[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 20th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 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
087/01:36:05
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 211
2
092/18:33:35
103 -0
7 1
4 1
4
N/A 1
1 0
0 220
2
000/00:03:10
206 0
5 -0
1 212
4
Coasting Arc #1 (Orbit 1420)
---------------------------------------
Vector Time (GMT): 2015/079/07:57:58
656
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4832548
69 A = 6779197
12 meter
Y = 2264339
15 meter E =
0013388
Z = -4191063
24 I = 51
71678
XDOT = -5194
520786 Wp = 96
04152
YDOT = 4230
397711 meter/sec RA = 166
80163 deg
ZDOT = -3715
582721 TA = 135
84909
MA = 135
74215
Ha = 221
992 n
mi
Hp = 210
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15854818
54 X = 4827227
68
Y = 7428934
22 feet Y = 2318349
41 meter
Z = -13750207
48 Z = -4167601
07
XDOT = -17042
391029 XDOT = -5223
391191
YDOT = 13879
257582 feet/sec YDOT = 4172
147135 meter/sec
ZDOT = -12190
232023 ZDOT = -3740
887420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 372569
30 X = 113559
12
Y = 17583241
93 feet Y = 5359372
14 meter
Z = -13650030
60 Z = -4160529
33
XDOT = -18659
544428 XDOT = -5687
429142
YDOT = -9122
965280 feet/sec YDOT = -2780
679817 meter/sec
ZDOT = -12299
281811 ZDOT = -3748
821096
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 15079
35493396
00016717 00000-0 10270-3 0 9001
2 25544 51
6441 167
7781 0007192 122
7194 237
4653 15
55090335 14219
Satellite: ISS
Catalog Number: 25544
Epoch time: 15079
35493396 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 167
7781 deg
Eccentricity:
0007192
Arg of perigee: 122
7194 deg
Mean anomaly: 237
4653 deg
Mean motion: 15
55090335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1421
Checksum: 314
Coasting Arc #2 (Orbit 1436)
---------------------------------------
Vector Time (GMT): 2015/080/07:57:58
656
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3057826
55 A = 6775379
91 meter
Y = -3231904
96 meter E =
0012309
Z = 5103103
26 I = 51
73493
XDOT = 6588
092654 Wp = 126
40562
YDOT = -3561
901488 meter/sec RA = 161
80444 deg
ZDOT = 1681
858027 TA = 307
33385
MA = 307
44594
Ha = 221
890 n
mi
Hp = 210
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10032239
34 X = -3046248
34
Y = -10603362
72 feet Y = -3266034
00 meter
Z = 16742464
77 Z = 5088277
58
XDOT = 21614
477211 XDOT = 6619
263196
YDOT = -11686
028504 feet/sec YDOT = -3488
054571 meter/sec
ZDOT = 5517
906912 ZDOT = 1713
938008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4799762
22 X = 1462967
53
Y = -13861676
68 feet Y = -4225039
05 meter
Z = 16679432
13 Z = 5083890
91
XDOT = 19241
822596 XDOT = 5864
907527
YDOT = 13507
770663 feet/sec YDOT = 4117
168498 meter/sec
ZDOT = 5655
895722 ZDOT = 1723
917016
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 15080
38311978
00016717 00000-0 10270-3 0 9012
2 25544 51
6438 162
6446 0007075 126
9501 233
2301 15
55142937 14372
Satellite: ISS
Catalog Number: 25544
Epoch time: 15080
38311978 = yrday
fracday
Element set: 901
Inclination: 51
6438 deg
RA of node: 162
6446 deg
Eccentricity:
0007075
Arg of perigee: 126
9501 deg
Mean anomaly: 233
2301 deg
Mean motion: 15
55142937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1437
Checksum: 298
Coasting Arc #3 (Orbit 1451)
---------------------------------------
Vector Time (GMT): 2015/081/07:57:58
656
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 984014
93 A = 6774430
97 meter
Y = 4123643
