[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 8th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11302 11 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 905 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 986)
---------------------------------------
Vector Time (GMT): 2015/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 295575
82 A = 6785295
14 meter
Y = 6414196
45 meter E =
0010708
Z = -2197504
46 I = 52
00993
XDOT = -4893
675637 Wp = 76
36497
YDOT = 2104
254115 meter/sec RA = 102
86462 deg
ZDOT = 5508
699544 TA = 259
37670
MA = 259
49732
Ha = 222
279 n
mi
Hp = 211
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 969736
94 X = 234503
53
Y = 21043951
60 feet Y = 6417160
18 meter
Z = -7209660
29 Z = -2196217
27
XDOT = -16055
366263 XDOT = -4943
601740
YDOT = 6903
720850 feet/sec YDOT = 2049
250943 meter/sec
ZDOT = 18073
161233 ZDOT = 5484
805347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14984353
73 X = -4567231
02
Y = -14809493
40 feet Y = -4513933
59 meter
Z = -7205243
82 Z = -2196158
32
XDOT = 6156
773405 XDOT = 1876
584534
YDOT = -14932
364748 feet/sec YDOT = -4551
384775 meter/sec
ZDOT = 17969
517372 ZDOT = 5477
108895
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 15308
50435963
00016717 00000-0 10270-3 0 9009
2 25544 51
6408 103
7740 0006540 107
6615 252
5253 15
54810279 9879
Satellite: ISS
Catalog Number: 25544
Epoch time: 15308
50435963 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 103
7740 deg
Eccentricity:
0006540
Arg of perigee: 107
6615 deg
Mean anomaly: 252
5253 deg
Mean motion: 15
54810279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 987
Checksum: 302
Coasting Arc #2 (Orbit 1002)
---------------------------------------
Vector Time (GMT): 2015/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 722678
52 A = 6787173
28 meter
Y = -6735364
01 meter E =
0018683
Z = 271079
99 I = 52
02215
XDOT = 4724
936254 Wp = 124
55818
YDOT = 252
462163 meter/sec RA = 97
91441 deg
ZDOT = -6039
342089 TA = 52
53412
MA = 52
36434
Ha = 222
141 n
mi
Hp = 211
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2370992
53 X = 796624
47
Y = -22097650
96 feet Y = -6726869
07 meter
Z = 889370
05 Z = 274770
69
XDOT = 15501
759365 XDOT = 4751
099266
YDOT = 828
287935 feet/sec YDOT = 305
445436 meter/sec
ZDOT = -19814
114465 ZDOT = -6016
325413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13513200
45 X = 4118823
50
Y = 17643422
80 feet Y = 5377715
27 meter
Z = 906536
31 Z = 276312
27
XDOT = -10608
238712 XDOT = -3233
391160
YDOT = 9184
872476 feet/sec YDOT = 2799
549131 meter/sec
ZDOT = -19714
681093 ZDOT = -6009
034797
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 15309
53273047
00016717 00000-0 10270-3 0 9017
2 25544 51
6401 98
6411 0006379 109
9274 250
2567 15
54860397 10034
Satellite: ISS
Catalog Number: 25544
Epoch time: 15309
53273047 = yrday
fracday
Element set: 901
Inclination: 51
6401 deg
RA of node: 98
6411 deg
Eccentricity:
0006379
Arg of perigee: 109
9274 deg
Mean anomaly: 250
2567 deg
Mean motion: 15
54860397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1003
Checksum: 305
Coasting Arc #3 (Orbit 1018)
---------------------------------------
Vector Time (GMT): 2015/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1613368
11 A = 6786006
24 meter
Y = 6377361
41 meter E =
0018698
Z = 1641226
88 I = 52
02321
XDOT = -4361
270289 Wp = 79
31688
YDOT = -2596
868461 meter/sec RA = 92
96621 deg
ZDOT = 5751
492488 TA = 298
56744
MA = 298
75549
Ha = 222
117 n
mi
Hp = 211
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5293202
46 X = -1692534
01
Y = 20923101
74 feet Y = 6358877
13 meter
Z = 5384602
62 Z = 1633196
62
XDOT = -14308
629558 XDOT = -4359
