[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 10th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11302 11 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 134 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 300 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 3593)
---------------------------------------
Vector Time (GMT): 2012/284/12:57:13
684
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4093186
20 A = 6788089
82 meter
Y = 1604383
88 meter E =
0025783
Z = -5188878
40 I = 51
27611
XDOT = -1339
709843 Wp = 120
64069
YDOT = -7424
648351 meter/sec RA = 267
44535 deg
ZDOT = -1256
421819 TA = 137
30458
MA = 137
10395
Ha = 232
210 n
mi
Hp = 215
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13429088
57 X = -4085615
93
Y = 5263726
62 feet Y = 1558653
15 meter
Z = -17023879
28 Z = -5208744
83
XDOT = -4395
373500 XDOT = -1250
482845
YDOT = -24359
082516 feet/sec YDOT = -7439
131045 meter/sec
ZDOT = -4122
118828 ZDOT = -1262
712690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8301948
89 X = 2530434
02
Y = -11675470
11 feet Y = -3558683
29 meter
Z = -17106161
06 Z = -5213957
89
XDOT = 16091
092510 XDOT = 4904
564997
YDOT = 17434
221239 feet/sec YDOT = 5313
950634 meter/sec
ZDOT = -4147
398315 ZDOT = -1264
127006
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 12284
55808960
00016717 00000-0 10270-3 0 9005
2 25544 51
6452 268
1577 0017592 151
7126 208
4984 15
50628051 35947
Satellite: ISS
Catalog Number: 25544
Epoch time: 12284
55808960 = yrday
fracday
Element set: 900
Inclination: 51
6452 deg
RA of node: 268
1577 deg
Eccentricity:
0017592
Arg of perigee: 151
7126 deg
Mean anomaly: 208
4984 deg
Mean motion: 15
50628051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3594
Checksum: 326
Coasting Arc #2 (Orbit 3609)
---------------------------------------
Vector Time (GMT): 2012/285/12:57:13
684
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4080896
59 A = 6787591
59 meter
Y = -1300728
33 meter E =
0019879
Z = 5258531
69 I = 51
27722
XDOT = 1520
600502 Wp = 150
01018
YDOT = 7488
562877 meter/sec RA = 262
45835 deg
ZDOT = 654
270065 TA = 293
60792
MA = 293
81653
Ha = 231
957 n
mi
Hp = 215
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13388768
33 X = 4069593
30
Y = -4267481
41 feet Y = -1255155
81 meter
Z = 17252400
57 Z = 5278329
38
XDOT = 4988
846791 XDOT = 1433
570489
YDOT = 24568
775844 feet/sec YDOT = 7505
080643 meter/sec
ZDOT = 2146
555330 ZDOT = 661
444910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8622675
42 X = -2628191
47
Y = 10967451
14 feet Y = 3342879
11 meter
Z = 17334368
30 Z = 5283515
46
XDOT = -17069
689861 XDOT = -5202
841470
YDOT = -16951
641134 feet/sec YDOT = -5166
860218 meter/sec
ZDOT = 2175
496224 ZDOT = 663
091249
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 12285
58922731
00016717 00000-0 10270-3 0 9013
2 25544 51
6452 263
0451 0017466 155
6563 204
5426 15
50666202 36107
Satellite: ISS
Catalog Number: 25544
Epoch time: 12285
58922731 = yrday
fracday
Element set: 901
Inclination: 51
6452 deg
RA of node: 263
0451 deg
Eccentricity:
0017466
Arg of perigee: 155
6563 deg
Mean anomaly: 204
5426 deg
Mean motion: 15
50666202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3610
Checksum: 294
Coasting Arc #3 (Orbit 3624)
---------------------------------------
Vector Time (GMT): 2012/286/12:57:13
684
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4157631
06 A = 6787435
99 meter
Y = 902408
95 meter E =
0026651
Z = -5306918
37 I = 51
28198
XDOT = -1652
343678 Wp = 127
84754
YDOT = -7466
524322 meter/sec RA = 257
46825 deg
ZDOT = 8
872583 TA = 142
33117
MA = 142
14425
Ha = 231
905 n
mi
Hp = 215
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13640521
84 X = -4141632
84
Y = 2960659
28 feet Y = 856004
51 meter
Z = -17411149