18 meter E =
0021029
Z = -5301921
04 I = 51
76223
XDOT = -7193
737665 Wp = 106
24747
YDOT = 2538
189254 meter/sec RA = 156
80251 deg
ZDOT = 635
340517 TA = 169
83964
MA = 169
79706
Ha = 221
753 n
mi
Hp = 210
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3228395
44 X = 963585
09
Y = 13529013
07 feet Y = 4134532
06 meter
Z = -17394754
08 Z = -5297191
11
XDOT = -23601
501525 XDOT = -7224
671902
YDOT = 8327
392564 feet/sec YDOT = 2457
571311 meter/sec
ZDOT = 2084
450516 ZDOT = 600
319092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10349458
06 X = -3154514
82
Y = 9328894
88 feet Y = 2843447
16 meter
Z = -17375115
52 Z = -5295935
21
XDOT = -17808
151544 XDOT = -5427
924591
YDOT = -16131
958730 feet/sec YDOT = -4917
021021 meter/sec
ZDOT = 1933
998738 ZDOT = 589
482815
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 15081
34702238
00016717 00000-0 10270-3 0 9023
2 25544 51
6442 157
8334 0007202 129
3208 230
8584 15
55175266 14526
Satellite: ISS
Catalog Number: 25544
Epoch time: 15081
34702238 = yrday
fracday
Element set: 902
Inclination: 51
6442 deg
RA of node: 157
8334 deg
Eccentricity:
0007202
Arg of perigee: 129
3208 deg
Mean anomaly: 230
8584 deg
Mean motion: 15
55175266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1452
Checksum: 293
Coasting Arc #4 (Orbit 1467)
---------------------------------------
Vector Time (GMT): 2015/082/07:57:58
656
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1099934
10 A = 6776974
93 meter
Y = -4766984
43 meter E =
0012539
Z = 4678309
96 I = 51
79926
XDOT = 7019
772612 Wp = 96
50621
YDOT = -1201
371949 meter/sec RA = 151
80319 deg
ZDOT = -2869
393684 TA = 21
91563
MA = 21
86205
Ha = 221
741 n
mi
Hp = 210
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3608707
66 X = 1130432
30
Y = -15639712
68 feet Y = -4754513
12 meter
Z = 15348785
97 Z = 4683727
95
XDOT = 23030
750041 XDOT = 7046
623425
YDOT = -3941
509018 feet/sec YDOT = -1122
722505 meter/sec
ZDOT = -9414
021274 ZDOT = -2835
227449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15367829
80 X = 4684114
52
Y = -4551632
52 feet Y = -1387337
59 meter
Z = 15372737
66 Z = 4685610
44
XDOT = 14359
138937 XDOT = 4376
665548
YDOT = 17123
885059 feet/sec YDOT = 5219
360166 meter/sec
ZDOT = -9267
422574 ZDOT = -2824
710400
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 15082
37516147
00016717 00000-0 10270-3 0 9030
2 25544 51
6439 152
6990 0007231 132
7438 227
4331 15
55162101 14681
Satellite: ISS
Catalog Number: 25544
Epoch time: 15082
37516147 = yrday
fracday
Element set: 903
Inclination: 51
6439 deg
RA of node: 152
6990 deg
Eccentricity:
0007231
Arg of perigee: 132
7438 deg
Mean anomaly: 227
4331 deg
Mean motion: 15
55162101 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1468
Checksum: 295
Coasting Arc #5 (Orbit 1482)
---------------------------------------
Vector Time (GMT): 2015/083/07:57:58
656
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2950350
50 A = 6781289
49 meter
Y = 5097491
00 meter E =
0010881
Z = -3374730
94 I = 51
84212
XDOT = -6057
987015 Wp = 117
42387
YDOT = -420
577412 meter/sec RA = 146
81897 deg
ZDOT = 4667
556796 TA = 203
35874
MA = 203
40821
Ha = 221
527 n
mi
Hp = 210
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9679627
63 X = -2990739
32
Y = 16724051
85 feet Y = 5064272
06 meter
Z = -11071951
91 Z = -3389161
89
XDOT = -19875
285481 XDOT = -6075
507121
YDOT = -1379
847153 feet/sec YDOT = -488
419229 meter/sec
ZDOT = 15313
506549 ZDOT = 4638
