[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 2nd 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 107 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 032 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
There are no maneuvers
Coasting Arc #1 (Orbit 2371)
---------------------------------------
Vector Time (GMT): 2016/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2798716
06 A = 6781025
59 meter
Y = -4507101
28 meter E =
0014870
Z = -4238856
09 I = 51
75893
XDOT = 6689
969153 Wp = 67
32117
YDOT = -724
508453 meter/sec RA = 19
13639 deg
ZDOT = -3651
344455 TA = 165
31053
MA = 165
26727
Ha = 223
005 n
mi
Hp = 211
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9182139
29 X = -2727518
19
Y = -14787077
70 feet Y = -4538000
41 meter
Z = -13907008
17 Z = -4252278
37
XDOT = 21948
717693 XDOT = 6715
310064
YDOT = -2376
996237 feet/sec YDOT = -649
555200 meter/sec
ZDOT = -11979
476558 ZDOT = -3618
785001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5399836
08 X = 1645870
04
Y = -16498929
02 feet Y = -5028873
57 meter
Z = -13964287
91 Z = -4256314
95
XDOT = 14854
116220 XDOT = 4527
534624
YDOT = 14868
212851 feet/sec YDOT = 4531
831277 meter/sec
ZDOT = -11838
134551 ZDOT = -3608
263411
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 16032
52271268
00016717 00000-0 10270-3 0 9002
2 25544 51
6398 19
5719 0006696 65
2884 294
8965 15
54349381 23726
Satellite: ISS
Catalog Number: 25544
Epoch time: 16032
52271268 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 19
5719 deg
Eccentricity:
0006696
Arg of perigee: 65
2884 deg
Mean anomaly: 294
8965 deg
Mean motion: 15
54349381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2372
Checksum: 342
Coasting Arc #2 (Orbit 2387)
---------------------------------------
Vector Time (GMT): 2016/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1056626
18 A = 6777703
15 meter
Y = 4380129
11 meter E =
0010607
Z = 5054120
79 I = 51
71734
XDOT = -7438
410302 Wp = 92
65971
YDOT = -359
046003 meter/sec RA = 14
14745 deg
ZDOT = 1862
407615 TA = 339
31524
MA = 339
35814
Ha = 222
938 n
mi
Hp = 211
988
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3466621
32 X = 983017
47
Y = 14370502
32 feet Y = 4391533
52 meter
Z = 16581761
11 Z = 5059074
70
XDOT = -24404
233275 XDOT = -7442
889208
YDOT = -1177
972452 feet/sec YDOT = -442
252247 meter/sec
ZDOT = 6110
261204 ZDOT = 1826
263172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8584184
44 X = -2616459
42
Y = 12006568
16 feet Y = 3659601
97 meter
Z = 16602340
21 Z = 5060393
30
XDOT = -14364
855756 XDOT = -4378
408035
YDOT = -18520
171692 feet/sec YDOT = -5644
948332 meter/sec
ZDOT = 5953
602408 ZDOT = 1814
658014
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 16033
55138459
00016717 00000-0 10270-3 0 9011
2 25544 51
6396 14
4419 0006606 67
8033 292
3820 15
54379012 23884
Satellite: ISS
Catalog Number: 25544
Epoch time: 16033
55138459 = yrday
fracday
Element set: 901
Inclination: 51
6396 deg
RA of node: 14
4419 deg
Eccentricity:
0006606
Arg of perigee: 67
8033 deg
Mean anomaly: 292
3820 deg
Mean motion: 15
54379012 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2388
Checksum: 309
Coasting Arc #3 (Orbit 2402)
---------------------------------------
Vector Time (GMT): 2016/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 842569
59 A = 6776644
74 meter
Y = -4127647
05 meter E =
0021253
Z = -5326316
55 I = 51
68255
XDOT = 7533
609929 Wp = 84
93478
YDOT = 1338
682699 meter/sec RA = 9
14872 deg
ZDOT = 156
693872 TA = 186
54664
MA = 186
57445
Ha = 222
996 n
mi
Hp = 211
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2764335
93 X = 914535
98
Y = -13542149
12 feet Y = -4117822
52 meter
Z = -17474791
