[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 6th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 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
048/10:50:37
748 1
4 2
6 2
7
N/A -2
1 -0
3 222
3
000/00:07:15
497 0
7 0
1 213
2
Coasting Arc #1 (Orbit 2433)
---------------------------------------
Vector Time (GMT): 2016/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4373996
38 A = 6781673
48 meter
Y = -3261919
60 meter E =
0013117
Z = -4039130
79 I = 51
63627
XDOT = 5852
437619 Wp = 92
93455
YDOT = 3012
982193 meter/sec RA = 359
15701 deg
ZDOT = 3914
750297 TA = 217
70546
MA = 217
79747
Ha = 222
957 n
mi
Hp = 211
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14350381
83 X = 4429766
89
Y = -10701835
97 feet Y = -3212694
85 meter
Z = -13251741
44 Z = -4017747
94
XDOT = 19200
910822 XDOT = 5799
294923
YDOT = 9885
112182 feet/sec YDOT = 3078
130891 meter/sec
ZDOT = 12843
668952 ZDOT = 3943
050377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17738558
37 X = 5406712
59
Y = 2876225
72 feet Y = 876673
60 meter
Z = -13158353
83 Z = -4010666
25
XDOT = 6463
004036 XDOT = 1969
923630
YDOT = 19301
049633 feet/sec YDOT = 5882
959928 meter/sec
ZDOT = 12965
753878 ZDOT = 3951
961782
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 16036
50874454
00016717 00000-0 10270-3 0 9000
2 25544 51
6401 359
6943 0006595 78
3022 281
8870 15
54418818 24347
Satellite: ISS
Catalog Number: 25544
Epoch time: 16036
50874454 = yrday
fracday
Element set: 900
Inclination: 51
6401 deg
RA of node: 359
6943 deg
Eccentricity:
0006595
Arg of perigee: 78
3022 deg
Mean anomaly: 281
8870 deg
Mean motion: 15
54418818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2434
Checksum: 321
Coasting Arc #2 (Orbit 2449)
---------------------------------------
Vector Time (GMT): 2016/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5668776
63 A = 6785569
34 meter
Y = 2651003
61 meter E =
0019916
Z = 2602805
38 I = 51
61833
XDOT = -4171
834093 Wp = 96
09984
YDOT = -3745
323750 meter/sec RA = 354
17125 deg
ZDOT = -5238
975896 TA = 54
56656
MA = 54
38077
Ha = 222
925 n
mi
Hp = 211
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18598348
54 X = -5710642
53
Y = 8697518
40 feet Y = 2587377
53 meter
Z = 8539387
74 Z = 2575166
77
XDOT = -13687
119728 XDOT = -4104
194768
YDOT = -12287
807578 feet/sec YDOT = -3791
597826 meter/sec
ZDOT = -17188
241129 ZDOT = -5259
076854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19367042
14 X = -5903074
44
Y = -6964520
73 feet Y = -2122785
92 meter
Z = 8419006
33 Z = 2566113
13
XDOT = -1488
242615 XDOT = -453
616349
YDOT = -16874
047251 feet/sec YDOT = -5143
209602 meter/sec
ZDOT = -17274
624653 ZDOT = -5265
305594
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 16037
53736281
00016717 00000-0 10270-3 0 9010
2 25544 51
6407 354
5632 0006587 81
9205 278
2695 15
54462350 24509
Satellite: ISS
Catalog Number: 25544
Epoch time: 16037
53736281 = yrday
fracday
Element set: 901
Inclination: 51
6407 deg
RA of node: 354
5632 deg
Eccentricity:
0006587
Arg of perigee: 81
9205 deg
Mean anomaly: 278
2695 deg
Mean motion: 15
54462350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2450
Checksum: 313
Coasting Arc #3 (Orbit 2464)
---------------------------------------
Vector Time (GMT): 2016/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6430294
20 A = 6787976
44 meter
Y = -1960976
04 meter E =
0015379
Z = -908991
61 I = 51
59509
