[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 9th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 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
077/06:09:19
968 -0
2 4
8 4
8
N/A -4
8 -0
0 193
5
000/00:10:39
937 0
2 0
2 186
0
Coasting Arc #1 (Orbit 2492)
---------------------------------------
Vector Time (GMT): 2011/066/16:12:18
798
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3559166
00 A = 6725122
64 meter
Y = 2418793
46 meter E =
0007115
Z = 5161957
30 I = 51
41018
XDOT = -5324
438097 Wp = 68
75702
YDOT = 5455
035947 meter/sec RA = 321
01731 deg
ZDOT = 1116
379692 TA = 10
56655
MA = 10
55161
Ha = 194
229 n
mi
Hp = 184
833
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11677053
81 X = 3506778
49
Y = 7935674
09 feet Y = 2458301
87 meter
Z = 16935555
46 Z = 5179120
02
XDOT = -17468
628928 XDOT = -5390
464731
YDOT = 17897
099565 feet/sec YDOT = 5395
125803 meter/sec
ZDOT = 3662
663030 ZDOT = 1090
352883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13681219
62 X = 4170035
74
Y = -3131161
82 feet Y = -954378
12 meter
Z = 17004752
37 Z = 5183048
52
XDOT = 1074
756905 XDOT = 327
585905
YDOT = 23992
760837 feet/sec YDOT = 7312
993503 meter/sec
ZDOT = 3557
469838 ZDOT = 1084
316807
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
72474036
00016717 00000-0 10270-3 0 9004
2 25544 51
6435 321
3257 0005809 37
3688 322
7878 15
72371270 24936
Satellite: ISS
Catalog Number: 25544
Epoch time: 11066
72474036 = yrday
fracday
Element set: 900
Inclination: 51
6435 deg
RA of node: 321
3257 deg
Eccentricity:
0005809
Arg of perigee: 37
3688 deg
Mean anomaly: 322
7878 deg
Mean motion: 15
72371270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2493
Checksum: 314
Coasting Arc #2 (Orbit 2507)
---------------------------------------
Vector Time (GMT): 2011/067/16:12:18
798
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3821807
19 A = 6735620
20 meter
Y = -5341574
67 meter E =
0014131
Z = -1468190
54 I = 51
42261
XDOT = 4747
549359 Wp = 38
39550
YDOT = 1818
796015 meter/sec RA = 315
85400 deg
ZDOT = 5781
686018 TA = 305
40091
MA = 305
53282
Ha = 194
181 n
mi
Hp = 184
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12538737
51 X = 3888385
80
Y = -17524851
26 feet Y = -5298464
79 meter
Z = -4816898
11 Z = -1449462
11
XDOT = 15575
949340 XDOT = 4698
772227
YDOT = 5967
178527 feet/sec YDOT = 1871
613830 meter/sec
ZDOT = 18968
786147 ZDOT = 5804
630763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4728935
82 X = -1441379
64
Y = -21040469
44 feet Y = -6413135
09 meter
Z = -4741167
48 Z = -1445107
85
XDOT = 13206
031379 XDOT = 4025
198364
YDOT = -7232
802342 feet/sec YDOT = -2204
558154 meter/sec
ZDOT = 19061
332085 ZDOT = 5809
894020
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
67802490
00016717 00000-0 10270-3 0 9019
2 25544 51
6428 316
4409 0005627 40
9096 319
2488 15
72471069 25085
Satellite: ISS
Catalog Number: 25544
Epoch time: 11067
67802490 = yrday
fracday
Element set: 901
Inclination: 51
6428 deg
RA of node: 316
4409 deg
Eccentricity:
0005627
Arg of perigee: 40
9096 deg
Mean anomaly: 319
2488 deg
Mean motion: 15
72471069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2508
Checksum: 318
Coasting Arc #3 (Orbit 2523)
---------------------------------------
Vector Time (GMT): 2011/068/16:12:18
798
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4561158
44 A = 6725790
76 meter
Y = -714345
92 meter E =
0017832
Z = -4907437
94 I = 51
36882
XDOT = 3362
979426 Wp = 65
