[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 23rd 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19116 7 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 110 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 964 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 1718)
---------------------------------------
Vector Time (GMT): 2015/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907469
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 996990
92 A = 6776944
44 meter
Y = -4664601
14 meter E =
0001416
Z = 4813764
34 I = 51
35198
XDOT = 6129
677115 Wp = 344
96073
YDOT = 3878
711230 meter/sec RA = 228
26010 deg
ZDOT = 2490
497664 TA = 80
47817
MA = 80
46217
Ha = 219
286 n
mi
Hp = 215
453
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3270967
58 X = 1025693
97
Y = -15303809
50 feet Y = -4653291
93 meter
Z = 15793190
11 Z = 4818676
99
XDOT = 20110
489221 XDOT = 6073
750884
YDOT = 12725
430545 feet/sec YDOT = 3946
944475 meter/sec
ZDOT = 8170
924094 ZDOT = 2520
138977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15238420
33 X = 4644670
52
Y = 3463873
77 feet Y = 1055788
72 meter
Z = 15815270
86 Z = 4820494
56
XDOT = -12857
588474 XDOT = -3918
992967
YDOT = 18697
698638 feet/sec YDOT = 5699
058545 meter/sec
ZDOT = 8298
373255 ZDOT = 2529
344168
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 15355
55265189
00016717 00000-0 10270-3 0 9007
2 25544 51
6429 229
0137 0008292 306
7246 53
3144 15
54993861 17191
Satellite: ISS
Catalog Number: 25544
Epoch time: 15355
55265189 = yrday
fracday
Element set: 900
Inclination: 51
6429 deg
RA of node: 229
0137 deg
Eccentricity:
0008292
Arg of perigee: 306
7246 deg
Mean anomaly: 53
3144 deg
Mean motion: 15
54993861 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1719
Checksum: 322
Coasting Arc #2 (Orbit 1733)
---------------------------------------
Vector Time (GMT): 2015/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907469
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2651528
18 A = 6774689
16 meter
Y = 3310523
83 meter E =
0010314
Z = -5290146
75 I = 51
36624
XDOT = -5737
495517 Wp = 54
16602
YDOT = -5072
508111 meter/sec RA = 223
23249 deg
ZDOT = -293
057137 TA = 212
99592
MA = 213
06033
Ha = 219
396 n
mi
Hp = 215
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8699239
43 X = -2662652
56
Y = 10861298
67 feet Y = 3280810
92 meter
Z = -17356124
52 Z = -5303054
17
XDOT = -18823
804189 XDOT = -5678
923495
YDOT = -16642
086979 feet/sec YDOT = -5136
341057 meter/sec
ZDOT = -961
473545 ZDOT = -320
787016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10841934
43 X = -3304621
62
Y = -8610221
89 feet Y = -2624395
63 meter
Z = -17412529
13 Z = -5307338
88
XDOT = 16053
040621 XDOT = 4892
966781
YDOT = -17992
338349 feet/sec YDOT = -5484
064729 meter/sec
ZDOT = -1080
460240 ZDOT = -329
324281
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 15356
51662887
00016717 00000-0 10270-3 0 9011
2 25544 51
6421 224
2012 0008456 309
9338 50
1071 15
55056155 17349
Satellite: ISS
Catalog Number: 25544
Epoch time: 15356
51662887 = yrday
fracday
Element set: 901
Inclination: 51
6421 deg
RA of node: 224
2012 deg
Eccentricity:
0008456
Arg of perigee: 309
9338 deg
Mean anomaly: 50
1071 deg
Mean motion: 15
55056155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1734
Checksum: 294
Coasting Arc #3 (Orbit 1749)
---------------------------------------
Vector Time (GMT): 2015/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907469
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4223661
31 A = 6775800
56 meter
Y = -1758254
68 meter E =
0009173
Z = 5002021
80 I = 51
39425
XDOT = 4718
548453 Wp = 351
19578
YDOT = 5713
151503 meter/sec RA = 218
20510 deg
ZDOT = -1967
659239 TA = 118
02413
MA = 117
93131
Ha = 219
481 n
mi
Hp = 214
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13857156
54 X = 4218710
68
Y = -5768552
10 feet Y = -1711051
