[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 11th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 105 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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 938)
---------------------------------------
Vector Time (GMT): 2011/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3872424
21 A = 6759443
37 meter
Y = 1719860
18 meter E =
0026629
Z = -5289014
81 I = 51
30167
XDOT = -3074
017858 Wp = 76
54497
YDOT = -7015
291676 meter/sec RA = 246
48462 deg
ZDOT = -24
543417 TA = 193
18489
MA = 193
25463
Ha = 215
764 n
mi
Hp = 200
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12704803
85 X = -3865675
75
Y = 5642585
90 feet Y = 1676594
51 meter
Z = -17352410
81 Z = -5307810
08
XDOT = -10085
360425 XDOT = -2995
223809
YDOT = -23016
048806 feet/sec YDOT = -7049
226655 meter/sec
ZDOT = -80
523021 ZDOT = -39
285798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13126153
52 X = 4000851
59
Y = 4277357
91 feet Y = 1303738
69 meter
Z = -17428863
42 Z = -5312317
57
XDOT = -7665
018304 XDOT = -2336
297579
YDOT = 22871
557691 feet/sec YDOT = 6971
250784 meter/sec
ZDOT = -140
119905 ZDOT = -42
708547
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 11222
51612112
00016717 00000-0 10270-3 0 9004
2 25544 51
6394 247
2998 0012577 60
6212 299
6198 15
60304301 9398
Satellite: ISS
Catalog Number: 25544
Epoch time: 11222
51612112 = yrday
fracday
Element set: 900
Inclination: 51
6394 deg
RA of node: 247
2998 deg
Eccentricity:
0012577
Arg of perigee: 60
6212 deg
Mean anomaly: 299
6198 deg
Mean motion: 15
60304301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 939
Checksum: 296
Coasting Arc #2 (Orbit 954)
---------------------------------------
Vector Time (GMT): 2011/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4919068
58 A = 6764385
28 meter
Y = 2364543
46 meter E =
0023379
Z = 3982707
42 I = 51
33022
XDOT = 23
698529 Wp = 70
77820
YDOT = 6607
102256 meter/sec RA = 241
40429 deg
ZDOT = -3925
504734 TA = 60
19761
MA = 59
96535
Ha = 215
687 n
mi
Hp = 200
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16138676
45 X = 4872915
44
Y = 7757688
52 feet Y = 2419293
20 meter
Z = 13066625
41 Z = 4006491
66
XDOT = 77
751079 XDOT = -31
116249
YDOT = 21676
844671 feet/sec YDOT = 6607
061011 meter/sec
ZDOT = -12878
952540 ZDOT = -3925
522365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6977823
51 X = -2126840
61
Y = -16413892
74 feet Y = -5002954
51 meter
Z = 13163183
98 Z = 4012138
48
XDOT = 12959
542289 XDOT = 3950
068490
YDOT = -15906
928260 feet/sec YDOT = -4848
431734 meter/sec
ZDOT = -12879
304549 ZDOT = -3925
612027
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 11223
54086233
00016717 00000-0 10270-3 0 9018
2 25544 51
6376 242
1425 0012736 64
1264 296
1203 15
60360470 9556
Satellite: ISS
Catalog Number: 25544
Epoch time: 11223
54086233 = yrday
fracday
Element set: 901
Inclination: 51
6376 deg
RA of node: 242
1425 deg
Eccentricity:
0012736
Arg of perigee: 64
1264 deg
Mean anomaly: 296
1203 deg
Mean motion: 15
60360470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 955
Checksum: 278
Coasting Arc #3 (Orbit 969)
---------------------------------------
Vector Time (GMT): 2011/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4223417
01 A = 6770941
59 meter
Y = -5226182
88 meter E =
0022291
Z = -778430
80 I = 51
36827
XDOT = 3331
731212 Wp = 55
67442
YDOT = -3556
669697 meter/sec RA = 236
36978 deg
ZDOT = 5935
824510 TA = 295
85423
MA = 296
08393
Ha = 215
725 n
mi
Hp = 200
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13856355
02 X = -4160881
55
Y = -17146269
29 feet Y = -5273062
02 meter
Z = -2553906
83 Z = -798795
89
XDOT = 10930
876681 XDOT = 3342
420600
YDOT = -11668
