[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 6th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 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
314/23:26:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
0
000/00:00:00
000 0
0 0
0 220
9
Coasting Arc #1 (Orbit 1677)
---------------------------------------
Vector Time (GMT): 2013/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886408
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3583584
61 A = 6789815
50 meter
Y = 2179802
33 meter E =
0015924
Z = -5353019
10 I = 51
92278
XDOT = -4043
734245 Wp = 91
59941
YDOT = 6493
327977 meter/sec RA = 122
28549 deg
ZDOT = -63
530164 TA = 177
79961
MA = 177
79260
Ha = 228
125 n
mi
Hp = 221
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11757167
36 X = 3584947
34
Y = 7151582
44 feet Y = 2219883
99 meter
Z = -17562398
63 Z = -5335606
62
XDOT = -13266
844635 XDOT = -4115
734909
YDOT = 21303
569479 feet/sec YDOT = 6447
705791 meter/sec
ZDOT = -208
432296 ZDOT = -83
349454
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13443863
61 X = -4097689
63
Y = 3345720
78 feet Y = 1019775
69 meter
Z = -17489501
00 Z = -5330799
90
XDOT = -5459
923140 XDOT = -1664
184573
YDOT = -23458
859853 feet/sec YDOT = -7150
260483 meter/sec
ZDOT = -292
668422 ZDOT = -89
205335
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 13310
51629608
00016717 00000-0 10270-3 0 9002
2 25544 51
6440 123
1754 0001219 117
1504 242
9771 15
49860824 16788
Satellite: ISS
Catalog Number: 25544
Epoch time: 13310
51629608 = yrday
fracday
Element set: 900
Inclination: 51
6440 deg
RA of node: 123
1754 deg
Eccentricity:
0001219
Arg of perigee: 117
1504 deg
Mean anomaly: 242
9771 deg
Mean motion: 15
49860824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1678
Checksum: 294
Coasting Arc #2 (Orbit 1693)
---------------------------------------
Vector Time (GMT): 2013/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901635
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3572796
86 A = 6789899
37 meter
Y = -2191611
77 meter E =
0003554
Z = 5338720
87 I = 51
93853
XDOT = 3706
439971 Wp = 91
26921
YDOT = -6703
384535 meter/sec RA = 117
34987 deg
ZDOT = -271
307957 TA = 1
30800
MA = 1
30707
Ha = 228
305 n
mi
Hp = 221
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11721774
48 X = -3573958
76
Y = -7190327
32 feet Y = -2231571
66 meter
Z = 17515488
42 Z = 5321361
37
XDOT = 12160
236126 XDOT = 3782
441187
YDOT = -21992
731413 feet/sec YDOT = -6661
511812 meter/sec
ZDOT = -890
117969 ZDOT = -253
117619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13387442
98 X = 4080492
62
Y = -3523900
59 feet Y = -1074084
90 meter
Z = 17442810
37 Z = 5316568
60
XDOT = 7126
054297 XDOT = 2172
021350
YDOT = 23048
227183 feet/sec YDOT = 7025
099645 meter/sec
ZDOT = -812
681145 ZDOT = -247
705213
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 13311
54795982
00016717 00000-0 10270-3 0 9016
2 25544 51
6440 118
0649 0001237 117
1667 242
9610 15
49833282 16942
Satellite: ISS
Catalog Number: 25544
Epoch time: 13311
54795982 = yrday
fracday
Element set: 901
Inclination: 51
6440 deg
RA of node: 118
0649 deg
Eccentricity:
0001237
Arg of perigee: 117
1667 deg
Mean anomaly: 242
9610 deg
Mean motion: 15
49833282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1694
Checksum: 312
Coasting Arc #3 (Orbit 1708)
---------------------------------------
Vector Time (GMT): 2013/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901635
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3591079
53 A = 6789806