82 Z = -5322048
79
XDOT = 24716
568009 XDOT = 7517
319395
YDOT = 4392
003606 feet/sec YDOT = 1422
837431 meter/sec
ZDOT = 514
087508 ZDOT = 193
250254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11957745
70 X = 3644720
89
Y = -6979960
83 feet Y = -2127492
06 meter
Z = -17455433
82 Z = -5320416
23
XDOT = 12860
907674 XDOT = 3920
004659
YDOT = 20370
828963 feet/sec YDOT = 6209
028668 meter/sec
ZDOT = 672
324630 ZDOT = 204
924547
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 16034
51575412
00016717 00000-0 10270-3 0 9023
2 25544 51
6398 9
6317 0006680 71
5885 288
5994 15
54379800 24030
Satellite: ISS
Catalog Number: 25544
Epoch time: 16034
51575412 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 9
6317 deg
Eccentricity:
0006680
Arg of perigee: 71
5885 deg
Mean anomaly: 288
5994 deg
Mean motion: 15
54379800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2403
Checksum: 327
Coasting Arc #4 (Orbit 2418)
---------------------------------------
Vector Time (GMT): 2016/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2722866
62 A = 6778142
13 meter
Y = 3730411
31 meter E =
0012916
Z = 4952769
21 I = 51
65613
XDOT = -7017
073315 Wp = 65
73577
YDOT = -2229
214194 meter/sec RA = 4
14869 deg
ZDOT = -2169
065490 TA = 45
43643
MA = 45
33105
Ha = 223
022 n
mi
Hp = 211
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8933289
44 X = -2788436
70
Y = 12238882
24 feet Y = 3699595
78 meter
Z = 16249242
81 Z = 4939383
14
XDOT = -23021
894077 XDOT = -6981
087940
YDOT = -7313
694863 feet/sec YDOT = -2307
482548 meter/sec
ZDOT = -7116
356593 ZDOT = -2203
064772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15107853
86 X = -4604873
86
Y = 1804031
66 feet Y = 549868
85 meter
Z = 16190429
66 Z = 4934842
96
XDOT = -10283
058294 XDOT = -3134
276168
YDOT = -20645
050554 feet/sec YDOT = -6292
611409 meter/sec
ZDOT = -7263
317463 ZDOT = -2213
859163
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 16035
54440296
00016717 00000-0 10270-3 0 9039
2 25544 51
6398 4
5012 0006616 74
5780 285
6103 15
54413483 24195
Satellite: ISS
Catalog Number: 25544
Epoch time: 16035
54440296 = yrday
fracday
Element set: 903
Inclination: 51
6398 deg
RA of node: 4
5012 deg
Eccentricity:
0006616
Arg of perigee: 74
5780 deg
Mean anomaly: 285
6103 deg
Mean motion: 15
54413483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2419
Checksum: 298
Coasting Arc #5 (Orbit 2433)
---------------------------------------
Vector Time (GMT): 2016/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4370883
98 A = 6781694
92 meter
Y = -3263663
04 meter E =
0013156
Z = -4041114
82 I = 51
63623
XDOT = 5855
359762 Wp = 92
60295
YDOT = 3010
630088 meter/sec RA = 359
15424 deg
ZDOT = 3912
182136 TA = 218
00436
MA = 218
09726
Ha = 222
989 n
mi
Hp = 211
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14340170
52 X = 4426683
85
Y = -10707555
90 feet Y = -3214472
92 meter
Z = -13258250
71 Z = -4019747
01
XDOT = 19210
497906 XDOT = 5802
255625
YDOT = 9877
395302 feet/sec YDOT = 3075
811679 meter/sec
ZDOT = 12835
243227 ZDOT = 3940
496505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17735563
00 X = 5405799
60
Y = 2864948
88 feet Y = 873236
42 meter
Z = -13164927
99 Z = -4012670
05
XDOT = 6474
436857 XDOT = 1973
408354
YDOT = 19302
791908 feet/sec YDOT = 5883
490974 meter/sec
ZDOT = 12957
390587 ZDOT = 3949
412651
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16036
50875035
00016717 00000-0 10270-3 0 9040
2 25544 51
6401 359
6913 0006647 77
6908 282
4989 15
54409112 24342
Satellite: ISS
Catalog Number: 25544
Epoch time: 16036
50875035 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 359
6913 deg
Eccentricity:
0006647
Arg of perigee: 77
6908 deg
