[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 10th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 298 16 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
342/17:12:15
308 5
5 -10
9 10
9
N/A -9
2 0
0 223
0
000/00:00:53
177 2
0 0
0 214
3
342/18:02:48
487 -11
2 -18
2 18
2
N/A 12
4 -0
0 214
2
000/00:01:27
994 -7
1 0
0 212
0
342/21:12:15
274 5
0 1
4 5
7
N/A 1
0 5
6 214
4
000/00:00:27
808 -2
7 -0
0 212
6
342/22:31:42
277 0
9 2
6 2
6
N/A -2
5 0
0 214
6
000/00:00:12
695 -0
1 0
0 214
0
343/01:10:46
376 -1
7 2
6 2
6
N/A 0
0 -0
0 216
9
000/00:00:12
692 -2
0 -0
0 215
1
343/07:50:50
000 0
0 0
0 0
0
N/A 0
0 0
0 216
6
000/00:00:00
000 0
0 0
0 215
0
Coasting Arc #1 (Orbit 6)
---------------------------------------
Vector Time (GMT): 2015/341/05:51:13
813
Vector Time (MET): N/A
Weight (LBS) : 15641
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1064994
43 A = 6793362
91 meter
Y = 6161506
51 meter E =
0003215
Z = 2653587
62 I = 51
34720
XDOT = -5496
819778 Wp = 79
40675
YDOT = 1283
079675 meter/sec RA = 299
64791 deg
ZDOT = -5179
406210 TA = 70
57767
MA = 70
54292
Ha = 223
927 n
mi
Hp = 221
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3494076
20 X = -1146705
06
Y = 20214916
39 feet Y = 6149140
08 meter
Z = 8705996
11 Z = 2648215
76
XDOT = -18034
185622 XDOT = -5485
598991
YDOT = 4209
578985 feet/sec YDOT = 1221
673529 meter/sec
ZDOT = -16992
802525 ZDOT = -5206
081761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9415773
39 X = 2869927
73
Y = -18237867
02 feet Y = -5558901
87 meter
Z = 8681543
61 Z = 2646134
49
XDOT = 17034
459114 XDOT = 5192
103138
YDOT = 641
324029 feet/sec YDOT = 195
475564 meter/sec
ZDOT = -17108
292942 ZDOT = -5214
607689
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 15341
28144070
00016717 00000-0 10270-3 0 9007
2 25544 51
6534 300
1802 0010668 289
3670 70
6328 15
51725938 75
Satellite: ISS
Catalog Number: 25544
Epoch time: 15341
28144070 = yrday
fracday
Element set: 900
Inclination: 51
6534 deg
RA of node: 300
1802 deg
Eccentricity:
0010668
Arg of perigee: 289
3670 deg
Mean anomaly: 70
6328 deg
Mean motion: 15
51725938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 7
Checksum: 286
Coasting Arc #2 (Orbit 21)
---------------------------------------
Vector Time (GMT): 2015/342/05:51:13
813
Vector Time (MET): N/A
Weight (LBS) : 15641
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1332819
00 A = 6794950
88 meter
Y = -6400394
75 meter E =
0011084
Z = -1824435
06 I = 51
33714
XDOT = 5188
760609 Wp = 332
00602
YDOT = -522
938177 meter/sec RA = 294
66466 deg
ZDOT = 5620
814594 TA = 7
85866
MA = 7
84131
Ha = 224
154 n
mi
Hp = 221
071
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4372765
76 X = 1413153
28
Y = -20998670
43 feet Y = -6385041
02 meter
Z = -5985679
34 Z = -1817765
59
XDOT = 17023
492811 XDOT = 5166
918383
YDOT = -1715
676435 feet/sec YDOT = -465
036443 meter/sec
ZDOT = 18440
992761 ZDOT = 5645
967872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10147754
37 X = -3093035
53
Y = 18906288
78 feet Y = 5762636
82 meter
Z = -5955579
17 Z = -1815260
53
XDOT = -15324
638964 XDOT = -4670
949956
YDOT = -2377
587150 feet/sec YDOT = -724
688563 meter/sec
ZDOT = 18549
752830 ZDOT = 5653
964663
