[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 8th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 91 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 ET - UTC (sec) : 68 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
254/00:50:36
690 3
7 3
8 3
8
N/A -0
2 -0
4 220
8
000/00:11:13
381 0
9 0
1 217
3
257/20:34:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 216
6
265/22:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 215
0
Coasting Arc #1 (Orbit 1778)
---------------------------------------
Vector Time (GMT): 2016/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893996
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4301446
43 A = 6780590
23 meter
Y = 2941208
59 meter E =
0008117
Z = 4335533
59 I = 51
68474
XDOT = -5888
907528 Wp = 56
07249
YDOT = -3466
599492 meter/sec RA = 6
74228 deg
ZDOT = -3481
776390 TA = 69
32388
MA = 69
23688
Ha = 219
818 n
mi
Hp = 215
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14112357
07 X = -4355076
28
Y = 9649634
49 feet Y = 2892807
48 meter
Z = 14224191
57 Z = 4314507
66
XDOT = -19320
562755 XDOT = -5832
792448
YDOT = -11373
357913 feet/sec YDOT = -3532
139765 meter/sec
ZDOT = -11423
150886 ZDOT = -3510
246669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16102250
79 X = 4907966
04
Y = -5967640
58 feet Y = -1818936
85 meter
Z = 14131754
29 Z = 4307358
71
XDOT = 15526
317547 XDOT = 4732
421588
YDOT = 14479
127792 feet/sec YDOT = 4413
238151 meter/sec
ZDOT = -11546
873664 ZDOT = -3519
487093
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 16251
54183962
00016717 00000-0 10270-3 0 9000
2 25544 51
6434 7
1214 0002962 300
9122 59
1740 15
54426286 17799
Satellite: ISS
Catalog Number: 25544
Epoch time: 16251
54183962 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 7
1214 deg
Eccentricity:
0002962
Arg of perigee: 300
9122 deg
Mean anomaly: 59
1740 deg
Mean motion: 15
54426286 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1779
Checksum: 293
Coasting Arc #2 (Orbit 1793)
---------------------------------------
Vector Time (GMT): 2016/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893996
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5629952
74 A = 6784560
90 meter
Y = -2239628
71 meter E =
0003850
Z = -3049638
17 I = 51
66719
XDOT = 4270
187207 Wp = 25
14617
YDOT = 4030
265781 meter/sec RA = 1
75805 deg
ZDOT = 4929
112555 TA = 299
88437
MA = 299
92262
Ha = 219
826 n
mi
Hp = 215
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18470973
55 X = 5669392
26
Y = -7347863
24 feet Y = -2176450
54 meter
Z = -10005374
56 Z = -3022193
23
XDOT = 14009
800547 XDOT = 4200
858825
YDOT = 13222
656761 feet/sec YDOT = 4077
630638 meter/sec
ZDOT = 16171
629117 ZDOT = 4949
687377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19706687
62 X = -6006598
39
Y = 3034479
48 feet Y = 924909
35 meter
Z = -9885032
89 Z = -3012958
03
XDOT = -10387
880796 XDOT = -3166
226067
YDOT = -14552
615166 feet/sec YDOT = -4435
637103 meter/sec
ZDOT = 16260
738450 ZDOT = 4956
273080
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 16252
50616530
00016717 00000-0 10270-3 0 9010
2 25544 51
6446 2
3125 0003234 306
7713 53
3143 15
54443328 17949
Satellite: ISS
Catalog Number: 25544
Epoch time: 16252
50616530 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 2
3125 deg
Eccentricity:
0003234
Arg of perigee: 306
7713 deg
Mean anomaly: 53
3143 deg
Mean motion: 15
54443328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1794
Checksum: 273
Coasting Arc #3 (Orbit 1809)
---------------------------------------
Vector Time (GMT): 2016/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893996
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6479488
52 A = 6787593
51 meter
Y = 1456593
69 meter E =
0010829
Z = 1378234
45 I = 51
64470