085634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19287058
26 X = -5878695
36
Y = 86368
82 feet Y = 26325
22 meter
Z = -11134592
26 Z = -3393823
72
XDOT = -8829
360929 XDOT = -2691
189211
YDOT = -16557
767168 feet/sec YDOT = -5046
807433 meter/sec
ZDOT = 15187
265118 ZDOT = 4629
078408
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 15083
33901656
00016717 00000-0 10270-3 0 9041
2 25544 51
6444 147
8865 0006990 135
9345 224
2366 15
55214752 14837
Satellite: ISS
Catalog Number: 25544
Epoch time: 15083
33901656 = yrday
fracday
Element set: 904
Inclination: 51
6444 deg
RA of node: 147
8865 deg
Eccentricity:
0006990
Arg of perigee: 135
9345 deg
Mean anomaly: 224
2366 deg
Mean motion: 15
55214752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1483
Checksum: 322
Coasting Arc #6 (Orbit 1498)
---------------------------------------
Vector Time (GMT): 2015/084/07:57:58
656
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4379765
05 A = 6785060
90 meter
Y = -4943259
36 meter E =
0020663
Z = 1506355
57 I = 51
88103
XDOT = 4520
804531 Wp = 125
50386
YDOT = 2227
282880 meter/sec RA = 141
85051 deg
ZDOT = -5791
368691 TA = 38
07746
MA = 37
93161
Ha = 221
441 n
mi
Hp = 210
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14369307
89 X = 4427398
90
Y = -16218042
52 feet Y = -4894015
49 meter
Z = 4942111
46 Z = 1527747
84
XDOT = 14832
035862 XDOT = 4523
694904
YDOT = 7307
358531 feet/sec YDOT = 2277
853077 meter/sec
ZDOT = -19000
553449 ZDOT = -5769
400639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21294127
81 X = 6490450
16
Y = 3890951
48 feet Y = 1185962
01 meter
Z = 5034579
98 Z = 1534539
98
XDOT = 1758
447831 XDOT = 535
974899
YDOT = 15023
338331 feet/sec YDOT = 4579
113523 meter/sec
ZDOT = -18906
742600 ZDOT = -5762
775144
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 15084
36710670
00016717 00000-0 10270-3 0 9050
2 25544 51
6444 142
7524 0007098 139
8450 220
3229 15
55255901 14996
Satellite: ISS
Catalog Number: 25544
Epoch time: 15084
36710670 = yrday
fracday
Element set: 905
Inclination: 51
6444 deg
RA of node: 142
7524 deg
Eccentricity:
0007098
Arg of perigee: 139
8450 deg
Mean anomaly: 220
3229 deg
Mean motion: 15
55255901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1499
Checksum: 310
Coasting Arc #7 (Orbit 1514)
---------------------------------------
Vector Time (GMT): 2015/085/07:57:58
656
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5224354
26 A = 6785806
92 meter
Y = 4289778
03 meter E =
0014624
Z = 559248
74 I = 51
90904
XDOT = -2619
964148 Wp = 79
54907
YDOT = -3990
008344 meter/sec RA = 136
89206 deg
ZDOT = 6000
409153 TA = 286
46422
MA = 286
62488
Ha = 221
311 n
mi
Hp = 211
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17140269
87 X = -5274651
91
Y = 14074074
90 feet Y = 4231074
71 meter
Z = 1834805
56 Z = 533747
29
XDOT = -8595
682901 XDOT = -2604
299949
YDOT = -13090
578555 feet/sec YDOT = -4019
218373 meter/sec
ZDOT = 19686
381736 ZDOT = 5987
720282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21038110
46 X = -6412416
07
Y = -7046835
49 feet Y = -2147875
46 meter
Z = 1724808
65 Z = 525721
68
XDOT = 5937
530803 XDOT = 1809
759389
YDOT = -12809
599509 feet/sec YDOT = -3904
365930 meter/sec
ZDOT = 19632
620008 ZDOT = 5984
022579
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 15085
39517187
00016717 00000-0 10270-3 0 9063
2 25544 51
6452 137
6186 0006990 142
1849 217
9797 15
55300378 15151
Satellite: ISS
Catalog Number: 25544
Epoch time: 15085
39517187 = yrday
fracday
