[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 5th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5432 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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
284/02:47:17
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 212
5
286/10:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 212
2
287/18:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 212
2
288/06:36:41
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 212
2
Coasting Arc #1 (Orbit 2182)
---------------------------------------
Vector Time (GMT): 2016/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -591198
10 A = 6782045
88 meter
Y = 5279295
36 meter E =
0014199
Z = -4231591
36 I = 51
32153
XDOT = -5759
400906 Wp = 52
09542
YDOT = -3531
324806 meter/sec RA = 236
77071 deg
ZDOT = -3600
739312 TA = 180
85444
MA = 180
85687
Ha = 223
193 n
mi
Hp = 213
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1939626
31 X = -629632
99
Y = 17320522
83 feet Y = 5272468
75 meter
Z = -13883173
76 Z = -4234557
32
XDOT = -18895
672264 XDOT = -5701
993540
YDOT = -11585
711306 feet/sec YDOT = -3595
409759 meter/sec
ZDOT = -11813
449185 ZDOT = -3628
577628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1721141
11 X = -524603
81
Y = -17332548
78 feet Y = -5282960
87 meter
Z = -13896963
73 Z = -4235794
54
XDOT = 19522
358585 XDOT = 5950
414897
YDOT = 7630
970372 feet/sec YDOT = 2325
919770 meter/sec
ZDOT = -11934
479859 ZDOT = -3637
629461
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 16277
52277146
00016717 00000-0 10270-3 0 9004
2 25544 51
6402 237
6460 0006993 30
8589 329
2973 15
54025236 21830
Satellite: ISS
Catalog Number: 25544
Epoch time: 16277
52277146 = yrday
fracday
Element set: 900
Inclination: 51
6402 deg
RA of node: 237
6460 deg
Eccentricity:
0006993
Arg of perigee: 30
8589 deg
Mean anomaly: 329
2973 deg
Mean motion: 15
54025236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2183
Checksum: 318
Coasting Arc #2 (Orbit 2198)
---------------------------------------
Vector Time (GMT): 2016/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1794432
15 A = 6778795
75 meter
Y = -4194670
22 meter E =
0008894
Z = 5005520
55 I = 51
33052
XDOT = 5711
336407 Wp = 74
23613
YDOT = 4749
126396 meter/sec RA = 231
75763 deg
ZDOT = 1931
858753 TA = 356
95383
MA = 356
95924
Ha = 223
019 n
mi
Hp = 213
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5887244
60 X = 1816889
55
Y = -13762041
42 feet Y = -4174477
55 meter
Z = 16422311
51 Z = 5014292
62
XDOT = 18737
980338 XDOT = 5648
421675
YDOT = 15581
123345 feet/sec YDOT = 4812
642830 meter/sec
ZDOT = 6338
119270 ZDOT = 1959
450149
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2600660
41 X = -792681
29
Y = 14697221
36 feet Y = 4479713
07 meter
Z = 16461287
86 Z = 5017400
54
XDOT = -20603
179199 XDOT = -6279
849020
YDOT = -10880
526486 feet/sec YDOT = -3316
384473 meter/sec
ZDOT = 6457
891538 ZDOT = 1968
365341
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 16278
55166946
00016717 00000-0 10270-3 0 9014
2 25544 51
6411 232
5187 0006809 33
2940 326
8640 15
54069005 21997
Satellite: ISS
Catalog Number: 25544
Epoch time: 16278
55166946 = yrday
fracday
Element set: 901
Inclination: 51
6411 deg
RA of node: 232
5187 deg
Eccentricity:
0006809
Arg of perigee: 33
2940 deg
Mean anomaly: 326
8640 deg
Mean motion: 15
54069005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2199