XDOT = -2247
901342 Wp = 116
71859
YDOT = -4476
089291 meter/sec RA = 356
78249 deg
ZDOT = -5807
000203 TA = 48
26337
MA = 48
17082
Ha = 219
846 n
mi
Hp = 215
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21258164
44 X = -6501989
83
Y = 4778850
68 feet Y = 1384009
99 meter
Z = 4521766
57 Z = 1346703
94
XDOT = -7375
004404 XDOT = -2169
473576
YDOT = -14685
332321 feet/sec YDOT = -4500
788727 meter/sec
ZDOT = -19051
837936 ZDOT = -5817
729143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21814927
83 X = 6649190
00
Y = -291796
34 feet Y = -88939
52 meter
Z = 4383733
66 Z = 1336162
02
XDOT = 4049
398599 XDOT = 1234
256693
YDOT = 14275
051012 feet/sec YDOT = 4351
035548 meter/sec
ZDOT = -19097
840967 ZDOT = -5821
021927
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 16253
53477214
00016717 00000-0 10270-3 0 9029
2 25544 51
6439 357
1828 0003047 311
1563 48
9326 15
54465531 18109
Satellite: ISS
Catalog Number: 25544
Epoch time: 16253
53477214 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 357
1828 deg
Eccentricity:
0003047
Arg of perigee: 311
1563 deg
Mean anomaly: 48
9326 deg
Mean motion: 15
54465531 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1810
Checksum: 302
Coasting Arc #4 (Orbit 1817)
---------------------------------------
Vector Time (GMT): 2016/254/00:56:13
381
Vector Time (MET): N/A
Weight (LBS) : 893592
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3352592
75 A = 6782155
34 meter
Y = -3883679
60 meter E =
0003344
Z = -4438377
70 I = 51
60254
XDOT = 6633
341331 Wp = 85
92127
YDOT = 1948
446453 meter/sec RA = 354
08479 deg
ZDOT = 3308
040638 TA = 217
48423
MA = 217
50756
Ha = 220
783 n
mi
Hp = 217
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10999320
04 X = 3417331
59
Y = -12741730
98 feet Y = -3845826
98 meter
Z = -14561606
62 Z = -4421934
14
XDOT = 21762
930875 XDOT = 6594
991270
YDOT = 6392
540857 feet/sec YDOT = 2022
410713 meter/sec
ZDOT = 10853
151698 ZDOT = 3340
170460
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10480818
12 X = 3194553
36
Y = -13251339
69 feet Y = -4039008
34 meter
Z = -14489016
01 Z = -4416252
08
XDOT = 21003
009331 XDOT = 6401
717244
YDOT = 4600
507315 feet/sec YDOT = 1402
234630 meter/sec
ZDOT = 10993
138192 ZDOT = 3350
708521
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 16254
04907298
00016717 00000-0 10270-3 0 9037
2 25544 51
6443 354
6204 0006193 303
3541 56
7018 15
53753357 18186
Satellite: ISS
Catalog Number: 25544
Epoch time: 16254
04907298 = yrday
fracday
Element set: 903
Inclination: 51
6443 deg
RA of node: 354
6204 deg
Eccentricity:
0006193
Arg of perigee: 303
3541 deg
Mean anomaly: 56
7018 deg
Mean motion: 15
53753357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1818
Checksum: 307
Coasting Arc #5 (Orbit 1833)
---------------------------------------
Vector Time (GMT): 2016/255/00:56:13
381
Vector Time (MET): N/A
Weight (LBS) : 893592
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4653334
12 A = 6785740
41 meter
Y = 3613266
39 meter E =
0008305
Z = 3364134
46 I = 51
58220
XDOT = -5465
815339 Wp = 65
58721
YDOT = -2700
787989 meter/sec RA = 349
09922 deg
ZDOT = -4647
215892 TA = 75
14898
MA = 75
05701
Ha = 220
903 n
mi
Hp = 217
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15266844
24 X = -4709734
21
Y = 11854548
52 feet Y = 3560914
55 meter
Z = 11037186
56 Z = 3341392
57
XDOT = -17932
465022 XDOT = -5412
634099
YDOT = -8860
852982 feet/sec YDOT = -2761
613342 meter/sec
ZDOT = -15246
771298 ZDOT = -4673
638035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14544231
05 X = -4433081
62
Y = 12816812
55 feet Y = 3906564
47 meter
Z = 10937138
56 Z = 3333639
83
XDOT = -17431
562339 XDOT = -5313
140201
YDOT = -6637
113983 feet/sec YDOT = -2022
992342 meter/sec
ZDOT = -15361
672896 ZDOT = -4682
237899
