[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 26th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 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 1749)
---------------------------------------
Vector Time (GMT): 2015/357/11:47:00
566
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -530133
73 A = 6777985
57 meter
Y = -5017893
24 meter E =
0003348
Z = 4522356
41 I = 51
40145
XDOT = 6684
591060 Wp = 39
67220
YDOT = 2104
373549 meter/sec RA = 218
29018 deg
ZDOT = 3119
812908 TA = 18
97608
MA = 18
96361
Ha = 219
655 n
mi
Hp = 214
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1739283
90 X = -495950
95
Y = -16462904
33 feet Y = -5023630
85 meter
Z = 14837127
34 Z = 4519863
67
XDOT = 21931
073031 XDOT = 6645
407733
YDOT = 6904
112692 feet/sec YDOT = 2178
905675 meter/sec
ZDOT = 10235
606654 ZDOT = 3152
190409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16523644
62 X = 5036406
88
Y = -1146553
94 feet Y = -349469
64 meter
Z = 14827247
14 Z = 4519344
93
XDOT = -7894
095621 XDOT = -2406
120345
YDOT = 20353
300663 feet/sec YDOT = 6203
686042 meter/sec
ZDOT = 10375
242058 ZDOT = 3162
373779
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
54485237
00016717 00000-0 10270-3 0 9006
2 25544 51
6428 219
0695 0008510 314
8018 45
2443 15
55045348 17504
Satellite: ISS
Catalog Number: 25544
Epoch time: 15357
54485237 = yrday
fracday
Element set: 900
Inclination: 51
6428 deg
RA of node: 219
0695 deg
Eccentricity:
0008510
Arg of perigee: 314
8018 deg
Mean anomaly: 45
2443 deg
Mean motion: 15
55045348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1750
Checksum: 304
Coasting Arc #2 (Orbit 1764)
---------------------------------------
Vector Time (GMT): 2015/358/11:47:00
566
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1359741
75 A = 6774856
03 meter
Y = 4097847
04 meter E =
0011822
Z = -5229361
71 I = 51
41592
XDOT = -6749
039315 Wp = 45
47676
YDOT = -3495
273279 meter/sec RA = 213
26774 deg
ZDOT = -977
325699 TA = 215
09412
MA = 215
17206
Ha = 219
735 n
mi
Hp = 214
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4461094
98 X = -1380061
64
Y = 13444380
06 feet Y = 4082528
45 meter
Z = -17156698
52 Z = -5236015
97
XDOT = -22142
517437 XDOT = -6704
705243
YDOT = -11467
432017 feet/sec YDOT = -3570
497503 meter/sec
ZDOT = -3206
449143 ZDOT = -1010
003798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13332153
18 X = -4063640
29
Y = -4678986
01 feet Y = -1426154
94 meter
Z = -17186209
86 Z = -5238356
77
XDOT = 11664
867950 XDOT = 3555
451751
YDOT = -20861
844551 feet/sec YDOT = -6358
690219 meter/sec
ZDOT = -3347
158465 ZDOT = -1020
213900
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
50879262
00016717 00000-0 10270-3 0 9019
2 25544 51
6414 214
2567 0008647 317
6405 42
4079 15
55106270 17658
Satellite: ISS
Catalog Number: 25544
Epoch time: 15358
50879262 = yrday
fracday
Element set: 901
Inclination: 51
6414 deg
RA of node: 214
2567 deg
Eccentricity:
0008647
Arg of perigee: 317
6405 deg
Mean anomaly: 42
4079 deg
Mean motion: 15
55106270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1765
Checksum: 311
Coasting Arc #3 (Orbit 1780)
---------------------------------------
Vector Time (GMT): 2015/359/11:47:00
566
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3274892
84 A = 6775020
27 meter
Y = -2916420
23 meter E =
0009323
Z = 5167800
77 I = 51
44391
XDOT = 6086
943913 Wp = 348
13527
YDOT = 4469
662273 meter/sec RA = 208
24245 deg
ZDOT = -1326
413870 TA = 114
69410
MA = 114
59701
Ha = 219
797 n
mi
Hp = 214
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10744399
09 X = 3282158
54
Y = -9568307
85 feet Y = -2879758
16 meter
Z = 16954726
92 Z = 5183726
76
XDOT = 19970
288428 XDOT = 6042
953825
YDOT = 14664
246302 feet/sec YDOT = 4537
484682 meter/sec
ZDOT = -4351
751543 ZDOT = -1296
951278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9488897
10 X = 2892215
83
Y = 10704999
85 feet Y = 3262883
95 meter
Z = 17024135
87 Z = 5188956
61
XDOT = -14028
618519 XDOT = -4275
922925
YDOT = 19198
