[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 15th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12378 5 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 940 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
329/19:52:15
137 0
9 1
0 1
0
N/A 0
1 -0
1 220
0
000/00:02:30
275 0
3 -0
0 212
9
Coasting Arc #1 (Orbit 1095)
---------------------------------------
Vector Time (GMT): 2015/315/11:29:00
069
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2203560
90 A = 6786757
97 meter
Y = -6397321
66 meter E =
0017439
Z = -417189
30 I = 52
00538
XDOT = 4591
767928 Wp = 135
07148
YDOT = -1199
251539 meter/sec RA = 68
23309 deg
ZDOT = -6028
534020 TA = 49
40736
MA = 49
25574
Ha = 221
713 n
mi
Hp = 211
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7229530
50 X = -2129834
10
Y = -20988588
11 feet Y = -6421551
10 meter
Z = -1368731
29 Z = -427714
88
XDOT = 15064
855408 XDOT = 4634
122140
YDOT = -3934
552293 feet/sec YDOT = -1147
666642 meter/sec
ZDOT = -19778
654921 ZDOT = -6006
124596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19353715
48 X = 5899012
48
Y = 10867268
94 feet Y = 3312343
57 meter
Z = -1412986
38 Z = -430678
25
XDOT = -7930
918643 XDOT = -2417
344002
YDOT = 11633
418748 feet/sec YDOT = 3545
866034 meter/sec
ZDOT = -19681
564269 ZDOT = -5998
940789
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 15315
50983502
00016717 00000-0 10270-3 0 9004
2 25544 51
6434 68
8130 0006272 130
4665 229
7036 15
54986895 10968
Satellite: ISS
Catalog Number: 25544
Epoch time: 15315
50983502 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 68
8130 deg
Eccentricity:
0006272
Arg of perigee: 130
4665 deg
Mean anomaly: 229
7036 deg
Mean motion: 15
54986895 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1096
Checksum: 316
Coasting Arc #2 (Orbit 1111)
---------------------------------------
Vector Time (GMT): 2015/316/11:29:00
069
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1119508
51 A = 6784404
34 meter
Y = 6268435
76 meter E =
0017782
Z = 2326330
75 I = 51
98651
XDOT = -5302
570420 Wp = 90
68553
YDOT = -1083
726593 meter/sec RA = 63
28103 deg
ZDOT = 5435
981493 TA = 295
13469
MA = 295
31905
Ha = 221
610 n
mi
Hp = 211
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3672928
20 X = 1038029
39
Y = 20565734
11 feet Y = 6280499
26 meter
Z = 7632318
74 Z = 2331571
35
XDOT = -17396
884581 XDOT = -5316
464489
YDOT = -3555
533442 feet/sec YDOT = -1143
101129 meter/sec
ZDOT = 17834
584951 ZDOT = 5410
188197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16607736
01 X = -5062037
94
Y = -12660784
67 feet Y = -3859007
17 meter
Z = 7653740
69 Z = 2332860
16
XDOT = 14357
804976 XDOT = 4376
258957
YDOT = -8048
519344 feet/sec YDOT = -2453
188696 meter/sec
ZDOT = 17723
312482 ZDOT = 5402
065645
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 15316
53809224
00016717 00000-0 10270-3 0 9017
2 25544 51
6446 63
6809 0006290 133
7326 226
4349 15
55030227 11127
Satellite: ISS
Catalog Number: 25544
Epoch time: 15316
53809224 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 63
6809 deg
Eccentricity:
0006290
Arg of perigee: 133
7326 deg
Mean anomaly: 226
4349 deg
Mean motion: 15
55030227 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1112
Checksum: 288
Coasting Arc #3 (Orbit 1126)
---------------------------------------
Vector Time (GMT): 2015/317/11:29:00
069
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 248921
38 A = 6780068
04 meter