Checksum: 315
Coasting Arc #3 (Orbit 2213)
---------------------------------------
Vector Time (GMT): 2016/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3041729
58 A = 6777614
62 meter
Y = 2956357
11 meter E =
0019906
Z = -5302825
57 I = 51
34739
XDOT = -5278
567297 Wp = 73
57312
YDOT = -5542
569080 meter/sec RA = 226
73799 deg
ZDOT = -56
861424 TA = 195
85063
MA = 195
91302
Ha = 223
249 n
mi
Hp = 212
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9979427
77 X = -3048802
94
Y = 9699334
37 feet Y = 2922302
38 meter
Z = -17397721
69 Z = -5317619
27
XDOT = -17318
134176 XDOT = -5215
920347
YDOT = -18184
281760 feet/sec YDOT = -5601
247287 meter/sec
ZDOT = -186
553228 ZDOT = -82
351140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7281219
21 X = 2219315
62
Y = -11763543
21 feet Y = -3585527
97 meter
Z = -17462808
59 Z = -5322664
06
XDOT = 20281
892005 XDOT = 6181
920683
YDOT = 13020
628005 feet/sec YDOT = 3968
687416 meter/sec
ZDOT = -297
034672 ZDOT = -90
536168
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 16279
51625459
00016717 00000-0 10270-3 0 9021
2 25544 51
6415 227
7105 0006954 37
1395 323
0237 15
54042331 22147
Satellite: ISS
Catalog Number: 25544
Epoch time: 16279
51625459 = yrday
fracday
Element set: 902
Inclination: 51
6415 deg
RA of node: 227
7105 deg
Eccentricity:
0006954
Arg of perigee: 37
1395 deg
Mean anomaly: 323
0237 deg
Mean motion: 15
54042331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2214
Checksum: 292
Coasting Arc #4 (Orbit 2229)
---------------------------------------
Vector Time (GMT): 2016/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4235259
01 A = 6778645
15 meter
Y = -1613926
97 meter E =
0012384
Z = 5035017
49 I = 51
37356
XDOT = 4471
612753 Wp = 47
62761
YDOT = 5957
470705 meter/sec RA = 221
72097 deg
ZDOT = -1840
633898 TA = 60
31611
MA = 60
19288
Ha = 223
197 n
mi
Hp = 212
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13895206
73 X = 4228533
20
Y = -5295035
98 feet Y = -1566602
63 meter
Z = 16519086
27 Z = 5055575
48
XDOT = 14670
645516 XDOT = 4413
603620
YDOT = 19545
507563 feet/sec YDOT = 6007
150772 meter/sec
ZDOT = -6038
825126 ZDOT = -1819
052956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11989789
68 X = -3654487
89
Y = 8624119
04 feet Y = 2628631
48 meter
Z = 16609151
13 Z = 5062469
26
XDOT = -18565
108712 XDOT = -5658
645135
YDOT = -14290
263922 feet/sec YDOT = -4355
672444 meter/sec
ZDOT = -5945
469314 ZDOT = -1812
179047
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 16280
54513569
00016717 00000-0 10270-3 0 9035
2 25544 51
6411 222
5831 0007033 41
1186 319
0496 15
54057571 22306
Satellite: ISS
Catalog Number: 25544
Epoch time: 16280
54513569 = yrday
fracday
Element set: 903
Inclination: 51
6411 deg
RA of node: 222
5831 deg
Eccentricity:
0007033
Arg of perigee: 41
1186 deg
Mean anomaly: 319
0496 deg
Mean motion: 15
54057571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2230
Checksum: 285
Coasting Arc #5 (Orbit 2244)
---------------------------------------
Vector Time (GMT): 2016/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5251108
14 A = 6781605
07 meter
Y = 351970
68 meter E =
0012993
Z = -4286875
32 I = 51
40816
XDOT = -3273
345988 Wp = 81
56273
YDOT = -5956
593250 meter/sec RA = 216
71106 deg
ZDOT = 3531
609618 TA = 224
53527
MA = 224
63977
Ha = 223
266 n
mi
Hp = 212
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17228045
07 X = -5233829
57
Y = 1154759