50 Z = -5327077
46
XDOT = -5421
075060 XDOT = -1568
771742
YDOT = -24496
470874 feet/sec YDOT = -7484
534584 meter/sec
ZDOT = 29
109525 ZDOT = 1
049405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9387804
82 X = 2861402
91
Y = -10187565
70 feet Y = -3105170
02 meter
Z = -17494573
22 Z = -5332345
92
XDOT = 17749
718193 XDOT = 5410
114105
YDOT = 16270
944595 feet/sec YDOT = 4959
383912 meter/sec
ZDOT = -2
525672 ZDOT = -
769825
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 12286
55590446
00016717 00000-0 10270-3 0 9026
2 25544 51
6455 258
2501 0017455 159
1660 201
0206 15
50674960 36251
Satellite: ISS
Catalog Number: 25544
Epoch time: 12286
55590446 = yrday
fracday
Element set: 902
Inclination: 51
6455 deg
RA of node: 258
2501 deg
Eccentricity:
0017455
Arg of perigee: 159
1660 deg
Mean anomaly: 201
0206 deg
Mean motion: 15
50674960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3625
Checksum: 301
Coasting Arc #4 (Orbit 3640)
---------------------------------------
Vector Time (GMT): 2012/287/12:57:13
684
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4237172
78 A = 6787439
73 meter
Y = -585611
79 meter E =
0017249
Z = 5261788
51 I = 51
29047
XDOT = 1805
391836 Wp = 153
22768
YDOT = 7427
344969 meter/sec RA = 252
48111 deg
ZDOT = -641
516828 TA = 302
84207
MA = 303
00802
Ha = 231
655 n
mi
Hp = 215
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13901485
51 X = 4217845
28
Y = -1921298
52 feet Y = -538336
46 meter
Z = 17263085
65 Z = 5282325
98
XDOT = 5923
201562 XDOT = 1725
319931
YDOT = 24367
929688 feet/sec YDOT = 7447
086198 meter/sec
ZDOT = -2104
714001 ZDOT = -632
941623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10033824
18 X = -3058309
61
Y = 9660462
78 feet Y = 2944509
05 meter
Z = 17348044
41 Z = 5287683
94
XDOT = -18418
023290 XDOT = -5613
813499
YDOT = -15496
579770 feet/sec YDOT = -4723
357514 meter/sec
ZDOT = -2069
956649 ZDOT = -630
922787
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 12287
58701207
00016717 00000-0 10270-3 0 9030
2 25544 51
6460 253
1373 0017395 162
9646 197
2093 15
50709124 36416
Satellite: ISS
Catalog Number: 25544
Epoch time: 12287
58701207 = yrday
fracday
Element set: 903
Inclination: 51
6460 deg
RA of node: 253
1373 deg
Eccentricity:
0017395
Arg of perigee: 162
9646 deg
Mean anomaly: 197
2093 deg
Mean motion: 15
50709124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3641
Checksum: 310
Coasting Arc #5 (Orbit 3655)
---------------------------------------
Vector Time (GMT): 2012/288/12:57:13
684
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4406413
38 A = 6787856
29 meter
Y = 202639
02 meter E =
0026228
Z = -5178415
27 I = 51
30243
XDOT = -1888
971871 Wp = 137
51002
YDOT = -7293
434623 meter/sec RA = 247
49201 deg
ZDOT = 1306
901363 TA = 145
22564
MA = 145
05394
Ha = 231
582 n
mi
Hp = 215
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14456736
80 X = -4383195
70
Y = 664826
19 feet Y = 153492
95 meter
Z = -16989551
43 Z = -5199765
53
XDOT = -6197
414275 XDOT = -1813
623542
YDOT = -23928
591284 feet/sec YDOT = -7314
136833 meter/sec
ZDOT = 4287
734130 ZDOT = 1297
908524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11066808
79 X = 3373163
32
Y = -9162823
81 feet Y = -2792828
70 meter
Z = -17077836
33 Z = -5205324
51
XDOT = 18696
041157 XDOT = 5698
553345
YDOT = 14565
851306 feet/sec YDOT = 4439
671478 meter/sec
ZDOT = 4251
231166 ZDOT = 1295
775259
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 12288
55366055
00016717 00000-0 10270-3 0 9047
2 25544 51
6463 248
3421 0017349 166
6446 193
5167 15
50725069 36560
Satellite: ISS
Catalog Number: 25544
Epoch time: 12288
55366055 = yrday
fracday
Element set: 904
Inclination: 51
6463 deg
RA of node: 248
3421 deg
Eccentricity:
0017349
Arg of perigee: 166
6446 deg
Mean anomaly: 193