66 meter
Y = 2228485
21 meter E =
0015801
Z = -5327781
10 I = 51
95327
XDOT = -3344
579022 Wp = 96
91092
YDOT = 6852
748013 meter/sec RA = 112
41593 deg
ZDOT = 611
707662 TA = 178
91861
MA = 178
91519
Ha = 228
062 n
mi
Hp = 221
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11781756
99 X = 3591774
50
Y = 7311303
18 feet Y = 2268646
89 meter
Z = -17479596
79 Z = -5310334
00
XDOT = -10973
028288 XDOT = -3423
930936
YDOT = 22482
769073 feet/sec YDOT = 6814
903114 meter/sec
ZDOT = 2006
914901 ZDOT = 595
267104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13454096
67 X = -4100808
66
Y = 3714904
08 feet Y = 1132302
76 meter
Z = -17406551
26 Z = -5305516
82
XDOT = -8687
495952 XDOT = -2647
948766
YDOT = -22383
543319 feet/sec YDOT = -6822
504004 meter/sec
ZDOT = 1936
797741 ZDOT = 590
335951
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 13312
51513000
00016717 00000-0 10270-3 0 9024
2 25544 51
6451 113
2746 0001277 122
4042 237
7232 15
49902297 17091
Satellite: ISS
Catalog Number: 25544
Epoch time: 13312
51513000 = yrday
fracday
Element set: 902
Inclination: 51
6451 deg
RA of node: 113
2746 deg
Eccentricity:
0001277
Arg of perigee: 122
4042 deg
Mean anomaly: 237
7232 deg
Mean motion: 15
49902297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1709
Checksum: 269
Coasting Arc #4 (Orbit 1724)
---------------------------------------
Vector Time (GMT): 2013/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901635
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3613092
45 A = 6790053
24 meter
Y = -2271787
85 meter E =
0004236
Z = 5277672
24 I = 51
96435
XDOT = 2990
105543 Wp = 74
67873
YDOT = -6991
772682 meter/sec RA = 107
48160 deg
ZDOT = -960
871502 TA = 24
48970
MA = 24
46958
Ha = 228
245 n
mi
Hp = 220
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11853977
86 X = -3613058
09
Y = -7453372
20 feet Y = -2312191
53 meter
Z = 17315197
65 Z = 5260120
05
XDOT = 9810
057557 XDOT = 3072
734565
YDOT = -22938
886752 feet/sec YDOT = -6957
873418 meter/sec
ZDOT = -3152
465559 ZDOT = -946
144933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13541439
59 X = 4127430
79
Y = -3903634
29 feet Y = -1189827
73 meter
Z = 17241713
11 Z = 5255274
16
XDOT = 10186
700394 XDOT = 3104
906280
YDOT = 21665
871510 feet/sec YDOT = 6603
757636 meter/sec
ZDOT = -3089
522334 ZDOT = -941
686407
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 13313
54676766
00016717 00000-0 10270-3 0 9038
2 25544 51
6447 108
1638 0001293 122
1553 237
9723 15
49874191 17257
Satellite: ISS
Catalog Number: 25544
Epoch time: 13313
54676766 = yrday
fracday
Element set: 903
Inclination: 51
6447 deg
RA of node: 108
1638 deg
Eccentricity:
0001293
Arg of perigee: 122
1553 deg
Mean anomaly: 237
9723 deg
Mean motion: 15
49874191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1725
Checksum: 319
Coasting Arc #5 (Orbit 1739)
---------------------------------------
Vector Time (GMT): 2013/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901635
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3670735
49 A = 6790123
48 meter
Y = 2329509
87 meter E =
0015109
Z = -5229176
83 I = 51
97473
XDOT = -2621
249966 Wp = 102
15930
YDOT = 7067
054372 meter/sec RA = 102
54936 deg
ZDOT = 1308
308781 TA = 180
37871
MA = 180
37986
Ha = 227
976 n
mi
Hp = 220
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12043095
45 X = 3669815
81
Y = 7642748
91 feet Y = 2370553
12 meter
Z = -17156091
95 Z = -5211346
80
XDOT = -8599
901464 XDOT = -2706
435996
YDOT = 23185
873924 feet/sec YDOT = 7037
265612 meter/sec