846391
YDOT = -8519
909648 feet/sec YDOT = -2645
630730 meter/sec
ZDOT = 18869
726011 ZDOT = 5730
309562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10879955
96 X = -3316210
58
Y = -18649550
59 feet Y = -5684383
02 meter
Z = 5348733
01 Z = 1630293
82
XDOT = 14898
908846 XDOT = 4541
187416
YDOT = -3256
863139 feet/sec YDOT = -992
691885 meter/sec
ZDOT = 18778
643600 ZDOT = 5723
730569
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 15310
56108478
00016717 00000-0 10270-3 0 9028
2 25544 51
6414 93
5090 0006516 115
2201 244
9628 15
54885721 10191
Satellite: ISS
Catalog Number: 25544
Epoch time: 15310
56108478 = yrday
fracday
Element set: 902
Inclination: 51
6414 deg
RA of node: 93
5090 deg
Eccentricity:
0006516
Arg of perigee: 115
2201 deg
Mean anomaly: 244
9628 deg
Mean motion: 15
54885721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1019
Checksum: 293
Coasting Arc #4 (Orbit 1033)
---------------------------------------
Vector Time (GMT): 2015/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2468740
15 A = 6782272
60 meter
Y = -5330071
09 meter E =
0010961
Z = -3396260
51 I = 52
01167
XDOT = 3812
820790 Wp = 106
19050
YDOT = 4731
149991 meter/sec RA = 88
01003 deg
ZDOT = -4668
927424 TA = 113
23636
MA = 113
12091
Ha = 222
078 n
mi
Hp = 211
360
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8099541
17 X = 2544656
90
Y = -17487109
88 feet Y = -5302039
75 meter
Z = -11142586
97 Z = -3384082
88
XDOT = 12509
254562 XDOT = 3782
312881
YDOT = 15522
145639 feet/sec YDOT = 4773
616589 meter/sec
ZDOT = -15318
003360 ZDOT = -4650
479527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6755850
61 X = 2059183
27
Y = 18081814
55 feet Y = 5511337
08 meter
Z = -11088971
48 Z = -3379918
51
XDOT = -18588
915290 XDOT = -5665
901380
YDOT = -2369
148656 feet/sec YDOT = -722
116510 meter/sec
ZDOT = -15239
139388 ZDOT = -4644
889685
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 15311
52515155
00016717 00000-0 10270-3 0 9030
2 25544 51
6415 88
6971 0006431 117
2554 242
9255 15
54888516 10340
Satellite: ISS
Catalog Number: 25544
Epoch time: 15311
52515155 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 88
6971 deg
Eccentricity:
0006431
Arg of perigee: 117
2554 deg
Mean anomaly: 242
9255 deg
Mean motion: 15
54888516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1034
Checksum: 304
Coasting Arc #5 (Orbit 1049)
---------------------------------------
Vector Time (GMT): 2015/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3198005
35 A = 6777870
30 meter
Y = 3751069
53 meter E =
0014646
Z = 4644208
61 I = 51
99623
XDOT = -3115
329894 Wp = 117
64718
YDOT = -6353
147895 meter/sec RA = 83
04060 deg
ZDOT = 2972
379247 TA = 302
84294
MA = 302
98386
Ha = 221
988 n
mi
Hp = 211
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10492143
53 X = -3262273
37
Y = 12306658
56 feet Y = 3714948
25 meter
Z = 15236904
88 Z = 4628516
64
XDOT = -10220
898602 XDOT = -3058
494933
YDOT = -20843
661074 feet/sec YDOT = -6387
667612 meter/sec
ZDOT = 9751
900417 ZDOT = 2957
383665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1642968
10 X = -500776
68
Y = -16153112
09 feet Y = -4923468
57 meter
Z = 15168382
13 Z = 4623322
87
XDOT = 21021
093967 XDOT = 6407
229441
YDOT = 7002
137076 feet/sec YDOT = 2134
251381 meter/sec
ZDOT = 9688
270298 ZDOT = 2952
984787
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 15312
55347044
00016717 00000-0 10270-3 0 9045
2 25544 51
6423 83
5645 0006342 121
5065 238
6709 15
54943876 10502
Satellite: ISS
Catalog Number: 25544
Epoch time: 15312
55347044 = yrday
fracday
Element set: 904
Inclination: 51
6423 deg
RA of node: 83
5645 deg
Eccentricity:
0006342
Arg of perigee: 121
5065 deg
Mean anomaly: 238
