[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 5th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 32291 73 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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
072/03:59:49
018 -1
1 1
6 1
6
N/A -1
1 -0
0 224
2
000/00:03:38
035 0
4 0
0 220
7
Coasting Arc #1 (Orbit 3492)
---------------------------------------
Vector Time (GMT): 2014/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4235739
34 A = 6786465
81 meter
Y = 388593
65 meter E =
0013702
Z = -5299740
89 I = 51
26895
XDOT = -871
939719 Wp = 103
11970
YDOT = -7602
521561 meter/sec RA = 262
63640 deg
ZDOT = 136
692426 TA = 168
20825
MA = 168
17613
Ha = 225
693 n
mi
Hp = 219
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13896782
62 X = -4214025
67
Y = 1274913
56 feet Y = 341347
53 meter
Z = -17387601
33 Z = -5320264
63
XDOT = -2860
694615 XDOT = -787
525812
YDOT = -24942
656040 feet/sec YDOT = -7611
800145 meter/sec
ZDOT = 448
465964 ZDOT = 132
662854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13413902
57 X = -4088557
50
Y = -3433970
91 feet Y = -1046674
33 meter
Z = -17474258
59 Z = -5326154
02
XDOT = 5434
682409 XDOT = 1656
491198
YDOT = -23476
155026 feet/sec YDOT = -7155
532052 meter/sec
ZDOT = 432
588291 ZDOT = 131
852911
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 14062
51590278
00016717 00000-0 10270-3 0 9007
2 25544 51
6449 263
4136 0003200 207
8568 152
2412 15
51006972 34939
Satellite: ISS
Catalog Number: 25544
Epoch time: 14062
51590278 = yrday
fracday
Element set: 900
Inclination: 51
6449 deg
RA of node: 263
4136 deg
Eccentricity:
0003200
Arg of perigee: 207
8568 deg
Mean anomaly: 152
2412 deg
Mean motion: 15
51006972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3493
Checksum: 290
Coasting Arc #2 (Orbit 3508)
---------------------------------------
Vector Time (GMT): 2014/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4318520
90 A = 6786679
64 meter
Y = 103662
73 meter E =
0001553
Z = 5233198
14 I = 51
27518
XDOT = 913
181570 Wp = 129
45835
YDOT = 7556
273789 meter/sec RA = 257
64388 deg
ZDOT = -904
041446 TA = 329
23267
MA = 329
24177
Ha = 225
447 n
mi
Hp = 220
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14168375
67 X = 4291619
72
Y = 340100
80 feet Y = 151805
49 meter
Z = 17169285
24 Z = 5254111
42
XDOT = 2996
002525 XDOT = 833
009265
YDOT = 24790
924504 feet/sec YDOT = 7566
037179 meter/sec
ZDOT = -2966
015244 ZDOT = -899
801125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13213126
53 X = 4027360
97
Y = 4820202
57 feet Y = 1469197
74 meter
Z = 17257515
11 Z = 5260090
61
XDOT = -4720
404903 XDOT = -1438
779414
YDOT = 23489
317357 feet/sec YDOT = 7159
543931 meter/sec
ZDOT = -2949
232225 ZDOT = -898
925982
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 14063
54679857
00016717 00000-0 10270-3 0 9013
2 25544 51
6453 258
2986 0003228 212
6336 147
4616 15
51019486 35090
Satellite: ISS
Catalog Number: 25544
Epoch time: 14063
54679857 = yrday
fracday
Element set: 901
Inclination: 51
6453 deg
RA of node: 258
2986 deg
Eccentricity:
0003228
Arg of perigee: 212
6336 deg
Mean anomaly: 147
4616 deg
Mean motion: 15
51019486 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3509
Checksum: 327
Coasting Arc #3 (Orbit 3523)
---------------------------------------
Vector Time (GMT): 2014/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4462271
80 A = 6787150
08 meter
Y = -601069
66 meter E =
0012524
Z = -5089788