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 15342
24747717
00016717 00000-0 10270-3 0 9012
2 25544 51
6531 295
3824 0010563 292
8638 67
1398 15
51718463 228
Satellite: ISS
Catalog Number: 25544
Epoch time: 15342
24747717 = yrday
fracday
Element set: 901
Inclination: 51
6531 deg
RA of node: 295
3824 deg
Eccentricity:
0010563
Arg of perigee: 292
8638 deg
Mean anomaly: 67
1398 deg
Mean motion: 15
51718463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 22
Checksum: 314
Coasting Arc #3 (Orbit 29)
---------------------------------------
Vector Time (GMT): 2015/342/17:12:41
897
Vector Time (MET): N/A
Weight (LBS) : 15624
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3106732
38 A = 6779168
61 meter
Y = 3214690
33 meter E =
0017064
Z = 5110774
00 I = 51
30032
XDOT = -3971
201267 Wp = 303
74483
YDOT = 6352
404666 meter/sec RA = 292
30771 deg
ZDOT = -1576
176856 TA = 161
58235
MA = 161
52050
Ha = 222
968 n
mi
Hp = 214
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10192691
53 X = 3045727
44
Y = 10546884
27 feet Y = 3249090
46 meter
Z = 16767631
25 Z = 5125718
14
XDOT = -13028
875548 XDOT = -4034
283675
YDOT = 20841
222658 feet/sec YDOT = 6307
643450 meter/sec
ZDOT = -5171
183910 ZDOT = -1595
621309
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4554696
29 X = 1388271
43
Y = 13864891
29 feet Y = 4226018
87 meter
Z = 16831539
36 Z = 5130253
20
XDOT = -19697
120577 XDOT = -6003
682352
YDOT = 12873
580907 feet/sec YDOT = 3923
867460 meter/sec
ZDOT = -5256
456155 ZDOT = -1602
167836
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 15342
76260965
00016717 00000-0 10270-3 0 9025
2 25544 51
6549 292
8242 0019397 290
3063 69
6005 15
53799449 308
Satellite: ISS
Catalog Number: 25544
Epoch time: 15342
76260965 = yrday
fracday
Element set: 902
Inclination: 51
6549 deg
RA of node: 292
8242 deg
Eccentricity:
0019397
Arg of perigee: 290
3063 deg
Mean anomaly: 69
6005 deg
Mean motion: 15
53799449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 30
Checksum: 327
Coasting Arc #4 (Orbit 29)
---------------------------------------
Vector Time (GMT): 2015/342/18:03:32
484
Vector Time (MET): N/A
Weight (LBS) : 15597
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1907792
48 A = 6772128
69 meter
Y = -4749261
77 meter E =
0004844
Z = -4439437
82 I = 51
30773
XDOT = 4836
761069 Wp = 141
81080
YDOT = -4983
917319 meter/sec RA = 292
11969 deg
ZDOT = 3251
365910 TA = 161
10143
MA = 161
08345
Ha = 214
208 n
mi
Hp = 211
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6259161
68 X = -1832977
85
Y = -15581567
49 feet Y = -4770177
39 meter
Z = -14565084
73 Z = -4448524
21
XDOT = 15868
638678 XDOT = 4876
338828
YDOT = -16351
434773 feet/sec YDOT = -4929
608365 meter/sec
ZDOT = 10667
210991 ZDOT = 3274
958131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2565279
08 X = -781897
06
Y = -16560937
91 feet Y = -5047773
87 meter
Z = -14603380
51 Z = -4451110
38
XDOT = 17818
327739 XDOT = 5431
026295
YDOT = -12262
409113 feet/sec YDOT = -3737
582298 meter/sec
ZDOT = 10770
125106 ZDOT = 3282
734132
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 15342
76261220
00016717 00000-0 10270-3 0 9031
2 25544 51
6537 292
8231 0005787 264
7027 95
3467 15
57151568 302
Satellite: ISS