07 meter
Z = 16410832
67 Z = 5022527
35
XDOT = 15480
802011 XDOT = 4663
870054
YDOT = 18743
935378 feet/sec YDOT = 5765
611892 meter/sec
ZDOT = -6455
574930 ZDOT = -1944
869690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5974550
87 X = 1821043
10
Y = 13662834
08 feet Y = 4164431
83 meter
Z = 16499821
72 Z = 5029145
66
XDOT = -17509
837876 XDOT = -5336
998585
YDOT = 15368
205719 feet/sec YDOT = 4684
229103 meter/sec
ZDOT = -6358
048009 ZDOT = -1937
933033
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 15357
54485277
00016717 00000-0 10270-3 0 9022
2 25544 51
6420 219
0682 0008542 313
2482 46
7957 15
55090938 17506
Satellite: ISS
Catalog Number: 25544
Epoch time: 15357
54485277 = yrday
fracday
Element set: 902
Inclination: 51
6420 deg
RA of node: 219
0682 deg
Eccentricity:
0008542
Arg of perigee: 313
2482 deg
Mean anomaly: 46
7957 deg
Mean motion: 15
55090938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1750
Checksum: 322
Coasting Arc #4 (Orbit 1764)
---------------------------------------
Vector Time (GMT): 2015/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907469
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5471878
10 A = 6779615
12 meter
Y = 226599
27 meter E =
0004127
Z = -3994011
69 I = 51
43137
XDOT = -3114
532654 Wp = 12
34847
YDOT = -5793
969347 meter/sec RA = 213
18701 deg
ZDOT = 3942
962770 TA = 298
74537
MA = 298
78683
Ha = 219
579 n
mi
Hp = 214
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17952355
97 X = -5454603
97
Y = 743435
91 feet Y = 165506
12 meter
Z = -13103712
89 Z = -4020550
94
XDOT = -10218
282987 XDOT = -3068
664953
YDOT = -19009
085784 feet/sec YDOT = -5828
542066 meter/sec
ZDOT = 12936
229560 ZDOT = 3927
943819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1319626
88 X = -402222
27
Y = -17834684
15 feet Y = -5436011
73 meter
Z = -13218536
20 Z = -4029009
83
XDOT = 17364
266202 XDOT = 5292
628338
YDOT = -10814
039564 feet/sec YDOT = -3296
119259 meter/sec
ZDOT = 12872
306476 ZDOT = 3923
479014
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 15358
50879672
00016717 00000-0 10270-3 0 9036
2 25544 51
6405 214
2549 0008570 316
6942 43
3547 15
55098124 17656
Satellite: ISS
Catalog Number: 25544
Epoch time: 15358
50879672 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 214
2549 deg
Eccentricity:
0008570
Arg of perigee: 316
6942 deg
Mean anomaly: 43
3547 deg
Mean motion: 15
55098124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1765
Checksum: 326
Coasting Arc #5 (Orbit 1780)
---------------------------------------
Vector Time (GMT): 2015/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907469
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6238852
96 A = 6783872
78 meter
Y = 1192993
68 meter E =
0008344
Z = 2380428
89 I = 51
47320
XDOT = 1021
079431 Wp = 69
25587
YDOT = 5386
928907 meter/sec RA = 208
18594 deg
ZDOT = -5357
766390 TA = 84
09201
MA = 83
99691
Ha = 219
833 n
mi
Hp = 214
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20468677
69 X = 6213485
79
Y = 3914021
26 feet Y = 1262618
56 meter
Z = 7809806
05 Z = 2410674
29
XDOT = 3349
998134 XDOT = 986
791382
YDOT = 17673
651269 feet/sec YDOT = 5398
156163 meter/sec
ZDOT = -17577
973721 ZDOT = -5352
888917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2898724
88 X = -883531
34
Y = 20587044
96 feet Y = 6274931
30 meter
Z = 7940426
53 Z = 2420242
01
XDOT = -15977
570179 XDOT = -4869
963390
YDOT = 4544
926596 feet/sec YDOT = 1385
293626 meter/sec
ZDOT = -17557
832013 ZDOT = -5351
627198
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 15359
53698355
00016717 00000-0 10270-3 0 9048
2 25544 51
6404 209
1215 0008697 321
1915 38
8613 15
55151321 17819
Satellite: ISS
Catalog Number: 25544
Epoch time: 15359
53698355 = yrday
fracday
Element set: 904
Inclination: 51
6404 deg
RA of node: 209
1215 deg
Eccentricity:
0008697
Arg of perigee: 321
1915 deg
Mean anomaly: 38