Y = -5500865
12 meter E =
0010961
Z = -3962959
88 I = 51
95711
XDOT = 5680
551711 Wp = 103
25128
YDOT = 3167
421329 meter/sec RA = 58
31700 deg
ZDOT = -4051
634882 TA = 124
62651
MA = 124
52310
Ha = 221
540 n
mi
Hp = 211
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 816671
20 X = 329665
95
Y = -18047457
74 feet Y = -5497629
98 meter
Z = -13001836
87 Z = -3961554
60
XDOT = 18636
980678 XDOT = 5664
392450
YDOT = 10391
802259 feet/sec YDOT = 3230
854721 meter/sec
ZDOT = -13292
765361 ZDOT = -4024
078375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11812348
17 X = 3600403
72
Y = 13675978
48 feet Y = 4168438
24 meter
Z = -12994671
52 Z = -3960775
88
XDOT = -19719
129821 XDOT = -6010
390769
YDOT = 4550
953396 feet/sec YDOT = 1387
130595 meter/sec
ZDOT = -13174
286558 ZDOT = -4015
522543
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 15317
50206744
00016717 00000-0 10270-3 0 9024
2 25544 51
6448 58
8694 0006177 137
2359 222
9276 15
55025676 11274
Satellite: ISS
Catalog Number: 25544
Epoch time: 15317
50206744 = yrday
fracday
Element set: 902
Inclination: 51
6448 deg
RA of node: 58
8694 deg
Eccentricity:
0006177
Arg of perigee: 137
2359 deg
Mean anomaly: 222
9276 deg
Mean motion: 15
55025676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1127
Checksum: 322
Coasting Arc #4 (Orbit 1142)
---------------------------------------
Vector Time (GMT): 2015/318/11:29:00
069
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1723004
54 A = 6775951
63 meter
Y = 4236977
30 meter E =
0012068
Z = 4994028
43 I = 51
92692
XDOT = -5618
919364 Wp = 131
29994
YDOT = -4782
915556 meter/sec RA = 53
33764 deg
ZDOT = 2108
207696 TA = 298
21511
MA = 298
33691
Ha = 221
405 n
mi
Hp = 211
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5652902
02 X = -1794515
05
Y = 13900844
17 feet Y = 4217309
56 meter
Z = 16384607
71 Z = 4985484
64
XDOT = -18434
774817 XDOT = -5575
259129
YDOT = -15691
980170 feet/sec YDOT = -4845
505957 meter/sec
ZDOT = 6916
691917 ZDOT = 2081
017392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5676116
77 X = -1730080
39
Y = -13935817
54 feet Y = -4247637
19 meter
Z = 16346829
28 Z = 4982513
56
XDOT = 23156
945871 XDOT = 7058
237101
YDOT = -1412
657490 feet/sec YDOT = -430
578003 meter/sec
ZDOT = 6800
124857 ZDOT = 2072
678057
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 15318
53028676
00016717 00000-0 10270-3 0 9035
2 25544 51
6453 53
7368 0006106 140
0747 220
0856 15
55098233 11437
Satellite: ISS
Catalog Number: 25544
Epoch time: 15318
53028676 = yrday
fracday
Element set: 903
Inclination: 51
6453 deg
RA of node: 53
7368 deg
Eccentricity:
0006106
Arg of perigee: 140
0747 deg
Mean anomaly: 220
0856 deg
Mean motion: 15
55098233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1143
Checksum: 296
Coasting Arc #5 (Orbit 1157)
---------------------------------------
Vector Time (GMT): 2015/319/11:29:00
069
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3257318
93 A = 6774551
28 meter
Y = -2636400
37 meter E =
0019228
Z = -5339054
70 I = 51
90224
XDOT = 4986
598463 Wp = 105
23135
YDOT = 5807
173497 meter/sec RA = 48
34776 deg
ZDOT = 170
328517 TA = 166
41451
MA = 166
36269
Ha = 221
285 n
mi
Hp = 211
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10686741
90 X = 3312493
32
Y = -8649607
51 feet Y = -2599666
21 meter
Z = -17516583
66 Z = -5323097
05
XDOT = 16360
231177 XDOT = 4920
463205
YDOT = 19052
406485 feet/sec YDOT = 5862
567140 meter/sec