22 I = 51
28414
XDOT = -911
549556 Wp = 116
28998
YDOT = -7413
246750 meter/sec RA = 252
65012 deg
ZDOT = 1672
391158 TA = 169
98473
MA = 169
95975
Ha = 225
422 n
mi
Hp = 219
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14639999
35 X = -4430494
42
Y = -1972013
31 feet Y = -650792
57 meter
Z = -16698780
25 Z = -5111387
94
XDOT = -2990
648150 XDOT = -836
709117
YDOT = -24321
675689 feet/sec YDOT = -7423
021624 meter/sec
ZDOT = 5486
847632 ZDOT = 1668
145669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13251060
51 X = -4038923
24
Y = -6291138
90 feet Y = -1917539
14 meter
Z = -16789837
57 Z = -5117542
49
XDOT = 4039
394451 XDOT = 1231
207429
YDOT = -23126
018352 feet/sec YDOT = -7048
810394 meter/sec
ZDOT = 5470
013674 ZDOT = 1667
260168
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 14064
51323700
00016717 00000-0 10270-3 0 9025
2 25544 51
6445 253
5015 0003188 215
3349 144
7591 15
51086360 35245
Satellite: ISS
Catalog Number: 25544
Epoch time: 14064
51323700 = yrday
fracday
Element set: 902
Inclination: 51
6445 deg
RA of node: 253
5015 deg
Eccentricity:
0003188
Arg of perigee: 215
3349 deg
Mean anomaly: 144
7591 deg
Mean motion: 15
51086360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3524
Checksum: 284
Coasting Arc #4 (Orbit 3539)
---------------------------------------
Vector Time (GMT): 2014/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4634205
64 A = 6788106
85 meter
Y = 1077510
87 meter E =
0004048
Z = 4838670
78 I = 51
29792
XDOT = 861
651489 Wp = 74
43657
YDOT = 7218
714323 meter/sec RA = 247
65948 deg
ZDOT = -2429
987878 TA = 39
54527
MA = 39
51574
Ha = 225
126 n
mi
Hp = 220
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15204086
76 X = 4598307
66
Y = 3535140
66 feet Y = 1129133
31 meter
Z = 15874904
14 Z = 4861095
68
XDOT = 2826
940582 XDOT = 792
670205
YDOT = 23683
445942 feet/sec YDOT = 7227
963915 meter/sec
ZDOT = -7972
401174 ZDOT = -2425
970413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13453959
62 X = 4100766
89
Y = 7722947
68 feet Y = 2353954
45 meter
Z = 15969380
22 Z = 4867467
09
XDOT = -3478
583741 XDOT = -1060
272324
YDOT = 22530
936987 feet/sec YDOT = 6867
429594 meter/sec
ZDOT = -7956
493129 ZDOT = -2425
139106
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 14065
54407746
00016717 00000-0 10270-3 0 9033
2 25544 51
6447 248
3864 0003216 221
0432 139
0478 15
51106612 35402
Satellite: ISS
Catalog Number: 25544
Epoch time: 14065
54407746 = yrday
fracday
Element set: 903
Inclination: 51
6447 deg
RA of node: 248
3864 deg
Eccentricity:
0003216
Arg of perigee: 221
0432 deg
Mean anomaly: 139
0478 deg
Mean motion: 15
51106612 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3540
Checksum: 289
Coasting Arc #5 (Orbit 3554)
---------------------------------------
Vector Time (GMT): 2014/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4851096
04 A = 6789264
64 meter
Y = -1525629
65 meter E =
0009021
Z = -4507318
66 I = 51
31494
XDOT = -746
213868 Wp = 129
30126
YDOT = -6937
343189 meter/sec RA = 242
66922 deg
ZDOT = 3149
911340 TA = 172
51611
MA = 172
50264
Ha = 225
144 n
mi
Hp = 219
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15915669
43 X = -4811780
60
Y = -5005346
62 feet Y = -1579658
30 meter
Z = -14787790
88 Z = -4530788
81
XDOT = -2448
208228 XDOT = -683
884634
YDOT = -22760
312299 feet/sec YDOT = -6945
339041 meter/sec
ZDOT = 10334
354790 ZDOT = 3146
438387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13878728
