Coasting Arc #15 (Orbit 2575)
---------------------------------------
Vector Time (GMT): 2011/071/23:54:14
789
Vector Time (MET): N/A
Weight (LBS) : 892232
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2104624
84 A = 6735224
63 meter
Y = -6345516
18 meter E =
0015361
Z = -766174
20 I = 51
35128
XDOT = 4805
888863 Wp = 46
03028
YDOT = 885
706551 meter/sec RA = 293
60753 deg
ZDOT = 5950
338935 TA = 305
58685
MA = 305
72990
Ha = 193
601 n
mi
Hp = 183
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6904937
14 X = 2179147
08
Y = -20818622
63 feet Y = -6321564
34 meter
Z = -2513694
87 Z = -755768
75
XDOT = 15767
351914 XDOT = 4766
722211
YDOT = 2905
861389 feet/sec YDOT = 939
230187 meter/sec
ZDOT = 19522
109366 ZDOT = 5973
590488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11079428
74 X = -3377009
88
Y = 18935406
72 feet Y = 5771511
97 meter
Z = -2471537
58 Z = -753324
65
XDOT = -13328
907054 XDOT = -4062
650870
YDOT = -5275
369493 feet/sec YDOT = -1607
932622 meter/sec
ZDOT = 19615
923795 ZDOT = 5978
933573
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 11071
99745569
00016717 00000-0 10270-3 0 9146
2 25544 51
6449 294
2805 0005066 60
0805 300
0860 15
72841985 25764
Satellite: ISS
Catalog Number: 25544
Epoch time: 11071
99745569 = yrday
fracday
Element set: 914
Inclination: 51
6449 deg
RA of node: 294
2805 deg
Eccentricity:
0005066
Arg of perigee: 60
0805 deg
Mean anomaly: 300
0860 deg
Mean motion: 15
72841985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2576
Checksum: 324
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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