[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 24th 2015
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) : 131 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 219 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
057/09:19:29
121 0
1 2
7 2
7
N/A 2
6 -0
2 222
6
000/00:05:58
241 0
7 0
2 211
2
062/07:21:36
413 -0
6 1
4 1
4
N/A -1
2 -0
1 222
7
000/00:03:12
826 -0
1 0
1 211
3
Coasting Arc #1 (Orbit 1034)
---------------------------------------
Vector Time (GMT): 2015/054/12:03:48
714
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3316879
14 A = 6774934
89 meter
Y = 2878959
51 meter E =
0010277
Z = 5154049
97 I = 51
29019
XDOT = -3677
033739 Wp = 41
46784
YDOT = 6606
339039 meter/sec RA = 291
08895 deg
ZDOT = -1314
752496 TA = 61
26651
MA = 61
16329
Ha = 221
051 n
mi
Hp = 211
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10882149
41 X = 3259403
20
Y = 9445405
22 feet Y = 2915730
20 meter
Z = 16909612
77 Z = 5170022
67
XDOT = -12063
758986 XDOT = -3744
247579
YDOT = 21674
340680 feet/sec YDOT = 6564
844097 meter/sec
ZDOT = -4313
492440 ZDOT = -1332
778598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5353983
84 X = 1631894
28
Y = 13291893
82 feet Y = 4051369
24 meter
Z = 16977404
85 Z = 5174713
00
XDOT = -19550
568943 XDOT = -5959
013414
YDOT = 13522
396614 feet/sec YDOT = 4121
626488 meter/sec
ZDOT = -4391
779209 ZDOT = -1338
614303
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 15054
54858180
00016717 00000-0 10270-3 0 9001
2 25544 51
6454 291
5977 0006145 32
2991 327
8538 15
55161309 10350
Satellite: ISS
Catalog Number: 25544
Epoch time: 15054
54858180 = yrday
fracday
Element set: 900
Inclination: 51
6454 deg
RA of node: 291
5977 deg
Eccentricity:
0006145
Arg of perigee: 32
2991 deg
Mean anomaly: 327
8538 deg
Mean motion: 15
55161309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1035
Checksum: 315
Coasting Arc #2 (Orbit 1049)
---------------------------------------
Vector Time (GMT): 2015/055/12:03:48
714
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2277256
32 A = 6778252
89 meter
Y = -4683837
78 meter E =
0011922
Z = -4347282
62 I = 51
29019
XDOT = 4370
189472 Wp = 80
50225
YDOT = -5285
812726 meter/sec RA = 286
05877 deg
ZDOT = 3415
733496 TA = 224
29143
MA = 224
38689
Ha = 221
151 n
mi
Hp = 211
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7471313
40 X = -2203594
01
Y = -15366921
84 feet Y = -4708892
06 meter
Z = -14262738
24 Z = -4358165
64
XDOT = 14337
891970 XDOT = 4412
379671
YDOT = -17341
905269 feet/sec YDOT = -5236
706210 meter/sec
ZDOT = 11206
474725 ZDOT = 3437
065788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 53106
03 X = 16186
72
Y = -17048582
36 feet Y = -5196407
90 meter
Z = -14308442
69 Z = -4361213
33
XDOT = 19153
769073 XDOT = 5838
068813
YDOT = -9395
667369 feet/sec YDOT = -2863
799414 meter/sec
ZDOT = 11298
657043 ZDOT = 3443
830667
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 15055
51248444
00016717 00000-0 10270-3 0 9016
2 25544 51
6448 286
7846 0006140 35
1777 324
9781 15
55164846 10507
Satellite: ISS
Catalog Number: 25544
Epoch time: 15055
51248444 = yrday
fracday
Element set: 901
Inclination: 51
6448 deg
RA of node: 286
7846 deg
Eccentricity:
0006140
Arg of perigee: 35
1777 deg
Mean anomaly: 324
9781 deg
Mean motion: 15
55164846 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1050
Checksum: 317
Coasting Arc #3 (Orbit 1065)
---------------------------------------
Vector Time (GMT): 2015/056/12:03:48
714
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1144131
