[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 2nd 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18029 55 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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
092/18:33:31
661 -0
5 1
3 1
4
N/A 1
1 -0
1 220
3
000/00:03:03
321 0
6 -0
0 212
4
Coasting Arc #1 (Orbit 1611)
---------------------------------------
Vector Time (GMT): 2015/091/13:51:37
487
Vector Time (MET): N/A
Weight (LBS) : 904364
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4270999
29 A = 6773825
86 meter
Y = -2689
40 meter E =
0009657
Z = 5254433
15 I = 51
97095
XDOT = 1286
683062 Wp = 147
44977
YDOT = -7494
333903 meter/sec RA = 105
84238 deg
ZDOT = 1033
218036 TA = 292
65730
MA = 292
75939
Ha = 220
662 n
mi
Hp = 211
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14012464
86 X = -4296175
83
Y = -8823
49 feet Y = -50590
51 meter
Z = 17238953
91 Z = 5233624
35
XDOT = 4221
401123 XDOT = 1365
371872
YDOT = -24587
709654 feet/sec YDOT = -7479
505246 meter/sec
ZDOT = 3389
822953 ZDOT = 1039
660705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11330017
79 X = -3453389
42
Y = 8429045
52 feet Y = 2569173
07 meter
Z = 17149713
40 Z = 5227232
64
XDOT = -10703
302992 XDOT = -3262
366752
YDOT = -21401
778089 feet/sec YDOT = -6523
261962 meter/sec
ZDOT = 3418
696470 ZDOT = 1042
018684
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 15091
62749961
00016717 00000-0 10270-3 0 9007
2 25544 51
6415 106
5020 0006478 161
2533 198
8860 15
55462677 16122
Satellite: ISS
Catalog Number: 25544
Epoch time: 15091
62749961 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 106
5020 deg
Eccentricity:
0006478
Arg of perigee: 161
2533 deg
Mean anomaly: 198
8860 deg
Mean motion: 15
55462677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1612
Checksum: 313
Coasting Arc #2 (Orbit 1626)
---------------------------------------
Vector Time (GMT): 2015/092/13:51:37
487
Vector Time (MET): N/A
Weight (LBS) : 904364
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3685334
76 A = 6774066
85 meter
Y = 2343152
79 meter E =
0017686
Z = -5193442
71 I = 51
97965
XDOT = -2495
886669 Wp = 119
97817
YDOT = 7097
816364 meter/sec RA = 100
85031 deg
ZDOT = 1426
277800 TA = 163
72566
MA = 163
66879
Ha = 220
418 n
mi
Hp = 211
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12090993
29 X = 3684087
02
Y = 7687509
16 feet Y = 2384356
86 meter
Z = -17038854
03 Z = -5175543
41
XDOT = -8188
604558 XDOT = -2581
998975
YDOT = 23286
799096 feet/sec YDOT = 7069
424460 meter/sec
ZDOT = 4679
389107 ZDOT = 1413
943024
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14353108
75 X = 4374827
55
Y = -1369284
59 feet Y = -417357
94 meter
Z = -16962481
88 Z = -5170164
48
XDOT = 7623
367840 XDOT = 2323
602518
YDOT = 22409
344390 feet/sec YDOT = 6830
368170 meter/sec
ZDOT = 4625
299975 ZDOT = 1409
791432
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 15092
59118226
00016717 00000-0 10270-3 0 9019
2 25544 51
6414 101
6876 0006464 164
5269 195
6083 15
55487491 16272
Satellite: ISS
Catalog Number: 25544
Epoch time: 15092
59118226 = yrday
fracday
Element set: 901
Inclination: 51
6414 deg
RA of node: 101
6876 deg
Eccentricity:
0006464
Arg of perigee: 164
5269 deg
Mean anomaly: 195
6083 deg
Mean motion: 15
55487491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1627
Checksum: 325
Coasting Arc #3 (Orbit 1629)
---------------------------------------
Vector Time (GMT): 2015/092/18:35:03
321
Vector Time (MET): N/A
Weight (LBS) : 904230
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2613481
