[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 14th 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
077/23:47:31
415 -2
2 2
2 2
2
N/A 0
1 -0
2 222
1
000/00:05:02
830 0
5 0
1 211
2
Coasting Arc #1 (Orbit 1314)
---------------------------------------
Vector Time (GMT): 2015/072/11:59:45
625
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4122272
33 A = 6776863
19 meter
Y = -2480864
34 meter E =
0015298
Z = 4760430
31 I = 51
49660
XDOT = 5705
456164 Wp = 81
91528
YDOT = 4415
594770 meter/sec RA = 200
87824 deg
ZDOT = -2630
108152 TA = 34
08895
MA = 33
99080
Ha = 222
618 n
mi
Hp = 210
017
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13524515
51 X = 4126583
28
Y = -8139318
71 feet Y = -2434741
84 meter
Z = 15618209
66 Z = 4780466
12
XDOT = 18718
688203 XDOT = 5668
431921
YDOT = 14486
859483 feet/sec YDOT = 4479
189636 meter/sec
ZDOT = -8628
963752 ZDOT = -2602
482636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14643493
99 X = 4463336
97
Y = -5659544
23 feet Y = -1725029
08 meter
Z = 15704367
05 Z = 4786691
08
XDOT = 15531
487457 XDOT = 4733
997377
YDOT = 16483
723528 feet/sec YDOT = 5024
238931 meter/sec
ZDOT = -8511
379225 ZDOT = -2594
268388
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 15072
54351892
00016717 00000-0 10270-3 0 9009
2 25544 51
6441 201
7830 0008753 98
7766 261
4379 15
55059589 13154
Satellite: ISS
Catalog Number: 25544
Epoch time: 15072
54351892 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 201
7830 deg
Eccentricity:
0008753
Arg of perigee: 98
7766 deg
Mean anomaly: 261
4379 deg
Mean motion: 15
55059589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1315
Checksum: 327
Coasting Arc #2 (Orbit 1329)
---------------------------------------
Vector Time (GMT): 2015/073/11:59:45
625
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5621011
16 A = 6780988
27 meter
Y = 1342594
46 meter E =
0013873
Z = -3561503
44 I = 51
54128
XDOT = -3963
029802 Wp = 100
15809
YDOT = -4805
917661 meter/sec RA = 195
87276 deg
ZDOT = 4455
440295 TA = 217
77522
MA = 217
87268
Ha = 222
537 n
mi
Hp = 209
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18441637
67 X = -5618306
28
Y = 4404837
48 feet Y = 1279751
44 meter
Z = -11684722
56 Z = -3588802
56
XDOT = -13002
066279 XDOT = -3930
637053
YDOT = -15767
446395 feet/sec YDOT = -4850
053313 meter/sec
ZDOT = 14617
586270 ZDOT = 4436
267938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18832657
62 X = -5740194
04
Y = 1441370
62 feet Y = 439329
76 meter
Z = -11801813
08 Z = -3597192
63
XDOT = -10329
081032 XDOT = -3148
303899
YDOT = -16266
583621 feet/sec YDOT = -4958
054688 meter/sec
ZDOT = 14536
237222 ZDOT = 4430
645105
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 15073
50743832
00016717 00000-0 10270-3 0 9016
2 25544 51
6446 196
9713 0008536 101
1728 259
0386 15
55111262 13305
Satellite: ISS
Catalog Number: 25544
Epoch time: 15073
50743832 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 196
9713 deg
Eccentricity:
0008536
Arg of perigee: 101
1728 deg
Mean anomaly: 259
0386 deg
Mean motion: 15
55111262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1330
Checksum: 295
Coasting Arc #3 (Orbit 1345)
---------------------------------------
Vector Time (GMT): 2015/074/11:59:45
625
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6536756
05 A = 6784955
67 meter
Y = -174351
21 meter E =
0022515
Z = 1772211
45 I = 51
58569
XDOT = 1680
333727 Wp = 111
18511
YDOT = 4898
412255 meter/sec RA = 190
88279 deg
ZDOT = -5665