40 A = 6782726
04 meter
Y = 6044102
23 meter E =
0017283
Z = 2846418
78 I = 51
29791
XDOT = -4756
651095 Wp = 80
72728
YDOT = 3288
040188 meter/sec RA = 281
04214 deg
ZDOT = -5040
905600 TA = 66
71766
MA = 66
53584
Ha = 221
186 n
mi
Hp = 211
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3753711
94 X = 1062633
09
Y = 19829731
74 feet Y = 6056441
20 meter
Z = 9338644
28 Z = 2851778
26
XDOT = -15605
810678 XDOT = -4768
578632
YDOT = 10787
533426 feet/sec YDOT = 3234
781125 meter/sec
ZDOT = -16538
404200 ZDOT = -5064
041477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4979963
99 X = -1517893
02
Y = 19547380
29 feet Y = 5958041
51 meter
Z = 9360490
03 Z = 2853077
36
XDOT = -17172
621739 XDOT = -5234
215106
YDOT = 3637
732048 feet/sec YDOT = 1108
780728 meter/sec
ZDOT = -16637
939560 ZDOT = -5071
243978
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 15056
54062706
00016717 00000-0 10270-3 0 9026
2 25544 51
6450 281
6510 0006253 38
5260 321
6338 15
55213054 10666
Satellite: ISS
Catalog Number: 25544
Epoch time: 15056
54062706 = yrday
fracday
Element set: 902
Inclination: 51
6450 deg
RA of node: 281
6510 deg
Eccentricity:
0006253
Arg of perigee: 38
5260 deg
Mean anomaly: 321
6338 deg
Mean motion: 15
55213054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1066
Checksum: 276
Coasting Arc #4 (Orbit 1079)
---------------------------------------
Vector Time (GMT): 2015/057/09:22:28
241
Vector Time (MET): N/A
Weight (LBS) : 905155
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4274877
07 A = 6775801
06 meter
Y = -444800
20 meter E =
0009724
Z = 5229941
81 I = 51
26549
XDOT = -216
386360 Wp = 68
50777
YDOT = 7629
287087 meter/sec RA = 276
61682 deg
ZDOT = 827
995764 TA = 13
55796
MA = 13
53186
Ha = 222
612 n
mi
Hp = 211
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14025187
25 X = 4254128
43
Y = -1459318
24 feet Y = -397111
36 meter
Z = 17158601
74 Z = 5250657
71
XDOT = -709
929001 XDOT = -305
704810
YDOT = 25030
469447 feet/sec YDOT = 7626
367967 meter/sec
ZDOT = 2716
521535 ZDOT = 826
727107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7347150
52 X = 2239411
48
Y = 11908136
12 feet Y = 3629599
89 meter
Z = 17247283
09 Z = 5256971
89
XDOT = -22002
678000 XDOT = -6706
416254
YDOT = 9661
345197 feet/sec YDOT = 2944
778016 meter/sec
ZDOT = 2709
747187 ZDOT = 825
930943
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 15057
44025746
00016717 00000-0 10270-3 0 9030
2 25544 51
6450 277
1595 0008076 50
4423 309
7442 15
54733688 10806
Satellite: ISS
Catalog Number: 25544
Epoch time: 15057
44025746 = yrday
fracday
Element set: 903
Inclination: 51
6450 deg
RA of node: 277
1595 deg
Eccentricity:
0008076
Arg of perigee: 50
4423 deg
Mean anomaly: 309
7442 deg
Mean motion: 15
54733688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1080
Checksum: 310
Coasting Arc #5 (Orbit 1094)
---------------------------------------
Vector Time (GMT): 2015/058/09:22:28
241
Vector Time (MET): N/A
Weight (LBS) : 905155
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4101198
32 A = 6776132
52 meter
Y = -1607706
42 meter E =
0020399
Z = -5166053
71 I = 51
26432
XDOT = 1263
042356 Wp = 83
18714
YDOT = -7434
165317 meter/sec RA = 271
58409 deg
ZDOT = 1317
730197 TA = 199
52279
MA = 199
60102
Ha = 222
764 n
mi
Hp = 210
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13455375
05 X = -4057821
38
Y = -5274627
35 feet Y = -1653326
54 meter
Z = -16948995
12 Z = -5185870
76
XDOT = 4143
839751 XDOT = 1339
678134
YDOT = -24390
306157 feet/sec YDOT = -7419
612560 meter/sec
