[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 31st 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1877 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 102 5 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
090/14:15:23
000 0
0 0
0 0
0
N/A 0
0 0
0 221
1
000/00:00:00
000 0
0 0
0 214
2
091/16:23:58
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 214
1
093/17:58:46
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 214
0
094/18:43:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 213
9
098/16:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 213
8
104/12:19:00
253 2
9 3
0 3
0
N/A 0
4 0
0 221
3
000/00:08:00
506 -0
8 -0
0 215
0
Coasting Arc #1 (Orbit 3273)
---------------------------------------
Vector Time (GMT): 2016/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919477
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4148773
79 A = 6777064
24 meter
Y = -785399
96 meter E =
0015515
Z = -5314215
36 I = 51
98931
XDOT = 573
714437 Wp = 76
25605
YDOT = 7606
022635 meter/sec RA = 89
64825 deg
ZDOT = -674
280976 TA = 187
31574
MA = 187
33841
Ha = 221
115 n
mi
Hp = 214
341
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13611462
58 X = 4183062
27
Y = -2576771
52 feet Y = -738814
36 meter
Z = -17435089
76 Z = -5293978
22
XDOT = 1882
265212 XDOT = 491
894741
YDOT = 24954
142503 feet/sec YDOT = 7611
980751 meter/sec
ZDOT = -2212
207925 ZDOT = -671
693396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13272539
92 X = 4045470
17
Y = -4337701
66 feet Y = -1322131
47 meter
Z = -17346989
60 Z = -5287362
43
XDOT = 4802
938357 XDOT = 1463
935611
YDOT = 23528
868657 feet/sec YDOT = 7171
599167 meter/sec
ZDOT = -2202
302820 ZDOT = -671
261900
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 16090
51724109
00016717 00000-0 10270-3 0 9002
2 25544 51
6404 90
4075 0002409 11
7783 348
3425 15
54280944 32746
Satellite: ISS
Catalog Number: 25544
Epoch time: 16090
51724109 = yrday
fracday
Element set: 900
Inclination: 51
6404 deg
RA of node: 90
4075 deg
Eccentricity:
0002409
Arg of perigee: 11
7783 deg
Mean anomaly: 348
3425 deg
Mean motion: 15
54280944 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3274
Checksum: 292
Coasting Arc #2 (Orbit 3275)
---------------------------------------
Vector Time (GMT): 2016/090/14:15:23
000
Vector Time (MET): N/A
Weight (LBS) : 907109
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3886515
91 A = 6778184
03 meter
Y = 2374632
14 meter E =
0005357
Z = 5015660
23 I = 51
99341
XDOT = -1717
723129 Wp = 98
98790
YDOT = -7185
625443 meter/sec RA = 89
19259 deg
ZDOT = 2068
274169 TA = 330
99014
MA = 331
01990
Ha = 221
128 n
mi
Hp = 214
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12751036
45 X = -3937144
80
Y = 7790787
86 feet Y = 2330887
89 meter
Z = 16455578
17 Z = 4996657
25
XDOT = -5635
574570 XDOT = -1647
290840
YDOT = -23574
886624 feet/sec YDOT = -7204
440175 meter/sec
ZDOT = 6785
676406 ZDOT = 2060
101561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4491712
60 X = -1369074
00
Y = 14346954
98 feet Y = 4372951
88 meter
Z = 16372561
18 Z = 4990356
65
XDOT = -18802
753575 XDOT = -5731
079290
YDOT = -13601
488441 feet/sec YDOT = -4145
733677 meter/sec
ZDOT = 6751
422743 ZDOT = 2057
833652
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 16090
64583088
00016717 00000-0 10270-3 0 9016
2 25544 51
6403 89
7664 0002498 5
7535 354
3646 15
54322163 32760
Satellite: ISS
Catalog Number: 25544
Epoch time: 16090
64583088 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 89
7664 deg
Eccentricity:
0002498
Arg of perigee: 5
7535 deg
Mean anomaly: 354
3646 deg
Mean motion: 15
54322163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3276
Checksum: 320