ZDOT = 558
820593 ZDOT = 194
392441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1363842
58 X = -415699
22
Y = 13769253
96 feet Y = 4196868
61 meter
Z = -17447075
53 Z = -5317868
62
XDOT = -24053
556374 XDOT = -7331
523983
YDOT = -1525
727388 feet/sec YDOT = -465
041708 meter/sec
ZDOT = 661
660140 ZDOT = 201
674011
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 15319
49422723
00016717 00000-0 10270-3 0 9043
2 25544 51
6452 48
9255 0005993 142
3447 217
8126 15
55098020 11586
Satellite: ISS
Catalog Number: 25544
Epoch time: 15319
49422723 = yrday
fracday
Element set: 904
Inclination: 51
6452 deg
RA of node: 48
9255 deg
Eccentricity:
0005993
Arg of perigee: 142
3447 deg
Mean anomaly: 217
8126 deg
Mean motion: 15
55098020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1158
Checksum: 313
Coasting Arc #6 (Orbit 1173)
---------------------------------------
Vector Time (GMT): 2015/320/11:29:00
069
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4604454
60 A = 6776378
87 meter
Y = 915446
76 meter E =
0009571
Z = 4878101
25 I = 51
88684
XDOT = -3806
359276 Wp = 97
52112
YDOT = -6209
927498 meter/sec RA = 43
35627 deg
ZDOT = -2424
614918 TA = 16
16190
MA = 16
13140
Ha = 221
300 n
mi
Hp = 211
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15106478
34 X = -4638045
47
Y = 3003434
27 feet Y = 863768
75 meter
Z = 16004269
18 Z = 4855651
80
XDOT = -12488
055368 XDOT = -3724
857404
YDOT = -20373
777881 feet/sec YDOT = -6252
036942 meter/sec
ZDOT = -7954
773354 ZDOT = -2442
907975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8259645
63 X = 2517539
99
Y = -13118957
35 feet Y = -3998658
20 meter
Z = 15907047
16 Z = 4848467
97
XDOT = 22394
732654 XDOT = 6825
914513
YDOT = 4348
595224 feet/sec YDOT = 1325
451824 meter/sec
ZDOT = -8032
579401 ZDOT = -2448
330201
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 15320
52241100
00016717 00000-0 10270-3 0 9058
2 25544 51
6452 43
7922 0005941 144
9855 215
1690 15
55140757 11744
Satellite: ISS
Catalog Number: 25544
Epoch time: 15320
52241100 = yrday
fracday
Element set: 905
Inclination: 51
6452 deg
RA of node: 43
7922 deg
Eccentricity:
0005941
Arg of perigee: 144
9855 deg
Mean anomaly: 215
1690 deg
Mean motion: 15
55140757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1174
Checksum: 286
Coasting Arc #7 (Orbit 1188)
---------------------------------------
Vector Time (GMT): 2015/321/11:29:00
069
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5628496
74 A = 6780584
75 meter
Y = 730688
78 meter E =
0010548
Z = -3722596
46 I = 51
87687
XDOT = 2080
403229 Wp = 124
86815
YDOT = 5972
295060 meter/sec RA = 38
37437 deg
ZDOT = 4320
597985 TA = 190
93284
MA = 190
95578
Ha = 221
063 n
mi
Hp = 211
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18466196
65 X = 5637990
87
Y = 2397272
89 feet Y = 793683
51 meter
Z = -12213242
98 Z = -3695230
91
XDOT = 6825
469911 XDOT = 1992
476847
YDOT = 19594
143898 feet/sec YDOT = 5995
067780 meter/sec
ZDOT = 14175
190240 ZDOT = 4330
490868
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14270578
57 X = -4349672
35
Y = 12081787
57 feet Y = 3682528
85 meter
Z = -12095107
95 Z = -3686588
90
XDOT = -18132
667802 XDOT = -5526
837146
YDOT = -7194
535432 feet/sec YDOT = -2192
894400 meter/sec
ZDOT = 14216
729224 ZDOT = 4333
259067
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 15321
48631667
00016717 00000-0 10270-3 0 9066
2 25544 51
6449 38
9804 0005924 148
8000 211
3506 15