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 16255
07815754
00016717 00000-0 10270-3 0 9047
2 25544 51
6440 349
4946 0006189 306
5287 53
5295 15
53743864 18347
Satellite: ISS
Catalog Number: 25544
Epoch time: 16255
07815754 = yrday
fracday
Element set: 904
Inclination: 51
6440 deg
RA of node: 349
4946 deg
Eccentricity:
0006189
Arg of perigee: 306
5287 deg
Mean anomaly: 53
5295 deg
Mean motion: 15
53743864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1834
Checksum: 338
Coasting Arc #6 (Orbit 1848)
---------------------------------------
Vector Time (GMT): 2016/256/00:56:13
381
Vector Time (MET): N/A
Weight (LBS) : 893592
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5609605
93 A = 6788695
16 meter
Y = -3246165
88 meter E =
0009391
Z = -1999813
28 I = 51
56243
XDOT = 3983
520755 Wp = 356
79849
YDOT = 3459
607843 meter/sec RA = 344
11823 deg
ZDOT = 5566
188786 TA = 341
08961
MA = 341
12446
Ha = 221
066 n
mi
Hp = 216
923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18404218
92 X = 5655202
64
Y = -10650150
51 feet Y = -3183180
70 meter
Z = -6561067
20 Z = -1972452
40
XDOT = 13069
293817 XDOT = 3917
500476
YDOT = 11350
419432 feet/sec YDOT = 3503
785488 meter/sec
ZDOT = 18261
774233 ZDOT = 5585
379030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17517749
79 X = 5339410
13
Y = -12117408
18 feet Y = -3693386
01 meter
Z = -6440919
53 Z = -1963192
27
XDOT = 12948
635445 XDOT = 3946
744084
YDOT = 8982
363152 feet/sec YDOT = 2737
824289 meter/sec
ZDOT = 18344
935565 ZDOT = 5591
536360
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 16256
04291443
00016717 00000-0 10270-3 0 9059
2 25544 51
6454 344
6874 0006345 310
4133 49
6466 15
53784003 18499
Satellite: ISS
Catalog Number: 25544
Epoch time: 16256
04291443 = yrday
fracday
Element set: 905
Inclination: 51
6454 deg
RA of node: 344
6874 deg
Eccentricity:
0006345
Arg of perigee: 310
4133 deg
Mean anomaly: 49
6466 deg
Mean motion: 15
53784003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1849
Checksum: 312
Coasting Arc #7 (Orbit 1864)
---------------------------------------
Vector Time (GMT): 2016/257/00:56:13
381
Vector Time (MET): N/A
Weight (LBS) : 893592
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6198423
56 A = 6790357
23 meter
Y = 2731138
02 meter E =
0006590
Z = 434709
55 I = 51
53658
XDOT = -2281
119670 Wp = 126
96895
YDOT = -4215
668899 meter/sec RA = 339
14322 deg
ZDOT = -5981
395318 TA = 48
33924
MA = 48
28285
Ha = 221
192 n
mi
Hp = 216
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20336035
30 X = -6230614
78
Y = 8960426
57 feet Y = 2661643
14 meter
Z = 1426212
43 Z = 404520
97
XDOT = -7483
988419 XDOT = -2204
754627
YDOT = -13830
934708 feet/sec YDOT = -4240
751428 meter/sec
ZDOT = -19624
000388 ZDOT = -5992
290508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19362620
60 X = -5901726
76
Y = 10922115
63 feet Y = 3329060
84 meter
Z = 1293820
59 Z = 394356
51
XDOT = -7887
956325 XDOT = -2404
249088
YDOT = -11628
283492 feet/sec YDOT = -3544
300808 meter/sec
ZDOT = -19670
783175 ZDOT = -5995
654712
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 16257
07198251
00016717 00000-0 10270-3 0 9067
2 25544 51
6449 339
5615 0006223 314
2600 45
8041 15
53751297 18659
Satellite: ISS
Catalog Number: 25544
Epoch time: 16257
07198251 = yrday
fracday
Element set: 906
Inclination: 51
6449 deg
RA of node: 339
5615 deg
Eccentricity:
0006223
Arg of perigee: 314
2600 deg
Mean anomaly: 45
8041 deg
Mean motion: 15
53751297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1865
Checksum: 310
Coasting Arc #8 (Orbit 1877)
---------------------------------------
Vector Time (GMT): 2016/257/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893592
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3464681
43 A = 6779173