934062 TA = 49
31245
MA = 49
11703
Ha = 222
462 n
mi
Hp = 209
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21446050
03 X = 6529611
21
Y = -572018
41 feet Y = -101292
72 meter
Z = 5814342
03 Z = 1803948
07
XDOT = 5512
905927 XDOT = 1652
956338
YDOT = 16070
906347 feet/sec YDOT = 4917
049217 meter/sec
ZDOT = -18589
022512 ZDOT = -5657
838384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21274804
13 X = 6484560
30
Y = 2458421
33 feet Y = 749326
82 meter
Z = 5950270
08 Z = 1813642
32
XDOT = 3483
548443 XDOT = 1061
785565
YDOT = 15152
141039 feet/sec YDOT = 4618
372589 meter/sec
ZDOT = -18555
105715 ZDOT = -5655
596222
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 15074
53559553
00016717 00000-0 10270-3 0 9026
2 25544 51
6447 191
8376 0008616 105
2899 254
9208 15
55155482 13464
Satellite: ISS
Catalog Number: 25544
Epoch time: 15074
53559553 = yrday
fracday
Element set: 902
Inclination: 51
6447 deg
RA of node: 191
8376 deg
Eccentricity:
0008616
Arg of perigee: 105
2899 deg
Mean anomaly: 254
9208 deg
Mean motion: 15
55155482 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1346
Checksum: 334
Coasting Arc #4 (Orbit 1361)
---------------------------------------
Vector Time (GMT): 2015/075/11:59:45
625
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6720196
31 A = 6786202
36 meter
Y = -881125
50 meter E =
0018351
Z = 233780
47 I = 51
62235
XDOT = 837
780242 Wp = 71
64909
YDOT = -4695
014816 meter/sec RA = 185
90447 deg
ZDOT = 6005
754070 TA = 290
87120
MA = 291
06759
Ha = 222
399 n
mi
Hp = 209
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22047888
16 X = -6710979
50
Y = -2890831
68 feet Y = -956223
56 meter
Z = 766996
28 Z = 201157
95
XDOT = 2748
622841 XDOT = 861
045403
YDOT = -15403
591916 feet/sec YDOT = -4685
515473 meter/sec
ZDOT = 19703
917553 ZDOT = 6009
880812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21522473
77 X = -6560050
01
Y = -5607497
92 feet Y = -1709165
37 meter
Z = 627417
96 Z = 191237
00
XDOT = 4107
450240 XDOT = 1251
950833
YDOT = -13387
263921 feet/sec YDOT = -4080
438043 meter/sec
ZDOT = 19722
306480 ZDOT = 6011
359015
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 15075
56372626
00016717 00000-0 10270-3 0 9035
2 25544 51
6456 186
7043 0008581 107
4222 252
7870 15
55199656 13623
Satellite: ISS
Catalog Number: 25544
Epoch time: 15075
56372626 = yrday
fracday
Element set: 903
Inclination: 51
6456 deg
RA of node: 186
7043 deg
Eccentricity:
0008581
Arg of perigee: 107
4222 deg
Mean anomaly: 252
7870 deg
Mean motion: 15
55199656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1362
Checksum: 322
Coasting Arc #5 (Orbit 1376)
---------------------------------------
Vector Time (GMT): 2015/076/11:59:45
625
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6095849
48 A = 6783938
80 meter
Y = 1905851
19 meter E =
0014210
Z = -2283645
55 I = 51
64691
XDOT = -3350
838882 Wp = 121
99146
YDOT = 4245
605201 meter/sec RA = 180
92725 deg
ZDOT = -5433
467484 TA = 83
43354
MA = 83
27179
Ha = 222
348 n
mi
Hp = 209
967
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19999506
16 X = 6085177
69
Y = 6252792
61 feet Y = 1973958
99 meter
Z = -7492275
41 Z = -2254059
65
XDOT = -10993
565887 XDOT = -3371
671801
YDOT = 13929
150921 feet/sec YDOT = 4208
016756 meter/sec
ZDOT = -17826
336889 ZDOT = -5449
796132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19261516
13 X = 5870910
11
Y = 8363624
88 feet Y = 2549232
86 meter
Z = -7365842
00 Z = -2245108
64
XDOT = -11699