ZDOT = 4323
261800 ZDOT = 1324
052407
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1278669
17 X = -389738
36
Y = -14295557
01 feet Y = -4357285
78 meter
Z = -17033475
93 Z = -5191803
46
XDOT = 22598
981856 XDOT = 6888
169670
YDOT = -7179
676828 feet/sec YDOT = -2188
365497 meter/sec
ZDOT = 4351
604070 ZDOT = 1326
368921
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 15058
40441923
00016717 00000-0 10270-3 0 9047
2 25544 51
6453 272
3488 0008121 53
2275 306
9622 15
54748690 10958
Satellite: ISS
Catalog Number: 25544
Epoch time: 15058
40441923 = yrday
fracday
Element set: 904
Inclination: 51
6453 deg
RA of node: 272
3488 deg
Eccentricity:
0008121
Arg of perigee: 53
2275 deg
Mean anomaly: 306
9622 deg
Mean motion: 15
54748690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1095
Checksum: 309
Coasting Arc #6 (Orbit 1110)
---------------------------------------
Vector Time (GMT): 2015/059/09:22:28
241
Vector Time (MET): N/A
Weight (LBS) : 905155
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3740500
70 A = 6779091
84 meter
Y = 3551354
21 meter E =
0017326
Z = 4390206
83 I = 51
27451
XDOT = -2277
833484 Wp = 63
36593
YDOT = 6531
237267 meter/sec RA = 266
55633 deg
ZDOT = -3324
722194 TA = 60
45112
MA = 60
27851
Ha = 222
653 n
mi
Hp = 210
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12271983
92 X = 3679185
02
Y = 11651424
56 feet Y = 3592840
44 meter
Z = 14403565
72 Z = 4408227
91
XDOT = -7473
206967 XDOT = -2334
548062
YDOT = 21427
943788 feet/sec YDOT = 6505
447668 meter/sec
ZDOT = -10907
881213 ZDOT = -3335
925547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4665150
51 X = -1421937
87
Y = 16198300
17 feet Y = 4937241
89 meter
Z = 14480035
62 Z = 4413514
86
XDOT = -21233
832067 XDOT = -6472
072014
YDOT = 3731
278185 feet/sec YDOT = 1137
293591 meter/sec
ZDOT = -10956
932691 ZDOT = -3339
673084
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 15059
43283800
00016717 00000-0 10270-3 0 9050
2 25544 51
6450 267
2171 0008138 55
9500 304
2425 15
54802176 11116
Satellite: ISS
Catalog Number: 25544
Epoch time: 15059
43283800 = yrday
fracday
Element set: 905
Inclination: 51
6450 deg
RA of node: 267
2171 deg
Eccentricity:
0008138
Arg of perigee: 55
9500 deg
Mean anomaly: 304
2425 deg
Mean motion: 15
54802176 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1111
Checksum: 280
Coasting Arc #7 (Orbit 1125)
---------------------------------------
Vector Time (GMT): 2015/060/09:22:28
241
Vector Time (MET): N/A
Weight (LBS) : 905155
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3250703
19 A = 6783316
74 meter
Y = -5099429
42 meter E =
0012479
Z = -3076053
39 I = 51
29128
XDOT = 3207
852018 Wp = 64
56251
YDOT = -4971
095408 meter/sec RA = 261
54044 deg
ZDOT = 4871
787141 TA = 259
91657
MA = 260
05738
Ha = 222
710 n
mi
Hp = 210
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10665036
72 X = -3178496
55
Y = -16730411
48 feet Y = -5135377
46 meter
Z = -10092038
68 Z = -3091668
51
XDOT = 10524
448878 XDOT = 3239
536719
YDOT = -16309
368138 feet/sec YDOT = -4935
045504 meter/sec
ZDOT = 15983
553612 ZDOT = 4887
447370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9599965
61 X = 2926069
52
Y = -17324992
10 feet Y = -5280657
59 meter
Z = -10157963
88 Z = -3096147
39
XDOT = 18045
287047 XDOT = 5500
203492
YDOT = 627
562250 feet/sec YDOT = 191
280974 meter/sec
ZDOT = 16051
391907 ZDOT = 4892
464253
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 15060
39696342
00016717 00000-0 10270-3 0 9067
2 25544 51
6449 262
4060 0008065 59
0150 301
1794 15