51 meter
Y = 2851327
06 meter E =
0001779
Z = 5081360
54 I = 51
47305
XDOT = -6086
281931 Wp = 353
51976
YDOT = 4336
628427 meter/sec RA = 335
07737 deg
ZDOT = 1718
237490 TA = 79
84638
MA = 79
82631
Ha = 221
159 n
mi
Hp = 216
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11367065
04 X = 3407856
80
Y = 9354747
56 feet Y = 2889754
23 meter
Z = 16671130
37 Z = 5098052
64
XDOT = -19968
116572 XDOT = -6142
669256
YDOT = 14227
783552 feet/sec YDOT = 4268
252435 meter/sec
ZDOT = 5637
262106 ZDOT = 1688
534718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2244621
26 X = -684160
56
Y = 14465995
64 feet Y = 4409235
47 meter
Z = 16743497
34 Z = 5103417
99
XDOT = -21428
018648 XDOT = -6531
260084
YDOT = -9691
772207 feet/sec YDOT = -2954
052169 meter/sec
ZDOT = 5506
694421 ZDOT = 1678
440460
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 16257
90809251
00016717 00000-0 10270-3 0 9079
2 25544 51
6424 335
3948 0006428 317
2327 42
8325 15
53820835 18782
Satellite: ISS
Catalog Number: 25544
Epoch time: 16257
90809251 = yrday
fracday
Element set: 907
Inclination: 51
6424 deg
RA of node: 335
3948 deg
Eccentricity:
0006428
Arg of perigee: 317
2327 deg
Mean anomaly: 42
8325 deg
Mean motion: 15
53820835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1878
Checksum: 325
Coasting Arc #9 (Orbit 1892)
---------------------------------------
Vector Time (GMT): 2016/258/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893592
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2041544
29 A = 6778326
68 meter
Y = -3704754
89 meter E =
0011879
Z = -5305811
10 I = 51
44152
XDOT = 6667
047123 Wp = 65
75926
YDOT = -3771
442831 meter/sec RA = 330
06869 deg
ZDOT = 72
982985 TA = 204
91015
MA = 204
96753
Ha = 221
404 n
mi
Hp = 216
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6697979
96 X = -1974191
91
Y = -12154707
64 feet Y = -3727208
85 meter
Z = -17407516
73 Z = -5315564
29
XDOT = 21873
514182 XDOT = 6708
370330
YDOT = -12373
500103 feet/sec YDOT = -3696
656381 meter/sec
ZDOT = 239
445489 ZDOT = 105
470392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6842047
72 X = 2085456
15
Y = -12013565
92 feet Y = -3661734
89 meter
Z = -17449415
71 Z = -5318581
91
XDOT = 21184
803618 XDOT = 6457
128143
YDOT = 11533
714753 feet/sec YDOT = 3515
476257 meter/sec
ZDOT = 382
054611 ZDOT = 116
450245
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 16258
87283203
00016717 00000-0 10270-3 0 9080
2 25544 51
6428 330
5879 0006427 321
5481 38
5213 15
53795798 18938
Satellite: ISS
Catalog Number: 25544
Epoch time: 16258
87283203 = yrday
fracday
Element set: 908
Inclination: 51
6428 deg
RA of node: 330
5879 deg
Eccentricity:
0006427
Arg of perigee: 321
5481 deg
Mean anomaly: 38
5213 deg
Mean motion: 15
53795798 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1893
Checksum: 342
Coasting Arc #10 (Orbit 1908)
---------------------------------------
Vector Time (GMT): 2016/259/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893592
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 559617
71 A = 6779515
61 meter
Y = 4508075
64 meter E =
0008653
Z = 5034003
91 I = 51
41816
XDOT = -6825
415463 Wp = 7
12326
YDOT = 2947
151641 meter/sec RA = 325
05927 deg
ZDOT = -1871
713970 TA = 101
12415
MA = 101
02685
Ha = 221
621 n
mi
Hp = 216
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1836016
11 X = 484712
78
Y = 14790274
40 feet Y = 4513915
53 meter
Z = 16515760
85 Z = 5036539
82
XDOT = -22393
095352 XDOT = -6848
772052
YDOT = 9669
132680 feet/sec YDOT = 2870
694417 meter/sec
ZDOT = -6140
793864 ZDOT = -1904
927077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11483874
65 X = -3500284
99
Y = 9481864
16 feet Y = 2890072
20 meter
Z = 16525991
75 Z = 5037122
28
XDOT = -19562
809857 XDOT = -5962
744444
YDOT = -12686