767054 XDOT = -3566
088998
YDOT = 11277
335266 feet/sec YDOT = 3437
331789 meter/sec
ZDOT = -17896
919159 ZDOT = -5454
980960
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 15076
52757495
00016717 00000-0 10270-3 0 9044
2 25544 51
6458 181
8918 0008547 111
1650 249
0417 15
55245295 13774
Satellite: ISS
Catalog Number: 25544
Epoch time: 15076
52757495 = yrday
fracday
Element set: 904
Inclination: 51
6458 deg
RA of node: 181
8918 deg
Eccentricity:
0008547
Arg of perigee: 111
1650 deg
Mean anomaly: 249
0417 deg
Mean motion: 15
55245295 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1377
Checksum: 332
Coasting Arc #6 (Orbit 1392)
---------------------------------------
Vector Time (GMT): 2015/077/11:59:45
625
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4762795
57 A = 6779431
41 meter
Y = -2778942
25 meter E =
0019537
Z = 3931887
83 I = 51
66461
XDOT = 5449
219343 Wp = 106
18203
YDOT = -3590
403458 meter/sec RA = 175
94020 deg
ZDOT = 4041
199995 TA = 301
56213
MA = 301
75274
Ha = 222
260 n
mi
Hp = 209
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15625969
72 X = -4750466
22
Y = -9117264
61 feet Y = -2832133
42 meter
Z = 12899894
46 Z = 3908781
73
XDOT = 17878
016217 XDOT = 5469
332682
YDOT = -11779
538904 feet/sec YDOT = -3529
353671 meter/sec
ZDOT = 13258
530168 ZDOT = 4067
720310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14823216
14 X = -4518116
28
Y = -10492892
04 feet Y = -3198233
49 meter
Z = 12801335
90 Z = 3901847
18
XDOT = 18016
311189 XDOT = 5491
371650
YDOT = -9048
129052 feet/sec YDOT = -2757
869735 meter/sec
ZDOT = 13372
675156 ZDOT = 4075
991388
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 15077
55565445
00016717 00000-0 10270-3 0 9051
2 25544 51
6464 176
7582 0008526 114
4251 245
7793 15
55308099 13931
Satellite: ISS
Catalog Number: 25544
Epoch time: 15077
55565445 = yrday
fracday
Element set: 905
Inclination: 51
6464 deg
RA of node: 176
7582 deg
Eccentricity:
0008526
Arg of perigee: 114
4251 deg
Mean anomaly: 245
7793 deg
Mean motion: 15
55308099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1393
Checksum: 336
Coasting Arc #7 (Orbit 1399)
---------------------------------------
Vector Time (GMT): 2015/077/23:50:02
830
Vector Time (MET): N/A
Weight (LBS) : 889173
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2021244
03 A = 6776703
80 meter
Y = 4177235
94 meter E =
0019036
Z = -4956194
45 I = 51
66657
XDOT = -7275
269291 Wp = 109
24974
YDOT = -912
818764 meter/sec RA = 173
43751 deg
ZDOT = 2198
436846 TA = 182
22313
MA = 182
23161
Ha = 222
147 n
mi
Hp = 211
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6631378
06 X = -2043729
56
Y = 13704842
32 feet Y = 4154506
57 meter
Z = -16260480
48 Z = -4966068
43
XDOT = -23868
993738 XDOT = -7275
200298
YDOT = -2994
812217 feet/sec YDOT = -994
174847 meter/sec
ZDOT = 7212
719312 ZDOT = 2163
095682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8173175
50 X = 2491183
89
Y = -12790589
54 feet Y = -3898571
69 meter
Z = -16303408
39 Z = -4969278
88
XDOT = 22427
463608 XDOT = 6835
890908
YDOT = 5333
537599 feet/sec YDOT = 1625
662260 meter/sec
ZDOT = 7061
461774 ZDOT = 2152
333549
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 15078
00543357
00016717 00000-0 10270-3 0 9061
2 25544 51
6458 174
5144 0006614 114
4372 245
7472 15
54881002 14006
Satellite: ISS
Catalog Number: 25544
Epoch time: 15078
00543357 = yrday
fracday
Element set: 906
Inclination: 51
6458 deg
RA of node: 174
5144 deg
Eccentricity:
0006614