85 A = 6778249
56 meter
Y = 4558802
10 meter E =
0011998
Z = -4294274
84 I = 51
99617
XDOT = -3821
499285 Wp = 135
11016
YDOT = 5579
802541 meter/sec RA = 99
85977 deg
ZDOT = 3595
608528 TA = 171
46656
MA = 171
44614
Ha = 220
296 n
mi
Hp = 212
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8574415
50 X = 2583170
04
Y = 14956699
81 feet Y = 4587857
64 meter
Z = -14088828
23 Z = -4281653
33
XDOT = -12537
727314 XDOT = -3901
076110
YDOT = 18306
438784 feet/sec YDOT = 5536
623636 meter/sec
ZDOT = 11796
615907 ZDOT = 3576
850258
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11384990
07 X = 3470144
97
Y = -13004088
53 feet Y = -3963646
18 meter
Z = -14035463
44 Z = -4278009
26
XDOT = 20437
967418 XDOT = 6229
492469
YDOT = 5241
246716 feet/sec YDOT = 1597
531999 meter/sec
ZDOT = 11715
230469 ZDOT = 3570
802247
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 15092
78391640
00016717 00000-0 10270-3 0 9024
2 25544 51
6448 100
7254 0005646 173
1870 186
9361 15
55273998 16305
Satellite: ISS
Catalog Number: 25544
Epoch time: 15092
78391640 = yrday
fracday
Element set: 902
Inclination: 51
6448 deg
RA of node: 100
7254 deg
Eccentricity:
0005646
Arg of perigee: 173
1870 deg
Mean anomaly: 186
9361 deg
Mean motion: 15
55273998 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1630
Checksum: 323
Coasting Arc #4 (Orbit 1645)
---------------------------------------
Vector Time (GMT): 2015/093/18:35:03
321
Vector Time (MET): N/A
Weight (LBS) : 904230
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1619717
61 A = 6782837
02 meter
Y = -5987540
42 meter E =
0015983
Z = 2720758
52 I = 52
01587
XDOT = 4382
493569 Wp = 121
70815
YDOT = -3556
508057 meter/sec RA = 94
89254 deg
ZDOT = -5203
629587 TA = 27
65164
MA = 27
56673
Ha = 220
277 n
mi
Hp = 212
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5314034
15 X = -1565859
64
Y = -19644161
47 feet Y = -6005351
62 meter
Z = 8926373
10 Z = 2713021
89
XDOT = 14378
259742 XDOT = 4447
215022
YDOT = -11668
333521 feet/sec YDOT = -3507
139034 meter/sec
ZDOT = -17072
275547 ZDOT = -5182
182423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16683232
48 X = -5085049
26
Y = 11677969
72 feet Y = 3559445
17 meter
Z = 8894208
95 Z = 2710954
89
XDOT = -15018
516994 XDOT = -4577
643980
YDOT = -8487
942319 feet/sec YDOT = -2587
124819 meter/sec
ZDOT = -16979
690351 ZDOT = -5175
409619
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 15093
81198102
00016717 00000-0 10270-3 0 9038
2 25544 51
6445 95
5914 0005724 176
5374 183
5820 15
55288827 16466
Satellite: ISS
Catalog Number: 25544
Epoch time: 15093
81198102 = yrday
fracday
Element set: 903
Inclination: 51
6445 deg
RA of node: 95
5914 deg
Eccentricity:
0005724
Arg of perigee: 176
5374 deg
Mean anomaly: 183
5820 deg
Mean motion: 15
55288827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1646
Checksum: 328
Coasting Arc #5 (Orbit 1660)
---------------------------------------
Vector Time (GMT): 2015/094/18:35:03
321
Vector Time (MET): N/A
Weight (LBS) : 904230
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 583470
31 A = 6785533
63 meter
Y = 6718983
78 meter E =
0007016
Z = -738242
24 I = 52
02798
XDOT = -4670
550889 Wp = 70
23931
YDOT = 1057
924861 meter/sec RA = 89
93799 deg
ZDOT = 5985
516871 TA = 281
82670
MA = 281
90539
Ha = 219
976 n
mi
Hp = 212
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1914272
67 X = 511879
82
Y = 22043910
05 feet Y = 6725108
14 meter
Z = -2422054
61 Z = -735582
65
XDOT = -15323
329688 XDOT = -4711
109422
YDOT = 3470