389077 feet/sec YDOT = 5851
668991 meter/sec
ZDOT = -4225
099498 ZDOT = -1287
810327
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
53698269
00016717 00000-0 10270-3 0 9020
2 25544 51
6414 209
1232 0008653 321
0102 39
0427 15
55119596 17812
Satellite: ISS
Catalog Number: 25544
Epoch time: 15359
53698269 = yrday
fracday
Element set: 902
Inclination: 51
6414 deg
RA of node: 209
1232 deg
Eccentricity:
0008653
Arg of perigee: 321
0102 deg
Mean anomaly: 39
0427 deg
Mean motion: 15
55119596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1781
Checksum: 306
Coasting Arc #4 (Orbit 1795)
---------------------------------------
Vector Time (GMT): 2015/360/11:47:00
566
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4924782
21 A = 6778222
36 meter
Y = 1657151
59 meter E =
0005149
Z = -4353091
97 I = 51
48203
XDOT = -4705
258997 Wp = 40
61987
YDOT = -4989
670347 meter/sec RA = 203
22383 deg
ZDOT = 3429
829596 TA = 264
21777
MA = 264
27648
Ha = 219
896 n
mi
Hp = 214
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16157421
94 X = -4921801
45
Y = 5436849
06 feet Y = 1602096
55 meter
Z = -14281797
80 Z = -4377007
89
XDOT = -15437
201434 XDOT = -4665
774187
YDOT = -16370
309538 feet/sec YDOT = -5042
067246 meter/sec
ZDOT = 11252
721772 ZDOT = 3407
068033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5594451
74 X = -1705188
89
Y = -16010907
25 feet Y = -4880124
53 meter
Z = -14385559
38 Z = -4384718
50
XDOT = 15047
186195 XDOT = 4586
382352
YDOT = -15262
526188 feet/sec YDOT = -4652
017982 meter/sec
ZDOT = 11155
127990 ZDOT = 3400
083011
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
50089772
00016717 00000-0 10270-3 0 9033
2 25544 51
6398 204
3091 0008687 324
5170 35
5404 15
55140564 17964
Satellite: ISS
Catalog Number: 25544
Epoch time: 15360
50089772 = yrday
fracday
Element set: 903
Inclination: 51
6398 deg
RA of node: 204
3091 deg
Eccentricity:
0008687
Arg of perigee: 324
5170 deg
Mean anomaly: 35
5404 deg
Mean motion: 15
55140564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1796
Checksum: 311
Coasting Arc #5 (Orbit 1811)
---------------------------------------
Vector Time (GMT): 2015/361/11:47:00
566
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6132808
72 A = 6782626
45 meter
Y = -383484
29 meter E =
0010157
Z = 2871677
15 I = 51
52743
XDOT = 2690
283051 Wp = 56
64621
YDOT = 5106
460040 meter/sec RA = 198
22211 deg
ZDOT = -5045
113322 TA = 90
61677
MA = 90
50039
Ha = 220
107 n
mi
Hp = 213
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20120763
51 X = 6122691
82
Y = -1258150
55 feet Y = -314959
99 meter
Z = 9421512
95 Z = 2901444
06
XDOT = 8826
387961 XDOT = 2657
488290
YDOT = 16753
477822 feet/sec YDOT = 5136
361652 meter/sec
ZDOT = -16552
209063 ZDOT = -5032
123849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1800623
69 X = 548830
10
Y = 20018514
69 feet Y = 6101643
28 meter
Z = 9550382
04 Z = 2910956
45
XDOT = -15043
816167 XDOT = -4585
355168
YDOT = 9251
853053 feet/sec YDOT = 2819
964811 meter/sec
ZDOT = -16496
899117 ZDOT = -5028
254851
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
52905820
00016717 00000-0 10270-3 0 9048
2 25544 51
6402 199
1754 0008917 328
3572 31
7044 15
55198804 18128
Satellite: ISS
Catalog Number: 25544
Epoch time: 15361
52905820 = yrday
fracday
Element set: 904
Inclination: 51
6402 deg
RA of node: 199
1754 deg
Eccentricity:
0008917
Arg of perigee: 328
3572 deg
Mean anomaly: 31
7044 deg
Mean motion: 15
55198804 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1812
Checksum: 310
Coasting Arc #6 (Orbit 1826)
---------------------------------------
Vector Time (GMT): 2015/362/11:47:00
566
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6660916
71 A = 6785893
29 meter
Y = -772629
23 meter E =
0015444
Z = -973878
19 I = 51
56719
XDOT = -293
569004 Wp = 7
50109
YDOT = -4887
456996 meter/sec RA = 193
23427 deg
ZDOT = 5910
917590 TA = 341
92643
MA = 341
98127
Ha = 220
223 n
mi
Hp = 213
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21853401
29 X = -6647051
28
Y = -2534872