54796348 11267
Satellite: ISS
Catalog Number: 25544
Epoch time: 15060
39696342 = yrday
fracday
Element set: 906
Inclination: 51
6449 deg
RA of node: 262
4060 deg
Eccentricity:
0008065
Arg of perigee: 59
0150 deg
Mean anomaly: 301
1794 deg
Mean motion: 15
54796348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1126
Checksum: 308
Coasting Arc #8 (Orbit 1141)
---------------------------------------
Vector Time (GMT): 2015/061/09:22:28
241
Vector Time (MET): N/A
Weight (LBS) : 905155
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2534777
57 A = 6786661
97 meter
Y = 6156267
37 meter E =
0019430
Z = 1288338
03 I = 51
30765
XDOT = -4083
036414 Wp = 100
32673
YDOT = 2910
667153 meter/sec RA = 256
53730 deg
ZDOT = -5803
840020 TA = 65
58522
MA = 65
38259
Ha = 222
784 n
mi
Hp = 210
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8316199
38 X = 2459490
21
Y = 20197727
58 feet Y = 6184192
09 meter
Z = 4226830
82 Z = 1300467
71
XDOT = -13395
788759 XDOT = -4087
088422
YDOT = 9549
432917 feet/sec YDOT = 2864
984696 meter/sec
ZDOT = -19041
469882 ZDOT = -5823
684360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13456881
57 X = -4101657
50
Y = 17192650
78 feet Y = 5240319
96 meter
Z = 4277682
53 Z = 1303837
64
XDOT = -13609
303510 XDOT = -4148
115710
YDOT = -5835
659856 feet/sec YDOT = -1778
709124 meter/sec
ZDOT = -19126
852062 ZDOT = -5829
864509
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 15061
42534495
00016717 00000-0 10270-3 0 9073
2 25544 51
6445 257
2739 0008081 63
8919 296
3065 15
54799318 11426
Satellite: ISS
Catalog Number: 25544
Epoch time: 15061
42534495 = yrday
fracday
Element set: 907
Inclination: 51
6445 deg
RA of node: 257
2739 deg
Eccentricity:
0008081
Arg of perigee: 63
8919 deg
Mean anomaly: 296
3065 deg
Mean motion: 15
54799318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1142
Checksum: 333
Coasting Arc #9 (Orbit 1155)
---------------------------------------
Vector Time (GMT): 2015/062/07:23:12
826
Vector Time (MET): N/A
Weight (LBS) : 905014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3752763
21 A = 6776131
16 meter
Y = 2092000
33 meter E =
0021366
Z = -5258503
25 I = 51
27781
XDOT = -2906
407747 Wp = 77
80567
YDOT = -7042
763912 meter/sec RA = 251
95524 deg
ZDOT = -725
741727 TA = 185
20207
MA = 185
22430
Ha = 222
720 n
mi
Hp = 211
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12312215
25 X = -3750334
21
Y = 6863518
14 feet Y = 2050047
42 meter
Z = -17252307
25 Z = -5276727
43
XDOT = -9535
458486 XDOT = -2823
912577
YDOT = -23106
180813 feet/sec YDOT = -7074
804091 meter/sec
ZDOT = -2381
042413 ZDOT = -739
658975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7016052
54 X = -2138492
81
Y = -12114671
23 feet Y = -3692551
79 meter
Z = -17330619
69 Z = -5282372
88
XDOT = 22100
500293 XDOT = 6736
232489
YDOT = -9300
557925 feet/sec YDOT = -2834
810055 meter/sec
ZDOT = -2439
409086 ZDOT = -743
531889
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 15062
32516150
00016717 00000-0 10270-3 0 9082
2 25544 51
6442 252
7825 0007070 64
0776 296
1105 15
54614351 11561
Satellite: ISS
Catalog Number: 25544
Epoch time: 15062
32516150 = yrday
fracday
Element set: 908
Inclination: 51
6442 deg
RA of node: 252
7825 deg
Eccentricity:
0007070
Arg of perigee: 64
0776 deg
Mean anomaly: 296
1105 deg
Mean motion: 15
54614351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1156
Checksum: 287
Coasting Arc #10 (Orbit 1171)
---------------------------------------
Vector Time (GMT): 2015/063/07:23:12
826
Vector Time (MET): N/A