Catalog Number: 25544
Epoch time: 15342
76261220 = yrday
fracday
Element set: 903
Inclination: 51
6537 deg
RA of node: 292
8231 deg
Eccentricity:
0005787
Arg of perigee: 264
7027 deg
Mean anomaly: 95
3467 deg
Mean motion: 15
57151568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 30
Checksum: 307
Coasting Arc #5 (Orbit 31)
---------------------------------------
Vector Time (GMT): 2015/342/21:12:29
178
Vector Time (MET): N/A
Weight (LBS) : 15588
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -721051
11 A = 6776176
40 meter
Y = -5772194
87 meter E =
0001295
Z = -3474630
87 I = 51
30456
XDOT = 5208
212011 Wp = 255
70652
YDOT = -3367
950153 meter/sec RA = 291
46472 deg
ZDOT = 4512
442090 TA = 63
21947
MA = 63
20623
Ha = 214
368 n
mi
Hp = 212
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2365653
25 X = -639572
73
Y = -18937647
22 feet Y = -5779802
36 meter
Z = -11399707
57 Z = -3477936
10
XDOT = 17087
309748 XDOT = 5223
566101
YDOT = -11049
705226 feet/sec YDOT = -3309
622918 meter/sec
ZDOT = 14804
600033 ZDOT = 4537
780023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12637182
14 X = -3851813
12
Y = -14291017
25 feet Y = -4355902
06 meter
Z = -11412825
42 Z = -3478629
19
XDOT = 6676
574094 XDOT = 2035
019784
YDOT = -17819
371935 feet/sec YDOT = -5431
344566 meter/sec
ZDOT = 14914
730049 ZDOT = 4546
009719
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 15342
89096908
00016717 00000-0 10270-3 0 9045
2 25544 51
6412 292
1874 0006282 269
6078 90
4356 15
56885966 321
Satellite: ISS
Catalog Number: 25544
Epoch time: 15342
89096908 = yrday
fracday
Element set: 904
Inclination: 51
6412 deg
RA of node: 292
1874 deg
Eccentricity:
0006282
Arg of perigee: 269
6078 deg
Mean anomaly: 90
4356 deg
Mean motion: 15
56885966 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 32
Checksum: 340
Coasting Arc #6 (Orbit 32)
---------------------------------------
Vector Time (GMT): 2015/342/22:31:48
625
Vector Time (MET): N/A
Weight (LBS) : 15585
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4038282
88 A = 6770703
70 meter
Y = -1299737
34 meter E =
0006687
Z = -5282680
29 I = 51
28208
XDOT = 2608
022796 Wp = 88
52724
YDOT = -7207
099272 meter/sec RA = 291
21531 deg
ZDOT = -220
529270 TA = 179
36067
MA = 179
35981
Ha = 214
568 n
mi
Hp = 214
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13248959
57 X = -3997787
11
Y = -4264230
13 feet Y = -1344669
33 meter
Z = -17331628
26 Z = -5302199
49
XDOT = 8556
505236 XDOT = 2689
491774
YDOT = -23645
338818 feet/sec YDOT = -7177
479105 meter/sec
ZDOT = -723
521228 ZDOT = -207
662391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11106560
32 X = -3385279
58
Y = 8212317
30 feet Y = 2503114
31 meter
Z = -17415685
14 Z = -5308300
83
XDOT = -13668
470496 XDOT = -4166
149807
YDOT = -19898
515910 feet/sec YDOT = -6065
067649 meter/sec
ZDOT = -666
491713 ZDOT = -203
146674
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 15342
95515870
00016717 00000-0 10270-3 0 9057
2 25544 51
6422 291
8665 0008193 268
2506 91
7710 15
56418617 334
Satellite: ISS
Catalog Number: 25544
Epoch time: 15342
95515870 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 291
8665 deg
Eccentricity:
0008193
Arg of perigee: 268