ZDOT = 4292
351643 ZDOT = 1295
367771
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13738649
80 X = -4187540
46
Y = 4153668
66 feet Y = 1266038
21 meter
Z = -17081445
73 Z = -5206424
66
XDOT = -11532
463098 XDOT = -3515
094752
YDOT = -20722
352759 feet/sec YDOT = -6316
173121 meter/sec
ZDOT = 4236
894635 ZDOT = 1291
405485
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 13314
51391296
00016717 00000-0 10270-3 0 9049
2 25544 51
6459 103
3738 0001263 127
0605 233
0661 15
49943118 17408
Satellite: ISS
Catalog Number: 25544
Epoch time: 13314
51391296 = yrday
fracday
Element set: 904
Inclination: 51
6459 deg
RA of node: 103
3738 deg
Eccentricity:
0001263
Arg of perigee: 127
0605 deg
Mean anomaly: 233
0661 deg
Mean motion: 15
49943118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1740
Checksum: 291
Coasting Arc #6 (Orbit 1747)
---------------------------------------
Vector Time (GMT): 2013/314/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886408
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4204838
68 A = 6792086
15 meter
Y = 2438845
22 meter E =
0008752
Z = 4738800
98 I = 51
98364
XDOT = -943
496515 Wp = 116
31829
YDOT = -7073
935244 meter/sec RA = 100
23578 deg
ZDOT = 2795
684206 TA = 306
06167
MA = 306
14271
Ha = 227
980 n
mi
Hp = 220
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13795402
48 X = -4254817
97
Y = 8001460
68 feet Y = 2391544
71 meter
Z = 15547247
30 Z = 4718252
53
XDOT = -3095
461006 XDOT = -877
904932
YDOT = -23208
448963 feet/sec YDOT = -7084
119202 meter/sec
ZDOT = 9172
192277 ZDOT = 2791
260245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5244960
89 X = -1598664
08
Y = 15149841
28 feet Y = 4617671
62 meter
Z = 15460468
81 Z = 4712350
89
XDOT = -16488
985553 XDOT = -5025
842797
YDOT = -15077
047657 feet/sec YDOT = -4595
484126 meter/sec
ZDOT = 9154
623734 ZDOT = 2790
329314
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 13315
02971837
00016717 00000-0 10270-3 0 9052
2 25544 51
6450 100
8222 0000860 111
7310 248
3932 15
49962639 17481
Satellite: ISS
Catalog Number: 25544
Epoch time: 13315
02971837 = yrday
fracday
Element set: 905
Inclination: 51
6450 deg
RA of node: 100
8222 deg
Eccentricity:
0000860
Arg of perigee: 111
7310 deg
Mean anomaly: 248
3932 deg
Mean motion: 15
49962639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1748
Checksum: 297
Coasting Arc #7 (Orbit 1762)
---------------------------------------
Vector Time (GMT): 2013/315/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886408
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4064586
71 A = 6791509
26 meter
Y = -2402220
01 meter E =
0012527
Z = -4893594
58 I = 51
98638
XDOT = 1264
621266 Wp = 75
01656
YDOT = 7135
919189 meter/sec RA = 95
30303 deg
ZDOT = -2454
664218 TA = 170
96658
MA = 170
94402
Ha = 227
911 n
mi
Hp = 221
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13335258
24 X = 4114918
89
Y = -7881299
26 feet Y = -2356485
98 meter
Z = -16055100
34 Z = -4873726
55
XDOT = 4149
019902 XDOT = 1196
656126
YDOT = 23411
808364 feet/sec YDOT = 7149
680884 meter/sec
ZDOT = -8053
360295 ZDOT = -2448
686061
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4723983
42 X = 1439870
15
Y = -14843030
06 feet Y = -4524155
56 meter
Z = -15971182
70 Z = -4868016
49
XDOT = 17689
105515 XDOT = 5391
639361
YDOT = 14261
896308 feet/sec YDOT = 4347
025995 meter/sec
ZDOT = -8029
274246 ZDOT = -2447
322790
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 13315
99684711
00016717 00000-0 10270-3 0 9061
2 25544 51
6451 96
0304 0000954 107
5720 252