62 X = -4230236
48
Y = -9100009
81 feet Y = -2773682
99 meter
Z = -14886621
52 Z = -4537442
24
XDOT = 3073
755131 XDOT = 936
880564
YDOT = -21578
652580 feet/sec YDOT = -6577
173306 meter/sec
ZDOT = 10320
695607 ZDOT = 3145
748021
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 14066
51046398
00016717 00000-0 10270-3 0 9044
2 25544 51
6446 243
5895 0003138 222
6837 137
4071 15
51168777 35558
Satellite: ISS
Catalog Number: 25544
Epoch time: 14066
51046398 = yrday
fracday
Element set: 904
Inclination: 51
6446 deg
RA of node: 243
5895 deg
Eccentricity:
0003138
Arg of perigee: 222
6837 deg
Mean anomaly: 137
4071 deg
Mean motion: 15
51168777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3555
Checksum: 326
Coasting Arc #6 (Orbit 3570)
---------------------------------------
Vector Time (GMT): 2014/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5076155
78 A = 6790772
19 meter
Y = 1937509
52 meter E =
0007920
Z = 4066788
29 I = 51
33493
XDOT = 553
229057 Wp = 88
14340
YDOT = 6614
572319 meter/sec RA = 237
68255 deg
ZDOT = -3835
130121 TA = 41
73225
MA = 41
67187
Ha = 224
849 n
mi
Hp = 220
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16654054
40 X = 5034357
87
Y = 6356658
54 feet Y = 1994040
99 meter
Z = 13342481
26 Z = 4091345
62
XDOT = 1815
055961 XDOT = 497
851970
YDOT = 21701
352752 feet/sec YDOT = 6620
448920 meter/sec
ZDOT = -12582
447903 ZDOT = -3832
577711
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14413051
43 X = 4393098
07
Y = 10356614
51 feet Y = 3156696
10 meter
Z = 13445851
64 Z = 4098295
58
XDOT = -2922
853342 XDOT = -890
885699
YDOT = 20419
013925 feet/sec YDOT = 6223
715444 meter/sec
ZDOT = -12572
618683 ZDOT = -3832
134175
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 14067
54124746
00016717 00000-0 10270-3 0 9053
2 25544 51
6442 238
4739 0003155 228
6320 131
4561 15
51193380 35710
Satellite: ISS
Catalog Number: 25544
Epoch time: 14067
54124746 = yrday
fracday
Element set: 905
Inclination: 51
6442 deg
RA of node: 238
4739 deg
Eccentricity:
0003155
Arg of perigee: 228
6320 deg
Mean anomaly: 131
4561 deg
Mean motion: 15
51193380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3571
Checksum: 297
Coasting Arc #7 (Orbit 3585)
---------------------------------------
Vector Time (GMT): 2014/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5318425
78 A = 6792263
30 meter
Y = -2293792
26 meter E =
0003875
Z = -3552923
10 I = 51
35852
XDOT = -280
816135 Wp = 131
90992
YDOT = -6230
357183 meter/sec RA = 232
69795 deg
ZDOT = 4443
320515 TA = 186
06585
MA = 186
07054
Ha = 224
851 n
mi
Hp = 219
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17448903
49 X = -5275122
04
Y = -7525565
17 feet Y = -2353024
50 meter
Z = -11656571
87 Z = -3578653
59
XDOT = -921
312780 XDOT = -232
709990
YDOT = -20440
804405 feet/sec YDOT = -6233
228081 meter/sec
ZDOT = 14577
823211 ZDOT = 4442
073758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15094188
79 X = -4600708
74
Y = -11433620
20 feet Y = -3484967
44 meter
Z = -11764855
54 Z = -3585927
97
XDOT = 3031
475045 XDOT = 923
993594
YDOT = -18995
658716 feet/sec YDOT = -5789
876777 meter/sec
ZDOT = 14573
441243 ZDOT = 4441
984891
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 14068
50757984
00016717 00000-0 10270-3 0 9067
2 25544 51
6448 233
6772 0003058 230
6165 129
4716 15
51256025 35863
Satellite: ISS
Catalog Number: 25544
Epoch time: 14068
50757984 = yrday
fracday
Element set: 906
Inclination: 51
6448 deg