2506 deg
Mean anomaly: 91
7710 deg
Mean motion: 15
56418617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 33
Checksum: 315
Coasting Arc #7 (Orbit 34)
---------------------------------------
Vector Time (GMT): 2015/343/01:10:52
722
Vector Time (MET): N/A
Weight (LBS) : 15581
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1455659
15 A = 6783581
57 meter
Y = 6514569
90 meter E =
0010344
Z = 1167974
42 I = 51
32108
XDOT = -4974
343747 Wp = 159
33204
YDOT = -62
925377 meter/sec RA = 290
64772 deg
ZDOT = -5842
267859 TA = 7
91318
MA = 7
89687
Ha = 216
889 n
mi
Hp = 215
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4775784
61 X = -1534072
14
Y = 21373260
84 feet Y = 6497853
25 meter
Z = 3831937
07 Z = 1160712
97
XDOT = -16320
025418 XDOT = -4944
890445
YDOT = -206
448087 feet/sec YDOT = -118
386710 meter/sec
ZDOT = -19167
545469 ZDOT = -5866
361064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21675833
30 X = 6606793
99
Y = 3167333
78 feet Y = 965403
34 meter
Z = 3799261
36 Z = 1158014
86
XDOT = 1250
242881 XDOT = 381
074030
YDOT = 14585
597090 feet/sec YDOT = 4445
689993 meter/sec
ZDOT = -19271
609462 ZDOT = -5873
986564
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 15343
08358606
00016717 00000-0 10270-3 0 9065
2 25544 51
6444 291
2246 0008293 253
5992 106
4250 15
55912020 355
Satellite: ISS
Catalog Number: 25544
Epoch time: 15343
08358606 = yrday
fracday
Element set: 906
Inclination: 51
6444 deg
RA of node: 291
2246 deg
Eccentricity:
0008293
Arg of perigee: 253
5992 deg
Mean anomaly: 106
4250 deg
Mean motion: 15
55912020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 35
Checksum: 294
Coasting Arc #8 (Orbit 38)
---------------------------------------
Vector Time (GMT): 2015/343/07:50:50
000
Vector Time (MET): N/A
Weight (LBS) : 15581
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3339088
33 A = 6772878
78 meter
Y = -2910647
24 meter E =
0007211
Z = -5129419
66 I = 51
28157
XDOT = 3551
262514 Wp = 128
08297
YDOT = -6637
487526 meter/sec RA = 289
25485 deg
ZDOT = 1451
654300 TA = 155
97898
MA = 155
94533
Ha = 216
567 n
mi
Hp = 215
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10955014
20 X = -3281375
44
Y = -9549367
58 feet Y = -2947664
08 meter
Z = -16828804
65 Z = -5145500
55
XDOT = 11651
123734 XDOT = 3618
168896
YDOT = -21776
533878 feet/sec YDOT = -6597
400970 meter/sec
ZDOT = 4762
645341 ZDOT = 1469
067932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12905076
83 X = 3933467
42
Y = 6506810
96 feet Y = 1983275
98 meter
Z = -16897687
01 Z = -5150415
00
XDOT = -5278
735535 XDOT = -1608
958591
YDOT = 23061
686696 feet/sec YDOT = 7029
202105 meter/sec
ZDOT = 4839
199315 ZDOT = 1474
987951
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 15343
34049583
00016717 00000-0 10270-3 0 9076
2 25544 51
6438 289
9437 0008039 257
1956 102
8300 15
55913858 392
Satellite: ISS
Catalog Number: 25544
Epoch time: 15343
34049583 = yrday
fracday
Element set: 907
Inclination: 51
6438 deg
RA of node: 289
9437 deg
Eccentricity:
0008039
Arg of perigee: 257
1956 deg
Mean anomaly: 102
8300 deg
Mean motion: 15
55913858 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 39
Checksum: 332
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