[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 30th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 28524 36 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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 2269)
---------------------------------------
Vector Time (GMT): 2014/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1844882
46 A = 6797228
92 meter
Y = 5793147
03 meter E =
0007865
Z = -3041064
33 I = 52
00982
XDOT = -4268
836439 Wp = 63
28533
YDOT = 3961
873860 meter/sec RA = 95
33060 deg
ZDOT = 4970
882420 TA = 262
13031
MA = 262
21960
Ha = 228
497 n
mi
Hp = 220
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6052763
98 X = 1794737
51
Y = 19006387
91 feet Y = 5813497
03 meter
Z = -9977245
19 Z = -3032224
55
XDOT = -14005
368894 XDOT = -4336
968630
YDOT = 12998
273818 feet/sec YDOT = 3913
756514 meter/sec
ZDOT = 16308
669357 ZDOT = 4949
979203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1870278
12 X = 570060
77
Y = -19877407
23 feet Y = -6058633
73 meter
Z = -9940568
20 Z = -3029885
19
XDOT = 16639
890036 XDOT = 5071
838483
YDOT = -6523
437012 feet/sec YDOT = -1988
343601 meter/sec
ZDOT = 16219
071585 ZDOT = 4943
573019
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 14241
50620882
00016717 00000-0 10270-3 0 9000
2 25544 51
6440 96
1823 0003434 53
3543 306
7923 15
50086510 22700
Satellite: ISS
Catalog Number: 25544
Epoch time: 14241
50620882 = yrday
fracday
Element set: 900
Inclination: 51
6440 deg
RA of node: 96
1823 deg
Eccentricity:
0003434
Arg of perigee: 53
3543 deg
Mean anomaly: 306
7923 deg
Mean motion: 15
50086510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2270
Checksum: 274
Coasting Arc #2 (Orbit 2285)
---------------------------------------
Vector Time (GMT): 2014/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2068514
94 A = 6797834
71 meter
Y = -5878085
86 meter E =
0016068
Z = 2701657
62 I = 52
01487
XDOT = 4096
012889 Wp = 92
66437
YDOT = -3848
294050 meter/sec RA = 90
40133 deg
ZDOT = -5210
814051 TA = 57
02519
MA = 56
87083
Ha = 228
409 n
mi
Hp = 219
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6786466
33 X = -2015754
87
Y = -19285058
59 feet Y = -5900922
09 meter
Z = 8863706
10 Z = 2691737
75
XDOT = 13438
362498 XDOT = 4164
053422
YDOT = -12625
636646 feet/sec YDOT = -3802
109817 meter/sec
ZDOT = -17095
846624 ZDOT = -5190
750600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -960846
45 X = -292866
00
Y = 20439567
54 feet Y = 6229980
19 meter
Z = 8822457
06 Z = 2689084
91
XDOT = -15825
147307 XDOT = -4823
504899
YDOT = 6635
050699 feet/sec YDOT = 2022
363453 meter/sec
ZDOT = -17009
832368 ZDOT = -5184
596906
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 14242
53771354
00016717 00000-0 10270-3 0 9016
2 25544 51
6443 91
0708 0003486 54
5282 305
6194 15
50162387 22861
Satellite: ISS
Catalog Number: 25544
Epoch time: 14242
53771354 = yrday
fracday
Element set: 901
Inclination: 51
6443 deg
RA of node: 91
0708 deg
Eccentricity:
0003486
Arg of perigee: 54
5282 deg
Mean anomaly: 305
6194 deg
Mean motion: 15
50162387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2286
Checksum: 301
Coasting Arc #3 (Orbit 2300)
---------------------------------------
Vector Time (GMT): 2014/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2335384
37 A = 6798533
03 meter
Y = 5922083
97 meter E =
0008956
Z = -2382605
59 I = 52
01518
XDOT = -3941
859065 Wp = 50
98410
YDOT = 3722
898427 meter/sec RA = 85
47115 deg
ZDOT = 5408
806303 TA = 282
60958
MA = 282
70973
Ha = 228
409 n
mi
Hp = 219
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7662022
22 X = 2280562
64
Y = 19429409
34 feet Y = 5947893
04 meter
Z = -7816947
46 Z = -2371394
22
XDOT = -12932