5535 15
49957662 17634
Satellite: ISS
Catalog Number: 25544
Epoch time: 13315
99684711 = yrday
fracday
Element set: 906
Inclination: 51
6451 deg
RA of node: 96
0304 deg
Eccentricity:
0000954
Arg of perigee: 107
5720 deg
Mean anomaly: 252
5535 deg
Mean motion: 15
49957662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1763
Checksum: 319
Coasting Arc #8 (Orbit 1778)
---------------------------------------
Vector Time (GMT): 2013/316/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886408
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3930164
21 A = 6790837
88 meter
Y = 2355091
91 meter E =
0006899
Z = 5008356
16 I = 51
98688
XDOT = -1606
369438 Wp = 121
46341
YDOT = -7189
875235 meter/sec RA = 90
37169 deg
ZDOT = 2114
716097 TA = 308
00642
MA = 308
06869
Ha = 227
879 n
mi
Hp = 220
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12894239
52 X = -3980536
96
Y = 7726679
51 feet Y = 2310860
86 meter
Z = 16431614
70 Z = 4989140
98
XDOT = -5270
240937 XDOT = -1536
124185
YDOT = -23588
829511 feet/sec YDOT = -7207
445836 meter/sec
ZDOT = 6938
044939 ZDOT = 2107
083254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4252070
55 X = -1296031
10
Y = 14510128
19 feet Y = 4422687
07 meter
Z = 16350444
24 Z = 4983615
40
XDOT = -18898
329486 XDOT = -5760
210827
YDOT = -13342
002594 feet/sec YDOT = -4066
642391 meter/sec
ZDOT = 6907
019814 ZDOT = 2105
259639
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 13317
02843565
00016717 00000-0 10270-3 0 9072
2 25544 51
6454 90
9206 0000758 109
4463 250
6769 15
50008711 17797
Satellite: ISS
Catalog Number: 25544
Epoch time: 13317
02843565 = yrday
fracday
Element set: 907
Inclination: 51
6454 deg
RA of node: 90
9206 deg
Eccentricity:
0000758
Arg of perigee: 109
4463 deg
Mean anomaly: 250
6769 deg
Mean motion: 15
50008711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1779
Checksum: 313
Coasting Arc #9 (Orbit 1793)
---------------------------------------
Vector Time (GMT): 2013/317/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886408
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3839898
49 A = 6790392
08 meter
Y = -2278640
64 meter E =
0014015
Z = -5128467
53 I = 51
98499
XDOT = 1941
118569 Wp = 78
49376
YDOT = 7192
300675 meter/sec RA = 85
43826 deg
ZDOT = -1743
545017 TA = 174
70057
MA = 174
68572
Ha = 227
792 n
mi
Hp = 220
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12598092
17 X = 3890006
62
Y = -7475855
13 feet Y = -2235420
44 meter
Z = -16825680
89 Z = -5109691
46
XDOT = 6368
499242 XDOT = 1869
018261
YDOT = 23596
786990 feet/sec YDOT = 7213
604308 meter/sec
ZDOT = -5720
292051 ZDOT = -1734
290387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3964234
12 X = 1208298
56
Y = -14196761
71 feet Y = -4327172
97 meter
Z = -16746363
14 Z = -5104291
48
XDOT = 19944
318428 XDOT = 6079
028257
YDOT = 12267
016495 feet/sec YDOT = 3738
986628 meter/sec
ZDOT = -5682
460713 ZDOT = -1732
014025
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 13317
99553867
00016717 00000-0 10270-3 0 9082
2 25544 51
6459 86
1286 0000818 104
6279 255
4962 15
50001604 17945
Satellite: ISS
Catalog Number: 25544
Epoch time: 13317
99553867 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node: 86
1286 deg
Eccentricity:
0000818
Arg of perigee: 104
6279 deg
Mean anomaly: 255
4962 deg
Mean motion: 15
50001604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1794
Checksum: 331
Coasting Arc #10 (Orbit 1809)
---------------------------------------
Vector Time (GMT): 2013/318/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886408