44 feet Y = 293345
55 meter
Z = -14064551
57 Z = -4312342
34
XDOT = -10739
324107 XDOT = -3223
649870
YDOT = -19542
628774 feet/sec YDOT = -5992
919864 meter/sec
ZDOT = 11586
645729 ZDOT = 3515
829435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16184206
47 X = 4932946
13
Y = -5750351
75 feet Y = -1752707
21 meter
Z = -14175878
56 Z = -4320807
79
XDOT = 15281
942733 XDOT = 4657
936145
YDOT = 14703
451605 feet/sec YDOT = 4481
612049 meter/sec
ZDOT = 11518
619365 ZDOT = 3510
875182
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 16281
50970331
00016717 00000-0 10270-3 0 9047
2 25544 51
6410 217
7757 0006932 44
2131 315
9574 15
54066453 22456
Satellite: ISS
Catalog Number: 25544
Epoch time: 16281
50970331 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 217
7757 deg
Eccentricity:
0006932
Arg of perigee: 44
2131 deg
Mean anomaly: 315
9574 deg
Mean motion: 15
54066453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2245
Checksum: 297
Coasting Arc #6 (Orbit 2260)
---------------------------------------
Vector Time (GMT): 2016/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5994655
59 A = 6785355
70 meter
Y = 843941
48 meter E =
0018418
Z = 3053204
11 I = 51
44823
XDOT = 1714
290859 Wp = 79
45581
YDOT = 5648
048135 meter/sec RA = 211
71188 deg
ZDOT = -4898
523315 TA = 65
38720
MA = 65
19544
Ha = 223
259 n
mi
Hp = 212
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19667505
21 X = 5969941
53
Y = 2768836
89 feet Y = 910839
78 meter
Z = 10017073
86 Z = 3082264
94
XDOT = 5624
313843 XDOT = 1674
800769
YDOT = 18530
341649 feet/sec YDOT = 5666
997334 meter/sec
ZDOT = -16071
270720 ZDOT = -4890
291930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19571638
50 X = -5965435
41
Y = 2978348
31 feet Y = 907800
56 meter
Z = 10143933
93 Z = 3091871
06
XDOT = -10592
568939 XDOT = -3228
615013
YDOT = -14675
071060 feet/sec YDOT = -4472
961659 meter/sec
ZDOT = -16036
169844 ZDOT = -4887
824569
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 16282
53856425
00016717 00000-0 10270-3 0 9059
2 25544 51
6417 212
6471 0006979 47
5332 312
6409 15
54102124 22615
Satellite: ISS
Catalog Number: 25544
Epoch time: 16282
53856425 = yrday
fracday
Element set: 905
Inclination: 51
6417 deg
RA of node: 212
6471 deg
Eccentricity:
0006979
Arg of perigee: 47
5332 deg
Mean anomaly: 312
6409 deg
Mean motion: 15
54102124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2261
Checksum: 298
Coasting Arc #7 (Orbit 2275)
---------------------------------------
Vector Time (GMT): 2016/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6349483
85 A = 6788330
06 meter
Y = -1815718
14 meter E =
0014931
Z = -1550054
78 I = 51
48537
XDOT = 62
977845 Wp = 44
43475
YDOT = -5083
521241 meter/sec RA = 206
72457 deg
ZDOT = 5740
776857 TA = 298
58526
MA = 298
73542
Ha = 223
323 n
mi
Hp = 212
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20831639
92 X = -6321178
54
Y = -5957080
52 feet Y = -1886564
18 meter
Z = -5085481
57 Z = -1580830
43
XDOT = 206
620227 XDOT = 91
931873
YDOT = -16678
219296 feet/sec YDOT = -5082
654669 meter/sec
ZDOT = 18834
569741 ZDOT = 5741
153489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21625228
01 X = 6591369
50
Y = -640592
08 feet Y = -195252
47 meter
Z = -5219703
86 Z = -1590965
74
XDOT = 4937
495541 XDOT = 1504
948641
YDOT = 14337
588160 feet/sec YDOT = 4370
096871 meter/sec
ZDOT = 18836
992335 ZDOT = 5741
515264
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 16283