Coasting Arc #3 (Orbit 3290)
---------------------------------------
Vector Time (GMT): 2016/091/14:15:23
000
Vector Time (MET): N/A
Weight (LBS) : 907109
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4147804
32 A = 6776863
48 meter
Y = -523326
05 meter E =
0015615
Z = -5346910
63 I = 51
98694
XDOT = 841
456611 Wp = 80
04159
YDOT = 7610
563309 meter/sec RA = 84
21558 deg
ZDOT = -89
727436 TA = 189
09209
MA = 189
12039
Ha = 221
120 n
mi
Hp = 214
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13608281
89 X = 4179321
04
Y = -1716948
99 feet Y = -476766
78 meter
Z = -17542357
72 Z = -5326685
02
XDOT = 2760
684420 XDOT = 756
726718
YDOT = 24969
039728 feet/sec YDOT = 7619
499276 meter/sec
ZDOT = -294
381353 ZDOT = -85
846287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8976742
40 X = 2736111
08
Y = -10518144
76 feet Y = -3205930
52 meter
Z = -17454348
77 Z = -5320085
51
XDOT = 18104
381314 XDOT = 5518
215424
YDOT = 15927
153496 feet/sec YDOT = 4854
596386 meter/sec
ZDOT = -278
869519 ZDOT = -84
999430
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 16091
61025407
00016717 00000-0 10270-3 0 9021
2 25544 51
6399 84
9573 0002566 11
5004 348
6207 15
54299278 32918
Satellite: ISS
Catalog Number: 25544
Epoch time: 16091
61025407 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 84
9573 deg
Eccentricity:
0002566
Arg of perigee: 11
5004 deg
Mean anomaly: 348
6207 deg
Mean motion: 15
54299278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3291
Checksum: 313
Coasting Arc #4 (Orbit 3292)
---------------------------------------
Vector Time (GMT): 2016/091/16:23:58
000
Vector Time (MET): N/A
Weight (LBS) : 907109
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2653679
47 A = 6781942
41 meter
Y = 4753358
12 meter E =
0011142
Z = 4034711
82 I = 52
00522
XDOT = -3700
307248 Wp = 88
29736
YDOT = -5433
036433 meter/sec RA = 83
79802 deg
ZDOT = 3957
937534 TA = 320
77722
MA = 320
85791
Ha = 221
192 n
mi
Hp = 214
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8706297
47 X = -2726234
39
Y = 15595006
95 feet Y = 4723277
57 meter
Z = 13237243
50 Z = 4021644
26
XDOT = -12140
115644 XDOT = -3658
504650
YDOT = -17824
922681 feet/sec YDOT = -5474
181662 meter/sec
ZDOT = 12985
359365 ZDOT = 3940
064340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12705080
99 X = 3872508
69
Y = 12613791
03 feet Y = 3844683
51 meter
Z = 13179592
78 Z = 4017139
88
XDOT = -19508
064792 XDOT = -5946
058149
YDOT = 6130
350474 feet/sec YDOT = 1868
530824 meter/sec
ZDOT = 12908
639520 ZDOT = 3934
553326
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 16091
73884347
00016717 00000-0 10270-3 0 9031
2 25544 51
6413 84
3171 0002541 12
4840 347
6376 15
54312039 32933
Satellite: ISS
Catalog Number: 25544
Epoch time: 16091
73884347 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 84
3171 deg
Eccentricity:
0002541
Arg of perigee: 12
4840 deg
Mean anomaly: 347
6376 deg
Mean motion: 15
54312039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3293
Checksum: 298
Coasting Arc #5 (Orbit 3307)
---------------------------------------
Vector Time (GMT): 2016/092/16:23:58
000
Vector Time (MET): N/A
Weight (LBS) : 907109
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3326107
89 A = 6778363
63 meter
Y = -3209768
17 meter E =
0013883
Z = -4970713
26 I = 51
98997
XDOT = 3085
618280 Wp = 64
52891
YDOT = 6645
830470 meter/sec RA = 78
82886 deg
ZDOT = -2225
769804 TA = 183
81831
MA = 183
82892
Ha = 221
113 n
mi
Hp = 214
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10912427
46 X = 3385898
68
Y = -10530735
48 feet Y = -3172239
56 meter
Z = -16308114
37 Z = -4954410
37
XDOT = 10123
419554 XDOT = 3021
885442
YDOT = 21803
905740 feet/sec YDOT = 6679