608480 XDOT = -4009
470669
YDOT = 12214
233684 feet/sec YDOT = 3678
440388 meter/sec
ZDOT = 17745
427503 ZDOT = 5389
492785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -148474
53 X = -45255
04
Y = -20902507
65 feet Y = -6371084
33 meter
Z = -7770220
63 Z = -2368363
25
XDOT = 15059
302522 XDOT = 4590
075409
YDOT = -6649
378552 feet/sec YDOT = -2026
730583 meter/sec
ZDOT = 17662
616240 ZDOT = 5383
565430
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 14243
50472877
00016717 00000-0 10270-3 0 9023
2 25544 51
6431 86
2778 0003350 59
5359 300
6122 15
50154967 23010
Satellite: ISS
Catalog Number: 25544
Epoch time: 14243
50472877 = yrday
fracday
Element set: 902
Inclination: 51
6431 deg
RA of node: 86
2778 deg
Eccentricity:
0003350
Arg of perigee: 59
5359 deg
Mean anomaly: 300
6122 deg
Mean motion: 15
50154967 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2301
Checksum: 297
Coasting Arc #4 (Orbit 2316)
---------------------------------------
Vector Time (GMT): 2014/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2571666
79 A = 6799017
86 meter
Y = -5962657
77 meter E =
0016190
Z = 1993863
73 I = 52
01475
XDOT = 3845
085888 Wp = 102
39705
YDOT = -3543
580708 meter/sec RA = 80
54249 deg
ZDOT = -5602
832905 TA = 55
73834
MA = 55
58512
Ha = 228
285 n
mi
Hp = 219
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8437226
99 X = -2514485
39
Y = -19562525
48 feet Y = -5991095
96 meter
Z = 6541547
69 Z = 1981510
20
XDOT = 12615
111182 XDOT = 3911
642025
YDOT = -11625
920958 feet/sec YDOT = -3500
210686 meter/sec
ZDOT = -18381
997719 ZDOT = -5583
992130
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1181602
11 X = 360152
32
Y = 21287438
90 feet Y = 6488411
38 meter
Z = 6489977
68 Z = 1978145
20
XDOT = -14416
466231 XDOT = -4394
138907
YDOT = 6414
963039 feet/sec YDOT = 1955
280734 meter/sec
ZDOT = -18301
219029 ZDOT = -5578
211560
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 14244
53618591
00016717 00000-0 10270-3 0 9033
2 25544 51
6436 81
1662 0003381 59
5407 300
6078 15
50236830 23176
Satellite: ISS
Catalog Number: 25544
Epoch time: 14244
53618591 = yrday
fracday
Element set: 903
Inclination: 51
6436 deg
RA of node: 81
1662 deg
Eccentricity:
0003381
Arg of perigee: 59
5407 deg
Mean anomaly: 300
6078 deg
Mean motion: 15
50236830 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2317
Checksum: 293
Coasting Arc #5 (Orbit 2331)
---------------------------------------
Vector Time (GMT): 2014/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2841544
81 A = 6799596
77 meter
Y = 5954802
10 meter E =
0010957
Z = -1629622
51 I = 52
00941
XDOT = -3774
717988 Wp = 46
09185
YDOT = 3366
954751 meter/sec RA = 75
61236 deg
ZDOT = 5752
667474 TA = 296
19527
MA = 296
30789
Ha = 228
325 n
mi
Hp = 219
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9322653
56 X = 2782661
82
Y = 19536752
30 feet Y = 5986248
77 meter
Z = -5346530
54 Z = -1615962
03
XDOT = -12384
245367 XDOT = -3840
032078
YDOT = 11046
439473 feet/sec YDOT = 3324
378513 meter/sec
ZDOT = 18873
580952 ZDOT = 5734
171640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2384776
65 X = -726879
92
Y = -21529444
14 feet Y = -6562174
57 meter
Z = -5289406
77 Z = -1612211
18
XDOT = 13878
405939 XDOT = 4230
138130
YDOT = -6129
136197 feet/sec YDOT = -1868
160713 meter/sec
ZDOT = 18794
291263 ZDOT = 5728
499977
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 14245
50315679
00016717 00000-0 10270-3 0 9043
2 25544 51
6425 76
3729 0003311 66
4763 293
6736 15
50225496 23324
Satellite: ISS
Catalog Number: 25544
Epoch time: 14245
50315679 = yrday
fracday
Element set: 904
Inclination: 51
6425 deg
RA of node: 76
3729 deg
Eccentricity:
0003311