882091 feet/sec YDOT = 1005
469760 meter/sec
ZDOT = 19637
522543 ZDOT = 5962
729359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19940955
65 X = 6078003
28
Y = -9591989
05 feet Y = -2923638
26 meter
Z = -2411802
79 Z = -735117
49
XDOT = 8006
031610 XDOT = 2440
238435
YDOT = 11770
927224 feet/sec YDOT = 3587
778618 meter/sec
ZDOT = 19539
610424 ZDOT = 5955
673257
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 15094
77576631
00016717 00000-0 10270-3 0 9042
2 25544 51
6452 90
7775 0005642 181
2047 178
9094 15
55353740 16610
Satellite: ISS
Catalog Number: 25544
Epoch time: 15094
77576631 = yrday
fracday
Element set: 904
Inclination: 51
6452 deg
RA of node: 90
7775 deg
Eccentricity:
0005642
Arg of perigee: 181
2047 deg
Mean anomaly: 178
9094 deg
Mean motion: 15
55353740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1661
Checksum: 326
Coasting Arc #6 (Orbit 1676)
---------------------------------------
Vector Time (GMT): 2015/095/18:35:03
321
Vector Time (MET): N/A
Weight (LBS) : 904230
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 521282
06 A = 6784940
77 meter
Y = -6609790
62 meter E =
0013404
Z = -1405035
92 I = 52
02548
XDOT = 4714
461085 Wp = 159
55347
YDOT = 1606
401674 meter/sec RA = 84
98818 deg
ZDOT = -5836
890367 TA = 35
69381
MA = 35
60427
Ha = 219
935 n
mi
Hp = 212
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1710242
97 X = 601980
79
Y = -21685664
76 feet Y = -6603510
26 meter
Z = -4609697
89 Z = -1402306
76
XDOT = 15467
392012 XDOT = 4724
501318
YDOT = 5270
346701 feet/sec YDOT = 1659
177270 meter/sec
ZDOT = -19149
902778 ZDOT = -5813
963957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20795581
26 X = -6338493
17
Y = 6391802
80 feet Y = 1948221
49 meter
Z = -4596842
26 Z = -1401117
52
XDOT = -394
241805 XDOT = -120
164902
YDOT = -14915
912604 feet/sec YDOT = -4546
370162 meter/sec
ZDOT = -19051
856208 ZDOT = -5807
005772
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 15095
80377979
00016717 00000-0 10270-3 0 9052
2 25544 51
6457 85
6431 0005787 185
7159 174
3929 15
55352116 16770
Satellite: ISS
Catalog Number: 25544
Epoch time: 15095
80377979 = yrday
fracday
Element set: 905
Inclination: 51
6457 deg
RA of node: 85
6431 deg
Eccentricity:
0005787
Arg of perigee: 185
7159 deg
Mean anomaly: 174
3929 deg
Mean motion: 15
55352116 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1677
Checksum: 356
Coasting Arc #7 (Orbit 1692)
---------------------------------------
Vector Time (GMT): 2015/096/18:35:03
321
Vector Time (MET): N/A
Weight (LBS) : 904230
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1616462
36 A = 6781009
85 meter
Y = 5695698
16 meter E =
0012862
Z = 3301051
89 I = 52
00941
XDOT = -4473
972026 Wp = 112
92612
YDOT = -4032
769625 meter/sec RA = 80
02969 deg
ZDOT = 4747
860336 TA = 285
23676
MA = 285
37894
Ha = 219
684 n
mi
Hp = 212
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5303354
18 X = -1696068
37
Y = 18686673
75 feet Y = 5677177
07 meter
Z = 10830222
72 Z = 3293005
34
XDOT = -14678
385913 XDOT = -4451
607777
YDOT = -13230
871473 feet/sec YDOT = -4082
674945 meter/sec
ZDOT = 15576
969605 ZDOT = 4726
181101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19314805
04 X = 5887152
58
Y = -2241353
28 feet Y = -683164
48 meter
Z = 10794707
37 Z = 3290226
81
XDOT = -6679
709109 XDOT = -2035
975336
YDOT = 17324
272157 feet/sec YDOT = 5280
438153 meter/sec
ZDOT = 15484
703622 ZDOT = 4719
737664
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 15096
83176629
00016717 00000-0 10270-3 0 9066
2 25544 51
6458 80