15747
YDOT = -6560
291228 meter/sec RA = 310
74388 deg
ZDOT = -2169
538808 TA = 183
64965
MA = 183
66268
Ha = 194
138 n
mi
Hp = 184
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14964430
57 X = -4528992
19
Y = -2343654
60 feet Y = -765172
12 meter
Z = -16100518
18 Z = -4929517
71
XDOT = 11033
397067 XDOT = 3446
627063
YDOT = -21523
265183 feet/sec YDOT = -6522
216837 meter/sec
ZDOT = -7117
909476 ZDOT = -2152
997836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11473112
23 X = -3497004
61
Y = 9742589
51 feet Y = 2969541
28 meter
Z = -16189602
54 Z = -4934590
85
XDOT = -8383
691237 XDOT = -2555
349089
YDOT = -21596
198983 feet/sec YDOT = -6582
521450 meter/sec
ZDOT = -7050
975901 ZDOT = -2149
137454
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
69482408
00016717 00000-0 10270-3 0 9026
2 25544 51
6424 311
2310 0005690 45
8875 314
2754 15
72544209 25240
Satellite: ISS
Catalog Number: 25544
Epoch time: 11068
69482408 = yrday
fracday
Element set: 902
Inclination: 51
6424 deg
RA of node: 311
2310 deg
Eccentricity:
0005690
Arg of perigee: 45
8875 deg
Mean anomaly: 314
2754 deg
Mean motion: 15
72544209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2524
Checksum: 300
Coasting Arc #4 (Orbit 2539)
---------------------------------------
Vector Time (GMT): 2011/069/16:12:18
798
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2024439
42 A = 6733836
75 meter
Y = 5990544
35 meter E =
0017367
Z = 2299449
19 I = 51
37734
XDOT = -5478
274302 Wp = 91
23366
YDOT = 236
940989 meter/sec RA = 305
56169 deg
ZDOT = -5405
581432 TA = 62
82663
MA = 62
64970
Ha = 193
981 n
mi
Hp = 184
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6641861
62 X = -2102446
60
Y = 19654016
91 feet Y = 5967469
84 meter
Z = 7544124
63 Z = 2289424
64
XDOT = -17973
340885 XDOT = -5454
257491
YDOT = 777
365451 feet/sec YDOT = 175
813524 meter/sec
ZDOT = -17734
847217 ZDOT = -5432
136394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10845346
21 X = 3305661
53
Y = 17702665
87 feet Y = 5395772
56 meter
Z = 7503506
47 Z = 2287068
77
XDOT = -9528
683736 XDOT = -2904
342803
YDOT = 13448
848056 feet/sec YDOT = 4099
208887 meter/sec
ZDOT = -17842
017058 ZDOT = -5438
246799
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
71158051
00016717 00000-0 10270-3 0 9035
2 25544 51
6423 306
0198 0005512 47
0475 313
1149 15
72621278 25404
Satellite: ISS
Catalog Number: 25544
Epoch time: 11069
71158051 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 306
0198 deg
Eccentricity:
0005512
Arg of perigee: 47
0475 deg
Mean anomaly: 313
1149 deg
Mean motion: 15
72621278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2540
Checksum: 283
Coasting Arc #5 (Orbit 2555)
---------------------------------------
Vector Time (GMT): 2011/070/16:12:18
798
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4853353
61 A = 6726998
39 meter
Y = -1141960
14 meter E =
0012243
Z = 4505430
80 I = 51
33784
XDOT = -1230
476871 Wp = 90
64090
YDOT = 6954
945642 meter/sec RA = 300
45934 deg
ZDOT = 3080
979681 TA = 328
52198
MA = 328
59518
Ha = 193
795 n
mi
Hp = 184
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15923076
14 X = 4843876
11
Y = -3746588
39 feet Y = -1087739
74 meter
Z = 14781597
10 Z = 4528985
24
XDOT = -4036
997608 XDOT = -1323
123666
YDOT = 22818
063130 feet/sec YDOT = 6940
667859 meter/sec
ZDOT = 10108
201052 ZDOT = 3074
776650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6984975
37 X = 2129020
49
Y = -14695961
77 feet Y = -4479329