863835 feet/sec YDOT = -3519
352696 meter/sec
ZDOT = 19474
489861 ZDOT = 5952
035446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -495156
26 X = -150923
63
Y = 22029966
73 feet Y = 6714733
86 meter
Z = -2636465
68 Z = -803594
74
XDOT = -14183
885254 XDOT = -4323
248226
YDOT = 1968
864244 feet/sec YDOT = 600
109822 meter/sec
ZDOT = 19540
520717 ZDOT = 5955
950715
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 11224
50155243
00016717 00000-0 10270-3 0 9024
2 25544 51
6381 237
3088 0012694 68
3169 291
9337 15
60379287 9700
Satellite: ISS
Catalog Number: 25544
Epoch time: 11224
50155243 = yrday
fracday
Element set: 902
Inclination: 51
6381 deg
RA of node: 237
3088 deg
Eccentricity:
0012694
Arg of perigee: 68
3169 deg
Mean anomaly: 291
9337 deg
Mean motion: 15
60379287 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 970
Checksum: 318
Coasting Arc #4 (Orbit 985)
---------------------------------------
Vector Time (GMT): 2011/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1753261
77 A = 6767809
74 meter
Y = 5876299
01 meter E =
0016299
Z = -2879837
52 I = 51
37376
XDOT = -5738
649881 Wp = 83
38618
YDOT = -741
383215 meter/sec RA = 231
34749 deg
ZDOT = -5029
193712 TA = 129
57782
MA = 129
43375
Ha = 215
853 n
mi
Hp = 200
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5752171
16 X = 1701410
89
Y = 19279196
22 feet Y = 5895615
18 meter
Z = -9448285
83 Z = -2871446
26
XDOT = -18827
591474 XDOT = -5705
502828
YDOT = -2432
359628 feet/sec YDOT = -805
370891 meter/sec
ZDOT = -16499
979370 ZDOT = -5056
990817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7687252
45 X = 2343074
55
Y = -18609677
72 feet Y = -5672229
77 meter
Z = -9414405
43 Z = -2869510
78
XDOT = 11615
154081 XDOT = 3540
298964
YDOT = 13164
466751 feet/sec YDOT = 4012
529466 meter/sec
ZDOT = -16612
936126 ZDOT = -5063
622931
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 11225
52628122
00016717 00000-0 10270-3 0 9039
2 25544 51
6369 232
1505 0012707 71
5728 288
6808 15
60341424 9860
Satellite: ISS
Catalog Number: 25544
Epoch time: 11225
52628122 = yrday
fracday
Element set: 903
Inclination: 51
6369 deg
RA of node: 232
1505 deg
Eccentricity:
0012707
Arg of perigee: 71
5728 deg
Mean anomaly: 288
6808 deg
Mean motion: 15
60341424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 986
Checksum: 303
Coasting Arc #5 (Orbit 1001)
---------------------------------------
Vector Time (GMT): 2011/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1626410
24 A = 6760228
25 meter
Y = -4155344
50 meter E =
0016524
Z = 5063883
83 I = 51
36761
XDOT = 6070
308853 Wp = 89
00576
YDOT = 4417
179256 meter/sec RA = 226
28665 deg
ZDOT = 1670
589439 TA = 344
82481
MA = 344
87432
Ha = 215
796 n
mi
Hp = 200
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5335991
59 X = 1648156
41
Y = -13633020
01 feet Y = -4137035
37 meter
Z = 16613792
11 Z = 5071837
58
XDOT = 19915
711459 XDOT = 6012
348716
YDOT = 14492
057927 feet/sec YDOT = 4484
737091 meter/sec
ZDOT = 5480
936480 ZDOT = 1699
937458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12548449
47 X = -3824767
40
Y = 7469137
24 feet Y = 2276593
03 meter
Z = 16646276
88 Z = 5073785
19
XDOT = -6106
621125 XDOT = -1861
298119
YDOT = -22772
410579 feet/sec YDOT = -6941
030745 meter/sec
ZDOT = 5600
070590 ZDOT = 1706
901516
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 11226
55100310
00016717 00000-0 10270-3 0 9048
2 25544 51
6362 226
9931 0012725 74
9063 285
3500 15
60356551 10026
Satellite: ISS
Catalog Number: 25544
Epoch time: 11226
55100310 = yrday
fracday
Element set: 904
Inclination: 51
6362 deg
RA of node: 226
9931 deg
Eccentricity:
0012725
Arg of perigee: 74
9063 deg
Mean anomaly: 285
3500 deg
Mean motion: 15
