[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 4th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14800 38 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 378 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 423)
---------------------------------------
Vector Time (GMT): 2014/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3113110
72 A = 6790130
01 meter
Y = -2959540
52 meter E =
0012959
Z = -5270145
23 I = 51
42545
XDOT = 5896
151043 Wp = 76
45706
YDOT = -4814
813688 meter/sec RA = 325
43859 deg
ZDOT = -777
701888 TA = 186
06540
MA = 186
08111
Ha = 227
215 n
mi
Hp = 222
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10213617
85 X = -3054184
02
Y = -9709778
62 feet Y = -2994023
73 meter
Z = -17290502
73 Z = -5285125
46
XDOT = 19344
327570 XDOT = 5953
331046
YDOT = -15796
632834 feet/sec YDOT = -4748
559414 meter/sec
ZDOT = -2551
515380 ZDOT = -748
919986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13974481
40 X = -4259421
93
Y = -1065733
28 feet Y = -324835
50 meter
Z = -17353309
69 Z = -5289288
79
XDOT = 4812
754009 XDOT = 1466
927422
YDOT = -23484
643865 feet/sec YDOT = -7158
119450 meter/sec
ZDOT = -2428
965863 ZDOT = -740
348795
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 14122
51740643
00016717 00000-0 10270-3 0 9007
2 25544 51
6450 325
9336 0002391 308
8376 51
2561 15
49813753 4240
Satellite: ISS
Catalog Number: 25544
Epoch time: 14122
51740643 = yrday
fracday
Element set: 900
Inclination: 51
6450 deg
RA of node: 325
9336 deg
Eccentricity:
0002391
Arg of perigee: 308
8376 deg
Mean anomaly: 51
2561 deg
Mean motion: 15
49813753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 424
Checksum: 291
Coasting Arc #2 (Orbit 439)
---------------------------------------
Vector Time (GMT): 2014/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3089236
08 A = 6790042
82 meter
Y = 2926366
99 meter E =
0001096
Z = 5290557
07 I = 51
40038
XDOT = -5659
218151 Wp = 45
10429
YDOT = 5145
481487 meter/sec RA = 320
46850 deg
ZDOT = 459
081418 TA = 40
50309
MA = 40
49493
Ha = 227
205 n
mi
Hp = 222
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10135288
98 X = 3030583
03
Y = 9600941
58 feet Y = 2960584
73 meter
Z = 17357470
70 Z = 5305421
94
XDOT = -18566
988684 XDOT = -5718
565579
YDOT = 16881
500942 feet/sec YDOT = 5081
864636 meter/sec
ZDOT = 1506
172630 ZDOT = 431
445360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13860190
43 X = 4224586
04
Y = 793555
01 feet Y = 241875
57 meter
Z = 17419797
43 Z = 5309554
26
XDOT = -3109
892170 XDOT = -947
895134
YDOT = 23889
586375 feet/sec YDOT = 7281
545927 meter/sec
ZDOT = 1388
411813 ZDOT = 423
187920
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 14123
54910334
00016717 00000-0 10270-3 0 9018
2 25544 51
6454 320
8237 0002377 312
8858 47
2093 15
49798100 4403
Satellite: ISS
Catalog Number: 25544
Epoch time: 14123
54910334 = yrday
fracday
Element set: 901
Inclination: 51
6454 deg
RA of node: 320
8237 deg
Eccentricity:
0002377
Arg of perigee: 312
8858 deg
Mean anomaly: 47
2093 deg
Mean motion: 15
49798100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 440
Checksum: 295
Coasting Arc #3 (Orbit 454)
---------------------------------------
Vector Time (GMT): 2014/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3082364
63 A = 6789832
73 meter
Y = -2919525
52 meter E =
0013325
Z = -5310290
26 I = 51
37580
XDOT = 5381
699767 Wp = 81
44894
YDOT = -5437
856134 meter/sec RA = 315
49547 deg
ZDOT = -132
500379 TA = 187
27135
MA = 187
29070
Ha = 227
254 n
mi
Hp = 221
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10112744
85 X = -3023692
80
Y = -9578495
80 feet Y = -2953666
34 meter
Z = -17422212
15 Z = -5325121
66
XDOT = 17656