RA of node: 233
6772 deg
Eccentricity:
0003058
Arg of perigee: 230
6165 deg
Mean anomaly: 129
4716 deg
Mean motion: 15
51256025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3586
Checksum: 324
Coasting Arc #8 (Orbit 3601)
---------------------------------------
Vector Time (GMT): 2014/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5538375
76 A = 6793877
29 meter
Y = 2604533
91 meter E =
0011022
Z = 2935900
02 I = 51
38294
XDOT = -88
564195 Wp = 108
27147
YDOT = 5822
538572 meter/sec RA = 227
71681 deg
ZDOT = -4986
247384 TA = 38
11705
MA = 38
03914
Ha = 224
595 n
mi
Hp = 220
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18170524
15 X = 5494578
18
Y = 8545058
75 feet Y = 2666222
97 meter
Z = 9632217
92 Z = 2962697
68
XDOT = -290
564945 XDOT = -129
445282
YDOT = 19102
816836 feet/sec YDOT = 5821
319136 meter/sec
ZDOT = -16359
079345 ZDOT = -4986
777462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15780082
84 X = 4809769
25
Y = 12328423
20 feet Y = 3757703
39 meter
Z = 9744976
43 Z = 2970268
82
XDOT = -3496
100362 XDOT = -1065
611390
YDOT = 17439
221085 feet/sec YDOT = 5315
474587 meter/sec
ZDOT = -16362
131611 ZDOT = -4987
177715
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 14069
53830445
00016717 00000-0 10270-3 0 9076
2 25544 51
6441 228
5609 0003081 236
7861 123
2995 15
51285751 36022
Satellite: ISS
Catalog Number: 25544
Epoch time: 14069
53830445 = yrday
fracday
Element set: 907
Inclination: 51
6441 deg
RA of node: 228
5609 deg
Eccentricity:
0003081
Arg of perigee: 236
7861 deg
Mean anomaly: 123
2995 deg
Mean motion: 15
51285751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3602
Checksum: 312
Coasting Arc #9 (Orbit 3616)
---------------------------------------
Vector Time (GMT): 2014/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5739728
64 A = 6795195
21 meter
Y = -2844322
89 meter E =
0003094
Z = -2263561
42 I = 51
41077
XDOT = 536
800364 Wp = 29
96901
YDOT = -5389
568000 meter/sec RA = 222
73881 deg
ZDOT = 5417
039459 TA = 304
80136
MA = 304
83046
Ha = 224
546 n
mi
Hp = 219
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18831130
71 X = -5696500
70
Y = -9331768
02 feet Y = -2908266
76 meter
Z = -7426382
62 Z = -2291338
51
XDOT = 1761
156050 XDOT = 570
713973
YDOT = -17682
309711 feet/sec YDOT = -5383
374958 meter/sec
ZDOT = 17772
439170 ZDOT = 5419
730066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16489874
07 X = -5026113
62
Y = -12962556
10 feet Y = -3950987
10 meter
Z = -7543257
25 Z = -2299184
81
XDOT = 4271
181137 XDOT = 1301
856010
YDOT = -15771
762016 feet/sec YDOT = -4807
233062 meter/sec
ZDOT = 17784
544168 ZDOT = 5420
729062
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 14070
50458089
00016717 00000-0 10270-3 0 9086
2 25544 51
6453 223
7642 0002973 240
0401 120
0455 15
51345242 36170
Satellite: ISS
Catalog Number: 25544
Epoch time: 14070
50458089 = yrday
fracday
Element set: 908
Inclination: 51
6453 deg
RA of node: 223
7642 deg
Eccentricity:
0002973
Arg of perigee: 240
0401 deg
Mean anomaly: 120
0455 deg
Mean motion: 15
51345242 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3617
Checksum: 280
Coasting Arc #10 (Orbit 3632)
---------------------------------------
Vector Time (GMT): 2014/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5881880
40 A = 6796299
78 meter
Y = 3039092
39 meter E =
0012210
Z = 1504698
43 I = 51
43753
XDOT = -1084
261944 Wp = 129
05116
YDOT = 4955
886427 meter/sec RA = 217
76375 deg