604571 feet/sec YDOT = -3866
877073 meter/sec
ZDOT = -6286
402529 ZDOT = -1916
095491
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 16259
90187946
00016717 00000-0 10270-3 0 9093
2 25544 51
6429 325
4616 0006471 326
4298 33
6444 15
53804289 19096
Satellite: ISS
Catalog Number: 25544
Epoch time: 16259
90187946 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 325
4616 deg
Eccentricity:
0006471
Arg of perigee: 326
4298 deg
Mean anomaly: 33
6444 deg
Mean motion: 15
53804289 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1909
Checksum: 343
Coasting Arc #11 (Orbit 1923)
---------------------------------------
Vector Time (GMT): 2016/260/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893592
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 813526
70 A = 6782380
56 meter
Y = -5172525
87 meter E =
0005398
Z = -4313277
94 I = 51
40109
XDOT = 6565
125283 Wp = 59
99855
YDOT = -1869
089655 meter/sec RA = 320
05299 deg
ZDOT = 3485
603733 TA = 245
55773
MA = 245
61405
Ha = 221
731 n
mi
Hp = 216
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2669050
86 X = 892258
76
Y = -16970229
24 feet Y = -5162988
89 meter
Z = -14151174
34 Z = -4309134
05
XDOT = 21539
124944 XDOT = 6568
606443
YDOT = -6132
183908 feet/sec YDOT = -1795
654048 meter/sec
ZDOT = 11435
707785 ZDOT = 3517
504149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15630781
78 X = 4764262
29
Y = -7164509
22 feet Y = -2183742
41 meter
Z = -14132116
50 Z = -4307469
11
XDOT = 16529
150340 XDOT = 5038
085024
YDOT = 13267
369645 feet/sec YDOT = 4043
894268 meter/sec
ZDOT = 11575
368627 ZDOT = 3528
172357
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 16260
86660559
00016717 00000-0 10270-3 0 9108
2 25544 51
6421 320
6553 0006502 329
9019 30
1759 15
53813503 19246
Satellite: ISS
Catalog Number: 25544
Epoch time: 16260
86660559 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 320
6553 deg
Eccentricity:
0006502
Arg of perigee: 329
9019 deg
Mean anomaly: 30
1759 deg
Mean motion: 15
53813503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1924
Checksum: 298
Coasting Arc #12 (Orbit 1939)
---------------------------------------
Vector Time (GMT): 2016/261/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893592
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2057251
55 A = 6785961
70 meter
Y = 5633204
16 meter E =
0011037
Z = 3172689
57 I = 51
38958
XDOT = -5956
751794 Wp = 63
40520
YDOT = 535
255233 meter/sec RA = 315
05364 deg
ZDOT = -4795
063951 TA = 79
83621
MA = 79
71174
Ha = 221
858 n
mi
Hp = 215
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6749512
95 X = -2135502
19
Y = 18481640
95 feet Y = 5609761
53 meter
Z = 10409086
53 Z = 3162505
05
XDOT = -19543
148929 XDOT = -5939
001993
YDOT = 1756
086724 feet/sec YDOT = 468
741387 meter/sec
ZDOT = -15731
837111 ZDOT = -4823
957425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19063075
66 X = -5810425
46
Y = 4967046
41 feet Y = 1513955
75 meter
Z = 10363573
51 Z = 3158817
21
XDOT = -12186
701975 XDOT = -3714
506762
YDOT = -13561
640305 feet/sec YDOT = -4133
587965 meter/sec
ZDOT = -15858
108936 ZDOT = -4833
551604
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 16261
89564100
00016717 00000-0 10270-3 0 9118
2 25544 51
6425 315
5285 0006564 333
3332 26
7482 15
53833469 19405
Satellite: ISS
Catalog Number: 25544
Epoch time: 16261
89564100 = yrday
fracday
Element set: 911
Inclination: 51
6425 deg
RA of node: 315
5285 deg
Eccentricity:
0006564
Arg of perigee: 333
3332 deg
Mean anomaly: 26
7482 deg
Mean motion: 15
53833469 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1940
Checksum: 307
Coasting Arc #13 (Orbit 1954)
---------------------------------------
Vector Time (GMT): 2016/262/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893592