979355 meter/sec
ZDOT = -7302
394370 ZDOT = -2210
936048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7461748
83 X = -2274341
04
Y = -13290031
95 feet Y = -4050801
74 meter
Z = -16236668
76 Z = -4948936
64
XDOT = 22678
267025 XDOT = 6912
335789
YDOT = -3884
766777 feet/sec YDOT = -1184
076914 meter/sec
ZDOT = -7239
111666 ZDOT = -2206
481236
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 16092
70325827
00016717 00000-0 10270-3 0 9043
2 25544 51
6422 79
5083 0002610 15
3326 344
7906 15
54337099 33086
Satellite: ISS
Catalog Number: 25544
Epoch time: 16092
70325827 = yrday
fracday
Element set: 904
Inclination: 51
6422 deg
RA of node: 79
5083 deg
Eccentricity:
0002610
Arg of perigee: 15
3326 deg
Mean anomaly: 344
7906 deg
Mean motion: 15
54337099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3308
Checksum: 303
Coasting Arc #6 (Orbit 3323)
---------------------------------------
Vector Time (GMT): 2016/093/16:23:58
000
Vector Time (MET): N/A
Weight (LBS) : 907109
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3926786
80 A = 6776653
20 meter
Y = 1429033
08 meter E =
0003713
Z = 5332148
77 I = 51
97751
XDOT = -2320
665849 Wp = 57
27786
YDOT = -7308
125936 meter/sec RA = 73
85203 deg
ZDOT = 251
407263 TA = 30
34877
MA = 30
32728
Ha = 221
202 n
mi
Hp = 213
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12883158
80 X = -3968375
99
Y = 4688428
74 feet Y = 1384889
13 meter
Z = 17493926
41 Z = 5312972
31
XDOT = -7613
733101 XDOT = -2239
993315
YDOT = -23976
791128 feet/sec YDOT = -7333
626072 meter/sec
ZDOT = 824
826978 ZDOT = 240
330744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1547494
11 X = 471676
21
Y = 13728840
78 feet Y = 4184550
67 meter
Z = 17410307
26 Z = 5306661
65
XDOT = -24088
939535 XDOT = -7342
308770
YDOT = 1736
279030 feet/sec YDOT = 529
217848 meter/sec
ZDOT = 778
005350 ZDOT = 237
136031
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 16093
73195699
00016717 00000-0 10270-3 0 9050
2 25544 51
6422 74
3791 0002570 15
6974 344
4258 15
54372040 33242
Satellite: ISS
Catalog Number: 25544
Epoch time: 16093
73195699 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 74
3791 deg
Eccentricity:
0002570
Arg of perigee: 15
6974 deg
Mean anomaly: 344
4258 deg
Mean motion: 15
54372040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3324
Checksum: 316
Coasting Arc #7 (Orbit 3324)
---------------------------------------
Vector Time (GMT): 2016/093/17:58:46
000
Vector Time (MET): N/A
Weight (LBS) : 922235
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4187418
16 A = 6776774
97 meter
Y = 467599
06 meter E =
0005065
Z = 5305163
04 I = 51
97875
XDOT = -1670
791154 Wp = 41
42761
YDOT = -7458
509561 meter/sec RA = 73
51800 deg
ZDOT = -657
320388 TA = 54
84020
MA = 54
79276
Ha = 221
189 n
mi
Hp = 213
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13738248
57 X = -4218105
90
Y = 1534117
65 feet Y = 420601
51 meter
Z = 17405390
56 Z = 5284747
08
XDOT = -5481
598273 XDOT = -1584
071094
YDOT = -24470
175724 feet/sec YDOT = -7476
708644 meter/sec
ZDOT = -2156
562953 ZDOT = -665
225275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3999354
37 X = 1219003
21
Y = 13348505
49 feet Y = 4068624
47 meter
Z = 17316557
89 Z = 5278086
84
XDOT = -22116
214218 XDOT = -6741
022094
YDOT = 9484
057825 feet/sec YDOT = 2890
740825 meter/sec
ZDOT = -2189
569630 ZDOT = -667
380823
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 16093
79624995
00016717 00000-0 10270-3 0 9063
2 25544 51
6436 74
0588 0002559 15
2130 344
9099 15
54374941 33256
Satellite: ISS
Catalog Number: 25544
Epoch time: 16093
79624995 = yrday
fracday
Element set: 906
Inclination: 51
6436 deg
RA of node: 74
0588 deg
Eccentricity:
0002559
Arg of perigee: 15
2130 deg
Mean anomaly: 344
9099 deg
Mean motion: 15
54374941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3325
Checksum: 333
Coasting Arc #8 (Orbit 3339)
---------------------------------------
Vector Time (GMT): 2016/094/17:58:46
000
Vector Time (MET): N/A
Weight (LBS) : 922235
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4580166
50 A = 6778927
04 meter
Y = 1335283
81 meter E =
0011724
Z = -4826394
14 I = 51
97497
XDOT = 639
362843 Wp = 95
22298
YDOT = 7177
611360 meter/sec RA = 68
54130 deg
ZDOT = 2596
897180 TA = 200
24593
MA = 200
29246
Ha = 221
175 n
mi
Hp = 214
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15026792
99 X = 4588339
12
Y = 4380852
38 feet Y = 1386547
41 meter
Z = -15834626
45 Z = -4804125
19
XDOT = 2097
647122 XDOT = 546
438903
YDOT = 23548
593700 feet/sec YDOT = 7184
241871 meter/sec
ZDOT = 8520
003870 ZDOT = 2599
776510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1319999
36 X = 402335
80
Y = -15694029
94 feet Y = -4783540
33 meter
Z = -15738068
36 Z = -4796963
24
XDOT = 21543
824047 XDOT = 6566
557569
YDOT = -6728
649330 feet/sec YDOT = -2050
892316 meter/sec
ZDOT = 8531
206724 ZDOT = 2600
311809
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 16094
76064955
00016717 00000-0 10270-3 0 9076
2 25544 51
6429 69
2500 0002629 19
5665 340
5588 15
54355952 33409
Satellite: ISS
Catalog Number: 25544
Epoch time: 16094
76064955 = yrday
fracday
Element set: 907
Inclination: 51
6429 deg
RA of node: 69
2500 deg
Eccentricity:
0002629
Arg of perigee: 19
5665 deg
Mean anomaly: 340
5588 deg
Mean motion: 15
54355952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3340
Checksum: 329
Coasting Arc #9 (Orbit 3340)
---------------------------------------
Vector Time (GMT): 2016/094/18:43:00
000
Vector Time (MET): N/A
Weight (LBS) : 922235
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4453521
09 A = 6777711
29 meter
Y = -439587
98 meter E =
0007725
Z = 5087173
68 I = 51
97064
XDOT = -1367
525371 Wp = 43
41332
YDOT = -7325
060163 meter/sec RA = 68
39384 deg
ZDOT = -1823
050792 TA = 64
18590
MA = 64
10622
Ha = 221
212 n
mi
Hp = 213
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14611289
67 X = -4472985
77
Y = -1442217
78 feet Y = -489498
46 meter
Z = 16690202
37 Z = 5065492
41
XDOT = -4486
631794 XDOT = -1276
657508
YDOT = -24032
349617 feet/sec YDOT = -7339
844880 meter/sec
ZDOT = -5981
137768 ZDOT = -1829
472320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4283087
30 X = 1305485
01
Y = 14154837
22 feet Y = 4314394
38 meter
Z = 16596035
05 Z = 5058471
48
XDOT = -19486
291162 XDOT = -5939
421546
YDOT = 12967
625688 feet/sec YDOT = 3952
532310 meter/sec
ZDOT = -6007
711198 ZDOT = -1831
150373
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 16094
82494106
00016717 00000-0 10270-3 0 9089
2 25544 51
6426 68
9292 0002610 17
9822 342
1423 15
54385630 33410
Satellite: ISS
Catalog Number: 25544
Epoch time: 16094
82494106 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 68
9292 deg
Eccentricity:
0002610
Arg of perigee: 17
9822 deg
Mean anomaly: 342
1423 deg
Mean motion: 15
54385630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3341
Checksum: 303
Coasting Arc #10 (Orbit 3355)
---------------------------------------
Vector Time (GMT): 2016/095/18:43:00
000
Vector Time (MET): N/A
Weight (LBS) : 922235
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4812617
74 A = 6780981
87 meter
Y = 2137910
31 meter E =
0008604
Z = -4279610
90 I = 51
96844
XDOT = 213
160930 Wp = 92
41999
YDOT = 6750
209205 meter/sec RA = 63
42033 deg
ZDOT = 3617
732067 TA = 214
38503
MA = 214
44074
Ha = 221
175 n
mi
Hp = 214
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15789428