XDOT = 2157
492633 Wp = 56
84358
YDOT = 4367
210369 meter/sec RA = 349
19365 deg
ZDOT = 5921
656856 TA = 293
31109
MA = 293
47286
Ha = 222
870 n
mi
Hp = 211
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21096765
74 X = 6456159
79
Y = -6433648
44 feet Y = -1888923
64 meter
Z = -2982255
94 Z = -877692
74
XDOT = 7078
387904 XDOT = 2079
732907
YDOT = 14328
118007 feet/sec YDOT = 4390
902270 meter/sec
ZDOT = 19428
008058 ZDOT = 5931
948169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19694505
22 X = 6002885
19
Y = 9969207
03 feet Y = 3038614
30 meter
Z = -2846152
27 Z = -867507
21
XDOT = -4171
091167 XDOT = -1271
348588
YDOT = 13719
929970 feet/sec YDOT = 4181
834655 meter/sec
ZDOT = 19471
734251 ZDOT = 5934
984600
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 16038
50167945
00016717 00000-0 10270-3 0 9024
2 25544 51
6409 349
7535 0006561 85
8019 274
3884 15
54482572 24658
Satellite: ISS
Catalog Number: 25544
Epoch time: 16038
50167945 = yrday
fracday
Element set: 902
Inclination: 51
6409 deg
RA of node: 349
7535 deg
Eccentricity:
0006561
Arg of perigee: 85
8019 deg
Mean anomaly: 274
3884 deg
Mean motion: 15
54482572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2465
Checksum: 336
Coasting Arc #4 (Orbit 2480)
---------------------------------------
Vector Time (GMT): 2016/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6628467
18 A = 6787816
61 meter
Y = 1083149
51 meter E =
0014663
Z = -958347
83 I = 51
56478
XDOT = 45
129565 Wp = 120
32438
YDOT = -4885
489011 meter/sec RA = 344
21750 deg
ZDOT = -5908
627965 TA = 70
06481
MA = 69
90691
Ha = 222
762 n
mi
Hp = 211
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21746939
57 X = -6635431
47
Y = 3553640
14 feet Y = 1008986
61 meter
Z = -3144185
79 Z = -990563
41
XDOT = 148
062876 XDOT = 128
457792
YDOT = -16028
507255 feet/sec YDOT = -4884
518722 meter/sec
ZDOT = -19385
262352 ZDOT = -5908
206110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18353696
26 X = -5594206
62
Y = -12157315
16 feet Y = -3705549
66 meter
Z = -3284077
44 Z = -1000986
80
XDOT = 10206
813755 XDOT = 3111
036833
YDOT = -10236
695203 feet/sec YDOT = -3120
144698 meter/sec
ZDOT = -19382
440344 ZDOT = -5907
767817
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 16039
53027075
00016717 00000-0 10270-3 0 9038
2 25544 51
6421 344
6224 0006514 89
1596 271
0303 15
54501265 24815
Satellite: ISS
Catalog Number: 25544
Epoch time: 16039
53027075 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 344
6224 deg
Eccentricity:
0006514
Arg of perigee: 89
1596 deg
Mean anomaly: 271
0303 deg
Mean motion: 15
54501265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2481
Checksum: 287
Coasting Arc #5 (Orbit 2496)
---------------------------------------
Vector Time (GMT): 2016/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6233876
23 A = 6785100
18 meter
Y = -106354
50 meter E =
0019884
Z = 2655860
54 I = 51
52544
XDOT = -2137
719377 Wp = 82
59838
YDOT = 5226
802627 meter/sec RA = 339
23544 deg
ZDOT = 5196
118555 TA = 307
44032
MA = 307
62107
Ha = 222
689 n
mi
Hp = 211
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20452349
82 X = 6221701
49
Y = -348932
07 feet Y = -36711
04 meter
Z = 8713453
23 Z = 2686112
84
XDOT = -7013
515018 XDOT = -2221
247784
YDOT = 17148
302581 feet/sec YDOT = 5202
430564 meter/sec
ZDOT = 17047
633054 ZDOT = 5185
531061
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15431395