6709 deg
Mean motion: 15
54943876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1050
Checksum: 301
Coasting Arc #6 (Orbit 1064)
---------------------------------------
Vector Time (GMT): 2015/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3858167
35 A = 6775187
58 meter
Y = -1770853
10 meter E =
0019843
Z = -5297101
56 I = 51
98313
XDOT = 2205
634499 Wp = 95
31628
YDOT = 7283
345901 meter/sec RA = 78
06002 deg
ZDOT = -832
846092 TA = 166
77243
MA = 166
72033
Ha = 221
875 n
mi
Hp = 211
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12658029
36 X = 3903414
69
Y = -5809885
51 feet Y = -1727455
80 meter
Z = -17378942
13 Z = -5278248
88
XDOT = 7236
333659 XDOT = 2128
072174
YDOT = 23895
491802 feet/sec YDOT = 7307
577045 meter/sec
ZDOT = -2732
434684 ZDOT = -822
320030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4341704
56 X = -1323351
55
Y = 13340436
57 feet Y = 4066165
07 meter
Z = -17297122
89 Z = -5272163
06
XDOT = -21545
247636 XDOT = -6566
991480
YDOT = -10478
570688 feet/sec YDOT = -3193
868346 meter/sec
ZDOT = -2688
313229 ZDOT = -819
397872
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 15313
51750509
00016717 00000-0 10270-3 0 9057
2 25544 51
6429 78
7536 0006341 123
2470 236
9292 15
54950791 10659
Satellite: ISS
Catalog Number: 25544
Epoch time: 15313
51750509 = yrday
fracday
Element set: 905
Inclination: 51
6429 deg
RA of node: 78
7536 deg
Eccentricity:
0006341
Arg of perigee: 123
2470 deg
Mean anomaly: 236
9292 deg
Mean motion: 15
54950791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1065
Checksum: 310
Coasting Arc #7 (Orbit 1080)
---------------------------------------
Vector Time (GMT): 2015/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4339824
89 A = 6775591
54 meter
Y = -336340
60 meter E =
0008889
Z = 5184628
01 I = 51
97782
XDOT = -1113
990997 Wp = 97
12680
YDOT = -7462
443671 meter/sec RA = 73
07395 deg
ZDOT = -1415
586829 TA = 6
41604
MA = 6
40467
Ha = 221
979 n
mi
Hp = 211
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14238270
63 X = -4360926
95
Y = -1103479
64 feet Y = -384989
19 meter
Z = 17009934
42 Z = 5163494
17
XDOT = -3654
826106 XDOT = -1023
584760
YDOT = -24483
082909 feet/sec YDOT = -7474
395610 meter/sec
ZDOT = -4644
313745 ZDOT = -1420
778681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10334119
45 X = 3149839
61
Y = -10012442
67 feet Y = -3051792
52 meter
Z = 16918654
01 Z = 5156805
74
XDOT = 20005
750257 XDOT = 6097
752678
YDOT = 12759
647478 feet/sec YDOT = 3889
140551 meter/sec
ZDOT = -4665
327364 ZDOT = -1421
991780
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 15314
54579126
00016717 00000-0 10270-3 0 9066
2 25544 51
6436 73
6205 0006329 126
1368 234
0372 15
54958937 10814
Satellite: ISS
Catalog Number: 25544
Epoch time: 15314
54579126 = yrday
fracday
Element set: 906
Inclination: 51
6436 deg
RA of node: 73
6205 deg
Eccentricity:
0006329
Arg of perigee: 126
1368 deg
Mean anomaly: 234
0372 deg
Mean motion: 15
54958937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1081
Checksum: 314
Coasting Arc #8 (Orbit 1095)
---------------------------------------
Vector Time (GMT): 2015/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4630372
91 A = 6778829
71 meter
Y = 2346388
60 meter E =
0014686
Z = -4375018
30 I = 51
97929
XDOT = -180
695741 Wp = 118
42438
YDOT = 6823
124377 meter/sec RA = 68
09460 deg
ZDOT = 3470
136818 TA = 186
68502
MA = 186
70463
Ha = 221
687 n
mi
Hp = 211
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15191512
18 X = 4625043
66
Y = 7698125
32 feet Y = 2398138
61 meter
Z = -14353734
57 Z = -4352537
21
XDOT = -592
833796 XDOT = -273
837240
YDOT = 22385
578666 feet/sec YDOT = 6820
582989 meter/sec
ZDOT = 11384