27 X = 4809141
92
Y = 7014141
42 feet Y = 2191708
20 meter
Z = -14040718
19 Z = -4256241
14
XDOT = 699
346884 XDOT = 120
089181
YDOT = 22146
355658 feet/sec YDOT = 6752
072990 meter/sec
ZDOT = 11869
199695 ZDOT = 3618
540606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 126163
77 X = 38454
72
Y = -17358561
85 feet Y = -5290889
65 meter
Z = -13939526
72 Z = -4248767
74
XDOT = 18810
777935 XDOT = 5733
525115
YDOT = -9380
806585 feet/sec YDOT = -2859
269847 meter/sec
ZDOT = 11871
470477 ZDOT = 3618
424201
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 16095
78933340
00016717 00000-0 10270-3 0 9094
2 25544 51
6424 64
1200 0002586 21
0466 339
0793 15
54369011 33563
Satellite: ISS
Catalog Number: 25544
Epoch time: 16095
78933340 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 64
1200 deg
Eccentricity:
0002586
Arg of perigee: 21
0466 deg
Mean anomaly: 339
0793 deg
Mean motion: 15
54369011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3356
Checksum: 301
Coasting Arc #11 (Orbit 3371)
---------------------------------------
Vector Time (GMT): 2016/096/18:43:00
000
Vector Time (MET): N/A
Weight (LBS) : 922235
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4924329
69 A = 6784892
60 meter
Y = -3603616
44 meter E =
0014194
Z = 2955131
49 I = 51
96765
XDOT = 1127
361340 Wp = 87
13150
YDOT = -5681
515560 meter/sec RA = 58
45629 deg
ZDOT = -5028
235863 TA = 59
27055
MA = 59
13081
Ha = 221
187 n
mi
Hp = 213
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16155937
30 X = -4898021
98
Y = -11822888
58 feet Y = -3658536
06 meter
Z = 9695313
28 Z = 2931274
65
XDOT = 3698
692059 XDOT = 1215
234774
YDOT = -18640
142912 feet/sec YDOT = -5668
418034 meter/sec
ZDOT = -16496
836822 ZDOT = -5022
545169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4067411
16 X = -1239746
92
Y = 19652947
97 feet Y = 5990218
54 meter
Z = 9592283
71 Z = 2923728
07
XDOT = -17115
446953 XDOT = -5216
788231
YDOT = 4531
731527 feet/sec YDOT = 1381
271769 meter/sec
ZDOT = -16471
046317 ZDOT = -5020
374917
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 16096
81800766
00016717 00000-0 10270-3 0 9106
2 25544 51
6433 58
9897 0002740 22
8854 337
2421 15
54408209 33727
Satellite: ISS
Catalog Number: 25544
Epoch time: 16096
81800766 = yrday
fracday
Element set: 910
Inclination: 51
6433 deg
RA of node: 58
9897 deg
Eccentricity:
0002740
Arg of perigee: 22
8854 deg
Mean anomaly: 337
2421 deg
Mean motion: 15
54408209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3372
Checksum: 317
Coasting Arc #12 (Orbit 3386)
---------------------------------------
Vector Time (GMT): 2016/097/18:43:00
000
Vector Time (MET): N/A
Weight (LBS) : 922235
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4742388
20 A = 6787908
10 meter
Y = 4664404
00 meter E =
0011555
Z = -1326400
97 I = 51
95842
XDOT = -2552
013984 Wp = 34
94875
YDOT = 4248
985486 meter/sec RA = 53
50123 deg
ZDOT = 5851
847286 TA = 310
67418
MA = 310
77455
Ha = 221
274 n
mi
Hp = 213
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15559016
39 X = 4696320
35
Y = 15303162
74 feet Y = 4717178
77 meter
Z = -4351709
23 Z = -1303475
99
XDOT = -8372
749290 XDOT = -2627
763528
YDOT = 13940
241097 feet/sec YDOT = 4220
024450 meter/sec
ZDOT = 19198
974035 ZDOT = 5839
265551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7144089
22 X = 2177518
39
Y = -20641745
22 feet Y = -6291603
94 meter
Z = -4252939
88 Z = -1296296
08
XDOT = 14732
772653 XDOT = 4490
549105
YDOT = 1178
506924 feet/sec YDOT = 359
208910 meter/sec
ZDOT = 19143
491977 ZDOT = 5834
936355
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 16097
78238302
00016717 00000-0 10270-3 0 9115
2 25544 51
6419 54
1800 0002694 26