09 X = 4703489
22
Y = 13341260
90 feet Y = 4066416
32 meter
Z = 8844627
59 Z = 2695842
49
XDOT = -15771
202041 XDOT = -4807
062382
YDOT = 6905
215028 feet/sec YDOT = 2104
709541 meter/sec
ZDOT = 17000
678756 ZDOT = 5181
806885
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 16040
55884797
00016717 00000-0 10270-3 0 9045
2 25544 51
6421 339
4923 0006499 93
1061 267
0836 15
54524081 24971
Satellite: ISS
Catalog Number: 25544
Epoch time: 16040
55884797 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 339
4923 deg
Eccentricity:
0006499
Arg of perigee: 93
1061 deg
Mean anomaly: 267
0836 deg
Mean motion: 15
54524081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2497
Checksum: 330
Coasting Arc #6 (Orbit 2511)
---------------------------------------
Vector Time (GMT): 2016/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5315641
82 A = 6780888
14 meter
Y = -1049646
30 meter E =
0013694
Z = -4090205
64 I = 51
48260
XDOT = 3984
336458 Wp = 82
07165
YDOT = -5303
997959 meter/sec RA = 334
24002 deg
ZDOT = -3826
079765 TA = 148
28589
MA = 148
20333
Ha = 222
681 n
mi
Hp = 211
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17439769
74 X = -5283641
32
Y = -3443721
46 feet Y = -1108910
76 meter
Z = -13419309
84 Z = -4115949
32
XDOT = 13071
970008 XDOT = 4061
935997
YDOT = -17401
568108 feet/sec YDOT = -5259
008915 meter/sec
ZDOT = -12552
755134 ZDOT = -3806
536341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10876212
24 X = -3315069
49
Y = -13953882
70 feet Y = -4253143
45 meter
Z = -13530699
45 Z = -4124157
19
XDOT = 20312
965025 XDOT = 6191
391740
YDOT = -3772
755277 feet/sec YDOT = -1149
935809 meter/sec
ZDOT = -12466
972014 ZDOT = -3799
933070
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 16041
52312646
00016717 00000-0 10270-3 0 9053
2 25544 51
6426 334
6819 0006513 96
0431 264
1464 15
54555202 25129
Satellite: ISS
Catalog Number: 25544
Epoch time: 16041
52312646 = yrday
fracday
Element set: 905
Inclination: 51
6426 deg
RA of node: 334
6819 deg
Eccentricity:
0006513
Arg of perigee: 96
0431 deg
Mean anomaly: 264
1464 deg
Mean motion: 15
54555202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2512
Checksum: 286
Coasting Arc #7 (Orbit 2527)
---------------------------------------
Vector Time (GMT): 2016/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3993310
56 A = 6777291
85 meter
Y = 2247093
13 meter E =
0011994
Z = 4985245
30 I = 51
44227
XDOT = -5388
591040 Wp = 111
40173
YDOT = 5080
413874 meter/sec RA = 329
23161 deg
ZDOT = 2018
198578 TA = 318
90589
MA = 318
99617
Ha = 222
466 n
mi
Hp = 211
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13101412
61 X = 3943670
48
Y = 7372352
79 feet Y = 2291471
90 meter
Z = 16355791
67 Z = 5004522
67
XDOT = -17679
104461 XDOT = -5454
804360
YDOT = 16668
024520 feet/sec YDOT = 5019
785047 meter/sec
ZDOT = 6621
386411 ZDOT = 1991
861313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5251993
29 X = 1600807
55
Y = 13988903
07 feet Y = 4263817
65 meter
Z = 16438907
40 Z = 5010578
98
XDOT = -23265
918111 XDOT = -7091
451840
YDOT = 1057
750835 feet/sec YDOT = 322
402454 meter/sec
ZDOT = 6506
211205 ZDOT = 1983
093175
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 16042
55167558
00016717 00000-0 10270-3 0 9068
2 25544 51
6423 329
5517 0006376 100
9978 259
1893 15
54594519 25283
Satellite: ISS
Catalog Number: 25544
Epoch time: 16042
55167558 = yrday
fracday
Element set: 906
Inclination: 51