50311060
00016717 00000-0 10270-3 0 9069
2 25544 51
6410 207
8397 0007024 51
1484 309
0295 15
54101433 22763
Satellite: ISS
Catalog Number: 25544
Epoch time: 16283
50311060 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 207
8397 deg
Eccentricity:
0007024
Arg of perigee: 51
1484 deg
Mean anomaly: 309
0295 deg
Mean motion: 15
54101433 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2276
Checksum: 276
Coasting Arc #8 (Orbit 2285)
---------------------------------------
Vector Time (GMT): 2016/284/02:47:17
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5676767
60 A = 6788752
91 meter
Y = 3525232
05 meter E =
0011884
Z = -1193969
45 I = 51
50516
XDOT = -3435
763673 Wp = 107
44961
YDOT = 3570
197860 meter/sec RA = 203
67062 deg
ZDOT = -5845
946758 TA = 85
53762
MA = 85
40186
Ha = 223
334 n
mi
Hp = 212
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18624565
61 X = 5642725
49
Y = 11565721
96 feet Y = 3588523
04 meter
Z = -3917222
61 Z = -1166475
84
XDOT = -11272
190528 XDOT = -3447
033821
YDOT = 11713
247572 feet/sec YDOT = 3531
713374 meter/sec
ZDOT = -19179
615348 ZDOT = -5862
664647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19320938
53 X = 5889022
06
Y = -10405028
48 feet Y = -3171452
68 meter
Z = -3797593
73 Z = -1157506
57
XDOT = 3839
328507 XDOT = 1170
227329
YDOT = 14092
419551 feet/sec YDOT = 4295
369479 meter/sec
ZDOT = -19253
226539 ZDOT = -5868
383449
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 16284
14613523
00016717 00000-0 10270-3 0 9070
2 25544 51
6414 204
6332 0006814 55
7661 304
4137 15
54129102 22862
Satellite: ISS
Catalog Number: 25544
Epoch time: 16284
14613523 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 204
6332 deg
Eccentricity:
0006814
Arg of perigee: 55
7661 deg
Mean anomaly: 304
4137 deg
Mean motion: 15
54129102 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2286
Checksum: 286
Coasting Arc #9 (Orbit 2301)
---------------------------------------
Vector Time (GMT): 2016/285/02:47:17
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4781719
85 A = 6786173
06 meter
Y = -3930337
10 meter E =
0020031
Z = 2757057
71 I = 51
52636
XDOT = 5093
215620 Wp = 72
74385
YDOT = -2580
605705 meter/sec RA = 198
68794 deg
ZDOT = 5129
688502 TA = 318
56976
MA = 318
72148
Ha = 223
391 n
mi
Hp = 212
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15688057
24 X = -4750807
14
Y = -12894806
75 feet Y = -3983636
40 meter
Z = 9045464
93 Z = 2733904
57
XDOT = 16710
024999 XDOT = 5096
776049
YDOT = -8466
554149 feet/sec YDOT = -2523
629574 meter/sec
ZDOT = 16829
686686 ZDOT = 5154
439151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18898876
45 X = -5760377
54
Y = 7552066
38 feet Y = 2301869
83 meter
Z = 8944852
10 Z = 2726390
92
XDOT = 1164
461230 XDOT = 354
927783
YDOT = -17246
164954 feet/sec YDOT = -5256
631078 meter/sec
ZDOT = 16938
265866 ZDOT = 5162
783436
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 16285
17496648
00016717 00000-0 10270-3 0 9082
2 25544 51
6414 199
5046 0006801 59
5409 300
6415 15
54130682 23025
Satellite: ISS
Catalog Number: 25544
Epoch time: 16285
17496648 = yrday
fracday
Element set: 908
Inclination: 51
6414 deg
RA of node: 199
5046 deg
Eccentricity:
0006801
Arg of perigee: 59
5409 deg
Mean anomaly: 300
6415 deg
Mean motion: 15
54130682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2302
Checksum: 311
Coasting Arc #10 (Orbit 2316)