55155866 11898
Satellite: ISS
Catalog Number: 25544
Epoch time: 15321
48631667 = yrday
fracday
Element set: 906
Inclination: 51
6449 deg
RA of node: 38
9804 deg
Eccentricity:
0005924
Arg of perigee: 148
8000 deg
Mean anomaly: 211
3506 deg
Mean motion: 15
55155866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1189
Checksum: 318
Coasting Arc #8 (Orbit 1204)
---------------------------------------
Vector Time (GMT): 2015/322/11:29:00
069
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6105927
36 A = 6784714
98 meter
Y = -2168406
00 meter E =
0018960
Z = 1976093
10 I = 51
86475
XDOT = 39
519953 Wp = 123
28445
YDOT = -5245
331129 meter/sec RA = 33
40467 deg
ZDOT = -5605
156017 TA = 34
94622
MA = 34
82192
Ha = 221
061 n
mi
Hp = 211
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20032570
08 X = -6090825
13
Y = -7114192
91 feet Y = -2236602
09 meter
Z = 6483245
08 Z = 1946468
04
XDOT = 129
658639 XDOT = 125
399625
YDOT = -17209
091629 feet/sec YDOT = -5244
408957 meter/sec
ZDOT = -18389
619477 ZDOT = -5604
755487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18610873
83 X = 5672594
34
Y = -10353224
78 feet Y = -3155662
91 meter
Z = 6355641
86 Z = 1937199
64
XDOT = 11991
567430 XDOT = 3655
029753
YDOT = 10210
014057 feet/sec YDOT = 3112
012285 meter/sec
ZDOT = -18386
811050 ZDOT = -5604
300008
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 15322
51446532
00016717 00000-0 10270-3 0 9077
2 25544 51
6444 33
8470 0005916 150
9322 209
2161 15
55169975 12056
Satellite: ISS
Catalog Number: 25544
Epoch time: 15322
51446532 = yrday
fracday
Element set: 907
Inclination: 51
6444 deg
RA of node: 33
8470 deg
Eccentricity:
0005916
Arg of perigee: 150
9322 deg
Mean anomaly: 209
2161 deg
Mean motion: 15
55169975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1205
Checksum: 297
Coasting Arc #9 (Orbit 1220)
---------------------------------------
Vector Time (GMT): 2015/323/11:29:00
069
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5952020
28 A = 6786288
15 meter
Y = 3254747
82 meter E =
0011859
Z = 34428
61 I = 51
84332
XDOT = -2307
009592 Wp = 73
07051
YDOT = 4137
019380 meter/sec RA = 28
44273 deg
ZDOT = 6028
312155 TA = 287
29929
MA = 287
42900
Ha = 220
881 n
mi
Hp = 211
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19527625
58 X = 5915015
28
Y = 10678306
50 feet Y = 3321100
33 meter
Z = 112954
74 Z = 63252
78
XDOT = -7568
929107 XDOT = -2382
382893
YDOT = 13572
898229 feet/sec YDOT = 4110
799472 meter/sec
ZDOT = 19777
927019 ZDOT = 6016
921930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20789432
20 X = -6336618
93
Y = 7944215
04 feet Y = 2421396
74 meter
Z = 236866
78 Z = 72196
99
XDOT = -4767
296395 XDOT = -1453
071941
YDOT = -13143
638652 feet/sec YDOT = -4006
181061 meter/sec
ZDOT = 19727
844577 ZDOT = 6013
047027
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 15323
54259578
00016717 00000-0 10270-3 0 9084
2 25544 51
6447 28
7133 0005695 153
9785 206
1655 15
55173701 12212
Satellite: ISS
Catalog Number: 25544
Epoch time: 15323
54259578 = yrday
fracday
Element set: 908
Inclination: 51
6447 deg
RA of node: 28
7133 deg
Eccentricity:
0005695
Arg of perigee: 153
9785 deg
Mean anomaly: 206
1655 deg
Mean motion: 15
55173701 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1221
Checksum: 320
Coasting Arc #10 (Orbit 1235)
---------------------------------------
Vector Time (GMT): 2015/324/11:29:00
069
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5064593