6423 deg
RA of node: 329
5517 deg
Eccentricity:
0006376
Arg of perigee: 100
9978 deg
Mean anomaly: 259
1893 deg
Mean motion: 15
54594519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2528
Checksum: 345
Coasting Arc #8 (Orbit 2542)
---------------------------------------
Vector Time (GMT): 2016/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2418491
13 A = 6776032
95 meter
Y = -3477394
80 meter E =
0021206
Z = -5307334
86 I = 51
41102
XDOT = 6237
202101 Wp = 94
21737
YDOT = -4435
090060 meter/sec RA = 324
21193 deg
ZDOT = 62
363200 TA = 176
38760
MA = 176
37226
Ha = 222
610 n
mi
Hp = 211
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7934682
20 X = -2353645
91
Y = -11408775
58 feet Y = -3504077
90 meter
Z = -17412515
94 Z = -5318925
29
XDOT = 20463
261486 XDOT = 6286
029886
YDOT = -14550
820408 feet/sec YDOT = -4365
068511 meter/sec
ZDOT = 204
603676 ZDOT = 92
780560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1069171
95 X = 325883
61
Y = -13793046
80 feet Y = -4204120
67 meter
Z = -17462067
02 Z = -5322438
03
XDOT = 24056
492186 XDOT = 7332
418818
YDOT = 1432
262543 feet/sec YDOT = 436
553623 meter/sec
ZDOT = 337
323135 ZDOT = 102
816092
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 16043
51593010
00016717 00000-0 10270-3 0 9072
2 25544 51
6426 324
7408 0006441 103
4647 256
7224 15
54586211 25434
Satellite: ISS
Catalog Number: 25544
Epoch time: 16043
51593010 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 324
7408 deg
Eccentricity:
0006441
Arg of perigee: 103
4647 deg
Mean anomaly: 256
7224 deg
Mean motion: 15
54586211 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2543
Checksum: 290
Coasting Arc #9 (Orbit 2558)
---------------------------------------
Vector Time (GMT): 2016/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 749117
20 A = 6777483
94 meter
Y = 4567101
54 meter E =
0011555
Z = 4941859
14 I = 51
39030
XDOT = -6544
826800 Wp = 81
80347
YDOT = 3394
348059 meter/sec RA = 319
19154 deg
ZDOT = -2138
930468 TA = 29
11826
MA = 29
05387
Ha = 222
480 n
mi
Hp = 211
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2457733
60 X = 673985
91
Y = 14983928
92 feet Y = 4575059
00 meter
Z = 16213448
63 Z = 4945315
25
XDOT = -21472
528870 XDOT = -6571
906926
YDOT = 11136
312530 feet/sec YDOT = 3321
007868 meter/sec
ZDOT = -7017
488412 ZDOT = -2170
789308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7343642
29 X = -2238342
17
Y = 13273005
68 feet Y = 4045612
13 meter
Z = 16227530
15 Z = 4946151
19
XDOT = -22781
796972 XDOT = -6943
891717
YDOT = -3831
762238 feet/sec YDOT = -1167
921130 meter/sec
ZDOT = -7156
239596 ZDOT = -2181
221829
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 16044
54445317
00016717 00000-0 10270-3 0 9083
2 25544 51
6421 319
6100 0006364 106
9532 253
2319 15
54621345 25598
Satellite: ISS
Catalog Number: 25544
Epoch time: 16044
54445317 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 319
6100 deg
Eccentricity:
0006364
Arg of perigee: 106
9532 deg
Mean anomaly: 253
2319 deg
Mean motion: 15
54621345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2559
Checksum: 295
Coasting Arc #10 (Orbit 2573)
---------------------------------------
Vector Time (GMT): 2016/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 824900
19 A = 6781133
57 meter
Y = -5427875
43 meter E =
0013251
Z = -3994251
64 I = 51
37948
XDOT = 6273
313480 Wp = 108
57076
YDOT = -1940
496172 meter/sec RA = 314