60356551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1002
Checksum: 268
Coasting Arc #6 (Orbit 1016)
---------------------------------------
Vector Time (GMT): 2011/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4669928
97 A = 6761378
44 meter
Y = 1010473
75 meter E =
0023540
Z = -4804823
63 I = 51
39351
XDOT = -3902
152191 Wp = 92
62480
YDOT = -6092
111809 meter/sec RA = 221
20409 deg
ZDOT = 2521
046703 TA = 202
22746
MA = 202
32967
Ha = 215
850 n
mi
Hp = 200
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15321289
27 X = -4657540
75
Y = 3315202
60 feet Y = 958320
92 meter
Z = -15763857
07 Z = -4827479
59
XDOT = -12802
336585 XDOT = -3845
985518
YDOT = -19987
243467 feet/sec YDOT = -6135
433960 meter/sec
ZDOT = 8271
150600 ZDOT = 2502
227011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14127177
84 X = 4305963
81
Y = 6575864
83 feet Y = 2004323
60 meter
Z = -15855992
90 Z = -4832906
63
XDOT = -1384
753579 XDOT = -422
072891
YDOT = 22658
865009 feet/sec YDOT = 6906
422055 meter/sec
ZDOT = 8194
861673 ZDOT = 2497
793838
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 11227
51167325
00016717 00000-0 10270-3 0 9055
2 25544 51
6365 222
1587 0012679 78
0440 282
2136 15
60345754 10176
Satellite: ISS
Catalog Number: 25544
Epoch time: 11227
51167325 = yrday
fracday
Element set: 905
Inclination: 51
6365 deg
RA of node: 222
1587 deg
Eccentricity:
0012679
Arg of perigee: 78
0440 deg
Mean anomaly: 282
2136 deg
Mean motion: 15
60345754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1017
Checksum: 295
Coasting Arc #7 (Orbit 1032)
---------------------------------------
Vector Time (GMT): 2011/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5997272
75 A = 6769163
74 meter
Y = 2288510
21 meter E =
0025835
Z = 2120925
76 I = 51
44338
XDOT = -83
941010 Wp = 96
32859
YDOT = 5366
428145 meter/sec RA = 216
15557 deg
ZDOT = -5498
363236 TA = 60
01876
MA = 59
76258
Ha = 215
748 n
mi
Hp = 200
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19676091
71 X = 5960933
56
Y = 7508235
59 feet Y = 2355372
25 meter
Z = 6958417
86 Z = 2149971
66
XDOT = -275
397013 XDOT = -117
233636
YDOT = 17606
391551 feet/sec YDOT = 5365
303154 meter/sec
ZDOT = -18039
249462 ZDOT = -5498
852038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11391879
76 X = -3472244
95
Y = -17666100
10 feet Y = -5384627
31 meter
Z = 7076422
03 Z = 2156893
43
XDOT = 9258
028207 XDOT = 2821
846997
YDOT = -13267
479180 feet/sec YDOT = -4043
927654 meter/sec
ZDOT = -18041
420855 ZDOT = -5499
025077
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 11228
53638097
00016717 00000-0 10270-3 0 9068
2 25544 51
6362 217
0004 0012694 81
2285 279
0308 15
60405290 10335
Satellite: ISS
Catalog Number: 25544
Epoch time: 11228
53638097 = yrday
fracday
Element set: 906
Inclination: 51
6362 deg
RA of node: 217
0004 deg
Eccentricity:
0012694
Arg of perigee: 81
2285 deg
Mean anomaly: 279
0308 deg
Mean motion: 15
60405290 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1033
Checksum: 287
Coasting Arc #8 (Orbit 1048)
---------------------------------------
Vector Time (GMT): 2011/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4893602
25 A = 6770065
83 meter
Y = -4399185
26 meter E =
0025987
Z = 1550095
20 I = 51
47169
XDOT = 4306
410848 Wp = 73
83014
YDOT = -2741
010770 meter/sec RA = 211
14358 deg
ZDOT = 5743
432730 TA = 303
21337
MA = 303
46224
Ha = 215
725 n
mi
Hp = 200
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16055125
50 X = -4851575
98
Y = -14433022
49 feet Y = -4453673
47 meter
Z = 5085614
18 Z = 1526424
63
XDOT = 14128
644514 XDOT = 4308
841131
YDOT = -8992
817486 feet/sec YDOT = -2692
840087 meter/sec
ZDOT = 18843
283236 ZDOT = 5764
358969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4798773