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3040792
35 A = 6788912
46 meter
Y = -5800658
76 meter E =
0012217
Z = -1759797
21 I = 51
37715
XDOT = 5094
177816 Wp = 9
69449
YDOT = 960
514009 meter/sec RA = 310
06061 deg
ZDOT = 5653
828387 TA = 330
90664
MA = 330
97466
Ha = 222
004 n
mi
Hp = 215
683
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9976352
84 X = 3113979
19
Y = -19031032
68 feet Y = -5766245
61 meter
Z = -5773612
90 Z = -1744847
14
XDOT = 16713
181810 XDOT = 5055
594410
YDOT = 3151
292681 feet/sec YDOT = 1017
265555 meter/sec
ZDOT = 18549
305733 ZDOT = 5678
480973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21291433
59 X = 6489628
96
Y = -3023964
78 feet Y = -921704
46 meter
Z = -5707269
00 Z = -1739575
59
XDOT = 6937
629430 XDOT = 2114
589450
YDOT = 13745
231734 feet/sec YDOT = 4189
546633 meter/sec
ZDOT = 18656
777099 ZDOT = 5686
585660
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 16262
86035562
00016717 00000-0 10270-3 0 9122
2 25544 51
6423 310
7214 0006615 337
3532 22
7327 15
53830036 19552
Satellite: ISS
Catalog Number: 25544
Epoch time: 16262
86035562 = yrday
fracday
Element set: 912
Inclination: 51
6423 deg
RA of node: 310
7214 deg
Eccentricity:
0006615
Arg of perigee: 337
3532 deg
Mean anomaly: 22
7327 deg
Mean motion: 15
53830036 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1955
Checksum: 288
Coasting Arc #14 (Orbit 1970)
---------------------------------------
Vector Time (GMT): 2016/263/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893592
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3798436
33 A = 6790170
03 meter
Y = 5624271
39 meter E =
0007257
Z = 153906
78 I = 51
36185
XDOT = -4045
395569 Wp = 107
65266
YDOT = -2562
050527 meter/sec RA = 305
07242 deg
ZDOT = -5983
436737 TA = 70
68410
MA = 70
60564
Ha = 222
118 n
mi
Hp = 215
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12462061
46 X = -3861793
68
Y = 18452333
96 feet Y = 5581440
50 meter
Z = 504943
52 Z = 135300
19
XDOT = -13272
295175 XDOT = -3987
380142
YDOT = -8405
677583 feet/sec YDOT = -2606
965179 meter/sec
ZDOT = -19630
697957 ZDOT = -6002
947240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22241879
99 X = -6779325
02
Y = 1080135
76 feet Y = 329225
38 meter
Z = 422674
22 Z = 128831
10
XDOT = -1068
848316 XDOT = -325
784967
YDOT = -13939
545135 feet/sec YDOT = -4248
773357 meter/sec
ZDOT = -19715
421319 ZDOT = -6009
260418
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 16263
88937941
00016717 00000-0 10270-3 0 9138
2 25544 51
6427 305
5941 0006567 341
5699 18
5214 15
53835291 19716
Satellite: ISS
Catalog Number: 25544
Epoch time: 16263
88937941 = yrday
fracday
Element set: 913
Inclination: 51
6427 deg
RA of node: 305
5941 deg
Eccentricity:
0006567
Arg of perigee: 341
5699 deg
Mean anomaly: 18
5214 deg
Mean motion: 15
53835291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1971
Checksum: 338
Coasting Arc #15 (Orbit 1986)
---------------------------------------
Vector Time (GMT): 2016/264/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893592
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4267183
81 A = 6789257
40 meter
Y = -5066124
23 meter E =
0016736
Z = 1441253
96 I = 51
34095
XDOT = 2940
983309 Wp = 38
43298
YDOT = 4123
889898 meter/sec RA = 300
08307 deg
ZDOT = 5765
097581 TA = 337
36668
MA = 337
44040
Ha = 222
178 n
mi
Hp = 215
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13999946
89 X = 4316516
29
Y = -16621142
49 feet Y = -5018129
74 meter
Z = 4728523
48 Z = 1462103
42
XDOT = 9648
895370 XDOT = 2866
645678
YDOT = 13529
822499 feet/sec YDOT = 4156
362872 meter/sec
ZDOT = 18914
362141 ZDOT = 5779
203324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21694765
60 X = 6612564
56
Y = 848508
32 feet Y = 258625
34 meter
Z = 4820477