17649 deg
ZDOT = 3939
189151 TA = 202
57966
MA = 202
63802
Ha = 222
488 n
mi
Hp = 211
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2706365
45 X = 904936
89
Y = -17807990
27 feet Y = -5418203
62 meter
Z = -13104500
12 Z = -3990049
74
XDOT = 20581
737140 XDOT = 6275
411647
YDOT = -6366
457258 feet/sec YDOT = -1870
331812 meter/sec
ZDOT = 12923
848920 ZDOT = 3969
668267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12923371
04 X = 3939043
49
Y = -12567425
50 feet Y = -3830551
29 meter
Z = -13085226
49 Z = -3988377
03
XDOT = 19298
235805 XDOT = 5882
102273
YDOT = 6273
228075 feet/sec YDOT = 1912
079917 meter/sec
ZDOT = 13056
327611 ZDOT = 3979
568656
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 16045
50868180
00016717 00000-0 10270-3 0 9098
2 25544 51
6426 314
7989 0006394 110
5832 249
6008 15
54631294 25746
Satellite: ISS
Catalog Number: 25544
Epoch time: 16045
50868180 = yrday
fracday
Element set: 909
Inclination: 51
6426 deg
RA of node: 314
7989 deg
Eccentricity:
0006394
Arg of perigee: 110
5832 deg
Mean anomaly: 249
6008 deg
Mean motion: 15
54631294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2574
Checksum: 328
Coasting Arc #11 (Orbit 2589)
---------------------------------------
Vector Time (GMT): 2016/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2222517
70 A = 6785265
71 meter
Y = 5891734
36 meter E =
0020083
Z = 2500980
16 I = 51
37134
XDOT = -5568
255892 Wp = 107
67127
YDOT = 153
437070 meter/sec RA = 309
17250 deg
ZDOT = -5280
704683 TA = 44
13188
MA = 43
97181
Ha = 222
486 n
mi
Hp = 211
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7291724
75 X = -2300383
91
Y = 19329837
15 feet Y = 5866445
46 meter
Z = 8205315
48 Z = 2489994
39
XDOT = -18268
556075 XDOT = -5543
906704
YDOT = 503
402462 feet/sec YDOT = 91
304993 meter/sec
ZDOT = -17325
146597 ZDOT = -5307
694454
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17285927
45 X = -5268750
69
Y = 11349289
01 feet Y = 3459263
29 meter
Z = 8156556
10 Z = 2486118
30
XDOT = -14172
841184 XDOT = -4319
881993
YDOT = -8982
161836 feet/sec YDOT = -2737
762928 meter/sec
ZDOT = -17442
150281 ZDOT = -5316
367406
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 16046
53717962
00016717 00000-0 10270-3 0 9105
2 25544 51
6424 309
6673 0006432 114
8552 245
3270 15
54625442 25906
Satellite: ISS
Catalog Number: 25544
Epoch time: 16046
53717962 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 309
6673 deg
Eccentricity:
0006432
Arg of perigee: 114
8552 deg
Mean anomaly: 245
3270 deg
Mean motion: 15
54625442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2590
Checksum: 305
Coasting Arc #12 (Orbit 2604)
---------------------------------------
Vector Time (GMT): 2016/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3287600
31 A = 6787530
18 meter
Y = -5889702
03 meter E =
0013307
Z = -736413
75 I = 51
36054
XDOT = 4515
225877 Wp = 67
26717
YDOT = 1790
194258 meter/sec RA = 304
17705 deg
ZDOT = 5930
713239 TA = 284
74577
MA = 284
89320
Ha = 222
332 n
mi
Hp = 211
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10786090
25 X = 3356793
21
Y = -19323169
39 feet Y = -5852551
06 meter
Z = -2416055
62 Z = -720275
30
XDOT = 14813
733191 XDOT = 4466
063432
YDOT = 5873
340741 feet/sec YDOT = 1840
411892 meter/sec
ZDOT = 19457
720602 ZDOT = 5952
527297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19918568
62 X = 6071179
72
Y = -9659900
20 feet Y = -2944337
58 meter