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3760756
94 A = 6789845
28 meter
Y = 2193535
23 meter E =
0005015
Z = 5207166
72 I = 51
98109
XDOT = -2288
218536 Wp = 122
16530
YDOT = -7185
536170 meter/sec RA = 80
50613 deg
ZDOT = 1370
755897 TA = 314
69310
MA = 314
73394
Ha = 227
785 n
mi
Hp = 220
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12338441
41 X = -3810301
66
Y = 7196637
88 feet Y = 2151203
12 meter
Z = 17083880
33 Z = 5188776
47
XDOT = -7507
278663 XDOT = -2214
357142
YDOT = -23574
593734 feet/sec YDOT = -7210
711479 meter/sec
ZDOT = 4497
230633 ZDOT = 1359
819206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3733749
26 X = -1138046
77
Y = 13882947
69 feet Y = 4231522
46 meter
Z = 17006192
40 Z = 5183487
44
XDOT = -20965
702039 XDOT = -6390
345982
YDOT = -11106
975971 feet/sec YDOT = -3385
406276 meter/sec
ZDOT = 4452
339703 ZDOT = 1357
073141
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 13319
02709982
00016717 00000-0 10270-3 0 9090
2 25544 51
6466 81
0189 0000674 105
7902 254
3323 15
50053836 18106
Satellite: ISS
Catalog Number: 25544
Epoch time: 13319
02709982 = yrday
fracday
Element set: 909
Inclination: 51
6466 deg
RA of node: 81
0189 deg
Eccentricity:
0000674
Arg of perigee: 105
7902 deg
Mean anomaly: 254
3323 deg
Mean motion: 15
50053836 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1810
Checksum: 300
Coasting Arc #11 (Orbit 1824)
---------------------------------------
Vector Time (GMT): 2013/319/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886408
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3729630
20 A = 6789575
22 meter
Y = -2093866
78 meter E =
0015054
Z = -5286082
18 I = 51
97455
XDOT = 2618
890120 Wp = 83
34797
YDOT = 7122
085826 meter/sec RA = 75
57172 deg
ZDOT = -974
034568 TA = 177
35501
MA = 177
34704
Ha = 227
689 n
mi
Hp = 220
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12236319
55 X = 3778446
11
Y = -6869641
66 feet Y = -2051886
75 meter
Z = -17342789
30 Z = -5267844
92
XDOT = 8592
159186 XDOT = 2543
786457
YDOT = 23366
423314 feet/sec YDOT = 7150
951992 meter/sec
ZDOT = -3195
651471 ZDOT = -961
494349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3659186
29 X = 1115319
98
Y = -13645362
77 feet Y = -4159106
57 meter
Z = -17265754
08 Z = -5262601
84
XDOT = 21775
637870 XDOT = 6637
214423
YDOT = 9814
768858 feet/sec YDOT = 2991
541548 meter/sec
ZDOT = -3144
022926 ZDOT = -958
298188
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 13319
99417724
00016717 00000-0 10270-3 0 9108
2 25544 51
6471 76
2271 0000721 100
4828 259
6404 15
50045433 18250
Satellite: ISS
Catalog Number: 25544
Epoch time: 13319
99417724 = yrday
fracday
Element set: 910
Inclination: 51
6471 deg
RA of node: 76
2271 deg
Eccentricity:
0000721
Arg of perigee: 100
4828 deg
Mean anomaly: 259
6404 deg
Mean motion: 15
50045433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1825
Checksum: 292
Coasting Arc #12 (Orbit 1840)
---------------------------------------
Vector Time (GMT): 2013/320/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886408
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3713516
39 A = 6789209
23 meter
Y = 1988655
47 meter E =
0003438
Z = 5321646
65 I = 51
96612
XDOT = -2952
367561 Wp = 110
55571
YDOT = -7050
005048 meter/sec RA = 70
63834 deg
ZDOT = 572
853646 TA = 333
99068
MA = 334
00796
Ha = 227
703 n
mi
Hp = 220
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12183452
71 X = -3761329
76
Y = 6524460
21 feet Y = 1946861
15 meter
Z = 17459470
63 Z = 5303490
15