Arg of perigee: 114
4372 deg
Mean anomaly: 245
7472 deg
Mean motion: 15
54881002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1400
Checksum: 291
Coasting Arc #8 (Orbit 1415)
---------------------------------------
Vector Time (GMT): 2015/078/23:50:02
830
Vector Time (MET): N/A
Weight (LBS) : 889173
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3904941
80 A = 6780533
85 meter
Y = -3933263
94 meter E =
0016908
Z = 3890300
18 I = 51
71088
XDOT = 6159
596367 Wp = 94
67233
YDOT = 2045
049364 meter/sec RA = 168
44276 deg
ZDOT = -4101
166152 TA = 38
27697
MA = 38
15707
Ha = 222
019 n
mi
Hp = 211
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12811488
85 X = 3929736
75
Y = -12904409
25 feet Y = -3889457
04 meter
Z = 12763452
03 Z = 3909330
40
XDOT = 20208
649497 XDOT = 6156
192161
YDOT = 6709
479542 feet/sec YDOT = 2113
910273 meter/sec
ZDOT = -13455
269529 ZDOT = -4071
252823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14033454
02 X = -4277396
78
Y = 11472451
91 feet Y = 3496803
34 meter
Z = 12845573
08 Z = 3915330
68
XDOT = -18626
086275 XDOT = -5677
231097
YDOT = -7810
413614 feet/sec YDOT = -2380
614070 meter/sec
ZDOT = -13327
424085 ZDOT = -4062
198861
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
03375436
00016717 00000-0 10270-3 0 9077
2 25544 51
6456 169
3828 0006646 117
8067 242
3761 15
54911591 14166
Satellite: ISS
Catalog Number: 25544
Epoch time: 15079
03375436 = yrday
fracday
Element set: 907
Inclination: 51
6456 deg
RA of node: 169
3828 deg
Eccentricity:
0006646
Arg of perigee: 117
8067 deg
Mean anomaly: 242
3761 deg
Mean motion: 15
54911591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1416
Checksum: 327
Coasting Arc #9 (Orbit 1430)
---------------------------------------
Vector Time (GMT): 2015/079/23:50:02
830
Vector Time (MET): N/A
Weight (LBS) : 889173
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5338441
54 A = 6784536
53 meter
Y = 3491366
30 meter E =
0009728
Z = -2318565
28 I = 51
75608
XDOT = -4405
092778 Wp = 86
85731
YDOT = -3148
981173 meter/sec RA = 163
46267 deg
ZDOT = 5420
934359 TA = 247
35954
MA = 247
46245
Ha = 221
925 n
mi
Hp = 211
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17514571
98 X = -5365823
35
Y = 11454613
85 feet Y = 3431514
87 meter
Z = -7606841
46 Z = -2344565
45
XDOT = -14452
404126 XDOT = -4395
885575
YDOT = -10331
303060 feet/sec YDOT = -3198
189412 meter/sec
ZDOT = 17785
217714 ZDOT = 5399
558188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18421006
70 X = 5614722
84
Y = -9844775
58 feet Y = -3000687
60 meter
Z = -7718766
29 Z = -2352679
97
XDOT = 12864
054159 XDOT = 3920
963708
YDOT = 10248
572058 feet/sec YDOT = 3123
764763 meter/sec
ZDOT = 17694
107713 ZDOT = 5393
164031
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
99778134
00016717 00000-0 10270-3 0 9085
2 25544 51
6461 164
5711 0006569 121
0268 239
1531 15
54967638 14313
Satellite: ISS
Catalog Number: 25544
Epoch time: 15079
99778134 = yrday
fracday
Element set: 908
Inclination: 51
6461 deg
RA of node: 164
5711 deg
Eccentricity:
0006569
Arg of perigee: 121
0268 deg
Mean anomaly: 239
1531 deg
Mean motion: 15
54967638 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1431
Checksum: 332
Coasting Arc #10 (Orbit 1446)
---------------------------------------
Vector Time (GMT): 2015/080/23:50:02
830
Vector Time (MET): N/A
Weight (LBS) : 889173
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6187286
81 A = 6786832
09 meter
Y = -2743391
32 meter E =
0019382