5083 0005544 188
7189 171
3869 15
55411194 16935
Satellite: ISS
Catalog Number: 25544
Epoch time: 15096
83176629 = yrday
fracday
Element set: 906
Inclination: 51
6458 deg
RA of node: 80
5083 deg
Eccentricity:
0005544
Arg of perigee: 188
7189 deg
Mean anomaly: 171
3869 deg
Mean motion: 15
55411194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1693
Checksum: 345
Coasting Arc #8 (Orbit 1707)
---------------------------------------
Vector Time (GMT): 2015/097/18:35:03
321
Vector Time (MET): N/A
Weight (LBS) : 904230
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2720251
53 A = 6776110
86 meter
Y = -4058767
01 meter E =
0008912
Z = -4701573
78 I = 51
98746
XDOT = 3906
845410 Wp = 101
87438
YDOT = 5936
355600 meter/sec RA = 75
05552 deg
ZDOT = -2870
658536 TA = 139
77457
MA = 139
70859
Ha = 219
474 n
mi
Hp = 212
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8924709
75 X = 2788274
26
Y = -13316164
72 feet Y = -4027967
47 meter
Z = -15425110
82 Z = -4688193
55
XDOT = 12817
734285 XDOT = 3854
118090
YDOT = 19476
232283 feet/sec YDOT = 5979
749421 meter/sec
ZDOT = -9418
171050 ZDOT = -2851
808182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15817972
23 X = -4821317
94
Y = -2924350
41 feet Y = -891342
00 meter
Z = -15366999
06 Z = -4683861
31
XDOT = 12463
309830 XDOT = 3798
816836
YDOT = -18453
149275 feet/sec YDOT = -5624
519899 meter/sec
ZDOT = -9338
387203 ZDOT = -2846
340420
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 15097
79547782
00016717 00000-0 10270-3 0 9075
2 25544 51
6460 75
6946 0005584 194
2777 165
8219 15
55474041 17084
Satellite: ISS
Catalog Number: 25544
Epoch time: 15097
79547782 = yrday
fracday
Element set: 907
Inclination: 51
6460 deg
RA of node: 75
6946 deg
Eccentricity:
0005584
Arg of perigee: 194
2777 deg
Mean anomaly: 165
8219 deg
Mean motion: 15
55474041 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1708
Checksum: 353
Coasting Arc #9 (Orbit 1723)
---------------------------------------
Vector Time (GMT): 2015/098/18:35:03
321
Vector Time (MET): N/A
Weight (LBS) : 904230
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3702847
00 A = 6773414
65 meter
Y = 1980942
66 meter E =
0006490
Z = 5314175
63 I = 51
97011
XDOT = -2995
856737 Wp = 171
61122
YDOT = -7042
356685 meter/sec RA = 70
06762 deg
ZDOT = 531
341528 TA = 273
30713
MA = 273
38137
Ha = 219
398 n
mi
Hp = 212
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12148448
15 X = -3750537
77
Y = 6499155
71 feet Y = 1939268
75 meter
Z = 17434959
41 Z = 5296071
70
XDOT = -9828
926301 XDOT = -2919
465865
YDOT = -23104
844766 feet/sec YDOT = -7075
431145 meter/sec
ZDOT = 1743
246483 ZDOT = 516
974133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11017942
43 X = 3358268
85
Y = 8434612
92 feet Y = 2570870
02 meter
Z = 17356954
70 Z = 5290399
79
XDOT = -16287
286119 XDOT = -4964
364809
YDOT = 17769
631649 feet/sec YDOT = 5416
183726 meter/sec
ZDOT = 1682
902687 ZDOT = 512
948739
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 15098
82341209
00016717 00000-0 10270-3 0 9087
2 25544 51
6465 70
5601 0005641 197
1536 162
9428 15
55509722 17243
Satellite: ISS
Catalog Number: 25544
Epoch time: 15098
82341209 = yrday
fracday
Element set: 908
Inclination: 51
6465 deg
RA of node: 70
5601 deg
Eccentricity:
0005641
Arg of perigee: 197
1536 deg
Mean anomaly: 162
9428 deg
Mean motion: 15
55509722 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1724
Checksum: 314
Coasting Arc #10 (Orbit 1738)
---------------------------------------
Vector Time (GMT): 2015/099/18:35:03
321