Arg of perigee: 66
4763 deg
Mean anomaly: 293
6736 deg
Mean motion: 15
50225496 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2332
Checksum: 311
Coasting Arc #6 (Orbit 2347)
---------------------------------------
Vector Time (GMT): 2014/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3071680
10 A = 6799860
17 meter
Y = -5940673
76 meter E =
0015739
Z = 1195147
81 I = 52
00290
XDOT = 3769
326995 Wp = 111
76451
YDOT = -3144
198191 meter/sec RA = 70
68337 deg
ZDOT = -5884
757704 TA = 55
33639
MA = 55
18815
Ha = 228
173 n
mi
Hp = 219
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10077690
61 X = -3010827
44
Y = -19490399
46 feet Y = -5974682
97 meter
Z = 3921088
61 Z = 1180374
16
XDOT = 12366
558384 XDOT = 3832
792134
YDOT = -10315
610863 feet/sec YDOT = -3101
692545 meter/sec
ZDOT = -19306
947849 ZDOT = -5866
292638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3477646
58 X = 1059986
68
Y = 21675395
09 feet Y = 6606660
42 meter
Z = 3859232
70 Z = 1176294
13
XDOT = -13513
592574 XDOT = -4118
943017
YDOT = 5625
037099 feet/sec YDOT = 1714
511308 meter/sec
ZDOT = -19227
819271 ZDOT = -5860
639314
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 14246
53456539
00016717 00000-0 10270-3 0 9059
2 25544 51
6429 71
2610 0003331 65
4315 294
7183 15
50313522 23488
Satellite: ISS
Catalog Number: 25544
Epoch time: 14246
53456539 = yrday
fracday
Element set: 905
Inclination: 51
6429 deg
RA of node: 71
2610 deg
Eccentricity:
0003331
Arg of perigee: 65
4315 deg
Mean anomaly: 294
7183 deg
Mean motion: 15
50313522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2348
Checksum: 291
Coasting Arc #7 (Orbit 2362)
---------------------------------------
Vector Time (GMT): 2014/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3323254
56 A = 6800225
43 meter
Y = 5874210
29 meter E =
0013233
Z = -790337
85 I = 51
99200
XDOT = -3794
192327 Wp = 47
77075
YDOT = 2940
223253 meter/sec RA = 65
75246 deg
ZDOT = 5971
713415 TA = 303
74063
MA = 303
86666
Ha = 228
242 n
mi
Hp = 219
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10903066
13 X = 3261159
97
Y = 19272343
46 feet Y = 5911025
84 meter
Z = -2592971
94 Z = -774345
17
XDOT = -12448
137557 XDOT = -3855
797019
YDOT = 9646
401749 feet/sec YDOT = 2897
449970 meter/sec
ZDOT = 19592
235612 ZDOT = 5953
132144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4694826
86 X = -1430983
23
Y = -21647214
49 feet Y = -6598070
98 meter
Z = -2525922
10 Z = -769901
06
XDOT = 13292
924100 XDOT = 4051
683266
YDOT = -5131
337920 feet/sec YDOT = -1564
031798 meter/sec
ZDOT = 19512
641276 ZDOT = 5947
453061
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 14247
50149062
00016717 00000-0 10270-3 0 9068
2 25544 51
6420 66
4675 0003329 73
8618 286
2899 15
50300755 23633
Satellite: ISS
Catalog Number: 25544
Epoch time: 14247
50149062 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 66
4675 deg
Eccentricity:
0003329
Arg of perigee: 73
8618 deg
Mean anomaly: 286
2899 deg
Mean motion: 15
50300755 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2363
Checksum: 315
Coasting Arc #8 (Orbit 2378)
---------------------------------------
Vector Time (GMT): 2014/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3523278
17 A = 6800184
30 meter
Y = -5801208
00 meter E =
0014601
Z = 317131
92 I = 51
97913
XDOT = 3887
296969 Wp = 119
99814
YDOT = -2701
200557 meter/sec RA = 60
82183 deg
ZDOT = -6025
201332 TA = 56
60531
MA = 56
46571
Ha = 228
082 n
mi
Hp = 219
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11559311
59 X = -3459686
38
Y = -19032834
65 feet Y = -5840251
99 meter
Z = 1040459
07 Z = 300171
34
XDOT = 12753
598980 XDOT = 3946
481664
YDOT = -8862
206551 feet/sec YDOT = -2657