---------------------------------------
Vector Time (GMT): 2016/286/02:47:17
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3457285
75 A = 6782278
36 meter
Y = 4181464
18 meter E =
0014033
Z = -4084721
99 I = 51
54546
XDOT = -6433
268286 Wp = 67
78329
YDOT = 1571
892793 meter/sec RA = 193
69782 deg
ZDOT = -3841
370444 TA = 162
39561
MA = 162
34693
Ha = 223
370 n
mi
Hp = 212
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11342801
01 X = 3430112
58
Y = 13718714
51 feet Y = 4219973
50 meter
Z = -13401318
85 Z = -4067993
67
XDOT = -21106
523247 XDOT = -6431
707577
YDOT = 5157
128585 feet/sec YDOT = 1499
959980 meter/sec
ZDOT = -12602
921404 ZDOT = -3872
618284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17472483
48 X = 5325612
96
Y = -3675949
46 feet Y = -1120429
40 meter
Z = -13328815
63 Z = -4062623
00
XDOT = -5556
614203 XDOT = -1693
656009
YDOT = 19717
420879 feet/sec YDOT = 6009
869884 meter/sec
ZDOT = -12739
762253 ZDOT = -3883
079535
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 16286
13948439
00016717 00000-0 10270-3 0 9090
2 25544 51
6424 194
6963 0006870 62
9434 297
2419 15
54152755 23178
Satellite: ISS
Catalog Number: 25544
Epoch time: 16286
13948439 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 194
6963 deg
Eccentricity:
0006870
Arg of perigee: 62
9434 deg
Mean anomaly: 297
2419 deg
Mean motion: 15
54152755 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2317
Checksum: 342
Coasting Arc #11 (Orbit 2321)
---------------------------------------
Vector Time (GMT): 2016/286/10:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 907704
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6002994
03 A = 6785427
63 meter
Y = 1127860
94 meter E =
0011463
Z = -2958071
25 I = 51
56640
XDOT = -3343
551583 Wp = 65
06385
YDOT = -4757
048496 meter/sec RA = 191
95993 deg
ZDOT = 4991
408813 TA = 261
12685
MA = 261
25665
Ha = 223
320 n
mi
Hp = 212
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19694862
29 X = -6000790
74
Y = 3700331
18 feet Y = 1060743
42 meter
Z = -9704958
17 Z = -2987227
32
XDOT = -10969
657423 XDOT = -3314
354880
YDOT = -15607
114487 feet/sec YDOT = -4794
274517 meter/sec
ZDOT = 16376
013167 ZDOT = 4975
237995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19295084
49 X = 5881141
75
Y = -5175530
01 feet Y = -1577501
55 meter
Z = -9832592
15 Z = -2996974
09
XDOT = 11848
049803 XDOT = 3611
285580
YDOT = 13315
101645 feet/sec YDOT = 4058
442981 meter/sec
ZDOT = 16306
029395 ZDOT = 4970
077760
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 16286
46098856
00016717 00000-0 10270-3 0 9107
2 25544 51
6418 193
0950 0006956 61
5772 298
6080 15
54159193 23223
Satellite: ISS
Catalog Number: 25544
Epoch time: 16286
46098856 = yrday
fracday
Element set: 910
Inclination: 51
6418 deg
RA of node: 193
0950 deg
Eccentricity:
0006956
Arg of perigee: 61
5772 deg
Mean anomaly: 298
6080 deg
Mean motion: 15
54159193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2322
Checksum: 334
Coasting Arc #12 (Orbit 2337)
---------------------------------------
Vector Time (GMT): 2016/287/10:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 907704
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6640923
32 A = 6788384
55 meter
Y = -266493
26 meter E =
0018780
Z = 1352601
60 I = 51
60866
XDOT = 1389
546052 Wp = 102
61361
YDOT = 4808
703506 meter/sec RA = 186
98160 deg
ZDOT = -5810
793920 TA = 62
64612
MA = 62
45511
Ha = 223
365 n
mi
Hp = 212