963314 ZDOT = 3469
032663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15781443
71 X = -4810184
04
Y = 6614851
41 feet Y = 2016206
71 meter
Z = -14257020
98 Z = -4345539
99
XDOT = -16100
901493 XDOT = -4907
554775
YDOT = -13902
426500 feet/sec YDOT = -4237
459597 meter/sec
ZDOT = 11378
869312 ZDOT = 3468
279366
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
50979206
00016717 00000-0 10270-3 0 9077
2 25544 51
6442 68
8095 0006214 129
9859 230
1841 15
54991506 10966
Satellite: ISS
Catalog Number: 25544
Epoch time: 15315
50979206 = yrday
fracday
Element set: 907
Inclination: 51
6442 deg
RA of node: 68
8095 deg
Eccentricity:
0006214
Arg of perigee: 129
9859 deg
Mean anomaly: 230
1841 deg
Mean motion: 15
54991506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1096
Checksum: 327
Coasting Arc #9 (Orbit 1111)
---------------------------------------
Vector Time (GMT): 2015/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4595234
22 A = 6783274
68 meter
Y = -4036917
07 meter E =
0018873
Z = 2908984
20 I = 51
98185
XDOT = 1638
093054 Wp = 109
43130
YDOT = -5530
380871 meter/sec RA = 63
12679 deg
ZDOT = -5066
569383 TA = 37
53272
MA = 37
40111
Ha = 221
756 n
mi
Hp = 211
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15076227
77 X = -4563882
03
Y = -13244478
59 feet Y = -4088128
72 meter
Z = 9543911
41 Z = 2886736
99
XDOT = 5374
321042 XDOT = 1724
425527
YDOT = -18144
294196 feet/sec YDOT = -5511
579910 meter/sec
ZDOT = -16622
602964 ZDOT = -5058
401945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19849779
09 X = 6050212
67
Y = -3241351
79 feet Y = -987964
03 meter
Z = 9448545
42 Z = 2879916
64
XDOT = 10267
683276 XDOT = 3129
589862
YDOT = 14331
381062 feet/sec YDOT = 4368
204948 meter/sec
ZDOT = -16586
216451 ZDOT = -5055
478774
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
53804381
00016717 00000-0 10270-3 0 9083
2 25544 51
6446 63
6769 0006317 133
1294 227
0388 15
55000321 11122
Satellite: ISS
Catalog Number: 25544
Epoch time: 15316
53804381 = yrday
fracday
Element set: 908
Inclination: 51
6446 deg
RA of node: 63
6769 deg
Eccentricity:
0006317
Arg of perigee: 133
1294 deg
Mean anomaly: 227
0388 deg
Mean motion: 15
55000321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1112
Checksum: 289
Coasting Arc #10 (Orbit 1126)
---------------------------------------
Vector Time (GMT): 2015/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4213779
62 A = 6786252
55 meter
Y = 5210985
39 meter E =
0010810
Z = -1063922
96 I = 51
97767
XDOT = -3131
619944 Wp = 72
24699
YDOT = 3730
016989 meter/sec RA = 58
17065 deg
ZDOT = 5918
650981 TA = 276
27240
MA = 276
39553
Ha = 221
535 n
mi
Hp = 211
553
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13824736
28 X = 4160364
19
Y = 17096408
75 feet Y = 5257808
01 meter
Z = -3490560
90 Z = -1043582
38
XDOT = -10274
343648 XDOT = -3201
848455
YDOT = 12237
588546 feet/sec YDOT = 3694
604377 meter/sec
ZDOT = 19418
146264 ZDOT = 5903
267283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21999542
56 X = -6705460
57
Y = 172191
33 feet Y = 52483
92 meter
Z = -3403677
17 Z = -1037440
80
XDOT = -3077
349266 XDOT = -937
976056
YDOT = -14155
836483 feet/sec YDOT = -4314
698960 meter/sec
ZDOT = 19350
913167 ZDOT = 5898
158333
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
50201241
00016717 00000-0 10270-3 0 9098
2 25544 51
6453 58
8652 0006084 134
9569 225
2079 15
55027647 11275
Satellite: ISS
Catalog Number: 25544
Epoch time: 15317
50201241 = yrday
fracday
Element set: 909
Inclination: 51
6453 deg
RA of node: 58
8652 deg
Eccentricity:
0006084
Arg of perigee: 134
9569 deg
Mean anomaly: 225
2079 deg
Mean motion: 15
55027647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1127