Z = 361227
95 I = 51
79351
XDOT = 2229
987576 Wp = 129
11704
YDOT = 4210
475792 meter/sec RA = 158
49554 deg
ZDOT = -6015
500793 TA = 46
99394
MA = 46
83168
Ha = 221
926 n
mi
Hp = 211
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20299497
41 X = 6215749
49
Y = -9000627
68 feet Y = -2674041
83 meter
Z = 1185131
06 Z = 391354
23
XDOT = 7316
232205 XDOT = 2211
960441
YDOT = 13813
896956 feet/sec YDOT = 4235
311241 meter/sec
ZDOT = -19735
894989 ZDOT = -6004
712355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20889612
29 X = -6367153
83
Y = 7508745
93 feet Y = 2288665
76 meter
Z = 1314633
87 Z = 400700
40
XDOT = -5874
833368 XDOT = -1790
649211
YDOT = -12791
080441 feet/sec YDOT = -3898
721319 meter/sec
ZDOT = -19690
308774 ZDOT = -6001
606114
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
02605367
00016717 00000-0 10270-3 0 9090
2 25544 51
6460 159
4385 0006588 125
0436 235
1336 15
54966155 14473
Satellite: ISS
Catalog Number: 25544
Epoch time: 15081
02605367 = yrday
fracday
Element set: 909
Inclination: 51
6460 deg
RA of node: 159
4385 deg
Eccentricity:
0006588
Arg of perigee: 125
0436 deg
Mean anomaly: 235
1336 deg
Mean motion: 15
54966155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1447
Checksum: 317
Coasting Arc #11 (Orbit 1462)
---------------------------------------
Vector Time (GMT): 2015/081/23:50:02
830
Vector Time (MET): N/A
Weight (LBS) : 889173
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6350610
17 A = 6785706
54 meter
Y = 1751980
60 meter E =
0017693
Z = 1604964
19 I = 51
81898
XDOT = 63
933486 Wp = 82
07914
YDOT = -5079
879742 meter/sec RA = 153
53189 deg
ZDOT = 5746
444841 TA = 295
44597
MA = 295
62895
Ha = 221
774 n
mi
Hp = 211
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20835335
22 X = -6377525
60
Y = 5747967
86 feet Y = 1680813
66 meter
Z = 5265630
55 Z = 1574048
40
XDOT = 209
755533 XDOT = 92
818936
YDOT = -16666
272121 feet/sec YDOT = -5079
002507 meter/sec
ZDOT = 18853
165490 ZDOT = 5746
826270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21153746
67 X = 6447661
99
Y = -4587997
55 feet Y = -1398421
65 meter
Z = 5132881
58 Z = 1564502
31
XDOT = -1344
279364 XDOT = -409
736350
YDOT = 15091
688453 feet/sec YDOT = 4599
946641 meter/sec
ZDOT = 18855
579273 ZDOT = 5747
180562
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
05430026
00016717 00000-0 10270-3 0 9104
2 25544 51
6457 154
3057 0006419 126
9171 233
2571 15
55019314 14633
Satellite: ISS
Catalog Number: 25544
Epoch time: 15082
05430026 = yrday
fracday
Element set: 910
Inclination: 51
6457 deg
RA of node: 154
3057 deg
Eccentricity:
0006419
Arg of perigee: 126
9171 deg
Mean anomaly: 233
2571 deg
Mean motion: 15
55019314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1463
Checksum: 281
Coasting Arc #12 (Orbit 1477)
---------------------------------------
Vector Time (GMT): 2015/082/23:50:02
830
Vector Time (MET): N/A
Weight (LBS) : 889173
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5849545
76 A = 6781824
41 meter
Y = -437253
31 meter E =
0010444
Z = -3407208
98 I = 51
83431
XDOT = -2270
422253 Wp = 114
99297
YDOT = 5662
144456 meter/sec RA = 148
56208 deg
ZDOT = -4639
945336 TA = 104
71213
MA = 104
59635
Ha = 221
662 n
mi
Hp = 211
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19191423
11 X = 5870551
51
Y = -1434558
09 feet Y = -371722
81 meter
Z = -11178507
17 Z = -3378741
82
XDOT = -7448
891905 XDOT = -2311
029721
YDOT = 18576
589423 feet/sec YDOT = 5636
527526 meter/sec
ZDOT = -15222