8792 333
2500 15
54371123 33870
Satellite: ISS
Catalog Number: 25544
Epoch time: 16097
78238302 = yrday
fracday
Element set: 911
Inclination: 51
6419 deg
RA of node: 54
1800 deg
Eccentricity:
0002694
Arg of perigee: 26
8792 deg
Mean anomaly: 333
2500 deg
Mean motion: 15
54371123 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3387
Checksum: 299
Coasting Arc #13 (Orbit 3400)
---------------------------------------
Vector Time (GMT): 2016/098/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922235
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3270082
45 A = 6776536
02 meter
Y = -2618969
01 meter E =
0016390
Z = -5340234
87 I = 51
90535
XDOT = 4925
577918 Wp = 83
16599
YDOT = 5860
722208 meter/sec RA = 49
10883 deg
ZDOT = 144
217088 TA = 188
19196
MA = 188
21875
Ha = 221
209 n
mi
Hp = 213
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10728616
98 X = 3325066
27
Y = -8592418
02 feet Y = -2582094
04 meter
Z = -17520455
62 Z = -5324215
54
XDOT = 16160
032541 XDOT = 4858
975229
YDOT = 19228
091232 feet/sec YDOT = 5915
430918 meter/sec
ZDOT = 473
153177 ZDOT = 167
982073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5607355
94 X = -1709122
09
Y = -12646839
69 feet Y = -3854756
74 meter
Z = -17450336
39 Z = -5318862
53
XDOT = 21737
480261 XDOT = 6625
583983
YDOT = -10421
474323 feet/sec YDOT = -3176
465374 meter/sec
ZDOT = 575
334671 ZDOT = 175
362008
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 16098
68246115
00016717 00000-0 10270-3 0 9127
2 25544 51
6439 49
6929 0002633 32
7569 327
3746 15
54414083 34010
Satellite: ISS
Catalog Number: 25544
Epoch time: 16098
68246115 = yrday
fracday
Element set: 912
Inclination: 51
6439 deg
RA of node: 49
6929 deg
Eccentricity:
0002633
Arg of perigee: 32
7569 deg
Mean anomaly: 327
3746 deg
Mean motion: 15
54414083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3401
Checksum: 321
Coasting Arc #14 (Orbit 3416)
---------------------------------------
Vector Time (GMT): 2016/099/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922235
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4460644
13 A = 6777960
49 meter
Y = 1111806
92 meter E =
0008769
Z = 4976752
31 I = 51
88981
XDOT = -3963
847582 Wp = 50
09553
YDOT = -6203
688096 meter/sec RA = 44
12513 deg
ZDOT = -2158
878000 TA = 60
90363
MA = 60
81585
Ha = 221
252 n
mi
Hp = 213
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14634659
21 X = -4496920
39
Y = 3647660
49 feet Y = 1061722
74 meter
Z = 16327927
53 Z = 4954995
06
XDOT = -13004
749285 XDOT = -3883
694734
YDOT = -20353
307401 feet/sec YDOT = -6247
566551 meter/sec
ZDOT = -7082
933070 ZDOT = -2177
938305
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 105443
97 X = 32139
32
Y = 15183984
94 feet Y = 4628078
61 meter
Z = 16233156
74 Z = 4947866
17
XDOT = -21710
580173 XDOT = -6617
384837
YDOT = 7838
626078 feet/sec YDOT = 2389
213229 meter/sec
ZDOT = -7164
584901 ZDOT = -2183
765478
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 16099
71110994
00016717 00000-0 10270-3 0 9138
2 25544 51
6448 44
5635 0002577 32
8251 327
3062 15
54461141 34179
Satellite: ISS
Catalog Number: 25544
Epoch time: 16099
71110994 = yrday
fracday
Element set: 913
Inclination: 51
6448 deg
RA of node: 44
5635 deg
Eccentricity:
0002577
Arg of perigee: 32
8251 deg
Mean anomaly: 327
3062 deg
Mean motion: 15
54461141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3417
Checksum: 301
Coasting Arc #15 (Orbit 3431)
---------------------------------------
Vector Time (GMT): 2016/100/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922235
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5426717
46 A = 6781575
46 meter
Y = 306820
76 meter E =
0008301
Z = -4062577
14 I = 51