495299 XDOT = 5442
750774
YDOT = -17840
735348 feet/sec YDOT = -5377
333155 meter/sec
ZDOT = -434
712529 ZDOT = -106
208394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13839729
67 X = -4218349
60
Y = -553412
31 feet Y = -168680
07 meter
Z = -17484401
16 Z = -5329245
47
XDOT = 1376
192038 XDOT = 419
463333
YDOT = -24053
152589 feet/sec YDOT = -7331
400909 meter/sec
ZDOT = -322
587301 ZDOT = -98
324609
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 14124
51630374
00016717 00000-0 10270-3 0 9020
2 25544 51
6443 316
0321 0002370 316
0772 44
0189 15
49854389 4555
Satellite: ISS
Catalog Number: 25544
Epoch time: 14124
51630374 = yrday
fracday
Element set: 902
Inclination: 51
6443 deg
RA of node: 316
0321 deg
Eccentricity:
0002370
Arg of perigee: 316
0772 deg
Mean anomaly: 44
0189 deg
Mean motion: 15
49854389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 455
Checksum: 289
Coasting Arc #4 (Orbit 470)
---------------------------------------
Vector Time (GMT): 2014/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3067885
46 A = 6789890
14 meter
Y = 2932401
94 meter E =
0002479
Z = 5299439
91 I = 51
35458
XDOT = -5101
145693 Wp = 21
50690
YDOT = 5714
057026 meter/sec RA = 310
52162 deg
ZDOT = -206
441526 TA = 70
48331
MA = 70
45653
Ha = 227
251 n
mi
Hp = 221
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10065241
00 X = 3009123
47
Y = 9620741
28 feet Y = 2966380
39 meter
Z = 17386613
89 Z = 5314200
70
XDOT = -16736
042301 XDOT = -5163
659607
YDOT = 18746
906254 feet/sec YDOT = 5656
663208 meter/sec
ZDOT = -677
301594 ZDOT = -231
374163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13840830
54 X = 4218685
15
Y = 378353
77 feet Y = 115322
23 meter
Z = 17448505
39 Z = 5318304
44
XDOT = 338
214795 XDOT = 103
087870
YDOT = 24116
188530 feet/sec YDOT = 7350
614264 meter/sec
ZDOT = -783
721581 ZDOT = -238
878338
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 14125
54797162
00016717 00000-0 10270-3 0 9034
2 25544 51
6445 310
9221 0002378 320
1857 39
9119 15
49836724 4714
Satellite: ISS
Catalog Number: 25544
Epoch time: 14125
54797162 = yrday
fracday
Element set: 903
Inclination: 51
6445 deg
RA of node: 310
9221 deg
Eccentricity:
0002378
Arg of perigee: 320
1857 deg
Mean anomaly: 39
9119 deg
Mean motion: 15
49836724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 471
Checksum: 312
Coasting Arc #5 (Orbit 485)
---------------------------------------
Vector Time (GMT): 2014/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3080506
06 A = 6789815
37 meter
Y = -2964444
49 meter E =
0013281
Z = -5286328
62 I = 51
33503
XDOT = 4785
927235 Wp = 86
54291
YDOT = -5945
361621 meter/sec RA = 305
54555 deg
ZDOT = 547
086843 TA = 188
69933
MA = 188
72237
Ha = 227
306 n
mi
Hp = 221
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10106647
19 X = -3021448
53
Y = -9725867
73 feet Y = -2998562
46 meter
Z = -17343597
85 Z = -5301149
97
XDOT = 15701
861006 XDOT = 4849
396319
YDOT = -19505
779596 feet/sec YDOT = -5891
487435 meter/sec
ZDOT = 1794
904340 ZDOT = 570
490543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13947831
43 X = -4251299
02
Y = -187888
78 feet Y = -57268
50 meter
Z = -17405743
40 Z = -5305270
59
XDOT = -2034
178705 XDOT = -620
017669
YDOT = -23934
313085 feet/sec YDOT = -7295
178628 meter/sec
ZDOT = 1894
892158 ZDOT = 577
563130
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 14126
51514489
00016717 00000-0 10270-3 0 9042
2 25544 51
6441 306
1307 0002323 324
1171 35
9823 15
49896758 4862
Satellite: ISS
Catalog Number: 25544
Epoch time: 14126
51514489 = yrday
fracday
Element set: 904
Inclination: 51
6441 deg
RA of node: 306
1307 deg
Eccentricity:
0002323
Arg of perigee: 324
1171 deg
Mean anomaly: 35