15 meter
Z = 14876683
70 Z = 4534413
19
XDOT = 14165
082277 XDOT = 4317
517078
YDOT = 16963
846028 feet/sec YDOT = 5170
580269 meter/sec
ZDOT = 10082
981495 ZDOT = 3073
292760
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
72829819
00016717 00000-0 10270-3 0 9046
2 25544 51
6421 300
8088 0005449 52
6167 307
5491 15
72675582 25562
Satellite: ISS
Catalog Number: 25544
Epoch time: 11070
72829819 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 300
8088 deg
Eccentricity:
0005449
Arg of perigee: 52
6167 deg
Mean anomaly: 307
5491 deg
Mean motion: 15
72675582 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2556
Checksum: 322
Coasting Arc #6 (Orbit 2570)
---------------------------------------
Vector Time (GMT): 2011/071/16:12:18
798
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 141460
13 A = 6731788
99 meter
Y = -6004122
27 meter E =
0009949
Z = -3043404
73 I = 51
34083
XDOT = 5444
799748 Wp = 64
14785
YDOT = -2348
162021 meter/sec RA = 295
26505 deg
ZDOT = 4902
307743 TA = 260
48150
MA = 260
59394
Ha = 193
916 n
mi
Hp = 183
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 464108
04 X = 223373
00
Y = -19698563
87 feet Y = -6002082
52 meter
Z = -9984923
65 Z = -3042518
28
XDOT = 17863
516232 XDOT = 5446
838401
YDOT = -7703
943638 feet/sec YDOT = -2287
263345 meter/sec
ZDOT = 16083
686822 ZDOT = 4928
763354
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15255945
46 X = -4650012
17
Y = -12473151
09 feet Y = -3801816
45 meter
Z = -9981189
57 Z = -3042266
58
XDOT = 3875
504579 XDOT = 1181
253796
YDOT = -17652
149442 feet/sec YDOT = -5380
375150 meter/sec
ZDOT = 16190
514875 ZDOT = 4934
868934
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
68143356
00016717 00000-0 10270-3 0 9058
2 25544 51
6430 295
9237 0005511 57
6346 302
5349 15
72723494 25716
Satellite: ISS
Catalog Number: 25544
Epoch time: 11071
68143356 = yrday
fracday
Element set: 905
Inclination: 51
6430 deg
RA of node: 295
9237 deg
Eccentricity:
0005511
Arg of perigee: 57
6346 deg
Mean anomaly: 302
5349 deg
Mean motion: 15
72723494 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2571
Checksum: 308
Coasting Arc #7 (Orbit 2586)
---------------------------------------
Vector Time (GMT): 2011/072/16:12:18
798
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4528334
75 A = 6728346
13 meter
Y = 2892060
28 meter E =
0013063
Z = -4063844
58 I = 51
31826
XDOT = -816
318387 Wp = 66
13223
YDOT = -6626
247344 meter/sec RA = 290
16732 deg
ZDOT = -3810
451105 TA = 164
46901
MA = 164
42889
Ha = 193
841 n
mi
Hp = 183
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14856741
31 X = -4540596
62
Y = 9488386
76 feet Y = 2841352
96 meter
Z = -13332823
43 Z = -4085872
82
XDOT = -2678
209932 XDOT = -723
651543
YDOT = -21739
656639 feet/sec YDOT = -6634
857950 meter/sec
ZDOT = -12501
480002 ZDOT = -3814
191345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1242298
64 X = -378652
63
Y = 17516519
08 feet Y = 5339035
02 meter
Z = -13421798
66 Z = -4090964
23
XDOT = -17697
752627 XDOT = -5394
275001
YDOT = -10834
538021 feet/sec YDOT = -3302
367189 meter/sec
ZDOT = -12516
409285 ZDOT = -3815
001550
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 11072
69806995
00016717 00000-0 10270-3 0 9066
2 25544 51
6433 290
7130 0005558 60
3590 299
8125 15
72799170 25878
Satellite: ISS
Catalog Number: 25544
Epoch time: 11072
69806995 = yrday
fracday
Element set: 906
Inclination: 51
6433 deg
RA of node: 290
7130 deg
Eccentricity:
0005558