Mean anomaly: 282
4989 deg
Mean motion: 15
54409112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2434
Checksum: 326
Coasting Arc #6 (Orbit 2449)
---------------------------------------
Vector Time (GMT): 2016/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5664176
29 A = 6785591
99 meter
Y = 2655365
92 meter E =
0019945
Z = 2608514
08 I = 51
61828
XDOT = -4179
904860 Wp = 95
79390
YDOT = -3741
385613 meter/sec RA = 354
16853 deg
ZDOT = -5235
281003 TA = 54
80210
MA = 54
61549
Ha = 222
962 n
mi
Hp = 211
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18583255
55 X = -5706119
04
Y = 8711830
44 feet Y = 2591790
86 meter
Z = 8558117
06 Z = 2580897
63
XDOT = -13713
598621 XDOT = -4112
326920
YDOT = -12274
887181 feet/sec YDOT = -3787
750285 meter/sec
ZDOT = -17176
118777 ZDOT = -5255
421316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19366496
83 X = -5902908
23
Y = -6943814
20 feet Y = -2116474
57 meter
Z = 8437830
84 Z = 2571850
84
XDOT = -1514
684443 XDOT = -461
675818
YDOT = -16883
620848 feet/sec YDOT = -5146
127634 meter/sec
ZDOT = -17262
673739 ZDOT = -5261
662956
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16037
53737590
00016717 00000-0 10270-3 0 9058
2 25544 51
6407 354
5603 0006640 81
2756 278
9148 15
54450270 24509
Satellite: ISS
Catalog Number: 25544
Epoch time: 16037
53737590 = yrday
fracday
Element set: 905
Inclination: 51
6407 deg
RA of node: 354
5603 deg
Eccentricity:
0006640
Arg of perigee: 81
2756 deg
Mean anomaly: 278
9148 deg
Mean motion: 15
54450270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2450
Checksum: 311
Coasting Arc #7 (Orbit 2464)
---------------------------------------
Vector Time (GMT): 2016/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6426185
77 A = 6788010
92 meter
Y = -1969358
34 meter E =
0015432
Z = -919952
16 I = 51
59506
XDOT = 2172
879777 Wp = 56
67924
YDOT = 4362
489173 meter/sec RA = 349
19096 deg
ZDOT = 5919
517015 TA = 293
35553
MA = 293
51780
Ha = 222
912 n
mi
Hp = 211
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21083286
65 X = 6452198
64
Y = -6461149
42 feet Y = -1897351
05 meter
Z = -3018215
75 Z = -888672
89
XDOT = 7128
870661 XDOT = 2095
182095
YDOT = 14312
628519 feet/sec YDOT = 4386
353490 meter/sec
ZDOT = 19420
987581 ZDOT = 5929
883223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19703977
37 X = 6005772
30
Y = 9940185
10 feet Y = 3029768
42 meter
Z = -2882195
34 Z = -878493
14
XDOT = -4126
015483 XDOT = -1257
609519
YDOT = 13743
026122 feet/sec YDOT = 4188
874362 meter/sec
ZDOT = 19465
039464 ZDOT = 5932
944029
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16038
50170087
00016717 00000-0 10270-3 0 9069
2 25544 51
6409 349
7507 0006614 85
1190 275
0717 15
54467909 24659
Satellite: ISS
Catalog Number: 25544
Epoch time: 16038
50170087 = yrday
fracday
Element set: 906
Inclination: 51
6409 deg
RA of node: 349
7507 deg
Eccentricity:
0006614
Arg of perigee: 85
1190 deg
Mean anomaly: 275
0717 deg
Mean motion: 15
54467909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2465
Checksum: 322
Coasting Arc #8 (Orbit 2480)
---------------------------------------
Vector Time (GMT): 2016/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6628616
35 A = 6787879
69 meter
Y = 1096717
78 meter E =
0014713
Z = -942333
17 I = 51
56483
XDOT = 21
899338 Wp = 119
96126
YDOT = -4881
645682 meter/sec RA = 344
21487 deg
ZDOT = -5911
861060 TA = 70
25231
MA = 70
09369
Ha = 222
809 n
mi
Hp = 211
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21747428
98 X = -6635810
14
Y = 3598155
46 feet Y = 1022551
93 meter
Z = -3091644
25 Z = -974550
03
XDOT = 71
848223 XDOT = 105
202019
YDOT = -16015
897908 feet/sec YDOT = -4880
935312 meter/sec