5167 deg
Mean motion: 15
50725069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3656
Checksum: 331
Coasting Arc #6 (Orbit 3671)
---------------------------------------
Vector Time (GMT): 2012/289/12:57:13
684
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4568877
79 A = 6788401
92 meter
Y = 91853
91 meter E =
0015873
Z = 5009120
81 I = 51
31795
XDOT = 1971
954010 Wp = 151
27795
YDOT = 7155
406829 meter/sec RA = 242
50670 deg
ZDOT = -1940
961601 TA = 317
57183
MA = 317
69444
Ha = 231
330 n
mi
Hp = 216
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14989756
52 X = 4543177
27
Y = 301357
96 feet Y = 142802
75 meter
Z = 16434123
38 Z = 5031254
34
XDOT = 6469
665387 XDOT = 1901
223195
YDOT = 23475
744189 feet/sec YDOT = 7177
062779 meter/sec
ZDOT = -6367
984255 ZDOT = -1931
554210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11924786
42 X = -3634674
90
Y = 8920050
24 feet Y = 2718831
31 meter
Z = 16525622
55 Z = 5037009
75
XDOT = -18921
365684 XDOT = -5767
232260
YDOT = -13635
472800 feet/sec YDOT = -4156
092110 meter/sec
ZDOT = -6329
750629 ZDOT = -1929
307992
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 12289
58473763
00016717 00000-0 10270-3 0 9057
2 25544 51
6471 243
2293 0017345 170
3494 189
7993 15
50753511 36726
Satellite: ISS
Catalog Number: 25544
Epoch time: 12289
58473763 = yrday
fracday
Element set: 905
Inclination: 51
6471 deg
RA of node: 243
2293 deg
Eccentricity:
0017345
Arg of perigee: 170
3494 deg
Mean anomaly: 189
7993 deg
Mean motion: 15
50753511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3672
Checksum: 337
Coasting Arc #7 (Orbit 3686)
---------------------------------------
Vector Time (GMT): 2012/290/12:57:13
684
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4812539
15 A = 6789326
80 meter
Y = -423472
20 meter E =
0024306
Z = -4789831
07 I = 51
33639
XDOT = -1967
271026 Wp = 148
88597
YDOT = -6926
327223 meter/sec RA = 237
52071 deg
ZDOT = 2574
448586 TA = 146
73284
MA = 146
57982
Ha = 231
247 n
mi
Hp = 216
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15789170
43 X = -4784177
55
Y = -1389344
49 feet Y = -477130
78 meter
Z = -15714668
86 Z = -4813141
89
XDOT = -6454
301267 XDOT = -1902
179613
YDOT = -22724
170678 feet/sec YDOT = -6947
962344 meter/sec
ZDOT = 8446
353628 ZDOT = 2565
050016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13078607
99 X = 3986359
71
Y = -8782992
99 feet Y = -2677056
26 meter
Z = -15811010
27 Z = -4819195
93
XDOT = 18703
401261 XDOT = 5700
796704
YDOT = 12629
552183 feet/sec YDOT = 3849
487505 meter/sec
ZDOT = 8408
132616 ZDOT = 2562
798821
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 12290
55135710
00016717 00000-0 10270-3 0 9064
2 25544 51
6474 238
4343 0017291 174
0505 186
0855 15
50778350 36876
Satellite: ISS
Catalog Number: 25544
Epoch time: 12290
55135710 = yrday
fracday
Element set: 906
Inclination: 51
6474 deg
RA of node: 238
4343 deg
Eccentricity:
0017291
Arg of perigee: 174
0505 deg
Mean anomaly: 186
0855 deg
Mean motion: 15
50778350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3687
Checksum: 314
Coasting Arc #8 (Orbit 3702)
---------------------------------------
Vector Time (GMT): 2012/291/12:57:13
684
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5034224
57 A = 6790349
44 meter
Y = 663885
47 meter E =
0016508
Z = 4493067
86 I = 51
35763
XDOT = 1942
283180 Wp = 147
73745
YDOT = 6709
479661 meter/sec RA = 232
53896 deg
ZDOT = -3175
894416 TA = 334
22180
MA = 334
30397
Ha = 230
985 n
mi
Hp = 216
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16516484
81 X = 5004599
82
Y = 2178101
92 feet Y = 720015
87 meter
Z = 14741036
29 Z = 4517452
55
XDOT = 6372
320144 XDOT = 1882
540211
YDOT = 22012
728546 feet/sec YDOT = 6730
865301 meter/sec
ZDOT = -10419
601104 ZDOT = -3166