917768 ZDOT = -4651
073945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19302574
30 X = -5883424
65
Y = 702467
62 feet Y = 214112
13 meter
Z = -11056439
98 Z = -3370002
90
XDOT = 8104
037820 XDOT = 2470
110727
YDOT = -16874
850360 feet/sec YDOT = -5143
454390 meter/sec
ZDOT = -15271
488018 ZDOT = -4654
749548
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
01825839
00016717 00000-0 10270-3 0 9112
2 25544 51
6458 149
4935 0006303 131
7543 228
4150 15
55051803 14787
Satellite: ISS
Catalog Number: 25544
Epoch time: 15083
01825839 = yrday
fracday
Element set: 911
Inclination: 51
6458 deg
RA of node: 149
4935 deg
Eccentricity:
0006303
Arg of perigee: 131
7543 deg
Mean anomaly: 228
4150 deg
Mean motion: 15
55051803 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1478
Checksum: 303
Coasting Arc #13 (Orbit 1493)
---------------------------------------
Vector Time (GMT): 2015/083/23:50:02
830
Vector Time (MET): N/A
Weight (LBS) : 889173
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4787466
89 A = 6777341
38 meter
Y = -1034605
84 meter E =
0014389
Z = 4677653
58 I = 51
84611
XDOT = 4084
906793 Wp = 123
69374
YDOT = -5824
145148 meter/sec RA = 143
57988 deg
ZDOT = 2878
476120 TA = 297
74405
MA = 297
88991
Ha = 221
657 n
mi
Hp = 211
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15706912
36 X = -4798264
23
Y = -3394376
13 feet Y = -1088202
33 meter
Z = 15346632
48 Z = 4654370
80
XDOT = 13401
925173 XDOT = 4135
747557
YDOT = -19108
087756 feet/sec YDOT = -5778
180500 meter/sec
ZDOT = 9443
819290 ZDOT = 2898
443933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15729903
24 X = 4794474
51
Y = 3721165
53 feet Y = 1134211
25 meter
Z = 15247002
49 Z = 4647286
36
XDOT = -13465
125198 XDOT = -4104
170160
YDOT = 17678
436115 feet/sec YDOT = 5388
387328 meter/sec
ZDOT = 9530
314316 ZDOT = 2904
839803
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
04645803
00016717 00000-0 10270-3 0 9128
2 25544 51
6457 144
3603 0006360 133
6023 226
5659 15
55093769 14947
Satellite: ISS
Catalog Number: 25544
Epoch time: 15084
04645803 = yrday
fracday
Element set: 912
Inclination: 51
6457 deg
RA of node: 144
3603 deg
Eccentricity:
0006360
Arg of perigee: 133
6023 deg
Mean anomaly: 226
5659 deg
Mean motion: 15
55093769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1494
Checksum: 309
Coasting Arc #14 (Orbit 1508)
---------------------------------------
Vector Time (GMT): 2015/084/23:50:02
830
Vector Time (MET): N/A
Weight (LBS) : 889173
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3309684
92 A = 6774520
42 meter
Y = 2636311
06 meter E =
0019039
Z = -5306399
16 I = 51
86198
XDOT = -5365
817412 Wp = 100
00992
YDOT = 5422
019722 meter/sec RA = 138
58628 deg
ZDOT = -658
219776 TA = 163
74568
MA = 163
68453
Ha = 221
331 n
mi
Hp = 211
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10858546
31 X = 3305735
60
Y = 8649314
51 feet Y = 2673299
56 meter
Z = -17409446
05 Z = -5290331
17
XDOT = -17604
387835 XDOT = -5422
851533
YDOT = 17788
778614 feet/sec YDOT = 5361
696692 meter/sec
ZDOT = -2159
513702 ZDOT = -684
424917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10937473
99 X = -3333742
07
Y = -8687309
45 feet Y = -2647891
92 meter
Z = -17340986
08 Z = -5285532
56
XDOT = 17020
924339 XDOT = 5187
977739
YDOT = -16927
413520 feet/sec YDOT = -5159
475641 meter/sec
ZDOT = -2272
699796 ZDOT = -692
718898
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
01037158
00016717 00000-0 10270-3 0 9135
2 25544 51