Checksum: 307
Coasting Arc #11 (Orbit 1142)
---------------------------------------
Vector Time (GMT): 2015/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3367991
81 A = 6786173
64 meter
Y = -5799527
66 meter E =
0015865
Z = -990467
46 I = 51
95982
XDOT = 4568
130429 Wp = 140
29225
YDOT = -1649
603952 meter/sec RA = 53
21927 deg
ZDOT = -5938
624577 TA = 50
39847
MA = 50
25850
Ha = 221
419 n
mi
Hp = 211
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11049841
88 X = -3298078
33
Y = -19027321
71 feet Y = -5836799
83 meter
Z = -3249565
15 Z = -1006659
21
XDOT = 14987
304557 XDOT = 4615
085434
YDOT = -5412
086458 feet/sec YDOT = -1598
257401 meter/sec
ZDOT = -19483
676433 ZDOT = -5916
318991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21806022
89 X = 6646475
78
Y = 2860649
07 feet Y = 871925
84 meter
Z = -3318388
69 Z = -1011444
87
XDOT = -4714
631301 XDOT = -1437
019621
YDOT = 13688
368510 feet/sec YDOT = 4172
214722 meter/sec
ZDOT = -19386
933238 ZDOT = -5909
137251
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
53022959
00016717 00000-0 10270-3 0 9101
2 25544 51
6449 53
7328 0006150 139
3352 220
8262 15
55064935 11431
Satellite: ISS
Catalog Number: 25544
Epoch time: 15318
53022959 = yrday
fracday
Element set: 910
Inclination: 51
6449 deg
RA of node: 53
7328 deg
Eccentricity:
0006150
Arg of perigee: 139
3352 deg
Mean anomaly: 220
8262 deg
Mean motion: 15
55064935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1143
Checksum: 296
Coasting Arc #12 (Orbit 1158)
---------------------------------------
Vector Time (GMT): 2015/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2141677
54 A = 6782985
34 meter
Y = 5761645
60 meter E =
0017149
Z = 2856953
34 I = 51
93013
XDOT = -5719
091422 Wp = 98
77607
YDOT = -415
022973 meter/sec RA = 48
26048 deg
ZDOT = 5095
639861 TA = 293
59375
MA = 293
77374
Ha = 221
289 n
mi
Hp = 211
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7026501
10 X = 2063211
97
Y = 18903036
75 feet Y = 5785156
43 meter
Z = 9373206
51 Z = 2867166
99
XDOT = -18763
423302 XDOT = -5738
778642
YDOT = -1361
623928 feet/sec YDOT = -479
087866 meter/sec
ZDOT = 16717
978548 ZDOT = 5067
809278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19331363
36 X = -5892199
55
Y = -5673384
84 feet Y = -1729247
70 meter
Z = 9416188
79 Z = 2870054
34
XDOT = 11925
329312 XDOT = 3634
840374
YDOT = -12931
642189 feet/sec YDOT = -3941
564539 meter/sec
ZDOT = 16597
767788 ZDOT = 5058
999622
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
55842847
00016717 00000-0 10270-3 0 9111
2 25544 51
6453 48
5998 0006091 142
0179 218
1405 15
55109951 11597
Satellite: ISS
Catalog Number: 25544
Epoch time: 15319
55842847 = yrday
fracday
Element set: 911
Inclination: 51
6453 deg
RA of node: 48
5998 deg
Eccentricity:
0006091
Arg of perigee: 142
0179 deg
Mean anomaly: 218
1405 deg
Mean motion: 15
55109951 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1159
Checksum: 322
Coasting Arc #13 (Orbit 1173)
---------------------------------------
Vector Time (GMT): 2015/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -508464
45 A = 6778424
45 meter
Y = -5174456
56 meter E =
0011765
Z = -4357879
67 I = 51
89236
XDOT = 6425
073020 Wp = 98
81845
YDOT = 2296
166803 meter/sec RA = 43
28774 deg
ZDOT = -3485
852523 TA = 135
90450
MA = 135
81063
Ha = 221
218 n
mi
Hp = 211
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1668190
47 X = -429395
37
Y = -16976563
51 feet Y = -5179700
31 meter
Z = -14297505
47 Z = -4360157
83
XDOT = 21079
635893 XDOT = 6415
852411
YDOT = 7533
355654 feet/sec YDOT = 2367
964758 meter/sec
ZDOT = -11436
524025 ZDOT = -3454
662626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14722577