Element set: 906
Inclination: 51
6452 deg
RA of node: 137
6186 deg
Eccentricity:
0006990
Arg of perigee: 142
1849 deg
Mean anomaly: 217
9797 deg
Mean motion: 15
55300378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1515
Checksum: 338
Coasting Arc #8 (Orbit 1529)
---------------------------------------
Vector Time (GMT): 2015/086/07:57:58
656
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5472449
19 A = 6783013
92 meter
Y = -3042860
89 meter E =
0012028
Z = -2600945
45 I = 51
92260
XDOT = 582
065202 Wp = 138
99566
YDOT = 5536
251859 meter/sec RA = 131
93233 deg
ZDOT = -5274
824677 TA = 70
16884
MA = 70
03923
Ha = 221
257 n
mi
Hp = 211
109
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17954229
61 X = 5518702
84
Y = -9983139
40 feet Y = -2981406
01 meter
Z = -8533285
59 Z = -2574248
80
XDOT = 1909
662735 XDOT = 545
737316
YDOT = 18163
555969 feet/sec YDOT = 5542
557288 meter/sec
ZDOT = -17305
855239 ZDOT = -5272
085869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18197119
01 X = 5546481
87
Y = 9634868
65 feet Y = 2936707
96 meter
Z = -8418346
78 Z = -2565912
10
XDOT = -13410
215034 XDOT = -4087
433542
YDOT = 10281
926507 feet/sec YDOT = 3133
931199 meter/sec
ZDOT = -17294
997280 ZDOT = -5271
515171
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 15086
35896086
00016717 00000-0 10270-3 0 9079
2 25544 51
6453 132
8057 0007003 146
1719 213
9882 15
55338284 15307
Satellite: ISS
Catalog Number: 25544
Epoch time: 15086
35896086 = yrday
fracday
Element set: 907
Inclination: 51
6453 deg
RA of node: 132
8057 deg
Eccentricity:
0007003
Arg of perigee: 146
1719 deg
Mean anomaly: 213
9882 deg
Mean motion: 15
55338284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1530
Checksum: 320
Coasting Arc #9 (Orbit 1541)
---------------------------------------
Vector Time (GMT): 2015/087/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904314
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4515618
54 A = 6785627
44 meter
Y = 5031308
62 meter E =
0013876
Z = 549294
04 I = 51
94415
XDOT = -3196
435362 Wp = 78
60983
YDOT = -3538
057994 meter/sec RA = 128
26121 deg
ZDOT = 6004
625810 TA = 287
29333
MA = 287
44510
Ha = 220
961 n
mi
Hp = 211
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14815021
47 X = -4574212
47
Y = 16506918
04 feet Y = 4980484
46 meter
Z = 1802145
81 Z = 527215
34
XDOT = -10486
992657 XDOT = -3185
802490
YDOT = -11607
801816 feet/sec YDOT = -3573
742585 meter/sec
ZDOT = 19700
215913 ZDOT = 5989
124388
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5210940
40 X = 1588294
63
Y = -21567204
04 feet Y = -6573683
79 meter
Z = 1706676
33 Z = 520194
95
XDOT = 13277
165710 XDOT = 4046
880109
YDOT = 4796
045952 feet/sec YDOT = 1461
834806 meter/sec
ZDOT = 19634
321717 ZDOT = 5984
541259
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 15087
12997559
00016717 00000-0 10270-3 0 9083
2 25544 51
6426 128
9563 0006493 147
1354 213
0205 15
55363013 15424
Satellite: ISS
Catalog Number: 25544
Epoch time: 15087
12997559 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 128
9563 deg
Eccentricity:
0006493
Arg of perigee: 147
1354 deg
Mean anomaly: 213
0205 deg
Mean motion: 15
55363013 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1542
Checksum: 311
Coasting Arc #10 (Orbit 1556)
---------------------------------------
Vector Time (GMT): 2015/088/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904314
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4954555
71 A = 6782801
36 meter
Y = -3822489