9823 deg
Mean motion: 15
49896758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 486
Checksum: 308
Coasting Arc #6 (Orbit 501)
---------------------------------------
Vector Time (GMT): 2014/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3089350
50 A = 6790038
50 meter
Y = 3017227
02 meter E =
0004175
Z = 5238926
53 I = 51
31806
XDOT = -4474
397237 Wp = 24
54616
YDOT = 6154
903761 meter/sec RA = 300
56840 deg
ZDOT = -902
259352 TA = 74
15222
MA = 74
10621
Ha = 227
317 n
mi
Hp = 221
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10135664
37 X = 3029932
34
Y = 9899038
79 feet Y = 3051441
94 meter
Z = 17188079
16 Z = 5253789
94
XDOT = -14679
780960 XDOT = -4538
507293
YDOT = 20193
253810 feet/sec YDOT = 6104
509711 meter/sec
ZDOT = -2960
168478 ZDOT = -924
151297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14091627
45 X = 4295128
05
Y = 50604
43 feet Y = 15424
23 meter
Z = 17250397
15 Z = 5257921
05
XDOT = 3669
334398 XDOT = 1118
413125
YDOT = 23655
685367 feet/sec YDOT = 7210
252900 meter/sec
ZDOT = -3053
791483 ZDOT = -930
795644
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 14127
54678348
00016717 00000-0 10270-3 0 9052
2 25544 51
6439 301
0203 0002340 328
5777 31
5234 15
49878143 5022
Satellite: ISS
Catalog Number: 25544
Epoch time: 14127
54678348 = yrday
fracday
Element set: 905
Inclination: 51
6439 deg
RA of node: 301
0203 deg
Eccentricity:
0002340
Arg of perigee: 328
5777 deg
Mean anomaly: 31
5234 deg
Mean motion: 15
49878143 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 502
Checksum: 298
Coasting Arc #7 (Orbit 516)
---------------------------------------
Vector Time (GMT): 2014/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3133378
82 A = 6790117
84 meter
Y = -3079418
99 meter E =
0012736
Z = -5188472
61 I = 51
30431
XDOT = 4136
465289 Wp = 91
29387
YDOT = -6314
884947 meter/sec RA = 295
59009 deg
ZDOT = 1252
293582 TA = 190
79610
MA = 190
82346
Ha = 227
360 n
mi
Hp = 221
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10280114
24 X = -3073506
99
Y = -10103080
69 feet Y = -3114123
77 meter
Z = -17022547
94 Z = -5203548
80
XDOT = 13571
080344 XDOT = 4200
689030
YDOT = -20718
126468 feet/sec YDOT = -6268
269220 meter/sec
ZDOT = 4108
574743 ZDOT = 1272
544248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14337845
86 X = -4370175
42
Y = 152185
77 feet Y = 46386
22 meter
Z = -17085758
46 Z = -5207739
18
XDOT = -5235
654060 XDOT = -1595
827358
YDOT = -23144
685403 feet/sec YDOT = -7054
500111 meter/sec
ZDOT = 4195
276007 ZDOT = 1278
720127
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 14128
51392916
00016717 00000-0 10270-3 0 9065
2 25544 51
6443 296
2292 0002300 332
6253 27
4776 15
49940269 5171
Satellite: ISS
Catalog Number: 25544
Epoch time: 14128
51392916 = yrday
fracday
Element set: 906
Inclination: 51
6443 deg
RA of node: 296
2292 deg
Eccentricity:
0002300
Arg of perigee: 332
6253 deg
Mean anomaly: 27
4776 deg
Mean motion: 15
49940269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 517
Checksum: 310
Coasting Arc #8 (Orbit 532)
---------------------------------------
Vector Time (GMT): 2014/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3177016
31 A = 6790516
64 meter
Y = 3161712
42 meter E =
0005975
Z = 5099533
25 I = 51
29227
XDOT = -3810
530261 Wp = 32
60186
YDOT = 6448
358971 meter/sec RA = 290
61019 deg
ZDOT = -1618
186458 TA = 73
13163
MA = 73
06611
Ha = 227
384 n
mi
Hp = 221
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10423281
87 X = 3116653
01
Y = 10373072
23 feet Y = 3196902
46 meter
Z = 16730752
12 Z = 5114820
24
XDOT = -12501
739701 XDOT = -3874
493336
YDOT = 21156
033368 feet/sec YDOT = 6405
389499 meter/sec
ZDOT = -5309
010689 ZDOT = -1636