87768
XDOT = 2581
359039 Wp = 90
08114
YDOT = 6060
515811 meter/sec RA = 39
14726 deg
ZDOT = 3912
730352 TA = 220
36553
MA = 220
42717
Ha = 221
270 n
mi
Hp = 213
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17804191
15 X = 5442617
74
Y = 1006629
79 feet Y = 367594
48 meter
Z = -13328665
16 Z = -4036176
51
XDOT = 8469
025719 XDOT = 2494
390336
YDOT = 19883
582056 feet/sec YDOT = 6088
896345 meter/sec
ZDOT = 12837
041838 ZDOT = 3925
058386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4860230
98 X = 1481398
40
Y = -17245998
59 feet Y = -5256580
37 meter
Z = -13213989
86 Z = -4027624
11
XDOT = 19972
413120 XDOT = 6087
591519
YDOT = -4229
932612 feet/sec YDOT = -1289
283460 meter/sec
ZDOT = 12889
447330 ZDOT = 3928
703546
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 16100
67546059
00016717 00000-0 10270-3 0 9142
2 25544 51
6446 39
7544 0002645 36
9827 323
1508 15
54430946 34327
Satellite: ISS
Catalog Number: 25544
Epoch time: 16100
67546059 = yrday
fracday
Element set: 914
Inclination: 51
6446 deg
RA of node: 39
7544 deg
Eccentricity:
0002645
Arg of perigee: 36
9827 deg
Mean anomaly: 323
1508 deg
Mean motion: 15
54430946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3432
Checksum: 313
Coasting Arc #16 (Orbit 3447)
---------------------------------------
Vector Time (GMT): 2016/101/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 943973
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6037480
04 A = 6785529
34 meter
Y = -1593317
11 meter E =
0015172
Z = 2641314
78 I = 51
86501
XDOT = -840
023460 Wp = 93
71752
YDOT = -5540
969442 meter/sec RA = 34
17953 deg
ZDOT = -5237
669172 TA = 56
59287
MA = 56
44783
Ha = 221
343 n
mi
Hp = 213
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19808005
37 X = -6032044
99
Y = -5227418
33 feet Y = -1660801
67 meter
Z = 8665730
90 Z = 2611999
12
XDOT = -2755
982481 XDOT = -752
557843
YDOT = -18179
033602 feet/sec YDOT = -5549
874425 meter/sec
ZDOT = -17183
953977 ZDOT = -5241
537054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9093526
38 X = -2771706
84
Y = 18416765
21 feet Y = 5613430
04 meter
Z = 8538642
07 Z = 2602578
10
XDOT = -16999
385542 XDOT = -5181
412713
YDOT = -380
850077 feet/sec YDOT = -116
083104 meter/sec
ZDOT = -17199
681764 ZDOT = -5242
463002
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 16101
70409129
00016717 00000-0 10270-3 0 9154
2 25544 51
6440 34
6251 0002740 43
1869 316
9498 15
54448324 34486
Satellite: ISS
Catalog Number: 25544
Epoch time: 16101
70409129 = yrday
fracday
Element set: 915
Inclination: 51
6440 deg
RA of node: 34
6251 deg
Eccentricity:
0002740
Arg of perigee: 43
1869 deg
Mean anomaly: 316
9498 deg
Mean motion: 15
54448324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3448
Checksum: 304
Coasting Arc #17 (Orbit 3462)
---------------------------------------
Vector Time (GMT): 2016/102/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 943973
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6188421
53 A = 6787984
37 meter
Y = 2609635
47 meter E =
0012580
Z = -946128
69 I = 51
84652
XDOT = -1095
427153 Wp = 39
62614
YDOT = 4730
676339 meter/sec RA = 29
21900 deg
ZDOT = 5936
135471 TA = 310
15580
MA = 310
26591
Ha = 221
251 n
mi
Hp = 213
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20303220
26 X = 6163375
94
Y = 8561796
16 feet Y = 2678698
43 meter
Z = -3104096
75 Z = -916127
54
XDOT = -3593
921106 XDOT = -1177
080827
YDOT = 15520
591665 feet/sec YDOT = 4717
970289 meter/sec
ZDOT = 19475
510077 ZDOT = 5930
615541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12138011
30 X = 3699665
84
Y = -18411494
72 feet Y = -5611823
59 meter
Z = -2974233
80 Z = -906546
46
XDOT = 13236
335406 XDOT = 4034
435032