6454 139
5473 0006194 137
4639 222
6995 15
55157749 15091
Satellite: ISS
Catalog Number: 25544
Epoch time: 15085
01037158 = yrday
fracday
Element set: 913
Inclination: 51
6454 deg
RA of node: 139
5473 deg
Eccentricity:
0006194
Arg of perigee: 137
4639 deg
Mean anomaly: 222
6995 deg
Mean motion: 15
55157749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1509
Checksum: 330
Coasting Arc #15 (Orbit 1524)
---------------------------------------
Vector Time (GMT): 2015/085/23:50:02
830
Vector Time (MET): N/A
Weight (LBS) : 889173
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1628911
12 A = 6775071
06 meter
Y = -4115920
87 meter E =
0008115
Z = 5121816
51 I = 51
88788
XDOT = 6031
576047 Wp = 104
11402
YDOT = -4449
921445 meter/sec RA = 133
59186 deg
ZDOT = -1657
476169 TA = 1
81492
MA = 1
81197
Ha = 221
247 n
mi
Hp = 211
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5344196
58 X = -1607644
67
Y = -13503677
39 feet Y = -4134017
05 meter
Z = 16803859
95 Z = 5113955
62
XDOT = 19788
635326 XDOT = 6088
939228
YDOT = -14599
479806 feet/sec YDOT = -4382
151836 meter/sec
ZDOT = -5437
913939 ZDOT = -1628
036270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5633710
84 X = 1717155
06
Y = 13426857
29 feet Y = 4092506
10 meter
Z = 16770815
57 Z = 5111744
59
XDOT = -18643
336633 XDOT = -5682
489006
YDOT = 14457
237503 feet/sec YDOT = 4406
565991 meter/sec
ZDOT = -5310
995924 ZDOT = -1618
791558
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
03852298
00016717 00000-0 10270-3 0 9149
2 25544 51
6457 134
4141 0006129 141
6697 218
4892 15
55205759 15251
Satellite: ISS
Catalog Number: 25544
Epoch time: 15086
03852298 = yrday
fracday
Element set: 914
Inclination: 51
6457 deg
RA of node: 134
4141 deg
Eccentricity:
0006129
Arg of perigee: 141
6697 deg
Mean anomaly: 218
4892 deg
Mean motion: 15
55205759 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1525
Checksum: 324
Coasting Arc #16 (Orbit 1539)
---------------------------------------
Vector Time (GMT): 2015/086/23:50:02
830
Vector Time (MET): N/A
Weight (LBS) : 889173
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -55927
04 A = 6778715
18 meter
Y = 5336679
38 meter E =
0013329
Z = -4194058
03 I = 51
92066
XDOT = -6037
425178 Wp = 125
38523
YDOT = 2871
374950 meter/sec RA = 128
60521 deg
ZDOT = 3734
991246 TA = 182
89776
MA = 182
90549
Ha = 221
081 n
mi
Hp = 211
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -183487
65 X = -95225
81
Y = 17508790
62 feet Y = 5335833
83 meter
Z = -13760032
90 Z = -4194425
68
XDOT = -19807
825387 XDOT = -6087
227972
YDOT = 9420
521490 feet/sec YDOT = 2803
582416 meter/sec
ZDOT = 12253
908288 ZDOT = 3705
541491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -442920
20 X = -135002
08
Y = -17502236
78 feet Y = -5334681
77 meter
Z = -13762465
31 Z = -4194799
43
XDOT = 18309
345542 XDOT = 5580
688521
YDOT = -9997
108930 feet/sec YDOT = -3047
118802 meter/sec
ZDOT = 12127
183353 ZDOT = 3696
365486
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
00239439
00016717 00000-0 10270-3 0 9154
2 25544 51
6451 129
6008 0006097 145
0971 215
0583 15
55217217 15409
Satellite: ISS
Catalog Number: 25544
Epoch time: 15087
00239439 = yrday
fracday
Element set: 915
Inclination: 51
6451 deg
RA of node: 129
6008 deg
Eccentricity:
0006097
Arg of perigee: 145
0971 deg
Mean anomaly: 215
0583 deg
Mean motion: 15
55217217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1540
Checksum: 297
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