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21787806
17 X = 6636839
32
Y = -874321
73 feet Y = -192252
66 meter
Z = 4437669
29 Z = 1384852
01
XDOT = 4558
878125 XDOT = 1363
897282
YDOT = 15776
586307 feet/sec YDOT = 4824
098190 meter/sec
ZDOT = -19064
284514 ZDOT = -5804
106691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21583421
68 X = -6578626
93
Y = 2890867
40 feet Y = 881136
38 meter
Z = 4578715
89 Z = 1395592
60
XDOT = -5916
189426 XDOT = -1803
254537
YDOT = -13698
003242 feet/sec YDOT = -4175
151388 meter/sec
ZDOT = -19035
762738 ZDOT = -5802
100483
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 16287
48979343
00016717 00000-0 10270-3 0 9110
2 25544 51
6425 187
9665 0006931 65
7496 294
4380 15
54170664 23388
Satellite: ISS
Catalog Number: 25544
Epoch time: 16287
48979343 = yrday
fracday
Element set: 911
Inclination: 51
6425 deg
RA of node: 187
9665 deg
Eccentricity:
0006931
Arg of perigee: 65
7496 deg
Mean anomaly: 294
4380 deg
Mean motion: 15
54170664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2338
Checksum: 352
Coasting Arc #13 (Orbit 2342)
---------------------------------------
Vector Time (GMT): 2016/287/18:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 907704
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5999663
36 A = 6787137
07 meter
Y = 2303968
14 meter E =
0010862
Z = -2186616
47 I = 51
61264
XDOT = -3533
411150 Wp = 102
50523
YDOT = 4026
544189 meter/sec RA = 185
37056 deg
ZDOT = -5477
674632 TA = 101
75806
MA = 101
63618
Ha = 223
347 n
mi
Hp = 212
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19683934
89 X = 5984075
66
Y = 7558950
58 feet Y = 2370972
96 meter
Z = -7173938
54 Z = -2157509
41
XDOT = -11592
556267 XDOT = -3551
565866
YDOT = 13210
446813 feet/sec YDOT = 3986
928987 meter/sec
ZDOT = -17971
373464 ZDOT = -5494
883891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4731685
25 X = 1442217
66
Y = 20591531
38 feet Y = 6276298
77 meter
Z = -7047014
33 Z = -2147929
97
XDOT = -15862
706264 XDOT = -4834
952869
YDOT = -2502
298202 feet/sec YDOT = -762
700492 meter/sec
ZDOT = -18047
218266 ZDOT = -5500
792127
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 16287
81129154
00016717 00000-0 10270-3 0 9125
2 25544 51
6399 186
3595 0006860 69
4374 290
7514 15
54207745 23435
Satellite: ISS
Catalog Number: 25544
Epoch time: 16287
81129154 = yrday
fracday
Element set: 912
Inclination: 51
6399 deg
RA of node: 186
3595 deg
Eccentricity:
0006860
Arg of perigee: 69
4374 deg
Mean anomaly: 290
7514 deg
Mean motion: 15
54207745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2343
Checksum: 334
Coasting Arc #14 (Orbit 2350)
---------------------------------------
Vector Time (GMT): 2016/288/06:36:41
000
Vector Time (MET): N/A
Weight (LBS) : 892578
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1020639
24 A = 6777614
84 meter
Y = -4193211
64 meter E =
0009672
Z = 5217627
12 I = 51
59635
XDOT = 7582
505888 Wp = 88
60715
YDOT = -482
685800 meter/sec RA = 182
91035 deg
ZDOT = 1093
804248 TA = 350
90762
MA = 350
92512
Ha = 223
394 n
mi
Hp = 212
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3348553
94 X = -999019
18
Y = -13757256
02 feet Y = -4204503
53 meter
Z = 17118199
22 Z = 5212722
11
XDOT = 24876
987822 XDOT = 7582
026546
YDOT = -1583
614831 feet/sec YDOT = -397
895663 meter/sec
ZDOT = 3588
596613 ZDOT = 1130
637590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9910879
64 X = -3020836
12