853214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14628597
32 X = 4458796
46
Y = -317614
50 feet Y = -96808
90 meter
Z = 16794843
27 Z = 5119068
23
XDOT = 6698
579175 XDOT = 2041
726933
YDOT = 22551
763309 feet/sec YDOT = 6873
777456 meter/sec
ZDOT = -5389
028364 ZDOT = -1642
575845
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 14129
54553819
00016717 00000-0 10270-3 0 9071
2 25544 51
6436 291
1181 0002320 337
4543 22
6506 15
49922818 5337
Satellite: ISS
Catalog Number: 25544
Epoch time: 14129
54553819 = yrday
fracday
Element set: 907
Inclination: 51
6436 deg
RA of node: 291
1181 deg
Eccentricity:
0002320
Arg of perigee: 337
4543 deg
Mean anomaly: 22
6506 deg
Mean motion: 15
49922818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 533
Checksum: 302
Coasting Arc #9 (Orbit 547)
---------------------------------------
Vector Time (GMT): 2014/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3261213
53 A = 6790765
12 meter
Y = -3241552
62 meter E =
0011629
Z = -5007527
46 I = 51
28465
XDOT = 3468
294891 Wp = 95
04958
YDOT = -6530
593668 meter/sec RA = 285
63044 deg
ZDOT = 1971
688850 TA = 194
21496
MA = 194
24771
Ha = 227
409 n
mi
Hp = 221
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10699519
46 X = -3200398
04
Y = -10635015
14 feet Y = -3277681
68 meter
Z = -16428895
87 Z = -5023222
43
XDOT = 11378
920246 XDOT = 3531
485718
YDOT = -21425
832245 feet/sec YDOT = -6491
455601 meter/sec
ZDOT = 6468
795441 ZDOT = 1988
691238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15002028
20 X = -4572618
19
Y = 596538
11 feet Y = 181824
82 meter
Z = -16494701
44 Z = -5027585
00
XDOT = -8047
122034 XDOT = -2452
762796
YDOT = -21756
381683 feet/sec YDOT = -6631
345137 meter/sec
ZDOT = 6541
781685 ZDOT = 1993
935058
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 14130
51265589
00016717 00000-0 10270-3 0 9085
2 25544 51
6446 286
3273 0002343 340
7008 19
4054 15
49983325 5482
Satellite: ISS
Catalog Number: 25544
Epoch time: 14130
51265589 = yrday
fracday
Element set: 908
Inclination: 51
6446 deg
RA of node: 286
3273 deg
Eccentricity:
0002343
Arg of perigee: 340
7008 deg
Mean anomaly: 19
4054 deg
Mean motion: 15
49983325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 548
Checksum: 311
Coasting Arc #10 (Orbit 563)
---------------------------------------
Vector Time (GMT): 2014/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3347309
77 A = 6791333
13 meter
Y = 3339373
86 meter E =
0007811
Z = 4872652
13 I = 51
27844
XDOT = -3147
711957 Wp = 42
14589
YDOT = 6582
810568 meter/sec RA = 280
64880 deg
ZDOT = -2341
166906 TA = 70
94960
MA = 70
86501
Ha = 227
441 n
mi
Hp = 221
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10981987
42 X = 3286049
13
Y = 10955950
99 feet Y = 3376463
18 meter
Z = 15986391
49 Z = 4888764
34
XDOT = -10327
138968 XDOT = -3209
715641
YDOT = 21597
147534 feet/sec YDOT = 6547
264112 meter/sec
ZDOT = -7680
993786 ZDOT = -2356
609043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15418890
08 X = 4699677
70
Y = -854527
98 feet Y = -260460
13 meter
Z = 16053947
59 Z = 4893243
23
XDOT = 9251
880541 XDOT = 2819
973189
YDOT = 20905
345360 feet/sec YDOT = 6371
949266 meter/sec
ZDOT = -7747
385490 ZDOT = -2361
403097
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 14131
54423522
00016717 00000-0 10270-3 0 9093
2 25544 51
6441 281
2157 0002357 345
7767 14
3316 15
49970458 5640
Satellite: ISS
Catalog Number: 25544
Epoch time: 14131
54423522 = yrday
fracday
Element set: 909
Inclination: 51
6441 deg
RA of node: 281
2157 deg
Eccentricity:
0002357
Arg of perigee: 345
7767 deg
Mean anomaly: 14
3316 deg
Mean motion: 15
49970458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 564