79 feet Y = -847038
40 meter
Z = -3195138
41 Z = -1006201
44
XDOT = -963
152899 XDOT = -267
606955
YDOT = -16034
963896 feet/sec YDOT = -4890
595137 meter/sec
ZDOT = 19392
774244 ZDOT = 5909
554223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1565480
60 X = 477158
49
Y = -21923353
75 feet Y = -6682238
22 meter
Z = -3334886
56 Z = -1016473
42
XDOT = 14370
530743 XDOT = 4380
137770
YDOT = -1910
804427 feet/sec YDOT = -582
413189 meter/sec
ZDOT = 19387
725754 ZDOT = 5909
378810
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
49294782
00016717 00000-0 10270-3 0 9054
2 25544 51
6389 194
3612 0008781 331
7997 28
2680 15
55161007 18278
Satellite: ISS
Catalog Number: 25544
Epoch time: 15362
49294782 = yrday
fracday
Element set: 905
Inclination: 51
6389 deg
RA of node: 194
3612 deg
Eccentricity:
0008781
Arg of perigee: 331
7997 deg
Mean anomaly: 28
2680 deg
Mean motion: 15
55161007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1827
Checksum: 336
Coasting Arc #7 (Orbit 1842)
---------------------------------------
Vector Time (GMT): 2015/363/11:47:00
566
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6446106
58 A = 6785710
22 meter
Y = 1815331
83 meter E =
0002440
Z = -1098775
92 I = 51
59841
XDOT = -2234
053446 Wp = 77
84563
YDOT = 4382
486496 meter/sec RA = 188
25559 deg
ZDOT = -5876
419768 TA = 114
07765
MA = 114
05211
Ha = 220
386 n
mi
Hp = 213
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21148643
63 X = 6430665
35
Y = 5955813
10 feet Y = 1887330
18 meter
Z = -3604907
89 Z = -1067499
95
XDOT = -7329
571672 XDOT = -2254
348507
YDOT = 14378
236534 feet/sec YDOT = 4357
390662 meter/sec
ZDOT = -19279
592414 ZDOT = -5887
321241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4642610
92 X = -1415067
81
Y = 21497406
20 feet Y = 6552409
41 meter
Z = -3469854
25 Z = -1057611
57
XDOT = -13224
608009 XDOT = -4030
860521
YDOT = -5969
822294 feet/sec YDOT = -1819
601835 meter/sec
ZDOT = -19327
535245 ZDOT = -5891
032743
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
52108117
00016717 00000-0 10270-3 0 9066
2 25544 51
6390 189
2274 0008806 336
1857 23
8888 15
55208604 18433
Satellite: ISS
Catalog Number: 25544
Epoch time: 15363
52108117 = yrday
fracday
Element set: 906
Inclination: 51
6390 deg
RA of node: 189
2274 deg
Eccentricity:
0008806
Arg of perigee: 336
1857 deg
Mean anomaly: 23
8888 deg
Mean motion: 15
55208604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1843
Checksum: 323
Coasting Arc #8 (Orbit 1858)
---------------------------------------
Vector Time (GMT): 2015/364/11:47:00
566
Vector Time (MET): N/A
Weight (LBS) : 922656
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5447319
32 A = 6782386
60 meter
Y = -2688149
11 meter E =
0013988
Z = 2995884
91 I = 51
61873
XDOT = 4550
868159 Wp = 45
90286
YDOT = -3680
656903 meter/sec RA = 183
27139 deg
ZDOT = 4967
257710 TA = 348
44808
MA = 348
48014
Ha = 220
489 n
mi
Hp = 213
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17871782
53 X = -5431407
56
Y = -8819386
85 feet Y = -2748975
78 meter
Z = 9829018
74 Z = 2969461
87
XDOT = 14930
669812 XDOT = 4567
559259
YDOT = -12075
646006 feet/sec YDOT = -3629
672945 meter/sec
ZDOT = 16296
777263 ZDOT = 4989
404987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7380805
06 X = 2249669
38
Y = -18572351
99 feet Y = -5660852
89 meter
Z = 9715104
88 Z = 2961163
97
XDOT = 11848
287096 XDOT = 3611
357907
YDOT = 13292
280113 feet/sec YDOT = 4051
486978 meter/sec
ZDOT = 16393
281217 ZDOT = 4996
672115
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
54919932
00016717 00000-0 10270-3 0 9075
2 25544 51
6385 184
0920 0008675 339
1205 20
9593 15
55235530 18598
Satellite: ISS
Catalog Number: 25544
Epoch time: 15364
54919932 = yrday
fracday
Element set: 907
Inclination: 51
6385 deg
RA of node: 184
0920 deg
Eccentricity:
0008675
Arg of perigee: 339
1205 deg
Mean anomaly: 20
9593 deg
Mean motion: 15
55235530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1859
Checksum: 327
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