63 meter E =
0011415
Z = -2609404
70 I = 51
95363
XDOT = 1394
425455 Wp = 140
61691
YDOT = 5392
037879 meter/sec RA = 123
30316 deg
ZDOT = -5272
276430 TA = 68
63928
MA = 68
51750
Ha = 220
910 n
mi
Hp = 211
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16255104
03 X = 5009606
90
Y = -12540976
49 feet Y = -3766777
03 meter
Z = -8561039
05 Z = -2585202
45
XDOT = 4574
886663 XDOT = 1359
637370
YDOT = 17690
412990 feet/sec YDOT = 5407
436171 meter/sec
ZDOT = -17297
494849 ZDOT = -5265
587704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8074484
05 X = -2461102
74
Y = 18923100
64 feet Y = 5767761
08 meter
Z = -8456645
75 Z = -2577585
63
XDOT = -11369
230158 XDOT = -3465
341352
YDOT = -12537
562130 feet/sec YDOT = -3821
448937 meter/sec
ZDOT = -17269
685961 ZDOT = -5263
800281
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 15088
09372653
00016717 00000-0 10270-3 0 9093
2 25544 51
6423 124
1428 0006483 150
0092 210
1434 15
55402710 15576
Satellite: ISS
Catalog Number: 25544
Epoch time: 15088
09372653 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 124
1428 deg
Eccentricity:
0006483
Arg of perigee: 150
0092 deg
Mean anomaly: 210
1434 deg
Mean motion: 15
55402710 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1557
Checksum: 283
Coasting Arc #11 (Orbit 1572)
---------------------------------------
Vector Time (GMT): 2015/089/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904314
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4874731
49 A = 6778087
80 meter
Y = 2093413
99 meter E =
0015295
Z = 4213462
90 I = 51
95439
XDOT = 330
305637 Wp = 124
07338
YDOT = -6713
210632 meter/sec RA = 118
33178 deg
ZDOT = 3699
603546 TA = 288
08669
MA = 288
25324
Ha = 220
795 n
mi
Hp = 211
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15993213
57 X = -4918245
55
Y = 6868156
13 feet Y = 2038658
77 meter
Z = 13823697
18 Z = 4189676
60
XDOT = 1083
679910 XDOT = 387
378618
YDOT = -22024
969265 feet/sec YDOT = -6709
197376 meter/sec
ZDOT = 12137
806910 ZDOT = 3701
347535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10413877
50 X = 3174149
86
Y = -14047226
09 feet Y = -4281594
51 meter
Z = 13721357
34 Z = 4182269
72
XDOT = 9224
079189 XDOT = 2811
499337
YDOT = 18760
736272 feet/sec YDOT = 5718
272416 meter/sec
ZDOT = 12146
377677 ZDOT = 3702
215916
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 15089
12170422
00016717 00000-0 10270-3 0 9100
2 25544 51
6419 119
0074 0006504 154
7024 205
4449 15
55440150 15732
Satellite: ISS
Catalog Number: 25544
Epoch time: 15089
12170422 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 119
0074 deg
Eccentricity:
0006504
Arg of perigee: 154
7024 deg
Mean anomaly: 205
4449 deg
Mean motion: 15
55440150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1573
Checksum: 276
Coasting Arc #12 (Orbit 1587)
---------------------------------------
Vector Time (GMT): 2015/090/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904314
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4383259
87 A = 6774185
90 meter
Y = 68753
16 meter E =
0016483
Z = -5177586
26 I = 51
95558
XDOT = -1868
529448 Wp = 102
15867
YDOT = 7276
568192 meter/sec RA = 113
34598 deg
ZDOT = -1492
618185 TA = 153
55702
MA = 153
47282
Ha = 220
709 n
mi
Hp = 211
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14380773
84 X = 4407315
93
Y = 225568
12 feet Y = 117903
45 meter
Z = -16986831
55 Z = -5156234
92
XDOT = -6130
345958 XDOT = -1942
508341
YDOT = 23873
255224 feet/sec YDOT = 7255
259236 meter/sec