57 Z = 1469281
56
XDOT = -4789
717455 XDOT = -1459
905880
YDOT = 14239
309440 feet/sec YDOT = 4340
141517 meter/sec
ZDOT = 18975
204064 ZDOT = 5783
642199
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 16264
91839859
00016717 00000-0 10270-3 0 9143
2 25544 51
6425 300
4666 0006658 345
2439 14
8519 15
53840550 19874
Satellite: ISS
Catalog Number: 25544
Epoch time: 16264
91839859 = yrday
fracday
Element set: 914
Inclination: 51
6425 deg
RA of node: 300
4666 deg
Eccentricity:
0006658
Arg of perigee: 345
2439 deg
Mean anomaly: 14
8519 deg
Mean motion: 15
53840550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1987
Checksum: 341
Coasting Arc #16 (Orbit 2001)
---------------------------------------
Vector Time (GMT): 2016/265/20:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 893592
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4522691
72 A = 6786409
84 meter
Y = 4133266
52 meter E =
0005487
Z = -2926976
21 I = 51
31772
XDOT = -1821
077788 Wp = 30
07651
YDOT = -5523
142541 meter/sec RA = 295
08801 deg
ZDOT = -4984
916661 TA = 183
44183
MA = 183
44561
Ha = 222
300 n
mi
Hp = 215
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14838227
44 X = -4554356
70
Y = 13560585
70 feet Y = 4082513
46 meter
Z = -9602940
33 Z = -2949023
77
XDOT = -5974
664658 XDOT = -1734
966456
YDOT = -18120
546395 feet/sec YDOT = -5543
025993 meter/sec
ZDOT = -16354
713455 ZDOT = -4993
553464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19825726
35 X = -6042881
39
Y = -3021663
16 feet Y = -921002
93 meter
Z = -9699951
93 Z = -2956545
35
XDOT = 10227
799805 XDOT = 3117
433380
YDOT = -14481
772311 feet/sec YDOT = -4414
044200 meter/sec
ZDOT = -16391
428699 ZDOT = -4996
107467
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 16265
88309690
00016717 00000-0 10270-3 0 9156
2 25544 51
6438 295
6600 0006657 347
6989 12
4000 15
53859184 20027
Satellite: ISS
Catalog Number: 25544
Epoch time: 16265
88309690 = yrday
fracday
Element set: 915
Inclination: 51
6438 deg
RA of node: 295
6600 deg
Eccentricity:
0006657
Arg of perigee: 347
6989 deg
Mean anomaly: 12
4000 deg
Mean motion: 15
53859184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2002
Checksum: 327
Coasting Arc #17 (Orbit 2002)
---------------------------------------
Vector Time (GMT): 2016/265/22:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 893592
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2998372
97 A = 6778883
15 meter
Y = -3297482
40 meter E =
0012460
Z = -5117210
13 I = 51
29144
XDOT = 4211
134652 Wp = 72
05305
YDOT = -6210
330894 meter/sec RA = 294
66577 deg
ZDOT = 1541
284357 TA = 212
85064
MA = 212
92815
Ha = 222
232 n
mi
Hp = 215
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9837181
65 X = -2936419
41
Y = -10818511
80 feet Y = -3330666
23 meter
Z = -16788747
14 Z = -5131624
85
XDOT = 13816
058569 XDOT = 4272
780207
YDOT = -20375
101358 feet/sec YDOT = -6162
894355 meter/sec
ZDOT = 5056
707207 ZDOT = 1561
891419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4635313
73 X = -1412843
63
Y = -13792277
79 feet Y = -4203886
27 meter
Z = -16851092
28 Z = -5136212
93
XDOT = 19731
403703 XDOT = 6014
131849
YDOT = -12893
357465 feet/sec YDOT = -3929
895355 meter/sec
ZDOT = 5147
802988 ZDOT = 1569
050351
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 16265
94740888
00016717 00000-0 10270-3 0 9162
2 25544 51
6437 295
3397 0006750 347
6816 12
4171 15
53881278 20038
Satellite: ISS
Catalog Number: 25544
Epoch time: 16265
94740888 = yrday
fracday
Element set: 916
Inclination: 51
6437 deg
RA of node: 295
3397 deg
Eccentricity:
0006750
Arg of perigee: 347
6816 deg
Mean anomaly: 12
4171 deg
Mean motion: 15
53881278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2003
Checksum: 334
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