Checksum: 307
Coasting Arc #11 (Orbit 578)
---------------------------------------
Vector Time (GMT): 2014/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3476068
41 A = 6791755
40 meter
Y = -3421450
09 meter E =
0009996
Z = -4735524
21 I = 51
27683
XDOT = 2821
869613 Wp = 96
63937
YDOT = -6585
990830 meter/sec RA = 275
66848 deg
ZDOT = 2690
840365 TA = 200
12528
MA = 200
16472
Ha = 227
452 n
mi
Hp = 221
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11404423
91 X = -3414546
47
Y = -11225229
96 feet Y = -3459977
73 meter
Z = -15536496
75 Z = -4752261
39
XDOT = 9258
102404 XDOT = 2882
234406
YDOT = -21607
581462 feet/sec YDOT = -6554
097352 meter/sec
ZDOT = 8828
216421 ZDOT = 2704
695532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15883189
79 X = -4841196
25
Y = 1266919
57 feet Y = 386157
09 meter
Z = -15606684
48 Z = -4756917
43
XDOT = -10308
200638 XDOT = -3141
939555
YDOT = -19898
146400 feet/sec YDOT = -6064
955023 meter/sec
ZDOT = 8887
894514 ZDOT = 2709
030248
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 14132
51132493
00016717 00000-0 10270-3 0 9107
2 25544 51
6454 276
4251 0002459 347
7744 12
3346 15
50024636 5792
Satellite: ISS
Catalog Number: 25544
Epoch time: 14132
51132493 = yrday
fracday
Element set: 910
Inclination: 51
6454 deg
RA of node: 276
4251 deg
Eccentricity:
0002459
Arg of perigee: 347
7744 deg
Mean anomaly: 12
3346 deg
Mean motion: 15
50024636 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 579
Checksum: 293
Coasting Arc #12 (Orbit 594)
---------------------------------------
Vector Time (GMT): 2014/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3607288
98 A = 6792468
78 meter
Y = 3518388
75 meter E =
0009605
Z = 4551192
41 I = 51
27702
XDOT = -2528
346051 Wp = 52
37560
YDOT = 6557
309765 meter/sec RA = 270
68658 deg
ZDOT = -3055
075369 TA = 68
40581
MA = 68
30350
Ha = 227
490 n
mi
Hp = 221
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11834937
60 X = 3545568
71
Y = 11543270
17 feet Y = 3558382
57 meter
Z = 14931733
63 Z = 4568566
68
XDOT = -8295
098594 XDOT = -2586
642542
YDOT = 21513
483480 feet/sec YDOT = 6528
710287 meter/sec
ZDOT = -10023
213153 ZDOT = -3067
499464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16381025
77 X = 4992936
65
Y = -1671346
76 feet Y = -509426
49 meter
Z = 15004602
56 Z = 4573402
86
XDOT = 11186
205106 XDOT = 3409
555316
YDOT = 18872
568032 feet/sec YDOT = 5752
358736 meter/sec
ZDOT = -10076
833370 ZDOT = -3071
418811
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 14133
54287464
00016717 00000-0 10270-3 0 9111
2 25544 51
6454 271
3134 0002451 353
1813 6
9303 15
50019874 5954
Satellite: ISS
Catalog Number: 25544
Epoch time: 14133
54287464 = yrday
fracday
Element set: 911
Inclination: 51
6454 deg
RA of node: 271
3134 deg
Eccentricity:
0002451
Arg of perigee: 353
1813 deg
Mean anomaly: 6
9303 deg
Mean motion: 15
50019874 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 595
Checksum: 289
Coasting Arc #13 (Orbit 609)
---------------------------------------
Vector Time (GMT): 2014/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3779605
59 A = 6793049
94 meter
Y = -3585823
44 meter E =
0008058
Z = -4366433
87 I = 51
28101
XDOT = 2240
305651 Wp = 93
60327
YDOT = -6486
139486 meter/sec RA = 265
70660 deg
ZDOT = 3392
306019 TA = 210
98303
MA = 211
03059
Ha = 227
500 n
mi
Hp = 221
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12400280
80 X = -3718015
96
Y = -11764512
59 feet Y = -3627744
85 meter
Z = -14325570
44 Z = -4384645
65
XDOT = 7350
084157 XDOT = 2296
189513
YDOT = -21279
985190 feet/sec YDOT = -6460
774638 meter/sec
ZDOT = 11129
612922 ZDOT = 3403
324811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16878174