8613 deg
Mean motion: 15
55151321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1781
Checksum: 311
Coasting Arc #6 (Orbit 1795)
---------------------------------------
Vector Time (GMT): 2015/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907469
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6340691
42 A = 6786319
02 meter
Y = -2352248
43 meter E =
0015512
Z = -421818
30 I = 51
50816
XDOT = 1317
253300 Wp = 9
08498
YDOT = -4616
624089 meter/sec RA = 203
19662 deg
ZDOT = 5988
731281 TA = 346
35324
MA = 346
39514
Ha = 219
944 n
mi
Hp = 214
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20802793
39 X = -6311867
74
Y = -7717350
50 feet Y = -2422993
02 meter
Z = -1383918
31 Z = -452550
00
XDOT = 4321
697180 XDOT = 1339
688985
YDOT = -15146
404493 feet/sec YDOT = -4601
768871 meter/sec
ZDOT = 19648
068508 ZDOT = 5995
184174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6313388
82 X = 1924320
91
Y = -21261947
54 feet Y = -6480641
61 meter
Z = -1516459
63 Z = -462216
90
XDOT = 13840
211504 XDOT = 4218
496466
YDOT = 2715
844583 feet/sec YDOT = 827
789429 meter/sec
ZDOT = 19676
801128 ZDOT = 5997
488984
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 15360
50089263
00016717 00000-0 10270-3 0 9050
2 25544 51
6388 204
3074 0008677 324
1834 35
8737 15
55134711 17965
Satellite: ISS
Catalog Number: 25544
Epoch time: 15360
50089263 = yrday
fracday
Element set: 905
Inclination: 51
6388 deg
RA of node: 204
3074 deg
Eccentricity:
0008677
Arg of perigee: 324
1834 deg
Mean anomaly: 35
8737 deg
Mean motion: 15
55134711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1796
Checksum: 319
Coasting Arc #7 (Orbit 1811)
---------------------------------------
Vector Time (GMT): 2015/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907469
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5733778
71 A = 6785240
19 meter
Y = 3245459
01 meter E =
0001011
Z = -1624674
33 I = 51
53403
XDOT = -3644
678175 Wp = 16
81508
YDOT = 3579
057308 meter/sec RA = 198
21318 deg
ZDOT = -5713
147151 TA = 180
98996
MA = 180
99016
Ha = 220
082 n
mi
Hp = 214
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18811609
93 X = 5704952
97
Y = 10647831
39 feet Y = 3309416
88 meter
Z = -5330296
36 Z = -1596890
91
XDOT = -11957
605561 XDOT = -3656
677311
YDOT = 11742
314001 feet/sec YDOT = 3538
233533 meter/sec
ZDOT = -18743
921099 ZDOT = -5730
880830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9029598
37 X = -2752221
58
Y = 19671821
46 feet Y = 5995971
18 meter
Z = -5210646
28 Z = -1588204
99
XDOT = -11257
270044 XDOT = -3431
215909
YDOT = -10152
626288 feet/sec YDOT = -3094
520493 meter/sec
ZDOT = -18821
282737 ZDOT = -5736
726978
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 15361
52904378
00016717 00000-0 10270-3 0 9067
2 25544 51
6383 199
1736 0008650 327
8275 32
2349 15
55165912 18122
Satellite: ISS
Catalog Number: 25544
Epoch time: 15361
52904378 = yrday
fracday
Element set: 906
Inclination: 51
6383 deg
RA of node: 199
1736 deg
Eccentricity:
0008650
Arg of perigee: 327
8275 deg
Mean anomaly: 32
2349 deg
Mean motion: 15
55165912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1812
Checksum: 323
Coasting Arc #8 (Orbit 1827)
---------------------------------------
Vector Time (GMT): 2015/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907469
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4414495
54 A = 6781268
52 meter
Y = -3830052
45 meter E =
0011195
Z = 3424394
11 I = 51
55139
XDOT = 5657
545935 Wp = 47
58953
YDOT = -2414
695041 meter/sec RA = 193
22137 deg
ZDOT = 4590
397082 TA = 352
61421
MA = 352
63069
Ha = 220
198 n
mi
Hp = 213
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14483253
09 X = -4387972
99
Y = -12565788
89 feet Y = -3879270
21 meter
Z = 11234888
82 Z = 3403013
87
XDOT = 18561
502411 XDOT = 5661
829134
YDOT = -7922
227824 feet/sec YDOT = -2351
405001 meter/sec
ZDOT = 15060
357879 ZDOT = 4617