604060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13994113
15 X = -4265405
69
Y = 8872553
52 feet Y = 2704354
31 meter
Z = 14841803
83 Z = 4523781
81
XDOT = -18417
321142 XDOT = -5613
599484
YDOT = -11727
265677 feet/sec YDOT = -3574
470578 meter/sec
ZDOT = -10381
804538 ZDOT = -3164
374023
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 12291
58240307
00016717 00000-0 10270-3 0 9078
2 25544 51
6478 233
3215 0017309 177
7624 182
3607 15
50798481 37034
Satellite: ISS
Catalog Number: 25544
Epoch time: 12291
58240307 = yrday
fracday
Element set: 907
Inclination: 51
6478 deg
RA of node: 233
3215 deg
Eccentricity:
0017309
Arg of perigee: 177
7624 deg
Mean anomaly: 182
3607 deg
Mean motion: 15
50798481 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3703
Checksum: 316
Coasting Arc #9 (Orbit 3717)
---------------------------------------
Vector Time (GMT): 2012/292/12:57:13
684
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5320053
50 A = 6791601
30 meter
Y = -915896
86 meter E =
0020979
Z = -4140945
83 I = 51
38142
XDOT = -1818
387679 Wp = 161
24127
YDOT = -6417
063022 meter/sec RA = 227
55758 deg
ZDOT = 3741
338507 TA = 147
59060
MA = 147
46158
Ha = 230
895 n
mi
Hp = 216
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17454243
76 X = -5289300
10
Y = -3004910
97 feet Y = -975217
17 meter
Z = -13585780
29 Z = -4166716
29
XDOT = -5965
838841 XDOT = -1764
670593
YDOT = -21053
356373 feet/sec YDOT = -6437
096927 meter/sec
ZDOT = 12274
732636 ZDOT = 3732
635297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15094864
78 X = 4600914
78
Y = -9106066
89 feet Y = -2775529
19 meter
Z = -13692265
86 Z = -4173402
63
XDOT = 17689
741796 XDOT = 5391
833299
YDOT = 10850
921699 feet/sec YDOT = 3307
360934 meter/sec
ZDOT = 12239
332567 ZDOT = 3730
548566
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 12292
54899308
00016717 00000-0 10270-3 0 9087
2 25544 51
6479 228
5266 0017268 181
4018 178
7087 15
50833749 37184
Satellite: ISS
Catalog Number: 25544
Epoch time: 12292
54899308 = yrday
fracday
Element set: 908
Inclination: 51
6479 deg
RA of node: 228
5266 deg
Eccentricity:
0017268
Arg of perigee: 181
4018 deg
Mean anomaly: 178
7087 deg
Mean motion: 15
50833749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3718
Checksum: 355
Coasting Arc #10 (Orbit 3733)
---------------------------------------
Vector Time (GMT): 2012/293/12:57:13
684
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5564334
02 A = 6792923
34 meter
Y = 1079949
84 meter E =
0018819
Z = 3721089
04 I = 51
40700
XDOT = 1658
750098 Wp = 148
22972
YDOT = 6155
282812 meter/sec RA = 222
58037 deg
ZDOT = -4272
657794 TA = 347
17072
MA = 347
21854
Ha = 230
626 n
mi
Hp = 217
085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18255689
05 X = 5533767
69
Y = 3543142
51 feet Y = 1142002
85 meter
Z = 12208297
38 Z = 3748046
57
XDOT = 5442
093496 XDOT = 1610
553154
YDOT = 20194
497416 feet/sec YDOT = 6173
562439 meter/sec
ZDOT = -14017
906147 ZDOT = -4264
716679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15898167
87 X = -4845761
57
Y = 9504738
32 feet Y = 2897044
24 meter
Z = 12319690
52 Z = 3755041
67
XDOT = -16907
999581 XDOT = -5153
558272
YDOT = -10178
211022 feet/sec YDOT = -3102
318719 meter/sec
ZDOT = -13985
627408 ZDOT = -4262
819234
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 12293
58000747
00016717 00000-0 10270-3 0 9094
2 25544 51
6477 223
4134 0017280 185
1437 174
9539 15
50841937 37346
Satellite: ISS
Catalog Number: 25544
Epoch time: 12293
58000747 = yrday
fracday
Element set: 909
Inclination: 51
6477 deg
RA of node: 223
4134 deg
Eccentricity:
0017280
Arg of perigee: 185
1437 deg
Mean anomaly: 174
9539 deg
Mean motion: 15
50841937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3734
Checksum: 324
Coasting Arc #11 (Orbit 3748)