44 X = 4487441
60
Y = 8601206
06 feet Y = 2621647
61 meter
Z = -14306299
26 Z = -4360560
01
XDOT = -17810
587420 XDOT = -5428
667046
YDOT = 11740
663786 feet/sec YDOT = 3578
554322 meter/sec
ZDOT = -11302
175876 ZDOT = -3444
903207
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
52235062
00016717 00000-0 10270-3 0 9126
2 25544 51
6447 43
7881 0006002 145
6864 214
4678 15
55106942 11745
Satellite: ISS
Catalog Number: 25544
Epoch time: 15320
52235062 = yrday
fracday
Element set: 912
Inclination: 51
6447 deg
RA of node: 43
7881 deg
Eccentricity:
0006002
Arg of perigee: 145
6864 deg
Mean anomaly: 214
4678 deg
Mean motion: 15
55106942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1174
Checksum: 295
Coasting Arc #14 (Orbit 1189)
---------------------------------------
Vector Time (GMT): 2015/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1298919
23 A = 6774911
45 meter
Y = 4160270
95 meter E =
0010050
Z = 5182702
22 I = 51
85760
XDOT = -6535
706783 Wp = 138
26509
YDOT = -3776
159875 meter/sec RA = 38
29891 deg
ZDOT = 1384
332611 TA = 298
42456
MA = 298
52581
Ha = 221
076 n
mi
Hp = 211
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4261546
04 X = -1370519
79
Y = 13649182
91 feet Y = 4145345
12 meter
Z = 17003616
21 Z = 5176218
43
XDOT = -21442
607556 XDOT = -6499
719740
YDOT = -12388
975967 feet/sec YDOT = -3849
045275 meter/sec
ZDOT = 4541
773659 ZDOT = 1352
670361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8751984
84 X = -2667604
98
Y = -11350987
20 feet Y = -3459780
90 meter
Z = 16974739
58 Z = 5173900
62
XDOT = 21564
726938 XDOT = 6572
928771
YDOT = -9995
127406 feet/sec YDOT = -3046
514833 meter/sec
ZDOT = 4405
689762 ZDOT = 1342
854239
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
55051589
00016717 00000-0 10270-3 0 9131
2 25544 51
6449 38
6546 0005919 148
8949 211
2556 15
55170790 11903
Satellite: ISS
Catalog Number: 25544
Epoch time: 15321
55051589 = yrday
fracday
Element set: 913
Inclination: 51
6449 deg
RA of node: 38
6546 deg
Eccentricity:
0005919
Arg of perigee: 148
8949 deg
Mean anomaly: 211
2556 deg
Mean motion: 15
55170790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1190
Checksum: 328
Coasting Arc #15 (Orbit 1204)
---------------------------------------
Vector Time (GMT): 2015/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3169585
60 A = 6774682
24 meter
Y = -2873177
61 meter E =
0018425
Z = -5268777
68 I = 51
83012
XDOT = 5910
389679 Wp = 111
78189
YDOT = 4774
332347 meter/sec RA = 33
30207 deg
ZDOT = 948
018468 TA = 167
30253
MA = 167
25606
Ha = 220
977 n
mi
Hp = 211
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10398902
89 X = 3227072
62
Y = -9426435
73 feet Y = -2837411
74 meter
Z = -17286016
01 Z = -5253240
68
XDOT = 19391
042254 XDOT = 5851
957486
YDOT = 15663
820036 feet/sec YDOT = 4840
099502 meter/sec
ZDOT = 3110
296811 ZDOT = 976
588412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2030054
19 X = 618760
52
Y = 13971802
52 feet Y = 4258605
41 meter
Z = -17218270
41 Z = -5248128
82
XDOT = -22751
501356 XDOT = -6934
657613
YDOT = 7305
929906 feet/sec YDOT = 2226
847435 meter/sec
ZDOT = 3232
804210 ZDOT = 985
358723
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
51440760
00016717 00000-0 10270-3 0 9142
2 25544 51
6441 33
8424 0005780 150
9537 209
1939 15
55159470 12050
Satellite: ISS
Catalog Number: 25544
Epoch time: 15322
51440760 = yrday
fracday
Element set: 914
Inclination: 51
6441 deg
RA of node: 33
8424 deg
Eccentricity:
0005780
Arg of perigee: 150
9537 deg
Mean anomaly: 209
1939 deg
Mean motion: 15
55159470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1205
Checksum: 296
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