Z = -2344972
36 Z = -714747
57
XDOT = 7975
463208 XDOT = 2430
921186
YDOT = 11773
552010 feet/sec YDOT = 3588
578653 meter/sec
ZDOT = 19551
916596 ZDOT = 5959
424178
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 16047
50138261
00016717 00000-0 10270-3 0 9113
2 25544 51
6430 304
8564 0006263 118
1132 242
0655 15
54670884 26050
Satellite: ISS
Catalog Number: 25544
Epoch time: 16047
50138261 = yrday
fracday
Element set: 911
Inclination: 51
6430 deg
RA of node: 304
8564 deg
Eccentricity:
0006263
Arg of perigee: 118
1132 deg
Mean anomaly: 242
0655 deg
Mean motion: 15
54670884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2605
Checksum: 287
Coasting Arc #13 (Orbit 2619)
---------------------------------------
Vector Time (GMT): 2016/048/10:54:15
497
Vector Time (MET): N/A
Weight (LBS) : 922210
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1781057
61 A = 6779692
98 meter
Y = -4542997
41 meter E =
0015016
Z = -4721360
91 I = 51
31299
XDOT = 5240
833200 Wp = 114
47411
YDOT = -4876
099166 meter/sec RA = 299
37976 deg
ZDOT = 2715
606045 TA = 182
54859
MA = 182
55625
Ha = 222
275 n
mi
Hp = 213
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5843364
87 X = -1707190
36
Y = -14904847
14 feet Y = -4562501
56 meter
Z = -15490029
23 Z = -4729833
09
XDOT = 17194
334647 XDOT = 5281
778414
YDOT = -15997
700677 feet/sec YDOT = -4817
263641 meter/sec
ZDOT = 8909
468652 ZDOT = 2741
163934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7828765
38 X = 2386207
69
Y = -13924725
45 feet Y = -4244256
32 meter
Z = -15525876
48 Z = -4732287
15
XDOT = 22232
807140 XDOT = 6776
559616
YDOT = 2443
941908 feet/sec YDOT = 744
913494 meter/sec
ZDOT = 9021
173676 ZDOT = 2749
653736
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 16048
46557501
00016717 00000-0 10270-3 0 9122
2 25544 51
6429 300
0444 0004260 129
4194 230
7337 15
54186600 26207
Satellite: ISS
Catalog Number: 25544
Epoch time: 16048
46557501 = yrday
fracday
Element set: 912
Inclination: 51
6429 deg
RA of node: 300
0444 deg
Eccentricity:
0004260
Arg of perigee: 129
4194 deg
Mean anomaly: 230
7337 deg
Mean motion: 15
54186600 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2620
Checksum: 283
Coasting Arc #14 (Orbit 2635)
---------------------------------------
Vector Time (GMT): 2016/049/10:54:15
497
Vector Time (MET): N/A
Weight (LBS) : 922210
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 670284
82 A = 6783381
65 meter
Y = 5652864
00 meter E =
0015021
Z = 3674576
08 I = 51
31016
XDOT = -5342
205392 Wp = 97
08880
YDOT = 3440
010697 meter/sec RA = 294
36684 deg
ZDOT = -4304
203645 TA = 38
89817
MA = 38
79017
Ha = 222
198 n
mi
Hp = 213
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2199097
19 X = 589174
13
Y = 18546141
74 feet Y = 5659906
23 meter
Z = 12055695
79 Z = 3677634
82
XDOT = -17526
920576 XDOT = -5359
367854
YDOT = 11286
124333 feet/sec YDOT = 3380
174449 meter/sec
ZDOT = -14121
403034 ZDOT = -4330
196065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12709549
15 X = -3873870
58
Y = 13673655
66 feet Y = 4167730
24 meter
Z = 12067879
04 Z = 3678289
53
XDOT = -18914
565523 XDOT = -5765
159572
YDOT = -4979
319875 feet/sec YDOT = -1517
696698 meter/sec
ZDOT = -14234
711300 ZDOT = -4338
740004
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 16049
49436349
00016717 00000-0 10270-3 0 9133
2 25544 51
6425 294
9153 0004292 132
9131 227
2382 15
54198005 26366
Satellite: ISS