YDOT = 5613
345382 feet/sec YDOT = 1710
947672 meter/sec
ZDOT = 19450
591612 ZDOT = 5928
540323
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 16102
66842199
00016717 00000-0 10270-3 0 9169
2 25544 51
6441 29
8158 0002584 43
7704 316
3654 15
54470397 34639
Satellite: ISS
Catalog Number: 25544
Epoch time: 16102
66842199 = yrday
fracday
Element set: 916
Inclination: 51
6441 deg
RA of node: 29
8158 deg
Eccentricity:
0002584
Arg of perigee: 43
7704 deg
Mean anomaly: 316
3654 deg
Mean motion: 15
54470397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3463
Checksum: 322
Coasting Arc #18 (Orbit 3478)
---------------------------------------
Vector Time (GMT): 2016/103/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 943973
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5802323
31 A = 6788008
61 meter
Y = -3397793
94 meter E =
0010057
Z = -907456
35 I = 51
81796
XDOT = 3102
179798 Wp = 126
43842
YDOT = -3725
054636 meter/sec RA = 24
26044 deg
ZDOT = -5939
261215 TA = 63
35805
MA = 63
25507
Ha = 221
217 n
mi
Hp = 213
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19036493
81 X = -5759489
03
Y = -11147617
91 feet Y = -3462439
92 meter
Z = -2977219
00 Z = -935538
58
XDOT = 10177
755244 XDOT = 3172
454299
YDOT = -12221
307862 feet/sec YDOT = -3689
971348 meter/sec
ZDOT = -19485
765140 ZDOT = -5924
020636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14152941
10 X = -4313816
45
Y = 16900129
12 feet Y = 5151159
36 meter
Z = -3098581
68 Z = -944447
69
XDOT = -9108
736166 XDOT = -2776
342783
YDOT = -11158
675328 feet/sec YDOT = -3401
164240 meter/sec
ZDOT = -19418
798572 ZDOT = -5918
849805
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 16103
69702970
00016717 00000-0 10270-3 0 9176
2 25544 51
6439 24
6853 0002480 47
7305 312
4058 15
54451391 34792
Satellite: ISS
Catalog Number: 25544
Epoch time: 16103
69702970 = yrday
fracday
Element set: 917
Inclination: 51
6439 deg
RA of node: 24
6853 deg
Eccentricity:
0002480
Arg of perigee: 47
7305 deg
Mean anomaly: 312
4058 deg
Mean motion: 15
54451391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3479
Checksum: 312
Coasting Arc #19 (Orbit 3491)
---------------------------------------
Vector Time (GMT): 2016/104/12:23:00
506
Vector Time (MET): N/A
Weight (LBS) : 943644
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 954974
39 A = 6777970
80 meter
Y = -4111675
21 meter E =
0014764
Z = -5315886
69 I = 51
75414
XDOT = 7295
997808 Wp = 83
09240
YDOT = 2280
115436 meter/sec RA = 20
02780 deg
ZDOT = -452
253626 TA = 182
59090
MA = 182
59856
Ha = 221
287 n
mi
Hp = 215
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3133118
07 X = 1026703
59
Y = -13489748
08 feet Y = -4100595
26 meter
Z = -17440573
14 Z = -5311073
22
XDOT = 23937
000683 XDOT = 7272
155598
YDOT = 7480
693687 feet/sec YDOT = 2361
570802 meter/sec
ZDOT = -1483
771740 ZDOT = -416
869370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3239077
80 X = -987270
91
Y = -13492801
63 feet Y = -4112605
94 meter
Z = -17418840
45 Z = -5309262
57
XDOT = 23746
516936 XDOT = 7237
938362
YDOT = -3980
221134 feet/sec YDOT = -1213
171402 meter/sec
ZDOT = -1330
460975 ZDOT = -405
524505
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 16104
53276780
00016717 00000-0 10270-3 0 9186
2 25544 51
6438 20
5171 0000856 353
3794 6
7347 15
53936289 34924
Satellite: ISS
Catalog Number: 25544
Epoch time: 16104
53276780 = yrday
fracday
Element set: 918
Inclination: 51
6438 deg
RA of node: 20
5171 deg
Eccentricity:
0000856
Arg of perigee: 353
3794 deg
Mean anomaly: 6
7347 deg
Mean motion: 15
53936289 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3492
Checksum: 324
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