66 A = 6784240
83 meter
Y = -3993005
11 meter E =
0011984
Z = -2090532
39 I = 51
80786
XDOT = 4492
405482 Wp = 146
87378
YDOT = -2806
664489 meter/sec RA = 23
47888 deg
ZDOT = -5547
367775 TA = 56
22599
MA = 56
11189
Ha = 220
717 n
mi
Hp = 211
857
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16616120
94 X = -5009411
33
Y = -13100410
46 feet Y = -4049332
23 meter
Z = -6858702
07 Z = -2115001
42
XDOT = 14738
863129 XDOT = 4550
403789
YDOT = -9208
216826 feet/sec YDOT = -2756
103251 meter/sec
ZDOT = -18200
025510 ZDOT = -5525
403336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20644555
98 X = 6292460
66
Y = -4479752
10 feet Y = -1365428
44 meter
Z = -6963630
72 Z = -2122514
64
XDOT = -2647
402525 XDOT = -806
928290
YDOT = 15818
169955 feet/sec YDOT = 4821
378202 meter/sec
ZDOT = -18104
516879 ZDOT = -5518
256745
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 15324
50645079
00016717 00000-0 10270-3 0 9097
2 25544 51
6441 23
9005 0005776 157
1864 202
9547 15
55220239 12364
Satellite: ISS
Catalog Number: 25544
Epoch time: 15324
50645079 = yrday
fracday
Element set: 909
Inclination: 51
6441 deg
RA of node: 23
9005 deg
Eccentricity:
0005776
Arg of perigee: 157
1864 deg
Mean anomaly: 202
9547 deg
Mean motion: 15
55220239 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1236
Checksum: 305
Coasting Arc #11 (Orbit 1251)
---------------------------------------
Vector Time (GMT): 2015/325/11:29:00
069
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3564546
83 A = 6779851
58 meter
Y = 4341902
33 meter E =
0014894
Z = 3790106
60 I = 51
76454
XDOT = -6243
425893 Wp = 117
01139
YDOT = 1420
918840 meter/sec RA = 18
50195 deg
ZDOT = 4224
698139 TA = 288
38974
MA = 288
55164
Ha = 220
546 n
mi
Hp = 211
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11694707
45 X = 3497318
47
Y = 14245086
39 feet Y = 4381387
63 meter
Z = 12434732
93 Z = 3807259
37
XDOT = -20483
680750 XDOT = -6279
373263
YDOT = 4661
807217 feet/sec YDOT = 1350
899823 meter/sec
ZDOT = 13860
558200 ZDOT = 4194
280950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18379463
26 X = -5602060
40
Y = 239749
91 feet Y = 73075
77 meter
Z = 12507961
54 Z = 3812426
68
XDOT = 9155
499869 XDOT = 2790
596360
YDOT = -17671
457897 feet/sec YDOT = -5386
260367 meter/sec
ZDOT = 13728
810694 ZDOT = 4184
541500
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 15325
53454526
00016717 00000-0 10270-3 0 9108
2 25544 51
6446 18
7668 0005697 161
0522 199
0844 15
55266863 12520
Satellite: ISS
Catalog Number: 25544
Epoch time: 15325
53454526 = yrday
fracday
Element set: 910
Inclination: 51
6446 deg
RA of node: 18
7668 deg
Eccentricity:
0005697
Arg of perigee: 161
0522 deg
Mean anomaly: 199
0844 deg
Mean motion: 15
55266863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1252
Checksum: 322
Coasting Arc #12 (Orbit 1266)
---------------------------------------
Vector Time (GMT): 2015/326/11:29:00
069
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1527265
93 A = 6775629
53 meter
Y = -4382609
64 meter E =
0013687
Z = -4947594
58 I = 51
71937
XDOT = 7329
657834 Wp = 97
84728
YDOT = -47
409922 meter/sec RA = 13
50742 deg
ZDOT = -2227
684548 TA = 150
44887
MA = 150
37144
Ha = 220
518 n
mi
Hp = 211
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5010715
01 X = -1454110
97
Y = -14378640
54 feet Y = -4399279
57 meter
Z = -16232265
68 Z = -4954836
14
XDOT = 24047
433839 XDOT = 7340
464696
YDOT = -155