72 X = 1462666
23
Y = 21071759
86 feet Y = 6422672
41 meter
Z = 4989526
21 Z = 1520807
59
XDOT = -15097
958999 XDOT = -4601
857903
YDOT = -1101
297709 feet/sec YDOT = -335
675542 meter/sec
ZDOT = 18928
453379 ZDOT = 5769
392590
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 11229
56108062
00016717 00000-0 10270-3 0 9077
2 25544 51
6363 211
8442 0012611 86
2894 273
9704 15
60439910 10490
Satellite: ISS
Catalog Number: 25544
Epoch time: 11229
56108062 = yrday
fracday
Element set: 907
Inclination: 51
6363 deg
RA of node: 211
8442 deg
Eccentricity:
0012611
Arg of perigee: 86
2894 deg
Mean anomaly: 273
9704 deg
Mean motion: 15
60439910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1049
Checksum: 301
Coasting Arc #9 (Orbit 1063)
---------------------------------------
Vector Time (GMT): 2011/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1584508
85 A = 6762502
59 meter
Y = 4788741
13 meter E =
0022112
Z = -4525052
71 I = 51
47247
XDOT = -6965
267025 Wp = 80
80856
YDOT = -640
798734 meter/sec RA = 206
10639 deg
ZDOT = -3126
730322 TA = 157
79591
MA = 157
70000
Ha = 215
826 n
mi
Hp = 200
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5198519
84 X = 1552824
10
Y = 15711092
95 feet Y = 4806282
80 meter
Z = -14845973
47 Z = -4517432
34
XDOT = -22851
925934 XDOT = -6942
394882
YDOT = -2102
358052 feet/sec YDOT = -718
560800 meter/sec
ZDOT = -10258
301582 ZDOT = -3160
511657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4480682
56 X = 1365712
04
Y = -15959349
55 feet Y = -4864409
74 meter
Z = -14815148
47 Z = -4515657
25
XDOT = 16481
667173 XDOT = 5023
612154
YDOT = 14248
325243 feet/sec YDOT = 4342
889534 meter/sec
ZDOT = -10395
631513 ZDOT = -3168
588485
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 11230
52173326
00016717 00000-0 10270-3 0 9081
2 25544 51
6364 207
0081 0012699 88
7899 271
4712 15
60392403 10649
Satellite: ISS
Catalog Number: 25544
Epoch time: 11230
52173326 = yrday
fracday
Element set: 908
Inclination: 51
6364 deg
RA of node: 207
0081 deg
Eccentricity:
0012699
Arg of perigee: 88
7899 deg
Mean anomaly: 271
4712 deg
Mean motion: 15
60392403 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1064
Checksum: 304
Coasting Arc #10 (Orbit 1079)
---------------------------------------
Vector Time (GMT): 2011/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2555578
62 A = 6759423
27 meter
Y = -3454338
49 meter E =
0015654
Z = 5204621
77 I = 51
49020
XDOT = 6783
695224 Wp = 85
07599
YDOT = 3477
272089 meter/sec RA = 201
03284 deg
ZDOT = -1019
095885 TA = 14
69614
MA = 14
65068
Ha = 215
682 n
mi
Hp = 200
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8384444
29 X = 2568732
86
Y = -11333131
52 feet Y = -3425686
81 meter
Z = 17075530
74 Z = 5217068
68
XDOT = 22256
217928 XDOT = 6749
258053
YDOT = 11408
372997 feet/sec YDOT = 3552
938946 meter/sec
ZDOT = -3343
490435 ZDOT = -986
224666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13143324
47 X = -4006085
30
Y = 4925129
22 feet Y = 1501179
39 meter
Z = 17126256
16 Z = 5220082
88
XDOT = -11996
231073 XDOT = -3656
451231
YDOT = -20806
454835 feet/sec YDOT = -6341
807434 meter/sec
ZDOT = -3209
944090 ZDOT = -978
390958
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 11231
54641968
00016717 00000-0 10270-3 0 9097
2 25544 51
6364 201
8514 0012578 92
1553 268
1043 15
60410683 10803
Satellite: ISS
Catalog Number: 25544
Epoch time: 11231
54641968 = yrday
fracday
Element set: 909
Inclination: 51
6364 deg
RA of node: 201
8514 deg
Eccentricity:
0012578
Arg of perigee: 92
1553 deg
Mean anomaly: 268
1043 deg
Mean motion: 15
60410683 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1080
Checksum: 294
Coasting Arc #11 (Orbit 1094)
---------------------------------------