ZDOT = -19395
869620 ZDOT = -5911
552111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18384556
53 X = -5603612
83
Y = -12125215
77 feet Y = -3695765
77 meter
Z = -3231544
20 Z = -984974
67
XDOT = 10144
724402 XDOT = 3092
111998
YDOT = -10276
939453 feet/sec YDOT = -3132
411145 meter/sec
ZDOT = -19393
537901 ZDOT = -5911
150352
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16039
53030266
00016717 00000-0 10270-3 0 9078
2 25544 51
6421 344
6197 0006569 88
4515 271
7391 15
54484199 24817
Satellite: ISS
Catalog Number: 25544
Epoch time: 16039
53030266 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 344
6197 deg
Eccentricity:
0006569
Arg of perigee: 88
4515 deg
Mean anomaly: 271
7391 deg
Mean motion: 15
54484199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2481
Checksum: 329
Coasting Arc #9 (Orbit 2496)
---------------------------------------
Vector Time (GMT): 2016/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6241785
58 A = 6785201
34 meter
Y = -126147
89 meter E =
0019967
Z = 2636431
35 I = 51
52560
XDOT = -2107
667347 Wp = 82
17757
YDOT = 5226
372030 meter/sec RA = 339
23299 deg
ZDOT = 5208
841446 TA = 307
61882
MA = 307
79989
Ha = 222
741 n
mi
Hp = 211
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20478299
16 X = 6229925
97
Y = -413871
02 feet Y = -56414
23 meter
Z = 8649709
17 Z = 2666722
84
XDOT = -6914
919117 XDOT = -2191
254972
YDOT = 17146
889861 feet/sec YDOT = 5202
335698 meter/sec
ZDOT = 17089
374823 ZDOT = 5198
399790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15494344
59 X = 4722676
23
Y = 13310439
92 feet Y = 4057022
09 meter
Z = 8781057
40 Z = 2676466
30
XDOT = -15699
236832 XDOT = -4785
127386
YDOT = 6965
141584 feet/sec YDOT = 2122
975155 meter/sec
ZDOT = 17043
052866 ZDOT = 5194
722514
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16040
55889203
00016717 00000-0 10270-3 0 9086
2 25544 51
6421 339
4896 0006554 92
3547 267
8356 15
54504521 24974
Satellite: ISS
Catalog Number: 25544
Epoch time: 16040
55889203 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 339
4896 deg
Eccentricity:
0006554
Arg of perigee: 92
3547 deg
Mean anomaly: 267
8356 deg
Mean motion: 15
54504521 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2497
Checksum: 334
Coasting Arc #10 (Orbit 2511)
---------------------------------------
Vector Time (GMT): 2016/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5335171
81 A = 6781016
47 meter
Y = -1023510
78 meter E =
0013684
Z = -4071534
66 I = 51
48284
XDOT = 3950
961124 Wp = 81
95059
YDOT = -5310
529081 meter/sec RA = 334
23788 deg
ZDOT = -3851
452101 TA = 148
09104
MA = 148
00808
Ha = 222
738 n
mi
Hp = 211
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17503844
53 X = -5303552
81
Y = -3357975
00 feet Y = -1082995
77 meter
Z = -13358053
33 Z = -4097374
13
XDOT = 12962
470878 XDOT = 4028
759421
YDOT = -17422
995671 feet/sec YDOT = -5265
912153 meter/sec
ZDOT = -12635
997707 ZDOT = -3832
070319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10981060
27 X = -3347027
17
Y = -13931161
18 feet Y = -4246217
93 meter
Z = -13469863
46 Z = -4105614
38
XDOT = 20246
201205 XDOT = 6171
042127
YDOT = -3852
578921 feet/sec YDOT = -1174
266055 meter/sec
ZDOT = -12550
914008 ZDOT = -3825
518590
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16041
52318342
00016717 00000-0 10270-3 0 9096
2 25544 51
6426 334
6793 0006570 95
2754 264
9149 15
54533311 25127
Satellite: ISS
Catalog Number: 25544
Epoch time: 16041
52318342 = yrday
fracday
Element set: 909
Inclination: 51
6426 deg
RA of node: 334
6793 deg
Eccentricity:
0006570
Arg of perigee: 95
2754 deg
Mean anomaly: 264
9149 deg
Mean motion: 15
54533311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2512