Y = 10147012
84 feet Y = 3092809
51 meter
Z = 17097375
42 Z = 5211280
03
XDOT = -13616
562279 XDOT = -4150
328183
YDOT = -19626
268135 feet/sec YDOT = -5982
086528 meter/sec
ZDOT = 3749
724979 ZDOT = 1142
916174
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 16288
32568863
00016717 00000-0 10270-3 0 9137
2 25544 51
6398 183
7990 0006881 69
0889 291
1000 15
54182773 23511
Satellite: ISS
Catalog Number: 25544
Epoch time: 16288
32568863 = yrday
fracday
Element set: 913
Inclination: 51
6398 deg
RA of node: 183
7990 deg
Eccentricity:
0006881
Arg of perigee: 69
0889 deg
Mean anomaly: 291
1000 deg
Mean motion: 15
54182773 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2351
Checksum: 342
Coasting Arc #15 (Orbit 2365)
---------------------------------------
Vector Time (GMT): 2016/289/06:36:41
000
Vector Time (MET): N/A
Weight (LBS) : 892578
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -829094
16 A = 6777408
49 meter
Y = 4204589
15 meter E =
0021032
Z = -5268605
25 I = 51
62886
XDOT = -7592
353383 Wp = 89
08846
YDOT = -411
663701 meter/sec RA = 177
90827 deg
ZDOT = 869
577527 TA = 189
22531
MA = 189
26401
Ha = 223
388 n
mi
Hp = 212
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2720125
20 X = -850456
22
Y = 13794583
82 feet Y = 4195197
53 meter
Z = -17285450
29 Z = -5272685
29
XDOT = -24909
295875 XDOT = -7591
409886
YDOT = -1350
602693 feet/sec YDOT = -496
561105 meter/sec
ZDOT = 2852
944644 ZDOT = 832
697415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13030299
07 X = 3971635
16
Y = -5221315
94 feet Y = -1591457
10 meter
Z = -17303918
10 Z = -5274234
24
XDOT = 11890
467246 XDOT = 3624
214417
YDOT = 20789
373848 feet/sec YDOT = 6336
601149 meter/sec
ZDOT = 2691
730653 ZDOT = 820
439503
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 16289
29017511
00016717 00000-0 10270-3 0 9144
2 25544 51
6406 178
9909 0006919 72
2967 287
8941 15
54188750 23665
Satellite: ISS
Catalog Number: 25544
Epoch time: 16289
29017511 = yrday
fracday
Element set: 914
Inclination: 51
6406 deg
RA of node: 178
9909 deg
Eccentricity:
0006919
Arg of perigee: 72
2967 deg
Mean anomaly: 287
8941 deg
Mean motion: 15
54188750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2366
Checksum: 353
Coasting Arc #16 (Orbit 2381)
---------------------------------------
Vector Time (GMT): 2016/290/06:36:41
000
Vector Time (MET): N/A
Weight (LBS) : 892578
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2626721
67 A = 6779511
71 meter
Y = -4086802
04 meter E =
0014486
Z = 4719319
07 I = 51
66777
XDOT = 7038
545774 Wp = 68
77987
YDOT = 1323
416709 meter/sec RA = 172
91120 deg
ZDOT = -2759
584367 TA = 48
56345
MA = 48
43909
Ha = 223
263 n
mi
Hp = 212
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8617853
24 X = 2649301
14
Y = -13408143
16 feet Y = -4057301
48 meter
Z = 15483330
28 Z = 4732134
64
XDOT = 23092
341777 XDOT = 7036
629057
YDOT = 4341
918338 feet/sec YDOT = 1402
115418 meter/sec
ZDOT = -9053
754485 ZDOT = -2725
396877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15880640
37 X = -4840419
18
Y = 305338
13 feet Y = 93067
06 meter
Z = 15539988
55 Z = 4736588
51
XDOT = -9146
546335 XDOT = -2787
867323
YDOT = -20538
113572 feet/sec YDOT = -6260
017017 meter/sec
ZDOT = -8904
438035 ZDOT = -2714
072713
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 16290
31895165
00016717 00000-0 10270-3 0 9159
2 25544 51
6398 173
8621 0006865 75
1302 285
0610 15
54224517 23828