Weight (LBS) : 905014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4406127
26 A = 6776398
22 meter
Y = -164186
47 meter E =
0011306
Z = 5138151
56 I = 51
28976
XDOT = 1901
732903 Wp = 62
18495
YDOT = 7305
741973 meter/sec RA = 246
92459 deg
ZDOT = -1389
807884 TA = 41
27436
MA = 41
18895
Ha = 222
465 n
mi
Hp = 211
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14455798
08 X = 4382677
01
Y = -538669
52 feet Y = -115044
70 meter
Z = 16857452
63 Z = 5159498
33
XDOT = 6239
281177 XDOT = 1826
648069
YDOT = 23968
969729 feet/sec YDOT = 7326
588378 meter/sec
ZDOT = -4559
737153 ZDOT = -1380
753179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 965511
91 X = 294288
03
Y = 14326189
89 feet Y = 4366622
68 meter
Z = 16948806
52 Z = 5165996
23
XDOT = -22725
978002 XDOT = -6926
878095
YDOT = 6910
766518 feet/sec YDOT = 2106
401635 meter/sec
ZDOT = -4522
198569 ZDOT = -1378
366124
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 15063
35367236
00016717 00000-0 10270-3 0 9096
2 25544 51
6439 247
6511 0006936 66
6020 293
5862 15
54669462 11724
Satellite: ISS
Catalog Number: 25544
Epoch time: 15063
35367236 = yrday
fracday
Element set: 909
Inclination: 51
6439 deg
RA of node: 247
6511 deg
Eccentricity:
0006936
Arg of perigee: 66
6020 deg
Mean anomaly: 293
5862 deg
Mean motion: 15
54669462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1172
Checksum: 324
Coasting Arc #11 (Orbit 1186)
---------------------------------------
Vector Time (GMT): 2015/064/07:23:12
826
Vector Time (MET): N/A
Weight (LBS) : 905014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4888432
11 A = 6779448
74 meter
Y = -1664442
11 meter E =
0015144
Z = -4406103
95 I = 51
31344
XDOT = -649
560093 Wp = 93
23829
YDOT = -6868
041329 meter/sec RA = 241
90020 deg
ZDOT = 3324
207093 TA = 210
50536
MA = 210
59353
Ha = 222
615 n
mi
Hp = 211
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16038163
10 X = -4848053
75
Y = -5460768
08 feet Y = -1718882
63 meter
Z = -14455721
61 Z = -4429752
29
XDOT = -2131
102667 XDOT = -588
859248
YDOT = -22532
943992 feet/sec YDOT = -6874
965243 meter/sec
ZDOT = 10906
191250 ZDOT = 3321
200160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4705602
83 X = 1434267
74
Y = -16185561
10 feet Y = -4933359
02 meter
Z = -14556629
59 Z = -4436860
70
XDOT = 21223
219418 XDOT = 6468
837279
YDOT = -3601
208174 feet/sec YDOT = -1097
648252 meter/sec
ZDOT = 10894
439990 ZDOT = 3320
625309
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 15064
31788470
00016717 00000-0 10270-3 0 9102
2 25544 51
6442 242
8403 0006954 69
5802 290
6097 15
54660952 11874
Satellite: ISS
Catalog Number: 25544
Epoch time: 15064
31788470 = yrday
fracday
Element set: 910
Inclination: 51
6442 deg
RA of node: 242
8403 deg
Eccentricity:
0006954
Arg of perigee: 69
5802 deg
Mean anomaly: 290
6097 deg
Mean motion: 15
54660952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1187
Checksum: 320
Coasting Arc #12 (Orbit 1202)
---------------------------------------
Vector Time (GMT): 2015/065/07:23:12
826
Vector Time (MET): N/A
Weight (LBS) : 905014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5071254
15 A = 6783618
31 meter
Y = 3286585
75 meter E =
0019708
Z = 3065768
56 I = 51
34344
XDOT = -834
360380 Wp = 87
70470
YDOT = 5864
290136 meter/sec RA = 236
88813 deg
ZDOT = -4878
545941 TA = 56
88970
MA = 56
70069
Ha = 222
584 n
mi
Hp = 211
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16637972
94 X = 5019233
70
Y = 10782761
65 feet Y = 3343005
44 meter
Z = 10058295
82 Z = 3090276
55
XDOT = -2737