Arg of perigee: 60
3590 deg
Mean anomaly: 299
8125 deg
Mean motion: 15
72799170 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2587
Checksum: 338
Coasting Arc #8 (Orbit 2602)
---------------------------------------
Vector Time (GMT): 2011/073/16:12:18
798
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1521561
47 A = 6729842
43 meter
Y = 5471007
53 meter E =
0017185
Z = 3600017
64 I = 51
31333
XDOT = -4746
761577 Wp = 79
09794
YDOT = 4208
964101 meter/sec RA = 284
96564 deg
ZDOT = -4369
342059 TA = 57
59254
MA = 57
42639
Ha = 193
752 n
mi
Hp = 183
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4991999
59 X = 1442782
62
Y = 17949499
76 feet Y = 5487582
25 meter
Z = 11811081
50 Z = 3607217
63
XDOT = -15573
364754 XDOT = -4772
249130
YDOT = 13808
937338 feet/sec YDOT = 4155
740212 meter/sec
ZDOT = -14335
111741 ZDOT = -4392
463526
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17440170
91 X = 5315764
09
Y = 6500830
93 feet Y = 1981453
27 meter
Z = 11840011
97 Z = 3608835
65
XDOT = 2623
137856 XDOT = 799
532418
YDOT = 19365
849107 feet/sec YDOT = 5902
710808 meter/sec
ZDOT = -14428
530135 ZDOT = -4397
815985
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 11073
71466508
00016717 00000-0 10270-3 0 9073
2 25544 51
6425 285
5011 0005428 64
5396 295
6328 15
72832644 26037
Satellite: ISS
Catalog Number: 25544
Epoch time: 11073
71466508 = yrday
fracday
Element set: 907
Inclination: 51
6425 deg
RA of node: 285
5011 deg
Eccentricity:
0005428
Arg of perigee: 64
5396 deg
Mean anomaly: 295
6328 deg
Mean motion: 15
72832644 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2603
Checksum: 314
Coasting Arc #9 (Orbit 2618)
---------------------------------------
Vector Time (GMT): 2011/074/16:12:18
798
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3652759
39 A = 6729629
29 meter
Y = -4380350
17 meter E =
0017031
Z = 3555962
61 I = 51
30784
XDOT = 2589
257369 Wp = 85
64830
YDOT = 5758
734847 meter/sec RA = 279
86747 deg
ZDOT = 4417
168846 TA = 317
02668
MA = 317
15959
Ha = 193
517 n
mi
Hp = 183
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11984118
74 X = 3684195
95
Y = -14371227
59 feet Y = -4339326
80 meter
Z = 11666544
00 Z = 3573783
99
XDOT = 8494
938875 XDOT = 2503
212299
YDOT = 18893
487031 feet/sec YDOT = 5787
208673 meter/sec
ZDOT = 14492
023774 ZDOT = 4429
537824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5004375
74 X = -1525333
73
Y = -17983929
47 feet Y = -5481501
70 meter
Z = 11738570
51 Z = 3577916
29
XDOT = 19002
793535 XDOT = 5792
051470
YDOT = 4239
868499 feet/sec YDOT = 1292
311918 meter/sec
ZDOT = 14541
821931 ZDOT = 4432
347324
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 11074
73121600
00016717 00000-0 10270-3 0 9088
2 25544 51
6435 280
2898 0005316 67
7706 292
4020 15
72940043 26193
Satellite: ISS
Catalog Number: 25544
Epoch time: 11074
73121600 = yrday
fracday
Element set: 908
Inclination: 51
6435 deg
RA of node: 280
2898 deg
Eccentricity:
0005316
Arg of perigee: 67
7706 deg
Mean anomaly: 292
4020 deg
Mean motion: 15
72940043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2619
Checksum: 295
Coasting Arc #10 (Orbit 2633)
---------------------------------------
Vector Time (GMT): 2011/075/16:12:18
798
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2908392
27 A = 6727845
48 meter
Y = -4504065
02 meter E =
0012186
Z = -4075246
97 I = 51
29826
XDOT = 3513
413641 Wp = 93
01042
YDOT = -5692
140999 meter/sec RA = 274
66528 deg
ZDOT = 3792