Checksum: 307
Coasting Arc #11 (Orbit 2527)
---------------------------------------
Vector Time (GMT): 2016/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4026479
06 A = 6777416
44 meter
Y = 2215598
50 meter E =
0012134
Z = 4972706
72 I = 51
44247
XDOT = -5356
766216 Wp = 110
90720
YDOT = 5098
262413 meter/sec RA = 329
22987 deg
ZDOT = 2057
604772 TA = 319
00020
MA = 319
09136
Ha = 222
528 n
mi
Hp = 211
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13210233
15 X = 3977249
60
Y = 7269023
96 feet Y = 2260350
48 meter
Z = 16314654
58 Z = 4992146
21
XDOT = -17574
692309 XDOT = -5423
372903
YDOT = 16726
582719 feet/sec YDOT = 5037
987277 meter/sec
ZDOT = 6750
671825 ZDOT = 2031
421144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5401952
26 X = 1646515
05
Y = 13979474
62 feet Y = 4260943
86 meter
Z = 16398479
33 Z = 4998256
50
XDOT = -23224
618797 XDOT = -7078
863809
YDOT = 1158
154506 feet/sec YDOT = 353
005494 meter/sec
ZDOT = 6636
159052 ZDOT = 2022
701279
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16042
55174791
00016717 00000-0 10270-3 0 9100
2 25544 51
6423 329
5492 0006435 100
1758 260
0121 15
54569792 25289
Satellite: ISS
Catalog Number: 25544
Epoch time: 16042
55174791 = yrday
fracday
Element set: 910
Inclination: 51
6423 deg
RA of node: 329
5492 deg
Eccentricity:
0006435
Arg of perigee: 100
1758 deg
Mean anomaly: 260
0121 deg
Mean motion: 15
54569792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2528
Checksum: 303
Coasting Arc #12 (Orbit 2542)
---------------------------------------
Vector Time (GMT): 2016/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2465970
84 A = 6776107
21 meter
Y = -3443538
44 meter E =
0021277
Z = -5307718
06 I = 51
41105
XDOT = 6213
411690 Wp = 93
71066
YDOT = -4468
615364 meter/sec RA = 324
21055 deg
ZDOT = 11
079090 TA = 176
40311
MA = 176
38779
Ha = 222
676 n
mi
Hp = 211
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8090455
50 X = -2401498
81
Y = -11297698
28 feet Y = -3470754
58 meter
Z = -17413773
15 Z = -5319540
04
XDOT = 20385
208956 XDOT = 6262
865243
YDOT = -14660
811561 feet/sec YDOT = -4398
856361 meter/sec
ZDOT = 36
348721 ZDOT = 41
382406
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 878192
23 X = 267672
99
Y = -13804301
81 feet Y = -4207551
19 meter
Z = -17464334
57 Z = -5323129
18
XDOT = 24064
770594 XDOT = 7334
942077
YDOT = 1312
237128 feet/sec YDOT = 399
969877 meter/sec
ZDOT = 168
580486 ZDOT = 51
383332
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16043
51601831
00016717 00000-0 10270-3 0 9118
2 25544 51
6426 324
7384 0006501 102
6326 257
5555 15
54559800 25439
Satellite: ISS
Catalog Number: 25544
Epoch time: 16043
51601831 = yrday
fracday
Element set: 911
Inclination: 51
6426 deg
RA of node: 324
7384 deg
Eccentricity:
0006501
Arg of perigee: 102
6326 deg
Mean anomaly: 257
5555 deg
Mean motion: 15
54559800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2543
Checksum: 291
Coasting Arc #13 (Orbit 2558)
---------------------------------------
Vector Time (GMT): 2016/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 808925
14 A = 6777482
85 meter
Y = 4535908
90 meter E =
0011495
Z = 4961136
20 I = 51
39006
XDOT = -6535
580015 Wp = 81
58061
YDOT = 3447
810024 meter/sec RA = 319
19033 deg
ZDOT = -2080
863893 TA = 28
74820
MA = 28
68489
Ha = 222
547 n
mi
Hp = 211
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2653953
87 X = 734044
57
Y = 14881590
89 feet Y = 4544536
58 meter
Z = 16276693
56 Z = 4964883
45
XDOT = -21442
191649 XDOT = -6563
540713
YDOT = 11311
712678 feet/sec YDOT = 3374
568319 meter/sec
ZDOT = -6826
981276 ZDOT = -2112
679959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7126257