---------------------------------------
Vector Time (GMT): 2012/294/12:57:13
684
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5849443
38 A = 6794224
96 meter
Y = -1237197
20 meter E =
0016639
Z = -3247506
60 I = 51
43501
XDOT = -1400
084279 Wp = 173
55796
YDOT = -5842
281825 meter/sec RA = 217
60438 deg
ZDOT = 4733
747468 TA = 148
82096
MA = 148
72214
Ha = 230
512 n
mi
Hp = 217
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19191087
19 X = -5819398
15
Y = -4059045
94 feet Y = -1302441
40 meter
Z = -10654549
20 Z = -3275850
33
XDOT = -4593
452359 XDOT = -1357
646416
YDOT = -19167
591291 feet/sec YDOT = -5857
701070 meter/sec
ZDOT = 15530
667547 ZDOT = 4727
049015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16775666
22 X = 5113223
06
Y = -10041967
43 feet Y = -3060791
67 meter
Z = -10771676
44 Z = -3283206
98
XDOT = 15747
309707 XDOT = 4799
779999
YDOT = 9628
570570 feet/sec YDOT = 2934
788310 meter/sec
ZDOT = 15503
492285 ZDOT = 4725
464448
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 12294
54656752
00016717 00000-0 10270-3 0 9106
2 25544 51
6479 218
6182 0017252 188
8149 171
2701 15
50888696 37496
Satellite: ISS
Catalog Number: 25544
Epoch time: 12294
54656752 = yrday
fracday
Element set: 910
Inclination: 51
6479 deg
RA of node: 218
6182 deg
Eccentricity:
0017252
Arg of perigee: 188
8149 deg
Mean anomaly: 171
2701 deg
Mean motion: 15
50888696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3749
Checksum: 346
Coasting Arc #12 (Orbit 3764)
---------------------------------------
Vector Time (GMT): 2012/295/12:57:13
684
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6071198
98 A = 6795573
93 meter
Y = 1316904
12 meter E =
0021577
Z = 2718059
39 I = 51
46383
XDOT = 1096
657902 Wp = 154
28973
YDOT = 5578
606260 meter/sec RA = 212
63237 deg
ZDOT = -5156
072278 TA = 354
88393
MA = 354
90595
Ha = 230
263 n
mi
Hp = 217
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19918631
83 X = 6042817
99
Y = 4320551
59 feet Y = 1384637
46 meter
Z = 8917517
68 Z = 2747484
35
XDOT = 3597
958996 XDOT = 1059
242574
YDOT = 18302
513975 feet/sec YDOT = 5590
660416 meter/sec
ZDOT = -16916
247630 ZDOT = -5150
835754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17313730
93 X = -5277225
19
Y = 10652234
97 feet Y = 3246801
22 meter
Z = 9039125
69 Z = 2755125
51
XDOT = -14575
931984 XDOT = -4442
744069
YDOT = -9364
654713 feet/sec YDOT = -2854
346757 meter/sec
ZDOT = -16895
087898 ZDOT = -5149
622791
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 12295
57755031
00016717 00000-0 10270-3 0 9111
2 25544 51
6476 213
5043 0017269 192
5270 167
5454 15
50881048 37653
Satellite: ISS
Catalog Number: 25544
Epoch time: 12295
57755031 = yrday
fracday
Element set: 911
Inclination: 51
6476 deg
RA of node: 213
5043 deg
Eccentricity:
0017269
Arg of perigee: 192
5270 deg
Mean anomaly: 167
5454 deg
Mean motion: 15
50881048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3765
Checksum: 318
Coasting Arc #13 (Orbit 3779)
---------------------------------------
Vector Time (GMT): 2012/296/12:57:13
684
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6307951
41 A = 6796598
14 meter
Y = -1381062
58 meter E =
0011972
Z = -2143447
55 I = 51
49453
XDOT = -707
539058 Wp = 183
67438
YDOT = -5292
125013 meter/sec RA = 207
66221 deg
ZDOT = 5478
631147 TA = 152
58625
MA = 152
52304
Ha = 230
087 n
mi
Hp = 217
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20695378
65 X = -6281626
77
Y = -4531045
20 feet Y = -1451454
94 meter
Z = -7032308
24 Z = -2174027
58
XDOT = -2321
322368 XDOT = -674
923037
YDOT = -17362
614871 feet/sec YDOT = -5299
854534 meter/sec
ZDOT = 17974
511636 ZDOT = 5475
273392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17835083
90 X = 5436133
57
Y = -11355402
62 feet Y = -3461126