ZDOT = -5747
299682 TA = 34
48376
MA = 34
40460
Ha = 224
341 n
mi
Hp = 219
949
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19297507
88 X = 5840150
20
Y = 9970775
57 feet Y = 3104634
20 meter
Z = 4936674
65 Z = 1533169
63
XDOT = -3557
289843 XDOT = -1111
681074
YDOT = 16259
469906 feet/sec YDOT = 4943
607521 meter/sec
ZDOT = -18855
970086 ZDOT = -5752
633983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17064535
94 X = 5201270
56
Y = 13394576
39 feet Y = 4082666
88 meter
Z = 5056468
03 Z = 1541211
46
XDOT = -5438
949831 XDOT = -1657
791909
YDOT = 14084
953413 feet/sec YDOT = 4293
093800 meter/sec
ZDOT = -18879
170560 ZDOT = -5754
371187
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 14071
53524490
00016717 00000-0 10270-3 0 9091
2 25544 51
6446 218
6473 0003000 246
8367 113
2469 15
51390066 36335
Satellite: ISS
Catalog Number: 25544
Epoch time: 14071
53524490 = yrday
fracday
Element set: 909
Inclination: 51
6446 deg
RA of node: 218
6473 deg
Eccentricity:
0003000
Arg of perigee: 246
8367 deg
Mean anomaly: 113
2469 deg
Mean motion: 15
51390066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3633
Checksum: 300
Coasting Arc #11 (Orbit 3642)
---------------------------------------
Vector Time (GMT): 2014/072/04:01:38
035
Vector Time (MET): N/A
Weight (LBS) : 901568
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4584751
19 A = 6788289
12 meter
Y = 1485973
90 meter E =
0007737
Z = -4787908
86 I = 51
42825
XDOT = -4524
031312 Wp = 118
12223
YDOT = -5607
715543 meter/sec RA = 214
43784 deg
ZDOT = 2591
298863 TA = 177
52924
MA = 177
52542
Ha = 224
240 n
mi
Hp = 220
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15041834
62 X = -4577769
15
Y = 4875242
44 feet Y = 1434742
69 meter
Z = -15708362
39 Z = -4810163
84
XDOT = -14842
622414 XDOT = -4473
575856
YDOT = -18398
016872 feet/sec YDOT = -5658
023715 meter/sec
ZDOT = 8501
636690 ZDOT = 2569
445352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5795092
81 X = 1766344
29
Y = -14610758
60 feet Y = -4453359
22 meter
Z = -15802533
32 Z = -4816612
16
XDOT = 22604
242571 XDOT = 6889
773135
YDOT = -131
840157 feet/sec YDOT = -40
184880 meter/sec
ZDOT = 8410
124919 ZDOT = 2563
406075
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 14072
17939418
00016717 00000-0 10270-3 0 9104
2 25544 51
6480 215
4545 0004029 269
5120 90
5570 15
51124253 36433
Satellite: ISS
Catalog Number: 25544
Epoch time: 14072
17939418 = yrday
fracday
Element set: 910
Inclination: 51
6480 deg
RA of node: 215
4545 deg
Eccentricity:
0004029
Arg of perigee: 269
5120 deg
Mean anomaly: 90
5570 deg
Mean motion: 15
51124253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3643
Checksum: 291
Coasting Arc #12 (Orbit 3658)
---------------------------------------
Vector Time (GMT): 2014/073/04:01:38
035
Vector Time (MET): N/A
Weight (LBS) : 901568
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4999644
13 A = 6789500
01 meter
Y = -1224834
37 meter E =
0005797
Z = 4425381
48 I = 51
45904
XDOT = 4267
116166 Wp = 51
66198
YDOT = 5437
806467 meter/sec RA = 209
45860 deg
ZDOT = -3309
317608 TA = 71
88034
MA = 71
81722
Ha = 224
042 n
mi
Hp = 220
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16403031
92 X = 4991472
11
Y = -4018485
46 feet Y = -1168970
20 meter
Z = 14518968
12 Z = 4449649
05
XDOT = 13999
724953 XDOT = 4222
067644
YDOT = 17840
572397 feet/sec YDOT = 5485
271742 meter/sec
ZDOT = -10857
341234 ZDOT = -3288
699029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7067313