Vector Time (GMT): 2011/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5782664
26 A = 6766248
58 meter
Y = 1111401
67 meter E =
0017428
Z = -3349144
97 I = 51
54192
XDOT = -3627
140308 Wp = 94
00887
YDOT = -4888
406958 meter/sec RA = 195
97563 deg
ZDOT = 4660
190025 TA = 226
84110
MA = 226
98691
Ha = 215
743 n
mi
Hp = 200
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18971995
59 X = -5778392
95
Y = 3646330
95 feet Y = 1046760
26 meter
Z = -10988008
45 Z = -3377226
60
XDOT = -11900
066626 XDOT = -3594
845817
YDOT = -16038
080572 feet/sec YDOT = -4928
787268 meter/sec
ZDOT = 15289
337353 ZDOT = 4642
647961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17926568
17 X = 5464017
98
Y = 7024747
80 feet Y = 2141143
13 meter
Z = -11102240
66 Z = -3383962
95
XDOT = 2074
282053 XDOT = 632
241170
YDOT = 18656
817720 feet/sec YDOT = 5686
598041 meter/sec
ZDOT = 15218
162627 ZDOT = 4638
495969
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 11232
50705614
00016717 00000-0 10270-3 0 9105
2 25544 51
6365 197
0169 0012624 95
3771 264
8825 15
60407571 10954
Satellite: ISS
Catalog Number: 25544
Epoch time: 11232
50705614 = yrday
fracday
Element set: 910
Inclination: 51
6365 deg
RA of node: 197
0169 deg
Eccentricity:
0012624
Arg of perigee: 95
3771 deg
Mean anomaly: 264
8825 deg
Mean motion: 15
60407571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1095
Checksum: 303
Coasting Arc #12 (Orbit 1110)
---------------------------------------
Vector Time (GMT): 2011/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6598303
93 A = 6771030
58 meter
Y = 1470840
48 meter E =
0023025
Z = -238489
71 I = 51
58808
XDOT = -1230
190813 Wp = 117
40257
YDOT = 4617
611336 meter/sec RA = 190
96351 deg
ZDOT = -6012
259419 TA = 65
17631
MA = 64
93702
Ha = 215
697 n
mi
Hp = 200
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21647978
76 X = 6582524
83
Y = 4825592
13 feet Y = 1544538
52 meter
Z = -782446
54 Z = -206473
68
XDOT = -4036
059099 XDOT = -1252
528145
YDOT = 15149
643491 feet/sec YDOT = 4603
729749 meter/sec
ZDOT = -19725
260562 ZDOT = -6018
289861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15986549
83 X = -4872700
39
Y = -15379801
45 feet Y = -4687763
48 meter
Z = -652286
84 Z = -198817
03
XDOT = 10100
902403 XDOT = 3078
755052
YDOT = -9737
667639 feet/sec YDOT = -2968
041096 meter/sec
ZDOT = -19749
938964 ZDOT = -6019
781396
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 11233
53172753
00016717 00000-0 10270-3 0 9112
2 25544 51
6371 191
8589 0012538 99
0803 261
1773 15
60439366 11118
Satellite: ISS
Catalog Number: 25544
Epoch time: 11233
53172753 = yrday
fracday
Element set: 911
Inclination: 51
6371 deg
RA of node: 191
8589 deg
Eccentricity:
0012538
Arg of perigee: 99
0803 deg
Mean anomaly: 261
1773 deg
Mean motion: 15
60439366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1111
Checksum: 304
Coasting Arc #13 (Orbit 1126)
---------------------------------------
Vector Time (GMT): 2011/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4575577
07 A = 6765336
59 meter
Y = -3380819
29 meter E =
0024357
Z = 3643897
26 I = 51
59937
XDOT = 5631
071403 Wp = 99
18378
YDOT = -2888
942808 meter/sec RA = 185
95136 deg
ZDOT = 4361
833052 TA = 304
30627
MA = 304
53658
Ha = 215
649 n
mi
Hp = 200
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15011735
80 X = -4555133
27
Y = -11091926
80 feet Y = -3431871
95 meter
Z = 11955043
51 Z = 3621718
89
XDOT = 18474
643710 XDOT = 5641
768793
YDOT = -9478
158820 feet/sec YDOT = -2825
913005 meter/sec
ZDOT = 14310
475894 ZDOT = 4389
214491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7414429
14 X = 2259918
00
Y = 17191724
80 feet Y = 5240037
72 meter
Z = 11864946
53 Z = 3616435
70