72 meter
Z = -7158703
87 Z = -2181972
94
XDOT = 13141
852093 XDOT = 4005
636518
YDOT = 9290
623180 feet/sec YDOT = 2831
781945 meter/sec
ZDOT = 17961
091604 ZDOT = 5474
540721
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 12296
54408023
00016717 00000-0 10270-3 0 9126
2 25544 51
6482 208
7089 0017228 196
4154 163
6441 15
50940807 37804
Satellite: ISS
Catalog Number: 25544
Epoch time: 12296
54408023 = yrday
fracday
Element set: 912
Inclination: 51
6482 deg
RA of node: 208
7089 deg
Eccentricity:
0017228
Arg of perigee: 196
4154 deg
Mean anomaly: 163
6441 deg
Mean motion: 15
50940807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3780
Checksum: 314
Coasting Arc #14 (Orbit 3795)
---------------------------------------
Vector Time (GMT): 2012/297/12:57:13
684
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6460364
98 A = 6797654
41 meter
Y = 1385724
70 meter E =
0023527
Z = 1527884
98 I = 51
52513
XDOT = 272
810291 Wp = 164
53320
YDOT = 5071
546260 meter/sec RA = 202
69586 deg
ZDOT = -5754
951420 TA = 358
74179
MA = 358
74770
Ha = 229
896 n
mi
Hp = 217
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21195423
16 X = 6436967
17
Y = 4546340
89 feet Y = 1457837
81 meter
Z = 5012746
00 Z = 1559212
53
XDOT = 895
046887 XDOT = 244
035460
YDOT = 16638
931300 feet/sec YDOT = 5074
435741 meter/sec
ZDOT = -18881
074214 ZDOT = -5753
696323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18004935
43 X = -5487904
32
Y = 12017586
74 feet Y = 3662960
44 meter
Z = 5142247
55 Z = 1567357
05
XDOT = -11764
779671 XDOT = -3585
904844
YDOT = -9551
520066 feet/sec YDOT = -2911
303316 meter/sec
ZDOT = -18876
328803 ZDOT = -5753
505019
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 12297
57503175
00016717 00000-0 10270-3 0 9135
2 25544 51
6483 203
5947 0017289 200
0475 159
9999 15
50915499 37968
Satellite: ISS
Catalog Number: 25544
Epoch time: 12297
57503175 = yrday
fracday
Element set: 913
Inclination: 51
6483 deg
RA of node: 203
5947 deg
Eccentricity:
0017289
Arg of perigee: 200
0475 deg
Mean anomaly: 159
9999 deg
Mean motion: 15
50915499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3796
Checksum: 357
Coasting Arc #15 (Orbit 3810)
---------------------------------------
Vector Time (GMT): 2012/298/12:57:13
684
Vector Time (MET): N/A
Weight (LBS) : 876233
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6603986
30 A = 6798095
01 meter
Y = -1376655
47 meter E =
0008008
Z = -881819
02 I = 51
55632
XDOT = 221
173670 Wp = 186
04787
YDOT = -4854
713694 meter/sec RA = 197
73136 deg
ZDOT = 5909
874462 TA = 164
42639
MA = 164
40174
Ha = 229
618 n
mi
Hp = 218
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21666621
73 X = -6583817
70
Y = -4516586
19 feet Y = -1450392
67 meter
Z = -2893107
02 Z = -913852
17
XDOT = 725
635401 XDOT = 246
734473
YDOT = -15927
538367 feet/sec YDOT = -4852
097018 meter/sec
ZDOT = 19389
351911 ZDOT = 5911
011389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18104998
79 X = 5518403
63
Y = -12699103
78 feet Y = -3870686
83 meter
Z = -3025540
97 Z = -922184
89
XDOT = 10274
591608 XDOT = 3131
695522
YDOT = 10018
195708 feet/sec YDOT = 3053
546052 meter/sec
ZDOT = 19394
481963 ZDOT = 5911
438102
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 12298
54153186
00016717 00000-0 10270-3 0 9147
2 25544 51
6488 198
7992 0017199 204
1980 155
8365 15
50990623 38116
Satellite: ISS
Catalog Number: 25544
Epoch time: 12298
54153186 = yrday
fracday
Element set: 914
Inclination: 51
6488 deg
RA of node: 198
7992 deg
Eccentricity:
0017199
Arg of perigee: 204
1980 deg
Mean anomaly: 155
8365 deg
Mean motion: 15
50990623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3811
Checksum: 347
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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