51 X = -5144467
59
Y = 2258992
28 feet Y = 688540
85 meter
Z = -14401974
45 Z = -4389721
81
XDOT = -11899
315457 XDOT = -3626
911351
YDOT = -17749
663664 feet/sec YDOT = -5410
097485 meter/sec
ZDOT = 11177
278362 ZDOT = 3406
834445
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 14134
50993668
00016717 00000-0 10270-3 0 9129
2 25544 51
6464 266
5229 0002621 354
1151 5
9968 15
50064159 6101
Satellite: ISS
Catalog Number: 25544
Epoch time: 14134
50993668 = yrday
fracday
Element set: 912
Inclination: 51
6464 deg
RA of node: 266
5229 deg
Eccentricity:
0002621
Arg of perigee: 354
1151 deg
Mean anomaly: 5
9968 deg
Mean motion: 15
50064159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 610
Checksum: 304
Coasting Arc #14 (Orbit 625)
---------------------------------------
Vector Time (GMT): 2014/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3952768
44 A = 6793868
89 meter
Y = 3664677
94 meter E =
0011273
Z = 4130320
67 I = 51
28732
XDOT = -1995
728702 Wp = 63
05577
YDOT = 6383
416439 meter/sec RA = 260
72594 deg
ZDOT = -3740
885453 TA = 65
73022
MA = 65
61249
Ha = 227
546 n
mi
Hp = 220
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12968400
40 X = 3891431
21
Y = 12023221
59 feet Y = 3708537
11 meter
Z = 13550920
83 Z = 4149374
32
XDOT = -6547
666346 XDOT = -2048
788781
YDOT = 20942
967320 feet/sec YDOT = 6360
802489 meter/sec
ZDOT = -12273
246236 ZDOT = -3750
709091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17391777
59 X = 5301013
81
Y = -2844281
18 feet Y = -866936
90 meter
Z = 13630878
86 Z = 4154691
88
XDOT = 12409
483057 XDOT = 3782
410436
YDOT = 16655
122783 feet/sec YDOT = 5076
481424 meter/sec
ZDOT = -12315
840292 ZDOT = -3753
868121
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 14135
54145697
00016717 00000-0 10270-3 0 9136
2 25544 51
6467 261
4117 0002586
1927 359
9224 15
50069425 6268
Satellite: ISS
Catalog Number: 25544
Epoch time: 14135
54145697 = yrday
fracday
Element set: 913
Inclination: 51
6467 deg
RA of node: 261
4117 deg
Eccentricity:
0002586
Arg of perigee:
1927 deg
Mean anomaly: 359
9224 deg
Mean motion: 15
50069425 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 626
Checksum: 308
Coasting Arc #15 (Orbit 640)
---------------------------------------
Vector Time (GMT): 2014/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4161672
64 A = 6794569
33 meter
Y = -3701073
46 meter E =
0006376
Z = -3896834
47 I = 51
29642
XDOT = 1765
711270 Wp = 81
19434
YDOT = -6248
948631 meter/sec RA = 255
74704 deg
ZDOT = 4055
983588 TA = 231
53016
MA = 231
58738
Ha = 227
558 n
mi
Hp = 220
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13653781
64 X = -4101047
20
Y = -12142629
45 feet Y = -3747272
66 meter
Z = -12784890
01 Z = -3916904
69
XDOT = 5793
015979 XDOT = 1815
754192
YDOT = -20501
799972 feet/sec YDOT = -6228
923834 meter/sec
ZDOT = 13307
032770 ZDOT = 4064
682367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17848435
11 X = -5440203
02
Y = 3625043
49 feet Y = 1104913
26 meter
Z = -12869150
69 Z = -3922517
13
XDOT = -12760
079097 XDOT = -3889
272109
YDOT = -15528
191656 feet/sec YDOT = -4732
992817 meter/sec
ZDOT = 13344
846383 ZDOT = 4067
509177
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 14136
50849172
00016717 00000-0 10270-3 0 9143
2 25544 51
6472 256
6210 0002800
3704 359
7448 15
50102689 6411
Satellite: ISS
Catalog Number: 25544
Epoch time: 14136
50849172 = yrday
fracday
Element set: 914
Inclination: 51
6472 deg
RA of node: 256
6210 deg
Eccentricity:
0002800
Arg of perigee:
3704 deg
Mean anomaly: 359
7448 deg
Mean motion: 15
50102689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 641
Checksum: 288
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