399729 meter/sec
ZDOT = -19767
720906 ZDOT = -6006
173692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5754161
73 X = 1753868
49
Y = 21515091
25 feet Y = 6557799
81 meter
Z = 969281
01 Z = 295436
85
XDOT = -13280
169471 XDOT = -4047
795655
YDOT = 4470
366702 feet/sec YDOT = 1362
567771 meter/sec
ZDOT = -19686
263917 ZDOT = -6000
373242
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 14248
53284935
00016717 00000-0 10270-3 0 9072
2 25544 51
6421 61
3549 0003352 72
2904 287
8612 15
50389053 23790
Satellite: ISS
Catalog Number: 25544
Epoch time: 14248
53284935 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 61
3549 deg
Eccentricity:
0003352
Arg of perigee: 72
2904 deg
Mean anomaly: 287
8612 deg
Mean motion: 15
50389053 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2379
Checksum: 316
Coasting Arc #9 (Orbit 2394)
---------------------------------------
Vector Time (GMT): 2014/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3731145
07 A = 6800228
64 meter
Y = 5676378
55 meter E =
0015258
Z = 120244
76 I = 51
96306
XDOT = -4010
139357 Wp = 53
82237
YDOT = 2496
990999 meter/sec RA = 55
88916 deg
ZDOT = 6033
959453 TA = 307
46527
MA = 307
60395
Ha = 228
141 n
mi
Hp = 219
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12241289
60 X = 3666809
09
Y = 18623289
19 feet Y = 5717742
91 meter
Z = 394503
80 Z = 138213
17
XDOT = -13156
625186 XDOT = -4067
073890
YDOT = 8192
227687 feet/sec YDOT = 2451
829178 meter/sec
ZDOT = 19796
454898 ZDOT = 6014
340533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6880614
84 X = -2097211
40
Y = -21195941
92 feet Y = -6460523
10 meter
Z = 469989
78 Z = 143252
89
XDOT = 13428
900752 XDOT = 4093
128949
YDOT = -3890
195421 feet/sec YDOT = -1185
731564 meter/sec
ZDOT = 19712
514908 ZDOT = 6008
374544
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 14249
56418456
00016717 00000-0 10270-3 0 9084
2 25544 51
6419 56
2416 0003375 81
3821 278
7712 15
50384123 23958
Satellite: ISS
Catalog Number: 25544
Epoch time: 14249
56418456 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 56
2416 deg
Eccentricity:
0003375
Arg of perigee: 81
3821 deg
Mean anomaly: 278
7712 deg
Mean motion: 15
50384123 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2395
Checksum: 316
Coasting Arc #10 (Orbit 2409)
---------------------------------------
Vector Time (GMT): 2014/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3874307
77 A = 6799838
86 meter
Y = -5548411
74 meter E =
0012714
Z = -620859
96 I = 51
94427
XDOT = 4198
069974 Wp = 125
72433
YDOT = -2271
276422 meter/sec RA = 50
95572 deg
ZDOT = -5992
431585 TA = 60
93858
MA = 60
81129
Ha = 228
002 n
mi
Hp = 219
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12710983
49 X = -3808960
30
Y = -18203450
58 feet Y = -5591371
44 meter
Z = -2036942
11 Z = -639521
24
XDOT = 13773
195453 XDOT = 4252
264828
YDOT = -7451
694299 feet/sec YDOT = -2224
028500 meter/sec
ZDOT = -19660
208611 ZDOT = -5971
906350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7793181
35 X = 2375361
68
Y = 20781609
04 feet Y = 6334234
44 meter
Z = -2115395
39 Z = -644772
52
XDOT = -13794
434942 XDOT = -4204
543770
YDOT = 3210
601066 feet/sec YDOT = 978
591205 meter/sec
ZDOT = -19572
451030 ZDOT = -5965
683074
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 14250
53103449
00016717 00000-0 10270-3 0 9097
2 25544 51
6419 51
4479 0003401 79
6932 280
4603 15
50458894 24101
Satellite: ISS
Catalog Number: 25544
Epoch time: 14250
53103449 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 51
4479 deg
Eccentricity:
0003401
Arg of perigee: 79
6932 deg
Mean anomaly: 280
4603 deg
Mean motion: 15
50458894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2410