402821 XDOT = -876
176399
YDOT = 19239
797035 feet/sec YDOT = 5854
725208 meter/sec
ZDOT = -16005
728152 ZDOT = -4882
701527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9696793
06 X = -2955582
52
Y = 17232312
16 feet Y = 5252408
75 meter
Z = 10162629
06 Z = 3097569
34
XDOT = -18111
373182 XDOT = -5520
346546
YDOT = -687
589024 feet/sec YDOT = -209
577134 meter/sec
ZDOT = -16024
448501 ZDOT = -4884
251903
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 15065
34635707
00016717 00000-0 10270-3 0 9111
2 25544 51
6443 237
7086 0007059 73
0524 287
1403 15
54693157 12037
Satellite: ISS
Catalog Number: 25544
Epoch time: 15065
34635707 = yrday
fracday
Element set: 911
Inclination: 51
6443 deg
RA of node: 237
7086 deg
Eccentricity:
0007059
Arg of perigee: 73
0524 deg
Mean anomaly: 287
1403 deg
Mean motion: 15
54693157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1203
Checksum: 302
Coasting Arc #13 (Orbit 1217)
---------------------------------------
Vector Time (GMT): 2015/066/07:23:12
826
Vector Time (MET): N/A
Weight (LBS) : 905014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4908289
64 A = 6786741
59 meter
Y = -4475178
83 meter E =
0014654
Z = -1376424
42 I = 51
37252
XDOT = 2415
287023 Wp = 54
74074
YDOT = -4412
851010 meter/sec RA = 231
88869 deg
ZDOT = 5786
630418 TA = 290
20467
MA = 290
36219
Ha = 222
514 n
mi
Hp = 211
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16103312
47 X = -4851196
24
Y = -14682345
24 feet Y = -4529747
52 meter
Z = -4515828
16 Z = -1400128
34
XDOT = 7924
170024 XDOT = 2436
344027
YDOT = -14477
857643 feet/sec YDOT = -4385
723045 meter/sec
ZDOT = 18985
007933 ZDOT = 5798
415144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13325755
85 X = 4061690
38
Y = -17216050
91 feet Y = -5247452
32 meter
Z = -4616542
01 Z = -1407122
01
XDOT = 13807
882467 XDOT = 4208
642576
YDOT = 5627
822417 feet/sec YDOT = 1715
360273 meter/sec
ZDOT = 19036
133156 ZDOT = 5802
213386
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 15066
31052955
00016717 00000-0 10270-3 0 9128
2 25544 51
6445 232
8974 0006910 75
5122 284
6797 15
54727930 12188
Satellite: ISS
Catalog Number: 25544
Epoch time: 15066
31052955 = yrday
fracday
Element set: 912
Inclination: 51
6445 deg
RA of node: 232
8974 deg
Eccentricity:
0006910
Arg of perigee: 75
5122 deg
Mean anomaly: 284
6797 deg
Mean motion: 15
54727930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1218
Checksum: 320
Coasting Arc #14 (Orbit 1233)
---------------------------------------
Vector Time (GMT): 2015/067/07:23:12
826
Vector Time (MET): N/A
Weight (LBS) : 905014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4281793
31 A = 6787501
85 meter
Y = 5231533
58 meter E =
0015642
Z = -561630
64 I = 51
39512
XDOT = -4021
443264 Wp = 117
17711
YDOT = 2666
139212 meter/sec RA = 226
89782 deg
ZDOT = -5959
176389 TA = 68
90444
MA = 68
73728
Ha = 222
571 n
mi
Hp = 211
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14047878
30 X = 4225703
00
Y = 17163824
08 feet Y = 5279101
68 meter
Z = -1842620
20 Z = -540967
68
XDOT = -13193
711496 XDOT = -4022
010494
YDOT = 8747
175892 feet/sec YDOT = 2621
164720 meter/sec
ZDOT = -19551
103638 ZDOT = -5978
713453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15695024
72 X = -4783843
53
Y = 15681870
74 feet Y = 4779834
20 meter
Z = -1755027
07 Z = -534932
25
XDOT = -8846
994751 XDOT = -2696
564000
YDOT = -10999
796117 feet/sec YDOT = -3352
737857 meter/sec
ZDOT = -19635
123274 ZDOT = -5984
785574
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 15067