Vector Time (MET): N/A
Weight (LBS) : 904230
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4504131
43 A = 6774431
08 meter
Y = 292705
60 meter E =
0013428
Z = -5063173
15 I = 51
96166
XDOT = 1696
800896 Wp = 128
85729
YDOT = 7219
254617 meter/sec RA = 65
07451 deg
ZDOT = 1922
024307 TA = 159
74423
MA = 159
69091
Ha = 219
086 n
mi
Hp = 213
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14777334
09 X = 4525118
82
Y = 960320
21 feet Y = 343190
76 meter
Z = -16611460
46 Z = -5041241
77
XDOT = 5566
932072 XDOT = 1606
610794
YDOT = 23685
218560 feet/sec YDOT = 7237
725196 meter/sec
ZDOT = 6305
854024 ZDOT = 1930
047585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5569115
47 X = -1697466
40
Y = -13834420
33 feet Y = -4216731
32 meter
Z = -16517451
47 Z = -5034519
21
XDOT = 17960
044455 XDOT = 5474
221550
YDOT = -14817
035034 feet/sec YDOT = -4516
232278 meter/sec
ZDOT = 6338
941880 ZDOT = 1932
109485
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 15099
78707478
00016717 00000-0 10270-3 0 9098
2 25544 51
6459 65
7452 0005648 201
9608 158
1304 15
55559712 17397
Satellite: ISS
Catalog Number: 25544
Epoch time: 15099
78707478 = yrday
fracday
Element set: 909
Inclination: 51
6459 deg
RA of node: 65
7452 deg
Eccentricity:
0005648
Arg of perigee: 201
9608 deg
Mean anomaly: 158
1304 deg
Mean motion: 15
55559712 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1739
Checksum: 349
Coasting Arc #11 (Orbit 1754)
---------------------------------------
Vector Time (GMT): 2015/100/18:35:03
321
Vector Time (MET): N/A
Weight (LBS) : 904230
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4948377
12 A = 6778447
95 meter
Y = -2411900
86 meter E =
0009032
Z = 3945471
66 I = 51
96194
XDOT = -73
569966 Wp = 110
25792
YDOT = -6508
509237 meter/sec RA = 60
09163 deg
ZDOT = -4066
517289 TA = 22
04053
MA = 22
00171
Ha = 218
933 n
mi
Hp = 213
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16234833
07 X = -4940204
66
Y = -7913060
56 feet Y = -2467190
91 meter
Z = 12944460
84 Z = 3921453
23
XDOT = -241
371281 XDOT = 18
968959
YDOT = -21353
376763 feet/sec YDOT = -6508
814776 meter/sec
ZDOT = -13341
592155 ZDOT = -4066
649516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 231288
50 X = 70496
73
Y = 18132228
63 feet Y = 5526703
29 meter
Z = 12841891
97 Z = 3914208
67
XDOT = -17701
968494 XDOT = -5395
559997
YDOT = 9684
789771 feet/sec YDOT = 2951
923922 meter/sec
ZDOT = -13340
954149 ZDOT = -4066
322825
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 15100
81495421
00016717 00000-0 10270-3 0 9109
2 25544 51
6462 60
6106 0005600 206
9598 153
1266 15
55630620 17550
Satellite: ISS
Catalog Number: 25544
Epoch time: 15100
81495421 = yrday
fracday
Element set: 910
Inclination: 51
6462 deg
RA of node: 60
6106 deg
Eccentricity:
0005600
Arg of perigee: 206
9598 deg
Mean anomaly: 153
1266 deg
Mean motion: 15
55630620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1755
Checksum: 283
Coasting Arc #12 (Orbit 1769)
---------------------------------------
Vector Time (GMT): 2015/101/18:35:03
321
Vector Time (MET): N/A
Weight (LBS) : 904230
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4935059
31 A = 6783060
85 meter
Y = 4121385
60 meter E =
0001343
Z = -2162359
50 I = 51
95944
XDOT = -1770
004484 Wp = 97
92920
YDOT = 5014
516867 meter/sec RA = 55
12237 deg
ZDOT = 5520
644140 TA = 238
19576
MA = 238
20884
Ha = 218
712 n
mi
Hp = 213
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16191139
47 X = 4899110
19
Y = 13521606
31 feet Y = 4176371
52 meter
Z = -7094355
33 Z = -2138473