813121 TA = 216
14801
MA = 216
23044
Ha = 193
553 n
mi
Hp = 183
429
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9541969
38 X = -2838014
41
Y = -14777116
21 feet Y = -4536195
28 meter
Z = -13370232
85 Z = -4089204
29
XDOT = 11526
947640 XDOT = 3558
378717
YDOT = -18675
003276 feet/sec YDOT = -5652
600131 meter/sec
ZDOT = 12443
612603 ZDOT = 3809
990629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17543548
15 X = -5347273
48
Y = -359194
37 feet Y = -109482
44 meter
Z = -13426480
07 Z = -4092391
13
XDOT = -9172
302046 XDOT = -2795
717664
YDOT = -18626
526983 feet/sec YDOT = -5677
365424 meter/sec
ZDOT = 12513
060089 ZDOT = 3813
980715
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 11075
68419531
00016717 00000-0 10270-3 0 9097
2 25544 51
6437 275
4045 0005352 69
7290 290
4448 15
72970103 26344
Satellite: ISS
Catalog Number: 25544
Epoch time: 11075
68419531 = yrday
fracday
Element set: 909
Inclination: 51
6437 deg
RA of node: 275
4045 deg
Eccentricity:
0005352
Arg of perigee: 69
7290 deg
Mean anomaly: 290
4448 deg
Mean motion: 15
72970103 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2634
Checksum: 315
Coasting Arc #11 (Orbit 2649)
---------------------------------------
Vector Time (GMT): 2011/076/16:12:18
798
Vector Time (MET): N/A
Weight (LBS) : 920310
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2438087
15 A = 6730691
94 meter
Y = 5461407
67 meter E =
0009482
Z = -3095936
45 I = 51
30699
XDOT = -3922
089167 Wp = 87
23870
YDOT = -4495
404864 meter/sec RA = 269
56277 deg
ZDOT = -4853
819513 TA = 128
84569
MA = 128
76103
Ha = 193
447 n
mi
Hp = 183
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7998973
60 X = -2483937
25
Y = 17918004
17 feet Y = 5433886
79 meter
Z = -10157271
82 Z = -3107892
43
XDOT = -12867
746611 XDOT = -3847
950690
YDOT = -14748
703623 feet/sec YDOT = -4538
850064 meter/sec
ZDOT = -15924
604703 ZDOT = -4872
692047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10755679
09 X = 3278330
99
Y = 16381975
55 feet Y = 4993226
15 meter
Z = -10205629
20 Z = -3110675
78
XDOT = -18122
907713 XDOT = -5523
862271
YDOT = 1955
742180 feet/sec YDOT = 596
110217 meter/sec
ZDOT = -16000
701843 ZDOT = -4877
013922
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 11076
70066351
00016717 00000-0 10270-3 0 9101
2 25544 51
6434 270
1917 0005304 73
1726 287
0018 15
73045614 26505
Satellite: ISS
Catalog Number: 25544
Epoch time: 11076
70066351 = yrday
fracday
Element set: 910
Inclination: 51
6434 deg
RA of node: 270
1917 deg
Eccentricity:
0005304
Arg of perigee: 73
1726 deg
Mean anomaly: 287
0018 deg
Mean motion: 15
73045614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2650
Checksum: 280
Coasting Arc #12 (Orbit 2658)
---------------------------------------
Vector Time (GMT): 2011/077/06:14:39
937
Vector Time (MET): N/A
Weight (LBS) : 919843
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4075064
17 A = 6726893
33 meter
Y = -2154898
08 meter E =
0013473
Z = -4911121
68 I = 51
28703
XDOT = 1273
687988 Wp = 95
70810
YDOT = -7273
645603 meter/sec RA = 266
51112 deg
ZDOT = 2138
384798 TA = 195
15578
MA = 195
19618
Ha = 193
506 n
mi
Hp = 185
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13369633
10 X = -4026807
90
Y = -7069875
61 feet Y = -2200198
73 meter
Z = -16112603
94 Z = -4930800
50
XDOT = 4178
766366 XDOT = 1344
540909
YDOT = -23863
666676 feet/sec YDOT = -7259
006021 meter/sec
ZDOT = 7015
698155 ZDOT = 2144
745280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7450519