544362 feet/sec YDOT = 34
615544 meter/sec
ZDOT = -7308
676337 ZDOT = -2192
051534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14399219
68 X = 4388882
16
Y = 4850546
84 feet Y = 1478446
68 meter
Z = -16262646
94 Z = -4956854
79
XDOT = -14175
352867 XDOT = -4320
647554
YDOT = 18170
734846 feet/sec YDOT = 5538
439981 meter/sec
ZDOT = -7154
682441 ZDOT = -2180
747208
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 15326
49837019
00016717 00000-0 10270-3 0 9117
2 25544 51
6442 13
9537 0005628 163
5532 196
5805 15
55260154 12672
Satellite: ISS
Catalog Number: 25544
Epoch time: 15326
49837019 = yrday
fracday
Element set: 911
Inclination: 51
6442 deg
RA of node: 13
9537 deg
Eccentricity:
0005628
Arg of perigee: 163
5532 deg
Mean anomaly: 196
5805 deg
Mean motion: 15
55260154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1267
Checksum: 313
Coasting Arc #13 (Orbit 1282)
---------------------------------------
Vector Time (GMT): 2015/327/11:29:00
069
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -726594
13 A = 6773877
83 meter
Y = 4135799
61 meter E =
0006294
Z = 5312034
19 I = 51
68287
XDOT = -7577
076892 Wp = 143
71123
YDOT = -1211
135215 meter/sec RA = 8
50105 deg
ZDOT = -98
359630 TA = 307
19611
MA = 307
25355
Ha = 220
346 n
mi
Hp = 212
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2383839
02 X = -798592
11
Y = 13568896
37 feet Y = 4127271
78 meter
Z = 17427933
68 Z = 5308329
58
XDOT = -24859
176154 XDOT = -7562
492727
YDOT = -3973
540731 feet/sec YDOT = -1295
785545 meter/sec
ZDOT = -322
702197 ZDOT = -135
133012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9429488
13 X = -2874107
98
Y = -10073243
87 feet Y = -3070324
73 meter
Z = 17411060
31 Z = 5306891
18
XDOT = 17236
206847 XDOT = 5253
595847
YDOT = -16938
845690 feet/sec YDOT = -5162
960166 meter/sec
ZDOT = -481
351292 ZDOT = -146
715874
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 15327
52643102
00016717 00000-0 10270-3 0 9121
2 25544 51
6443 8
8203 0005542 166
9367 193
1931 15
55321469 12832
Satellite: ISS
Catalog Number: 25544
Epoch time: 15327
52643102 = yrday
fracday
Element set: 912
Inclination: 51
6443 deg
RA of node: 8
8203 deg
Eccentricity:
0005542
Arg of perigee: 166
9367 deg
Mean anomaly: 193
1931 deg
Mean motion: 15
55321469 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1283
Checksum: 297
Coasting Arc #14 (Orbit 1297)
---------------------------------------
Vector Time (GMT): 2015/328/11:29:00
069
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2972000
34 A = 6775918
27 meter
Y = -3676399
49 meter E =
0015102
Z = -4868292
32 I = 51
65776
XDOT = 6876
214875 Wp = 125
50105
YDOT = 2341
941861 meter/sec RA = 3
49160 deg
ZDOT = 2425
965705 TA = 168
33724
MA = 168
30222
Ha = 220
266 n
mi
Hp = 212
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9750657
29 X = 3036538
75
Y = -12061678
11 feet Y = -3642803
65 meter
Z = -15972087
66 Z = -4853697
90
XDOT = 22559
760090 XDOT = 6837
730937
YDOT = 7683
536289 feet/sec YDOT = 2418
621000 meter/sec
ZDOT = 7959
205069 ZDOT = 2459
276394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4103009
19 X = 1250597
20
Y = 15025304
73 feet Y = 4579712
88 meter
Z = -15908253
02 Z = -4848835
52
XDOT = -18227
554261 XDOT = -5555
758539
YDOT = 13567
630489 feet/sec YDOT = 4135
413773 meter/sec
ZDOT = 8102
645405 ZDOT = 2469
686319
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 15328
49022442
00016717 00000-0 10270-3 0 9137
2 25544 51
6443 4