42
XDOT = -5807
101324 XDOT = -1852
763787
YDOT = 16451
826991 feet/sec YDOT = 4994
261133 meter/sec
ZDOT = 18112
349542 ZDOT = 5511
844437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4465717
99 X = 1361150
84
Y = -20651308
92 feet Y = -6294518
96 meter
Z = -6992675
79 Z = -2131367
58
XDOT = 15819
393931 XDOT = 4821
751270
YDOT = -2695
929248 feet/sec YDOT = -821
719235 meter/sec
ZDOT = 18073
671193 ZDOT = 5508
854979
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 15101
77856749
00016717 00000-0 10270-3 0 9110
2 25544 51
6450 55
7954 0005715 210
3551 149
7273 15
55621038 17707
Satellite: ISS
Catalog Number: 25544
Epoch time: 15101
77856749 = yrday
fracday
Element set: 911
Inclination: 51
6450 deg
RA of node: 55
7954 deg
Eccentricity:
0005715
Arg of perigee: 210
3551 deg
Mean anomaly: 149
7273 deg
Mean motion: 15
55621038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1770
Checksum: 311
Coasting Arc #13 (Orbit 1785)
---------------------------------------
Vector Time (GMT): 2015/102/18:35:03
321
Vector Time (MET): N/A
Weight (LBS) : 904230
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4326953
89 A = 6784900
69 meter
Y = -5214345
61 meter E =
0014395
Z = -22378
28 I = 51
94696
XDOT = 3650
637250 Wp = 157
80243
YDOT = -3008
897254 meter/sec RA = 50
16540 deg
ZDOT = -6043
521354 TA = 22
43788
MA = 22
37498
Ha = 218
608 n
mi
Hp = 213
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14196042
94 X = -4268215
54
Y = -17107433
11 feet Y = -5262404
01 meter
Z = -73419
55 Z = -43254
78
XDOT = 11977
156333 XDOT = 3713
369360
YDOT = -9871
710151 feet/sec YDOT = -2967
723121 meter/sec
ZDOT = -19827
825963 ZDOT = -6025
634642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8235432
29 X = -2510159
76
Y = 20648213
25 feet Y = 6293575
40 meter
Z = -161980
62 Z = -49371
69
XDOT = -12953
509804 XDOT = -3948
229788
YDOT = -5306
503343 feet/sec YDOT = -1617
422219 meter/sec
ZDOT = -19750
543982 ZDOT = -6019
965806
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 15102
80639395
00016717 00000-0 10270-3 0 9122
2 25544 51
6449 50
6602 0005798 213
0097 147
0695 15
55654269 17863
Satellite: ISS
Catalog Number: 25544
Epoch time: 15102
80639395 = yrday
fracday
Element set: 912
Inclination: 51
6449 deg
RA of node: 50
6602 deg
Eccentricity:
0005798
Arg of perigee: 213
0097 deg
Mean anomaly: 147
0695 deg
Mean motion: 15
55654269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1786
Checksum: 329
Coasting Arc #14 (Orbit 1801)
---------------------------------------
Vector Time (GMT): 2015/103/18:35:03
321
Vector Time (MET): N/A
Weight (LBS) : 904230
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3135126
38 A = 6782583
46 meter
Y = 5597161
27 meter E =
0009557
Z = 2193559
94 I = 51
91814
XDOT = -5283
994411 Wp = 91
21425
YDOT = 795
760803 meter/sec RA = 45
20471 deg
ZDOT = 5500
775330 TA = 293
05513
MA = 293
15587
Ha = 218
331 n
mi
Hp = 213
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10285847
69 X = 3061649
07
Y = 18363389
99 feet Y = 5631809
65 meter
Z = 7196718
96 Z = 2208610
85
XDOT = -17335
939667 XDOT = -5319
220833
YDOT = 2610
763788 feet/sec YDOT = 736
475232 meter/sec
ZDOT = 18047
163157 ZDOT = 5475
021039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10923183
24 X = 3329386
25
Y = -17966047
27 feet Y = -5476051
21 meter
Z = 7260215
68 Z = 2212913
74
XDOT = 9570
086269 XDOT = 2916
962295
YDOT = 13094
202157 feet/sec YDOT = 3991
112817 meter/sec
ZDOT = 17936
553750 ZDOT = 5467
061583
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 15103