ZDOT = -4897
041290 ZDOT = -1501
875749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12495650
03 X = -3808674
13
Y = 7336090
58 feet Y = 2236040
41 meter
Z = -16895280
07 Z = -5149681
37
XDOT = -6657
155299 XDOT = -2029
100935
YDOT = -22655
406568 feet/sec YDOT = -6905
367922 meter/sec
ZDOT = -4937
933767 ZDOT = -1505
082212
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 15090
08541218
00016717 00000-0 10270-3 0 9113
2 25544 51
6416 114
1931 0006692 156
4685 203
6775 15
55474434 15887
Satellite: ISS
Catalog Number: 25544
Epoch time: 15090
08541218 = yrday
fracday
Element set: 911
Inclination: 51
6416 deg
RA of node: 114
1931 deg
Eccentricity:
0006692
Arg of perigee: 156
4685 deg
Mean anomaly: 203
6775 deg
Mean motion: 15
55474434 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1588
Checksum: 314
Coasting Arc #13 (Orbit 1603)
---------------------------------------
Vector Time (GMT): 2015/091/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904314
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3575889
74 A = 6773729
65 meter
Y = -2304233
50 meter E =
0006937
Z = 5266199
06 I = 51
96535
XDOT = 3091
980551 Wp = 130
84397
YDOT = -6960
755061 meter/sec RA = 108
35308 deg
ZDOT = -949
759009 TA = 328
17368
MA = 328
21558
Ha = 220
759 n
mi
Hp = 211
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11731921
72 X = -3575438
64
Y = -7559821
19 feet Y = -2344218
16 meter
Z = 17277555
96 Z = 5248829
55
XDOT = 10144
293145 XDOT = 3174
201124
YDOT = -22837
122904 feet/sec YDOT = -6925
718927 meter/sec
ZDOT = -3116
007246 ZDOT = -934
538113
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14047780
49 X = 4281763
49
Y = 64137
39 feet Y = 19549
08 meter
Z = 17203446
55 Z = 5243610
51
XDOT = 3611
821751 XDOT = 1100
883270
YDOT = 23710
997664 feet/sec YDOT = 7227
112088 meter/sec
ZDOT = -3049
581805 ZDOT = -929
512534
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
11334396
00016717 00000-0 10270-3 0 9126
2 25544 51
6412 109
0575 0006724 160
1726 199
9690 15
55467605 16048
Satellite: ISS
Catalog Number: 25544
Epoch time: 15091
11334396 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 109
0575 deg
Eccentricity:
0006724
Arg of perigee: 160
1726 deg
Mean anomaly: 199
9690 deg
Mean motion: 15
55467605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1604
Checksum: 308
Coasting Arc #14 (Orbit 1618)
---------------------------------------
Vector Time (GMT): 2015/092/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904314
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2577720
94 A = 6776697
43 meter
Y = 4375238
38 meter E =
0014644
Z = -4502101
94 I = 51
98551
XDOT = -3965
208136 Wp = 132
38205
YDOT = 5686
956519 meter/sec RA = 103
36501 deg
ZDOT = 3253
524875 TA = 170
26345
MA = 170
23504
Ha = 220
459 n
mi
Hp = 211
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8457089
71 X = 2550473
94
Y = 14354456
63 feet Y = 4403911
13 meter
Z = -14770675
67 Z = -4489646
70
XDOT = -13009
213045 XDOT = -4044
310743
YDOT = 18657
993828 feet/sec YDOT = 5642
173164 meter/sec
ZDOT = 10674
294210 ZDOT = 3234
069685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15023592
56 X = -4579191
01
Y = -7308770
72 feet Y = -2227713
32 meter
Z = -14717988
59 Z = -4486042
92
XDOT = 162
711860 XDOT = 49
594575
YDOT = -21678
806786 feet/sec YDOT = -6607
700308 meter/sec
ZDOT = 10589
909555 ZDOT = 3227
804432
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
07700599
00016717 00000-0 10270-3 0 9135
2 25544 51