24 X = 2270918
27
Y = -13063503
57 feet Y = -3981755
89 meter
Z = -16192000
29 Z = -4935321
69
XDOT = 22781
498092 XDOT = 6943
800618
YDOT = 4280
221443 feet/sec YDOT = 1304
611496 meter/sec
ZDOT = 7041
494793 ZDOT = 2146
247613
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 11077
27240910
00016717 00000-0 10270-3 0 9110
2 25544 51
6444 267
2643 0002447 30
7677 329
3628 15
72153026 26590
Satellite: ISS
Catalog Number: 25544
Epoch time: 11077
27240910 = yrday
fracday
Element set: 911
Inclination: 51
6444 deg
RA of node: 267
2643 deg
Eccentricity:
0002447
Arg of perigee: 30
7677 deg
Mean anomaly: 329
3628 deg
Mean motion: 15
72153026 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2659
Checksum: 304
Coasting Arc #13 (Orbit 2674)
---------------------------------------
Vector Time (GMT): 2011/078/06:14:39
937
Vector Time (MET): N/A
Weight (LBS) : 919843
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -84454
33 A = 6736520
38 meter
Y = 6599610
67 meter E =
0008335
Z = -1337853
22 I = 51
32324
XDOT = -4890
987804 Wp = 127
12904
YDOT = -1234
431520 meter/sec RA = 261
39514 deg
ZDOT = -5810
522816 TA = 67
61311
MA = 67
52482
Ha = 193
454 n
mi
Hp = 186
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -277081
15 X = -151747
19
Y = 21652265
99 feet Y = 6598289
81 meter
Z = -4389282
21 Z = -1338427
86
XDOT = -16046
547912 XDOT = -4848
594513
YDOT = -4049
972178 feet/sec YDOT = -1288
889281 meter/sec
ZDOT = -19063
395064 ZDOT = -5834
179799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21647701
64 X = -6598219
46
Y = -503136
36 feet Y = -153355
96 meter
Z = -4391703
77 Z = -1338591
31
XDOT = 4199
424289 XDOT = 1279
984523
YDOT = -14305
384371 feet/sec YDOT = -4360
281156 meter/sec
ZDOT = -19158
866666 ZDOT = -5839
622560
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 11078
28941443
00016717 00000-0 10270-3 0 9122
2 25544 51
6447 262
0554 0002384 32
9864 327
1447 15
72200660 26759
Satellite: ISS
Catalog Number: 25544
Epoch time: 11078
28941443 = yrday
fracday
Element set: 912
Inclination: 51
6447 deg
RA of node: 262
0554 deg
Eccentricity:
0002384
Arg of perigee: 32
9864 deg
Mean anomaly: 327
1447 deg
Mean motion: 15
72200660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2675
Checksum: 305
Coasting Arc #14 (Orbit 2690)
---------------------------------------
Vector Time (GMT): 2011/079/06:14:39
937
Vector Time (MET): N/A
Weight (LBS) : 919843
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4277362
68 A = 6725143
59 meter
Y = -8333
26 meter E =
0005688
Z = 5186469
49 I = 51
29166
XDOT = 1111
835526 Wp = 47
35036
YDOT = 7567
402844 meter/sec RA = 256
22858 deg
ZDOT = -900
359807 TA = 51
29136
MA = 51
24051
Ha = 193
139 n
mi
Hp = 185
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14033342
13 X = 4251943
17
Y = -27340
08 feet Y = 39357
37 meter
Z = 17015976
00 Z = 5207187
05
XDOT = 3647
754351 XDOT = 1031
506514
YDOT = 24827
437151 feet/sec YDOT = 7579
386798 meter/sec
ZDOT = -2953
936375 ZDOT = -895
154673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 103965
24 X = 31688
61
Y = 13930960
66 feet Y = 4246156
81 meter
Z = 17099602
46 Z = 5211958
83
XDOT = -23790
743070 XDOT = -7251
418488
YDOT = 3795
463261 feet/sec YDOT = 1156
857202 meter/sec
ZDOT = -2933
035952 ZDOT = -893
989358
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 11079
30637564
00016717 00000-0 10270-3 0 9133
2 25544 51
6445 256
8464 0002463 31
4503 328
6806 15
72322094 26919
Satellite: ISS