XDOT = -9686
245279 XDOT = -2876
096257
YDOT = -23129
937823 feet/sec YDOT = -7082
593854 meter/sec
ZDOT = 1879
441096 ZDOT = 558
696094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3640200
46 X = -1109533
10
Y = 13432272
14 feet Y = 4094156
55 meter
Z = 17382785
20 Z = 5298272
93
XDOT = -22531
037599 XDOT = -6867
460260
YDOT = -8468
872638 feet/sec YDOT = -2581
312380 meter/sec
ZDOT = 1821
014702 ZDOT = 555
045281
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 13321
02571114
00016717 00000-0 10270-3 0 9110
2 25544 51
6479 71
1175 0000617 100
8966 259
2254 15
50096996 18413
Satellite: ISS
Catalog Number: 25544
Epoch time: 13321
02571114 = yrday
fracday
Element set: 911
Inclination: 51
6479 deg
RA of node: 71
1175 deg
Eccentricity:
0000617
Arg of perigee: 100
8966 deg
Mean anomaly: 259
2254 deg
Mean motion: 15
50096996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1841
Checksum: 297
Coasting Arc #13 (Orbit 1855)
---------------------------------------
Vector Time (GMT): 2013/321/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886408
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3745246
42 A = 6789151
08 meter
Y = -1884895
06 meter E =
0015515
Z = -5353130
01 I = 51
95510
XDOT = 3258
742156 Wp = 89
06194
YDOT = 6919
937596 meter/sec RA = 65
70243 deg
ZDOT = -156
794815 TA = 179
44767
MA = 179
44596
Ha = 227
609 n
mi
Hp = 220
894
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12287553
87 X = 3792050
06
Y = -6184038
91 feet Y = -1842751
46 meter
Z = -17562762
51 Z = -5334821
87
XDOT = 10691
411274 XDOT = 3181
881370
YDOT = 22703
207335 feet/sec YDOT = 6955
949176 meter/sec
ZDOT = -514
418683 ZDOT = -141
150224
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3731299
22 X = 1137300
00
Y = -13342166
45 feet Y = -4066692
33 meter
Z = -17485449
52 Z = -5329565
01
XDOT = 23036
762314 XDOT = 7021
605153
YDOT = 7031
273449 feet/sec YDOT = 2143
132147 meter/sec
ZDOT = -449
731365 ZDOT = -137
078120
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 13321
99276319
00016717 00000-0 10270-3 0 9126
2 25544 51
6483 66
3258 0000685 96
0092 264
1137 15
50088612 18564
Satellite: ISS
Catalog Number: 25544
Epoch time: 13321
99276319 = yrday
fracday
Element set: 912
Inclination: 51
6483 deg
RA of node: 66
3258 deg
Eccentricity:
0000685
Arg of perigee: 96
0092 deg
Mean anomaly: 264
1137 deg
Mean motion: 15
50088612 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1856
Checksum: 314
Coasting Arc #14 (Orbit 1871)
---------------------------------------
Vector Time (GMT): 2013/322/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886408
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3793959
12 A = 6789013
50 meter
Y = 1779465
52 meter E =
0003102
Z = 5338742
52 I = 51
94203
XDOT = -3557
540902 Wp = 80
03223
YDOT = -6783
887456 meter/sec RA = 60
76707 deg
ZDOT = -266
351019 TA = 12
50110
MA = 12
49341
Ha = 227
635 n
mi
Hp = 220
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12447372
44 X = -3839510
25
Y = 5838141
48 feet Y = 1736784
12 meter
Z = 17515559
45 Z = 5320200
84
XDOT = -11671
722120 XDOT = -3480
123676
YDOT = -22256
848610 feet/sec YDOT = -6823
237266 meter/sec
ZDOT = -873
855048 ZDOT = -283
445873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3866664
40 X = -1178559
31
Y = 13296846
88 feet Y = 4052878
93 meter
Z = 17437275
28 Z = 5314881
51
XDOT = -23465
615562 XDOT = -7152
319623
YDOT = -5582
069210 feet/sec YDOT = -1701
414695 meter/sec
ZDOT = -944
652153 ZDOT = -287
929976
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 13323