Checksum: 302
Coasting Arc #11 (Orbit 2425)
---------------------------------------
Vector Time (GMT): 2014/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4011607
14 A = 6799464
71 meter
Y = 5373987
32 meter E =
0016620
Z = 1078581
78 I = 51
92352
XDOT = -4410
900461 Wp = 62
71795
YDOT = 2094
437304 meter/sec RA = 46
02046 deg
ZDOT = 5907
824353 TA = 308
91975
MA = 309
06781
Ha = 228
001 n
mi
Hp = 219
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13161440
75 X = 3945976
47
Y = 17631192
01 feet Y = 5418480
88 meter
Z = 3538654
14 Z = 1097909
31
XDOT = -14471
458206 XDOT = -4462
691131
YDOT = 6871
513465 feet/sec YDOT = 2044
822927 meter/sec
ZDOT = 19382
625831 ZDOT = 5886
270989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8710724
71 X = -2655028
89
Y = -20189691
37 feet Y = -6153817
93 meter
Z = 3619967
52 Z = 1103366
10
XDOT = 14313
970265 XDOT = 4362
898137
YDOT = -2681
077133 feet/sec YDOT = -817
192310 meter/sec
ZDOT = 19290
525933 ZDOT = 5879
752304
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 14251
56231650
00016717 00000-0 10270-3 0 9109
2 25544 51
6427 46
3347 0003395 88
0128 272
1411 15
50473634 24261
Satellite: ISS
Catalog Number: 25544
Epoch time: 14251
56231650 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 46
3347 deg
Eccentricity:
0003395
Arg of perigee: 88
0128 deg
Mean anomaly: 272
1411 deg
Mean motion: 15
50473634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2426
Checksum: 284
Coasting Arc #12 (Orbit 2440)
---------------------------------------
Vector Time (GMT): 2014/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4071753
92 A = 6798723
17 meter
Y = -5204253
97 meter E =
0010263
Z = -1590241
27 I = 51
89948
XDOT = 4677
539502 Wp = 125
88773
YDOT = -1910
368597 meter/sec RA = 41
08352 deg
ZDOT = -5756
592358 TA = 71
40973
MA = 71
29828
Ha = 227
908 n
mi
Hp = 219
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13358772
69 X = -4005531
29
Y = -17074324
04 feet Y = -5249416
90 meter
Z = -5217327
01 Z = -1609859
60
XDOT = 15346
258208 XDOT = 4726
517554
YDOT = -6267
613506 feet/sec YDOT = -1857
788260 meter/sec
ZDOT = -18886
457868 ZDOT = -5733
750442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9358411
96 X = 2852443
96
Y = 19533075
63 feet Y = 5953681
45 meter
Z = -5299899
29 Z = -1615409
30
XDOT = -15024
512700 XDOT = -4579
471471
YDOT = 2128
244564 feet/sec YDOT = 648
688943 meter/sec
ZDOT = -18788
910430 ZDOT = -5726
859899
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 14252
52911756
00016717 00000-0 10270-3 0 9119
2 25544 51
6429 41
5408 0003417 86
9504 273
2038 15
50523265 24418
Satellite: ISS
Catalog Number: 25544
Epoch time: 14252
52911756 = yrday
fracday
Element set: 911
Inclination: 51
6429 deg
RA of node: 41
5408 deg
Eccentricity:
0003417
Arg of perigee: 86
9504 deg
Mean anomaly: 273
2038 deg
Mean motion: 15
50523265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2441
Checksum: 291
Coasting Arc #13 (Orbit 2456)
---------------------------------------
Vector Time (GMT): 2014/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4113703
56 A = 6797890
00 meter
Y = 4998218
88 meter E =
0017022
Z = 2051203
75 I = 51
87425
XDOT = -4960
556286 Wp = 73
57564
YDOT = 1785
191178 meter/sec RA = 36
14471 deg
ZDOT = 5564
879634 TA = 309
00515
MA = 309
15661
Ha = 227
823 n
mi
Hp = 219
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13496402
77 X = 4047542
51
Y = 16398355
92 feet Y = 5043851
33 meter
Z = 6729671
10 Z = 2071026
14
XDOT = -16274
790965 XDOT = -5007
182401
YDOT = 5856
926437 feet/sec YDOT = 1729
459086 meter/sec
ZDOT = 18257
479114 ZDOT = 5540
668482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9952011
26 X = -3033373