49 X = -2154117
15
Y = 15240399
49 feet Y = 4645273
77 meter
Z = 14621607
98 Z = 4456666
11
XDOT = -21606
769757 XDOT = -6585
743422
YDOT = 334
379681 feet/sec YDOT = 101
918927 meter/sec
ZDOT = -10771
006333 ZDOT = -3283
002730
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 14073
21020755
00016717 00000-0 10270-3 0 9116
2 25544 51
6480 210
3391 0004058 275
4323 84
6365 15
51186743 36594
Satellite: ISS
Catalog Number: 25544
Epoch time: 14073
21020755 = yrday
fracday
Element set: 911
Inclination: 51
6480 deg
RA of node: 210
3391 deg
Eccentricity:
0004058
Arg of perigee: 275
4323 deg
Mean anomaly: 84
6365 deg
Mean motion: 15
51186743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3659
Checksum: 294
Coasting Arc #13 (Orbit 3673)
---------------------------------------
Vector Time (GMT): 2014/074/04:01:38
035
Vector Time (MET): N/A
Weight (LBS) : 901568
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5407381
77 A = 6790996
35 meter
Y = 1019868
09 meter E =
0002919
Z = -3982967
64 I = 51
49258
XDOT = -3913
822874 Wp = 119
12558
YDOT = -5252
407703 meter/sec RA = 204
48207 deg
ZDOT = 3969
407076 TA = 192
34553
MA = 192
35269
Ha = 224
090 n
mi
Hp = 220
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17740753
83 X = -5399036
49
Y = 3346023
91 feet Y = 959445
32 meter
Z = -13067479
14 Z = -4009215
55
XDOT = -12840
626227 XDOT = -3874
080292
YDOT = -17232
308738 feet/sec YDOT = -5295
951751 meter/sec
ZDOT = 13022
989094 ZDOT = 3950
491823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8159995
84 X = 2487166
73
Y = -16013490
27 feet Y = -4880911
84 meter
Z = -13178460
86 Z = -4016794
87
XDOT = 20367
952335 XDOT = 6208
151872
YDOT = -271
153885 feet/sec YDOT = -82
647704 meter/sec
ZDOT = 12943
809948 ZDOT = 3945
273272
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 14074
17656672
00016717 00000-0 10270-3 0 9126
2 25544 51
6488 205
5429 0004149 280
0547 80
0136 15
51215816 36748
Satellite: ISS
Catalog Number: 25544
Epoch time: 14074
17656672 = yrday
fracday
Element set: 912
Inclination: 51
6488 deg
RA of node: 205
5429 deg
Eccentricity:
0004149
Arg of perigee: 280
0547 deg
Mean anomaly: 80
0136 deg
Mean motion: 15
51215816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3674
Checksum: 308
Coasting Arc #14 (Orbit 3689)
---------------------------------------
Vector Time (GMT): 2014/075/04:01:38
035
Vector Time (MET): N/A
Weight (LBS) : 901568
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5794407
16 A = 6792560
02 meter
Y = -844242
99 meter E =
0008424
Z = 3436578
49 I = 51
52710
XDOT = 3460
140030 Wp = 81
43161
YDOT = 5082
718314 meter/sec RA = 199
50988 deg
ZDOT = -4574
647982 TA = 58
28914
MA = 58
20704
Ha = 224
082 n
mi
Hp = 220
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19010522
17 X = 5786723
34
Y = -2769826
09 feet Y = -779488
62 meter
Z = 11274863
80 Z = 3464708
18
XDOT = 11352
165454 XDOT = 3425
268786
YDOT = 16675
585020 feet/sec YDOT = 5121
216100 meter/sec
ZDOT = -15008
687606 ZDOT = -4557
924753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9111237
65 X = -2777105
24
Y = 16833349
31 feet Y = 5130804
87 meter
Z = 11393776
49 Z = 3472823
07
XDOT = -18981
324639 XDOT = -5785
507750
YDOT = -138
626889 feet/sec YDOT = -42
253476 meter/sec
ZDOT = -14938
733538 ZDOT = -4553
325982
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 14075
20731956
00016717 00000-0 10270-3 0 9131
2 25544 51
6490 200
4273 0004104 285