0066 0005419 168
6881 191
4395 15
55318583 12984
Satellite: ISS
Catalog Number: 25544
Epoch time: 15328
49022442 = yrday
fracday
Element set: 913
Inclination: 51
6443 deg
RA of node: 4
0066 deg
Eccentricity:
0005419
Arg of perigee: 168
6881 deg
Mean anomaly: 191
4395 deg
Mean motion: 15
55318583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1298
Checksum: 315
Coasting Arc #15 (Orbit 1313)
---------------------------------------
Vector Time (GMT): 2015/329/11:29:00
069
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4860777
66 A = 6780177
74 meter
Y = 3004895
39 meter E =
0013515
Z = 3633742
99 I = 51
64012
XDOT = -5346
150869 Wp = 109
29751
YDOT = -3332
395138 meter/sec RA = 358
49192 deg
ZDOT = -4386
805851 TA = 27
52184
MA = 27
45034
Ha = 220
171 n
mi
Hp = 212
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15947433
27 X = -4911669
62
Y = 9858580
67 feet Y = 2950254
24 meter
Z = 11921728
97 Z = 3610006
27
XDOT = -17539
865057 XDOT = -5287
179936
YDOT = -10933
054914 feet/sec YDOT = -3391
849394 meter/sec
ZDOT = -14392
407648 ZDOT = -4412
633914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 950263
27 X = 289640
24
Y = -18789868
27 feet Y = -5727151
85 meter
Z = 11818532
57 Z = 3602288
73
XDOT = 17523
558194 XDOT = 5341
180538
YDOT = -8254
702993 feet/sec YDOT = -2516
033472 meter/sec
ZDOT = -14503
300987 ZDOT = -4420
606141
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 15329
51825233
00016717 00000-0 10270-3 0 9141
2 25544 51
6438 358
8724 0005363 172
0268 188
0971 15
55378695 13146
Satellite: ISS
Catalog Number: 25544
Epoch time: 15329
51825233 = yrday
fracday
Element set: 914
Inclination: 51
6438 deg
RA of node: 358
8724 deg
Eccentricity:
0005363
Arg of perigee: 172
0268 deg
Mean anomaly: 188
0971 deg
Mean motion: 15
55378695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1314
Checksum: 331
Coasting Arc #16 (Orbit 1318)
---------------------------------------
Vector Time (GMT): 2015/329/19:53:30
275
Vector Time (MET): N/A
Weight (LBS) : 906927
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3157836
07 A = 6777311
02 meter
Y = -3842058
49 meter E =
0012570
Z = -4616491
31 I = 51
61843
XDOT = 6771
904306 Wp = 130
85799
YDOT = 1980
219658 meter/sec RA = 356
74516 deg
ZDOT = 2981
459492 TA = 168
92821
MA = 168
90052
Ha = 220
030 n
mi
Hp = 212
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10360354
56 X = 3222989
87
Y = -12605178
78 feet Y = -3806380
94 meter
Z = -15145968
85 Z = -4600992
77
XDOT = 22217
533811 XDOT = 6734
774576
YDOT = 6496
783655 feet/sec YDOT = 2055
739795 meter/sec
ZDOT = 9781
691246 ZDOT = 3014
266714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10017336
35 X = 3053284
12
Y = -12958742
13 feet Y = -3949824
60 meter
Z = -15078190
41 Z = -4595832
44
XDOT = 21419
874654 XDOT = 6528
777794
YDOT = 5001
536531 feet/sec YDOT = 1524
468335 meter/sec
ZDOT = 9923
024269 ZDOT = 3024
537797
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 15329
83950905
00016717 00000-0 10270-3 0 9152
2 25544 51
6447 357
2679 0004824 181
0118 179
1026 15
55186279 13195
Satellite: ISS
Catalog Number: 25544
Epoch time: 15329
83950905 = yrday
fracday
Element set: 915
Inclination: 51
6447 deg
RA of node: 357
2679 deg
Eccentricity:
0004824
Arg of perigee: 181
0118 deg
Mean anomaly: 179
1026 deg
Mean motion: 15
55186279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1319
Checksum: 331
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