Catalog Number: 25544
Epoch time: 11079
30637564 = yrday
fracday
Element set: 913
Inclination: 51
6445 deg
RA of node: 256
8464 deg
Eccentricity:
0002463
Arg of perigee: 31
4503 deg
Mean anomaly: 328
6806 deg
Mean motion: 15
72322094 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2691
Checksum: 306
Coasting Arc #15 (Orbit 2706)
---------------------------------------
Vector Time (GMT): 2011/080/06:14:39
937
Vector Time (MET): N/A
Weight (LBS) : 919843
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1992933
62 A = 6736874
33 meter
Y = -6422792
37 meter E =
0015216
Z = 244844
23 I = 51
34041
XDOT = 4664
625405 Wp = 45
41031
YDOT = -1210
098403 meter/sec RA = 251
09229 deg
ZDOT = 6006
367402 TA = 317
26035
MA = 317
37858
Ha = 193
285 n
mi
Hp = 185
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6538496
13 X = -1922154
02
Y = -21072153
44 feet Y = -6444682
78 meter
Z = 803294
72 Z = 235335
23
XDOT = 15303
889125 XDOT = 4648
632450
YDOT = -3970
139118 feet/sec YDOT = -1158
024468 meter/sec
ZDOT = 19705
929798 ZDOT = 6028
989415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20917823
69 X = 6375752
66
Y = -7020846
77 feet Y = -2139954
10 meter
Z = 765001
55 Z = 233172
47
XDOT = 3801
818496 XDOT = 1158
794278
YDOT = 13566
180563 feet/sec YDOT = 4134
971836 meter/sec
ZDOT = 19797
262222 ZDOT = 6034
205525
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 11080
32329694
00016717 00000-0 10270-3 0 9140
2 25544 51
6451 251
6369 0002591 34
2679 325
8651 15
72344338 27070
Satellite: ISS
Catalog Number: 25544
Epoch time: 11080
32329694 = yrday
fracday
Element set: 914
Inclination: 51
6451 deg
RA of node: 251
6369 deg
Eccentricity:
0002591
Arg of perigee: 34
2679 deg
Mean anomaly: 325
8651 deg
Mean motion: 15
72344338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2707
Checksum: 314
Coasting Arc #16 (Orbit 2721)
---------------------------------------
Vector Time (GMT): 2011/081/06:14:39
937
Vector Time (MET): N/A
Weight (LBS) : 919843
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3705874
82 A = 6724599
54 meter
Y = 2015061
00 meter E =
0016734
Z = -5251354
39 I = 51
31154
XDOT = -3342
934497 Wp = 80
61218
YDOT = -6915
021810 meter/sec RA = 245
94677 deg
ZDOT = -292
447558 TA = 186
58282
MA = 186
60483
Ha = 193
187 n
mi
Hp = 185
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12158381
95 X = -3702622
03
Y = 6611092
52 feet Y = 1973637
39 meter
Z = -17228852
99 Z = -5269349
82
XDOT = -10967
632865 XDOT = -3263
940294
YDOT = -22687
079430 feet/sec YDOT = -6951
962875 meter/sec
ZDOT = -959
473616 ZDOT = -308
495064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7086638
28 X = -2160007
35
Y = -11781468
17 feet Y = -3590991
50 meter
Z = -17301524
12 Z = -5273504
55
XDOT = 21372
066563 XDOT = 6514
205888
YDOT = -11342
351313 feet/sec YDOT = -3457
148680 meter/sec
ZDOT = -1024
156724 ZDOT = -312
162969
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 11081
27661895
00016717 00000-0 10270-3 0 9158
2 25544 51
6457 246
7530 0002628 35
4417 324
6919 15
72435361 27223
Satellite: ISS
Catalog Number: 25544
Epoch time: 11081
27661895 = yrday
fracday
Element set: 915
Inclination: 51
6457 deg
RA of node: 246
7530 deg
Eccentricity:
0002628
Arg of perigee: 35
4417 deg
Mean anomaly: 324
6919 deg
Mean motion: 15
72435361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2722
Checksum: 315
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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