02427005
00016717 00000-0 10270-3 0 9133
2 25544 51
6487 61
2160 0000596 95
1776 264
9442 15
50138234 18725
Satellite: ISS
Catalog Number: 25544
Epoch time: 13323
02427005 = yrday
fracday
Element set: 913
Inclination: 51
6487 deg
RA of node: 61
2160 deg
Eccentricity:
0000596
Arg of perigee: 95
1776 deg
Mean anomaly: 264
9442 deg
Mean motion: 15
50138234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1872
Checksum: 292
Coasting Arc #15 (Orbit 1886)
---------------------------------------
Vector Time (GMT): 2013/323/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886408
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3885975
73 A = 6789190
10 meter
Y = -1691423
68 meter E =
0015268
Z = -5317160
42 I = 51
92705
XDOT = 3818
707432 Wp = 95
15102
YDOT = 6593
029044 meter/sec RA = 55
82909 deg
ZDOT = 693
947473 TA = 181
46309
MA = 181
46756
Ha = 227
545 n
mi
Hp = 220
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12749264
21 X = 3930430
60
Y = -5549290
30 feet Y = -1647719
39 meter
Z = -17444752
04 Z = -5298174
46
XDOT = 12528
567691 XDOT = 3741
327834
YDOT = 21630
672718 feet/sec YDOT = 6635
299570 meter/sec
ZDOT = 2276
730554 ZDOT = 712
311152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4052546
79 X = 1235216
26
Y = -13405408
62 feet Y = -4085968
55 meter
Z = -17364608
23 Z = -5292732
59
XDOT = 23623
642629 XDOT = 7200
486273
YDOT = 4095
424299 feet/sec YDOT = 1248
285326 meter/sec
ZDOT = 2352
885996 ZDOT = 717
159652
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 13323
99129688
00016717 00000-0 10270-3 0 9146
2 25544 51
6491 56
4243 0000691 92
3707 267
7523 15
50131201 18871
Satellite: ISS
Catalog Number: 25544
Epoch time: 13323
99129688 = yrday
fracday
Element set: 914
Inclination: 51
6491 deg
RA of node: 56
4243 deg
Eccentricity:
0000691
Arg of perigee: 92
3707 deg
Mean anomaly: 267
7523 deg
Mean motion: 15
50131201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1887
Checksum: 311
Coasting Arc #16 (Orbit 1902)
---------------------------------------
Vector Time (GMT): 2013/324/23:26:00
000
Vector Time (MET): N/A
Weight (LBS) : 886408
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3994640
52 A = 6789310
62 meter
Y = 1605716
41 meter E =
0004451
Z = 5246718
33 I = 51
90974
XDOT = -4061
698160 Wp = 60
32756
YDOT = -6401
116349 meter/sec RA = 50
89100 deg
ZDOT = -1130
538582 TA = 40
49048
MA = 40
45737
Ha = 227
576 n
mi
Hp = 220
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13105775
99 X = -4037786
64
Y = 5268098
45 feet Y = 1560804
27 meter
Z = 17213642
81 Z = 5227207
71
XDOT = -13325
781365 XDOT = -3984
325649
YDOT = -21001
037891 feet/sec YDOT = -6446
104168 meter/sec
ZDOT = -3709
116083 ZDOT = -1150
082661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4263669
26 X = -1299566
39
Y = 13570679
45 feet Y = 4136343
10 meter
Z = 17131302
00 Z = 5221620
85
XDOT = -23693
594330 XDOT = -7221
807552
YDOT = -2647
456221 feet/sec YDOT = -806
944656 meter/sec
ZDOT = -3790
260608 ZDOT = -1155
271433
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 13325
02277700
00016717 00000-0 10270-3 0 9152
2 25544 51
6490 51
3140 0000607 89
6629 270
4591 15
50178728 19039
Satellite: ISS
Catalog Number: 25544
Epoch time: 13325
02277700 = yrday
fracday
Element set: 915
Inclination: 51
6490 deg
RA of node: 51
3140 deg
Eccentricity:
0000607
Arg of perigee: 89
6629 deg
Mean anomaly: 270
4591 deg
Mean motion: 15
50178728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1903
Checksum: 295
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