6416 104
2425 0006814 163
4044 196
7333 15
55543383 16195
Satellite: ISS
Catalog Number: 25544
Epoch time: 15092
07700599 = yrday
fracday
Element set: 913
Inclination: 51
6416 deg
RA of node: 104
2425 deg
Eccentricity:
0006814
Arg of perigee: 163
4044 deg
Mean anomaly: 196
7333 deg
Mean motion: 15
55543383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1619
Checksum: 304
Coasting Arc #15 (Orbit 1629)
---------------------------------------
Vector Time (GMT): 2015/092/18:35:10
206
Vector Time (MET): N/A
Weight (LBS) : 904173
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2508120
66 A = 6778499
36 meter
Y = 4709134
39 meter E =
0011457
Z = -4193551
03 I = 51
99724
XDOT = -3910
171285 Wp = 135
88622
YDOT = 5418
589250 meter/sec RA = 99
84931 deg
ZDOT = 3744
288596 TA = 172
46491
MA = 172
44768
Ha = 220
227 n
mi
Hp = 212
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8228742
33 X = 2475646
36
Y = 15449915
97 feet Y = 4736999
63 meter
Z = -13758369
53 Z = -4181446
62
XDOT = -12828
645947 XDOT = -3988
661028
YDOT = 17777
523787 feet/sec YDOT = 5374
424857 meter/sec
ZDOT = 12284
411405 ZDOT = 3725
102238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11957293
16 X = 3644582
95
Y = -12838977
27 feet Y = -3913320
27 meter
Z = -13707247
69 Z = -4177969
09
XDOT = 20046
701563 XDOT = 6110
234636
YDOT = 5637
133433 feet/sec YDOT = 1718
198270 meter/sec
ZDOT = 12201
217059 ZDOT = 3718
930960
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
78367845
00016717 00000-0 10270-3 0 9147
2 25544 51
6447 100
7164 0005630 173
4685 186
6542 15
55310950 16302
Satellite: ISS
Catalog Number: 25544
Epoch time: 15092
78367845 = yrday
fracday
Element set: 914
Inclination: 51
6447 deg
RA of node: 100
7164 deg
Eccentricity:
0005630
Arg of perigee: 173
4685 deg
Mean anomaly: 186
6542 deg
Mean motion: 15
55310950 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1630
Checksum: 313
Coasting Arc #16 (Orbit 1645)
---------------------------------------
Vector Time (GMT): 2015/093/18:35:10
206
Vector Time (MET): N/A
Weight (LBS) : 904173
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1491038
61 A = 6783084
02 meter
Y = -6088367
42 meter E =
0016274
Z = 2566413
22 I = 52
01691
XDOT = 4440
627517 Wp = 123
39424
YDOT = -3329
598378 meter/sec RA = 94
88305 deg
ZDOT = -5303
575543 TA = 27
87329
MA = 27
78620
Ha = 220
208 n
mi
Hp = 212
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4891858
94 X = -1435312
98
Y = -19974958
71 feet Y = -6104729
23 meter
Z = 8419990
87 Z = 2559306
24
XDOT = 14568
987917 XDOT = 4503
292795
YDOT = -10923
879193 feet/sec YDOT = -3279
590774 meter/sec
ZDOT = -17400
182228 ZDOT = -5281
851002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17132384
22 X = -5221950
71
Y = 11397617
46 feet Y = 3473993
80 meter
Z = 8390544
28 Z = 2557437
90
XDOT = -14408
188361 XDOT = -4391
615812
YDOT = -8880
004261 feet/sec YDOT = -2706
625299 meter/sec
ZDOT = -17306
445929 ZDOT = -5275
004719
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
81171984
00016717 00000-0 10270-3 0 9150
2 25544 51
6445 95
5822 0005709 176
8751 183
2439 15
55322394 16460
Satellite: ISS
Catalog Number: 25544
Epoch time: 15093
81171984 = yrday
fracday
Element set: 915
Inclination: 51
6445 deg
RA of node: 95
5822 deg
Eccentricity:
0005709
Arg of perigee: 176
8751 deg
Mean anomaly: 183
2439 deg
Mean motion: 15
55322394 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1646
Checksum: 334
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