83418994
00016717 00000-0 10270-3 0 9137
2 25544 51
6439 45
5230 0005938 217
5236 142
5504 15
55735689 18026
Satellite: ISS
Catalog Number: 25544
Epoch time: 15103
83418994 = yrday
fracday
Element set: 913
Inclination: 51
6439 deg
RA of node: 45
5230 deg
Eccentricity:
0005938
Arg of perigee: 217
5236 deg
Mean anomaly: 142
5504 deg
Mean motion: 15
55735689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1802
Checksum: 317
Coasting Arc #15 (Orbit 1816)
---------------------------------------
Vector Time (GMT): 2015/104/18:35:03
321
Vector Time (MET): N/A
Weight (LBS) : 904230
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1380590
55 A = 6777743
68 meter
Y = -5288419
05 meter E =
0003694
Z = -4008862
48 I = 51
87841
XDOT = 6416
727639 Wp = 127
55343
YDOT = 1338
004935 meter/sec RA = 40
23040 deg
ZDOT = -3979
592776 TA = 101
19192
MA = 101
15040
Ha = 218
170 n
mi
Hp = 213
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4529496
55 X = -1301877
97
Y = -17350456
20 feet Y = -5303418
01 meter
Z = -13152435
96 Z = -4015377
42
XDOT = 21052
256034 XDOT = 6420
620277
YDOT = 4389
779970 feet/sec YDOT = 1409
782344 meter/sec
ZDOT = -13056
406744 ZDOT = -3948
412145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12684929
64 X = -3866366
56
Y = 12646654
40 feet Y = 3854700
26 meter
Z = -13179375
29 Z = -4017073
59
XDOT = -6038
041773 XDOT = -1840
395133
YDOT = -19507
575657 feet/sec YDOT = -5945
909060 meter/sec
ZDOT = -12922
932691 ZDOT = -3938
909884
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 15104
79772551
00016717 00000-0 10270-3 0 9146
2 25544 51
6431 40
7077 0005821 220
5206 139
5515 15
55756487 18179
Satellite: ISS
Catalog Number: 25544
Epoch time: 15104
79772551 = yrday
fracday
Element set: 914
Inclination: 51
6431 deg
RA of node: 40
7077 deg
Eccentricity:
0005821
Arg of perigee: 220
5206 deg
Mean anomaly: 139
5515 deg
Mean motion: 15
55756487 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1817
Checksum: 309
Coasting Arc #16 (Orbit 1832)
---------------------------------------
Vector Time (GMT): 2015/105/18:35:03
321
Vector Time (MET): N/A
Weight (LBS) : 904230
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -701766
05 A = 6773593
61 meter
Y = 4407754
06 meter E =
0007178
Z = 5096800
49 I = 51
83991
XDOT = -6788
239955 Wp = 177
70985
YDOT = -3111
930294 meter/sec RA = 35
23647 deg
ZDOT = 1749
483372 TA = 255
38641
MA = 255
46602
Ha = 218
054 n
mi
Hp = 213
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2302382
05 X = -775760
95
Y = 14461135
37 feet Y = 4399493
29 meter
Z = 16721786
40 Z = 5093211
21
XDOT = -22271
128460 XDOT = -6761
435481
YDOT = -10209
745058 feet/sec YDOT = -3187
690764 meter/sec
ZDOT = 5739
774844 ZDOT = 1716
572673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13587175
99 X = 4141371
24
Y = -5509684
95 feet Y = -1679351
97 meter
Z = 16705554
77 Z = 5091853
09
XDOT = 2560
554023 XDOT = 780
456866
YDOT = 23362
037827 feet/sec YDOT = 7120
749130 meter/sec
ZDOT = 5599
227411 ZDOT = 1706
644515
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 15105
82546971
00016717 00000-0 10270-3 0 9157
2 25544 51
6434 35
5707 0005813 223
9591 136
1101 15
55752415 18338
Satellite: ISS
Catalog Number: 25544
Epoch time: 15105
82546971 = yrday
fracday
Element set: 915
Inclination: 51
6434 deg
RA of node: 35
5707 deg
Eccentricity:
0005813
Arg of perigee: 223
9591 deg
Mean anomaly: 136
1101 deg
Mean motion: 15
55752415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1833
Checksum: 299
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