890091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11030727
12 X = 3362165
62
Y = -15749359
55 feet Y = -4800404
79 meter
Z = 11143030
59 Z = 3396395
72
XDOT = 8596
414354 XDOT = 2620
187095
YDOT = 16765
993370 feet/sec YDOT = 5110
274779 meter/sec
ZDOT = 15179
758070 ZDOT = 4626
790260
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 15362
55717506
00016717 00000-0 10270-3 0 9077
2 25544 51
6379 194
0379 0008682 330
9696 29
0973 15
55214875 18288
Satellite: ISS
Catalog Number: 25544
Epoch time: 15362
55717506 = yrday
fracday
Element set: 907
Inclination: 51
6379 deg
RA of node: 194
0379 deg
Eccentricity:
0008682
Arg of perigee: 330
9696 deg
Mean anomaly: 29
0973 deg
Mean motion: 15
55214875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1828
Checksum: 349
Coasting Arc #9 (Orbit 1842)
---------------------------------------
Vector Time (GMT): 2015/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907469
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2550646
58 A = 6776743
74 meter
Y = 4152592
68 meter E =
0013224
Z = -4719914
34 I = 51
56722
XDOT = -7048
714617 Wp = 30
76599
YDOT = 1190
235375 meter/sec RA = 188
21811 deg
ZDOT = -2754
262785 TA = 211
87323
MA = 211
95332
Ha = 220
295 n
mi
Hp = 213
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8368263
07 X = 2526948
87
Y = 13623991
72 feet Y = 4180983
43 meter
Z = -15485283
25 Z = -4707581
35
XDOT = -23125
704124 XDOT = -7048
121308
YDOT = 3904
971704 feet/sec YDOT = 1111
415450 meter/sec
ZDOT = -9036
295227 ZDOT = -2788
501967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12527407
11 X = -3818353
69
Y = 10016645
39 feet Y = 3053073
51 meter
Z = -15432623
27 Z = -4703863
57
XDOT = -5870
143946 XDOT = -1789
219875
YDOT = -21531
430542 feet/sec YDOT = -6562
780029 meter/sec
ZDOT = -9184
695077 ZDOT = -2799
495060
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 15363
52103261
00016717 00000-0 10270-3 0 9083
2 25544 51
6373 189
2244 0008606 335
9203 24
1547 15
55234557 18433
Satellite: ISS
Catalog Number: 25544
Epoch time: 15363
52103261 = yrday
fracday
Element set: 908
Inclination: 51
6373 deg
RA of node: 189
2244 deg
Eccentricity:
0008606
Arg of perigee: 335
9203 deg
Mean anomaly: 24
1547 deg
Mean motion: 15
55234557 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1843
Checksum: 300
Coasting Arc #10 (Orbit 1858)
---------------------------------------
Vector Time (GMT): 2015/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907469
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -309454
27 A = 6774288
92 meter
Y = -4218828
56 meter E =
0007034
Z = 5290979
38 I = 51
59094
XDOT = 7655
302949 Wp = 357
34578
YDOT = 41
311873 meter/sec RA = 183
20370 deg
ZDOT = 487
580927 TA = 88
04177
MA = 87
96122
Ha = 220
446 n
mi
Hp = 213
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1015269
93 X = -287956
47
Y = -13841301
04 feet Y = -4222169
07 meter
Z = 17358856
22 Z = 5289528
19
XDOT = 25115
823323 XDOT = 7651
903586
YDOT = 135
537641 feet/sec YDOT = 126
899506 meter/sec
ZDOT = 1599
674956 ZDOT = 524
760040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13560455
00 X = 4133226
68
Y = -2986509
23 feet Y = -910288
01 meter
Z = 17353302
27 Z = 5289286
53
XDOT = 3040
537997 XDOT = 926
755982
YDOT = 23904
238293 feet/sec YDOT = 7286
011832 meter/sec
ZDOT = 1760
605511 ZDOT = 536
632560
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 15364
54912926
00016717 00000-0 10270-3 0 9093
2 25544 51
6376 184
0891 0008616 339
9863 20
0951 15
55211699 18597
Satellite: ISS
Catalog Number: 25544
Epoch time: 15364
54912926 = yrday
fracday
Element set: 909
Inclination: 51
6376 deg
RA of node: 184
0891 deg
Eccentricity:
0008616
Arg of perigee: 339
9863 deg
Mean anomaly: 20
0951 deg
Mean motion: 15
55211699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1859
Checksum: 344
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list