Satellite: ISS
Catalog Number: 25544
Epoch time: 16290
31895165 = yrday
fracday
Element set: 915
Inclination: 51
6398 deg
RA of node: 173
8621 deg
Eccentricity:
0006865
Arg of perigee: 75
1302 deg
Mean anomaly: 285
0610 deg
Mean motion: 15
54224517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2382
Checksum: 311
Coasting Arc #17 (Orbit 2396)
---------------------------------------
Vector Time (GMT): 2016/291/06:36:41
000
Vector Time (MET): N/A
Weight (LBS) : 892578
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4167179
29 A = 6783203
04 meter
Y = 3877976
44 meter E =
0012357
Z = -3699462
44 I = 51
71151
XDOT = -5910
091964 Wp = 89
55179
YDOT = -2231
685812 meter/sec RA = 167
92522 deg
ZDOT = 4330
526581 TA = 226
48021
MA = 226
58296
Ha = 223
323 n
mi
Hp = 211
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13671848
05 X = -4192263
23
Y = 12723019
80 feet Y = 3831235
65 meter
Z = -12137343
98 Z = -3719767
37
XDOT = -19390
065498 XDOT = -5905
733813
YDOT = -7321
803846 feet/sec YDOT = -2297
751660 meter/sec
ZDOT = 14207
764372 ZDOT = 4301
826878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18184688
13 X = 5542692
94
Y = 3991712
80 feet Y = 1216674
06 meter
Z = -12226738
22 Z = -3726709
81
XDOT = 5297
915278 XDOT = 1614
804577
YDOT = 18874
366324 feet/sec YDOT = 5752
906856 meter/sec
ZDOT = 14082
573222 ZDOT = 4292
368318
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 16291
28342239
00016717 00000-0 10270-3 0 9166
2 25544 51
6394 169
0541 0006832 78
5781 281
6139 15
54212029 23973
Satellite: ISS
Catalog Number: 25544
Epoch time: 16291
28342239 = yrday
fracday
Element set: 916
Inclination: 51
6394 deg
RA of node: 169
0541 deg
Eccentricity:
0006832
Arg of perigee: 78
5781 deg
Mean anomaly: 281
6139 deg
Mean motion: 15
54212029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2397
Checksum: 323
Coasting Arc #18 (Orbit 2412)
---------------------------------------
Vector Time (GMT): 2016/292/06:36:41
000
Vector Time (MET): N/A
Weight (LBS) : 892578
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5373936
44 A = 6786827
84 meter
Y = -3482179
86 meter E =
0020195
Z = 2224894
08 I = 51
75613
XDOT = 4340
474356 Wp = 100
00046
YDOT = 3178
578955 meter/sec RA = 162
95107 deg
ZDOT = -5470
279596 TA = 55
29811
MA = 55
10802
Ha = 223
264 n
mi
Hp = 211
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17631025
07 X = 5401667
80
Y = -11424474
60 feet Y = -3421929
69 meter
Z = 7299521
27 Z = 2251067
59
XDOT = 14240
401430 XDOT = 4331
181029
YDOT = 10428
408644 feet/sec YDOT = 3227
064721 meter/sec
ZDOT = -17947
111534 ZDOT = -5449
216902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19511145
26 X = -5946997
07
Y = -7680784
23 feet Y = -2341103
03 meter
Z = 7414542
47 Z = 2259952
55
XDOT = -408
465280 XDOT = -124
500217
YDOT = -16319
804623 feet/sec YDOT = -4974
276449 meter/sec
ZDOT = -17855
459209 ZDOT = -5442
343967
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 16292
31218134
00016717 00000-0 10270-3 0 9178
2 25544 51
6403 163
9243 0006811 82
0799 278
1127 15
54245568 24133
Satellite: ISS
Catalog Number: 25544
Epoch time: 16292
31218134 = yrday
fracday
Element set: 917
Inclination: 51
6403 deg
RA of node: 163
9243 deg
Eccentricity:
0006811
Arg of perigee: 82
0799 deg
Mean anomaly: 278
1127 deg
Mean motion: 15
54245568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2413
Checksum: 305
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