33896105
00016717 00000-0 10270-3 0 9135
2 25544 51
6446 227
7657 0006824 80
3090 279
8833 15
54714486 12349
Satellite: ISS
Catalog Number: 25544
Epoch time: 15067
33896105 = yrday
fracday
Element set: 913
Inclination: 51
6446 deg
RA of node: 227
7657 deg
Eccentricity:
0006824
Arg of perigee: 80
3090 deg
Mean anomaly: 279
8833 deg
Mean motion: 15
54714486 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1234
Checksum: 328
Coasting Arc #15 (Orbit 1249)
---------------------------------------
Vector Time (GMT): 2015/068/07:23:12
826
Vector Time (MET): N/A
Weight (LBS) : 905014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3240562
35 A = 6785054
82 meter
Y = -5455896
37 meter E =
0020543
Z = 2376192
56 I = 51
40949
XDOT = 5425
949958 Wp = 76
29865
YDOT = -874
750524 meter/sec RA = 221
90462 deg
ZDOT = 5357
007718 TA = 310
35859
MA = 310
53779
Ha = 222
443 n
mi
Hp = 211
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10631766
23 X = -3190855
00
Y = -17899922
47 feet Y = -5491856
18 meter
Z = 7795907
35 Z = 2360572
11
XDOT = 17801
673090 XDOT = 5409
306090
YDOT = -2869
916416 feet/sec YDOT = -814
166293 meter/sec
ZDOT = 17575
484640 ZDOT = 5383
325551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16544208
96 X = 5042674
89
Y = -12678934
40 feet Y = -3864539
21 meter
Z = 7729917
29 Z = 2356078
79
XDOT = 3969
951603 XDOT = 1210
041249
YDOT = 16033
166161 feet/sec YDOT = 4886
909046 meter/sec
ZDOT = 17688
243290 ZDOT = 5391
376555
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 15068
36736885
00016717 00000-0 10270-3 0 9148
2 25544 51
6442 222
6333 0006779 81
6140 278
5781 15
54790584 12508
Satellite: ISS
Catalog Number: 25544
Epoch time: 15068
36736885 = yrday
fracday
Element set: 914
Inclination: 51
6442 deg
RA of node: 222
6333 deg
Eccentricity:
0006779
Arg of perigee: 81
6140 deg
Mean anomaly: 278
5781 deg
Mean motion: 15
54790584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1250
Checksum: 330
Coasting Arc #16 (Orbit 1264)
---------------------------------------
Vector Time (GMT): 2015/069/07:23:12
826
Vector Time (MET): N/A
Weight (LBS) : 905014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1748839
73 A = 6780818
93 meter
Y = 5244007
92 meter E =
0013242
Z = -3940178
46 I = 51
41888
XDOT = -6466
694150 Wp = 79
69657
YDOT = -852
019244 meter/sec RA = 216
90298 deg
ZDOT = -4013
391165 TA = 148
24739
MA = 148
16747
Ha = 222
388 n
mi
Hp = 211
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5737663
14 X = 1709209
90
Y = 17204750
41 feet Y = 5263342
48 meter
Z = -12927094
69 Z = -3931779
90
XDOT = -21216
188157 XDOT = -6437
190518
YDOT = -2795
338726 feet/sec YDOT = -924
169608 meter/sec
ZDOT = -13167
293850 ZDOT = -4044
733297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16279277
67 X = -4961923
83
Y = 8050852
69 feet Y = 2453899
90 meter
Z = -12891969
66 Z = -3929472
35
XDOT = 554
738178 XDOT = 169
084197
YDOT = -20129
386176 feet/sec YDOT = -6135
436906 meter/sec
ZDOT = -13301
293191 ZDOT = -4054
234165
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 15069
33148239
00016717 00000-0 10270-3 0 9157
2 25544 51
6434 217
8219 0006708 85
0308 275
1611 15
54806516 12658
Satellite: ISS
Catalog Number: 25544
Epoch time: 15069
33148239 = yrday
fracday
Element set: 915
Inclination: 51
6434 deg
RA of node: 217
8219 deg
Eccentricity:
0006708
Arg of perigee: 85
0308 deg
Mean anomaly: 275
1611 deg
Mean motion: 15
54806516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1265
Checksum: 309
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