03
Y = -18731953
04 feet Y = -5709499
29 meter
Z = 6813137
67 Z = 2076644
36
XDOT = 15857
435642 XDOT = 4833
346384
YDOT = -1782
325648 feet/sec YDOT = -543
252858 meter/sec
ZDOT = 18154
131570 ZDOT = 5533
379303
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 14253
56034477
00016717 00000-0 10270-3 0 9121
2 25544 51
6442 36
4279 0003362 93
5898 266
5637 15
50565654 24576
Satellite: ISS
Catalog Number: 25544
Epoch time: 14253
56034477 = yrday
fracday
Element set: 912
Inclination: 51
6442 deg
RA of node: 36
4279 deg
Eccentricity:
0003362
Arg of perigee: 93
5898 deg
Mean anomaly: 266
5637 deg
Mean motion: 15
50565654 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2457
Checksum: 331
Coasting Arc #14 (Orbit 2471)
---------------------------------------
Vector Time (GMT): 2014/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4069328
75 A = 6796831
47 meter
Y = -4809205
88 meter E =
0008132
Z = -2552378
73 I = 51
84547
XDOT = 5277
344389 Wp = 114
19063
YDOT = -1665
127846 meter/sec RA = 31
20340 deg
ZDOT = -5292
912549 TA = 94
33337
MA = 94
24044
Ha = 227
784 n
mi
Hp = 218
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13350816
09 X = -4002849
98
Y = -15778234
52 feet Y = -4854340
37 meter
Z = -8373945
96 Z = -2571984
93
XDOT = 17314
122011 XDOT = 5321
283354
YDOT = -5463
017868 feet/sec YDOT = -1605
868159 meter/sec
ZDOT = -17365
198653 ZDOT = -5267
168947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10231283
12 X = 3118495
10
Y = 17920048
76 feet Y = 5462030
86 meter
Z = -8456514
88 Z = -2577545
74
XDOT = -16816
549910 XDOT = -5125
684412
YDOT = 1483
760548 feet/sec YDOT = 452
250215 meter/sec
ZDOT = -17255
356074 ZDOT = -5259
432531
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 14254
52709563
00016717 00000-0 10270-3 0 9134
2 25544 51
6444 31
6343 0003369 93
3731 266
7805 15
50588418 24727
Satellite: ISS
Catalog Number: 25544
Epoch time: 14254
52709563 = yrday
fracday
Element set: 913
Inclination: 51
6444 deg
RA of node: 31
6343 deg
Eccentricity:
0003369
Arg of perigee: 93
3731 deg
Mean anomaly: 266
7805 deg
Mean motion: 15
50588418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2472
Checksum: 315
Coasting Arc #15 (Orbit 2487)
---------------------------------------
Vector Time (GMT): 2014/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3997332
42 A = 6795597
37 meter
Y = 4598042
08 meter E =
0016311
Z = 2994319
67 I = 51
81598
XDOT = -5599
379863 Wp = 85
80339
YDOT = 1608
000424 meter/sec RA = 26
25957 deg
ZDOT = 4983
571285 TA = 308
33135
MA = 308
47786
Ha = 227
631 n
mi
Hp = 218
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13114607
67 X = 3931073
44
Y = 15085439
89 feet Y = 4642372
69 meter
Z = 9823883
44 Z = 3013576
79
XDOT = -18370
668842 XDOT = -5641
153445
YDOT = 5275
591943 feet/sec YDOT = 1545
151518 meter/sec
ZDOT = 16350
299491 ZDOT = 4956
268512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10409276
12 X = -3172747
36
Y = -17017937
02 feet Y = -5187067
20 meter
Z = 9904994
05 Z = 3019042
19
XDOT = 17846
622247 XDOT = 5439
650461
YDOT = -1425
455233 feet/sec YDOT = -434
478755 meter/sec
ZDOT = 16233
836935 ZDOT = 4948
073498
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 14255
55826695
00016717 00000-0 10270-3 0 9145
2 25544 51
6456 26
5214 0003297 97
9137 262
2388 15
50655427 24889
Satellite: ISS
Catalog Number: 25544
Epoch time: 14255
55826695 = yrday
fracday
Element set: 914
Inclination: 51
6456 deg
RA of node: 26
5214 deg
Eccentricity:
0003297
Arg of perigee: 97
9137 deg
Mean anomaly: 262
2388 deg
Mean motion: 15
50655427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2488
Checksum: 338
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