6561 74
4137 15
51268655 36905
Satellite: ISS
Catalog Number: 25544
Epoch time: 14075
20731956 = yrday
fracday
Element set: 913
Inclination: 51
6490 deg
RA of node: 200
4273 deg
Eccentricity:
0004104
Arg of perigee: 285
6561 deg
Mean anomaly: 74
4137 deg
Mean motion: 15
51268655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3690
Checksum: 300
Coasting Arc #15 (Orbit 3704)
---------------------------------------
Vector Time (GMT): 2014/076/04:01:38
035
Vector Time (MET): N/A
Weight (LBS) : 901568
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6134805
26 A = 6794085
59 meter
Y = 723829
86 meter E =
0003614
Z = -2823495
19 I = 51
56238
XDOT = -2921
125891 Wp = 1
80328
YDOT = -4928
713474 meter/sec RA = 194
54069 deg
ZDOT = 5087
121960 TA = 326
14253
MA = 326
16560
Ha = 224
076 n
mi
Hp = 220
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20127313
85 X = -6128727
74
Y = 2374769
87 feet Y = 655260
05 meter
Z = -9263435
66 Z = -2853282
47
XDOT = -9583
746361 XDOT = -2890
506338
YDOT = -16170
319798 feet/sec YDOT = -4961
207347 meter/sec
ZDOT = 16690
032676 ZDOT = 5073
006760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9800724
77 X = 2987260
91
Y = -17673301
89 feet Y = -5386822
41 meter
Z = -9389341
27 Z = -2861871
22
XDOT = 17493
557333 XDOT = 5332
036275
YDOT = 871
797780 feet/sec YDOT = 265
723963 meter/sec
ZDOT = 16631
066227 ZDOT = 5069
148986
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 14076
17362066
00016717 00000-0 10270-3 0 9141
2 25544 51
6493 195
6307 0004306 290
2385 69
8303 15
51305255 37059
Satellite: ISS
Catalog Number: 25544
Epoch time: 14076
17362066 = yrday
fracday
Element set: 914
Inclination: 51
6493 deg
RA of node: 195
6307 deg
Eccentricity:
0004306
Arg of perigee: 290
2385 deg
Mean anomaly: 69
8303 deg
Mean motion: 15
51305255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3705
Checksum: 304
Coasting Arc #16 (Orbit 3720)
---------------------------------------
Vector Time (GMT): 2014/077/04:01:38
035
Vector Time (MET): N/A
Weight (LBS) : 901568
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6422480
19 A = 6795465
60 meter
Y = -619314
08 meter E =
0009709
Z = 2118358
06 I = 51
59759
XDOT = 2286
706203 Wp = 107
75636
YDOT = 4813
267772 meter/sec RA = 189
57632 deg
ZDOT = -5507
761643 TA = 48
78795
MA = 48
70429
Ha = 224
200 n
mi
Hp = 220
410
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21071129
24 X = 6418637
85
Y = -2031870
33 feet Y = -547514
94 meter
Z = 6949993
65 Z = 2149548
35
XDOT = 7502
316938 XDOT = 2259
468169
YDOT = 15791
560931 feet/sec YDOT = 4838
686034 meter/sec
ZDOT = -18070
084129 ZDOT = -5496
720046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10323288
82 X = -3146538
43
Y = 18430977
18 feet Y = 5617761
85 meter
Z = 7081820
68 Z = 2158538
94
XDOT = -15969
501986 XDOT = -4867
504205
YDOT = -1996
940291 feet/sec YDOT = -608
667401 meter/sec
ZDOT = -18024
080294 ZDOT = -5493
739674
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 14077
20431253
00016717 00000-0 10270-3 0 9152
2 25544 51
6493 190
5151 0004190 294
8859 65
1856 15
51344886 37210
Satellite: ISS
Catalog Number: 25544
Epoch time: 14077
20431253 = yrday
fracday
Element set: 915
Inclination: 51
6493 deg
RA of node: 190
5151 deg
Eccentricity:
0004190
Arg of perigee: 294
8859 deg
Mean anomaly: 65
1856 deg
Mean motion: 15
51344886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3721
Checksum: 316
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