11 X = -2172083
17
Y = 13312466
47 feet Y = 4057639
78 meter
Z = 16292043
10 Z = 4965814
74
XDOT = -22863
649926 XDOT = -6968
840498
YDOT = -3691
282389 feet/sec YDOT = -1125
102872 meter/sec
ZDOT = -6965
557574 ZDOT = -2123
101948
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16044
54455988
00016717 00000-0 10270-3 0 9123
2 25544 51
6421 319
6077 0006420 106
0888 254
0972 15
54593194 25593
Satellite: ISS
Catalog Number: 25544
Epoch time: 16044
54455988 = yrday
fracday
Element set: 912
Inclination: 51
6421 deg
RA of node: 319
6077 deg
Eccentricity:
0006420
Arg of perigee: 106
0888 deg
Mean anomaly: 254
0972 deg
Mean motion: 15
54593194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2559
Checksum: 330
Coasting Arc #14 (Orbit 2573)
---------------------------------------
Vector Time (GMT): 2016/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 756652
05 A = 6781081
38 meter
Y = -5406540
52 meter E =
0013513
Z = -4036724
52 I = 51
37904
XDOT = 6284
083306 Wp = 108
45805
YDOT = -2015
350765 meter/sec RA = 314
17520 deg
ZDOT = 3883
663917 TA = 201
99132
MA = 202
04936
Ha = 222
565 n
mi
Hp = 211
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2482454
24 X = 836661
57
Y = -17737993
82 feet Y = -5397632
06 meter
Z = -13243846
85 Z = -4032854
22
XDOT = 20617
071213 XDOT = 6287
287430
YDOT = -6612
043193 feet/sec YDOT = -1945
059790 meter/sec
ZDOT = 12741
679518 ZDOT = 3914
198041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12703005
48 X = 3871876
07
Y = -12645341
99 feet Y = -3854300
24 meter
Z = -13226014
56 Z = -4031289
24
XDOT = 19469
194344 XDOT = 5934
210436
YDOT = 6114
794414 feet/sec YDOT = 1863
789337 meter/sec
ZDOT = 12874
411267 ZDOT = 3924
120554
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16045
50880741
00016717 00000-0 10270-3 0 9130
2 25544 51
6426 314
7967 0006454 109
6804 250
5046 15
54599406 25748
Satellite: ISS
Catalog Number: 25544
Epoch time: 16045
50880741 = yrday
fracday
Element set: 913
Inclination: 51
6426 deg
RA of node: 314
7967 deg
Eccentricity:
0006454
Arg of perigee: 109
6804 deg
Mean anomaly: 250
5046 deg
Mean motion: 15
54599406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2574
Checksum: 322
Coasting Arc #15 (Orbit 2589)
---------------------------------------
Vector Time (GMT): 2016/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2151878
42 A = 6785219
98 meter
Y = 5889358
50 meter E =
0020089
Z = 2567395
76 I = 51
37090
XDOT = -5603
610944 Wp = 106
72633
YDOT = 248
994424 meter/sec RA = 309
17099 deg
ZDOT = -5239
512355 TA = 44
25761
MA = 44
09713
Ha = 222
568 n
mi
Hp = 211
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7059968
57 X = -2230045
92
Y = 19322042
32 feet Y = 5864857
85 meter
Z = 8423214
43 Z = 2556752
40
XDOT = -18384
550342 XDOT = -5580
527767
YDOT = 816
910841 feet/sec YDOT = 186
459907 meter/sec
ZDOT = -17190
001165 ZDOT = -5266
676950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17094794
67 X = -5210493
42
Y = 11478094
32 feet Y = 3498523
15 meter
Z = 8375939
54 Z = 2552986
37
XDOT = -14441
979819 XDOT = -4401
915449
YDOT = -8810
703316 feet/sec YDOT = -2685
502371 meter/sec
ZDOT = -17307
781141 ZDOT = -5275
411692
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 16046
53732692
00016717 00000-0 10270-3 0 9146
2 25544 51
6424 309
6653 0006494 113
9157 246
2677 15
54591885 25907
Satellite: ISS
Catalog Number: 25544
Epoch time: 16046
53732692 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 309
6653 deg
Eccentricity:
0006494
Arg of perigee: 113
9157 deg
Mean anomaly: 246
2677 deg
Mean motion: 15
54591885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2590
Checksum: 337
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