Catalog Number: 25544
Epoch time: 16049
49436349 = yrday
fracday
Element set: 913
Inclination: 51
6425 deg
RA of node: 294
9153 deg
Eccentricity:
0004292
Arg of perigee: 132
9131 deg
Mean anomaly: 227
2382 deg
Mean motion: 15
54198005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2636
Checksum: 313
Coasting Arc #15 (Orbit 2650)
---------------------------------------
Vector Time (GMT): 2016/050/10:54:15
497
Vector Time (MET): N/A
Weight (LBS) : 922210
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 326321
05 A = 6786842
70 meter
Y = -6391861
85 meter E =
0007080
Z = -2261786
17 I = 51
31039
XDOT = 5170
552478 Wp = 79
71808
YDOT = -1644
867398 meter/sec RA = 289
36289 deg
ZDOT = 5410
150635 TA = 255
01211
MA = 255
09050
Ha = 222
087 n
mi
Hp = 213
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1070607
10 X = 408758
71
Y = -20970675
38 feet Y = -6387751
91 meter
Z = -7420558
31 Z = -2260000
42
XDOT = 16963
754848 XDOT = 5162
281927
YDOT = -5396
546580 feet/sec YDOT = -1587
092778 meter/sec
ZDOT = 17749
838042 ZDOT = 5435
247317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16435568
02 X = 5009561
13
Y = -13073642
35 feet Y = -3984846
19 meter
Z = -7411618
61 Z = -2259061
35
XDOT = 14260
272512 XDOT = 4346
531062
YDOT = 7832
180609 feet/sec YDOT = 2387
248650 meter/sec
ZDOT = 17858
921650 ZDOT = 5443
399319
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 16050
45883980
00016717 00000-0 10270-3 0 9149
2 25544 51
6430 290
1062 0004185 137
2145 222
9334 15
54237740 26519
Satellite: ISS
Catalog Number: 25544
Epoch time: 16050
45883980 = yrday
fracday
Element set: 914
Inclination: 51
6430 deg
RA of node: 290
1062 deg
Eccentricity:
0004185
Arg of perigee: 137
2145 deg
Mean anomaly: 222
9334 deg
Mean motion: 15
54237740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2651
Checksum: 292
Coasting Arc #16 (Orbit 2666)
---------------------------------------
Vector Time (GMT): 2016/051/10:54:15
497
Vector Time (MET): N/A
Weight (LBS) : 922210
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1239774
91 A = 6788975
11 meter
Y = 6642523
06 meter E =
0017199
Z = 558360
97 I = 51
30716
XDOT = -4822
820916 Wp = 132
15959
YDOT = -390
683103 meter/sec RA = 284
36697 deg
ZDOT = -5954
127855 TA = 41
78390
MA = 41
65270
Ha = 222
071 n
mi
Hp = 213
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4067502
99 X = -1316673
32
Y = 21793054
67 feet Y = 6628229
15 meter
Z = 1831892
95 Z = 552151
34
XDOT = -15822
903269 XDOT = -4789
171877
YDOT = -1281
768709 feet/sec YDOT = -444
427384 meter/sec
ZDOT = -19534
540206 ZDOT = -5977
473582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18815665
97 X = -5735014
99
Y = 11728378
04 feet Y = 3574809
63 meter
Z = 1803747
93 Z = 549782
37
XDOT = -8811
542614 XDOT = -2685
758189
YDOT = -11061
751657 feet/sec YDOT = -3371
621905 meter/sec
ZDOT = -19635
655546 ZDOT = -5984
947810
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 16051
48760380
00016717 00000-0 10270-3 0 9152
2 25544 51
6427 284
9767 0004253 142
2297 217
9154 15
54207758 26675
Satellite: ISS
Catalog Number: 25544
Epoch time: 16051
48760380 = yrday
fracday
Element set: 915
Inclination: 51
6427 deg
RA of node: 284
9767 deg
Eccentricity:
0004253
Arg of perigee: 142
2297 deg
Mean anomaly: 217
9154 deg
Mean motion: 15
54207758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2667
Checksum: 331
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