XDOT = -19403
408337 XDOT = -5914
158861
YDOT = -1650
414207 feet/sec YDOT = -503
046250 meter/sec
ZDOT = 14421
944350 ZDOT = 4395
808638
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 11234
55638981
00016717 00000-0 10270-3 0 9126
2 25544 51
6373 186
7027 0012475 103
5575 256
6972 15
60479172 11273
Satellite: ISS
Catalog Number: 25544
Epoch time: 11234
55638981 = yrday
fracday
Element set: 912
Inclination: 51
6373 deg
RA of node: 186
7027 deg
Eccentricity:
0012475
Arg of perigee: 103
5575 deg
Mean anomaly: 256
6972 deg
Mean motion: 15
60479172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1127
Checksum: 323
Coasting Arc #14 (Orbit 1141)
---------------------------------------
Vector Time (GMT): 2011/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 506527
91 A = 6759117
19 meter
Y = 4202048
00 meter E =
0026748
Z = -5292689
51 I = 51
60868
XDOT = -7636
890084 Wp = 95
56040
YDOT = 284
626803 meter/sec RA = 180
89453 deg
ZDOT = -509
649684 TA = 169
59725
MA = 169
54180
Ha = 215
582 n
mi
Hp = 200
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1661836
97 X = 485212
78
Y = 13786246
71 feet Y = 4207593
26 meter
Z = -17364466
91 Z = -5290280
49
XDOT = -25055
413663 XDOT = -7637
029487
YDOT = 933
814969 feet/sec YDOT = 199
225670 meter/sec
ZDOT = -1672
079016 ZDOT = -546
749606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5218651
84 X = 1590645
08
Y = -12881124
18 feet Y = -3926166
65 meter
Z = -17354806
95 Z = -5289745
16
XDOT = 21347
198799 XDOT = 6506
626194
YDOT = 11083
739437 feet/sec YDOT = 3378
323780 meter/sec
ZDOT = -1823
009465 ZDOT = -555
653285
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 11235
51700547
00016717 00000-0 10270-3 0 9132
2 25544 51
6374 181
8668 0012418 106
4124 253
8398 15
60452077 11423
Satellite: ISS
Catalog Number: 25544
Epoch time: 11235
51700547 = yrday
fracday
Element set: 913
Inclination: 51
6374 deg
RA of node: 181
8668 deg
Eccentricity:
0012418
Arg of perigee: 106
4124 deg
Mean anomaly: 253
8398 deg
Mean motion: 15
60452077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1142
Checksum: 299
Coasting Arc #15 (Orbit 1157)
---------------------------------------
Vector Time (GMT): 2011/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901745
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3774692
12 A = 6763109
88 meter
Y = -3644474
91 meter E =
0021148
Z = 4248102
13 I = 51
65329
XDOT = 6366
099308 Wp = 93
95284
YDOT = 2387
355568 meter/sec RA = 175
83326 deg
ZDOT = -3594
594365 TA = 32
69334
MA = 32
56261
Ha = 215
450 n
mi
Hp = 200
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12384160
51 X = 3794528
61
Y = -11956938
67 feet Y = -3602153
19 meter
Z = 13937342
94 Z = 4266487
39
XDOT = 20886
152584 XDOT = 6356
391917
YDOT = 7832
531392 feet/sec YDOT = 2458
490994 meter/sec
ZDOT = -11793
288599 ZDOT = -3563
691833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16503987
56 X = -5030415
41
Y = 4675487
99 feet Y = 1425088
74 meter
Z = 14012264
24 Z = 4270938
14
XDOT = -14377
137132 XDOT = -4382
151398
YDOT = -15646
016980 feet/sec YDOT = -4768
905975 meter/sec
ZDOT = -11667
640869 ZDOT = -3556
296937
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 11236
54165319
00016717 00000-0 10270-3 0 9149
2 25544 51
6378 176
7099 0012417 110
0431 250
2062 15
60477641 11589
Satellite: ISS
Catalog Number: 25544
Epoch time: 11236
54165319 = yrday
fracday
Element set: 914
Inclination: 51
6378 deg
RA of node: 176
7099 deg
Eccentricity:
0012417
Arg of perigee: 110
0431 deg
Mean anomaly: 250
2062 deg
Mean motion: 15
60477641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1158
Checksum: 292
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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