[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 25th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24756 99 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 133 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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 86)
---------------------------------------
Vector Time (GMT): 2014/358/13:17:12
615
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -143731
13 A = 6786540
95 meter
Y = 5422216
53 meter E =
0009144
Z = -4082405
79 I = 51
34260
XDOT = -5911
669119 Wp = 119
45761
YDOT = -3025
052686 meter/sec RA = 234
50090 deg
ZDOT = -3820
600827 TA = 110
90312
MA = 110
80521
Ha = 224
811 n
mi
Hp = 216
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -471558
84 X = -184522
19
Y = 17789424
32 feet Y = 5420381
49 meter
Z = -13393719
77 Z = -4083202
64
XDOT = -19395
239893 XDOT = -5858
843902
YDOT = -9924
713538 feet/sec YDOT = -3090
865133 meter/sec
ZDOT = -12534
779617 ZDOT = -3849
190444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16696513
51 X = -5089097
32
Y = 6147824
81 feet Y = 1873857
00 meter
Z = -13398074
55 Z = -4083733
12
XDOT = 2619
355127 XDOT = 798
379443
YDOT = -20390
396585 feet/sec YDOT = -6214
992879 meter/sec
ZDOT = -12656
226507 ZDOT = -3857
617839
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 14358
57688702
00016717 00000-0 10270-3 0 9001
2 25544 51
6444 235
3561 0006883 171
2705 188
8568 15
52661148 877
Satellite: ISS
Catalog Number: 25544
Epoch time: 14358
57688702 = yrday
fracday
Element set: 900
Inclination: 51
6444 deg
RA of node: 235
3561 deg
Eccentricity:
0006883
Arg of perigee: 171
2705 deg
Mean anomaly: 188
8568 deg
Mean motion: 15
52661148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 87
Checksum: 332
Coasting Arc #2 (Orbit 102)
---------------------------------------
Vector Time (GMT): 2014/359/13:17:12
615
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 921017
46 A = 6783991
54 meter
Y = -4760765
18 meter E =
0012802
Z = 4742354
49 I = 51
35303
XDOT = 6078
503051 Wp = 144
10821
YDOT = 3840
659349 meter/sec RA = 229
50142 deg
ZDOT = 2661
211825 TA = 279
43244
MA = 279
57714
Ha = 224
707 n
mi
Hp = 216
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3021710
83 X = 951148
50
Y = -15619308
33 feet Y = -4750297
58 meter
Z = 15558905
79 Z = 4746901
49
XDOT = 19942
595311 XDOT = 6022
177008
YDOT = 12600
588414 feet/sec YDOT = 3908
318014 meter/sec
ZDOT = 8731
009924 ZDOT = 2690
603339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15550820
49 X = 4739890
09
Y = -3261219
68 feet Y = -994019
76 meter
Z = 15579136
91 Z = 4748520
93
XDOT = -4291
522055 XDOT = -1308
055922
YDOT = 22057
728115 feet/sec YDOT = 6723
195529 meter/sec
ZDOT = 8855
755515 ZDOT = 2699
234281
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 14359
60667247
00016717 00000-0 10270-3 0 9018
2 25544 51
6442 230
2330 0006804 173
7558 186
3680 15
52680891 1032
Satellite: ISS
Catalog Number: 25544
Epoch time: 14359
60667247 = yrday
fracday
Element set: 901
Inclination: 51
6442 deg
RA of node: 230
2330 deg
Eccentricity:
0006804
Arg of perigee: 173
7558 deg
Mean anomaly: 186
3680 deg
Mean motion: 15
52680891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 103
Checksum: 304
Coasting Arc #3 (Orbit 117)
---------------------------------------
Vector Time (GMT): 2014/360/13:17:12
615
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1836350
57 A = 6781964
48 meter
Y = 3994445
23 meter E =
0014527
Z = -5175191
56 I = 51
36676
XDOT = -6064
977325 Wp = 107
67824
YDOT = -4484
343374 meter/sec RA = 224
49753 deg
ZDOT = -1316
522020 TA = 149
64831
MA = 149
56412
Ha = 224
448 n
mi
Hp = 216
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6024772
20 X = -1855741
83
Y = 13105135
26 feet Y = 3973801
77 meter
Z = -16978974
95 Z = -5184159
10
XDOT = -19898
219570 XDOT = -6007
986432
YDOT = -14712
412644 feet/sec YDOT = -4551
847176 meter/sec
ZDOT = -4319
297966 ZDOT = -1345
846201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14376029
17 X = -4381813
69
Y = -218704
70 feet Y = -66661
19 meter
Z = -17017931
55 Z = -5187065
54
XDOT = 5582
092396 XDOT = 1701
421762
YDOT = -23034
173961 feet/sec YDOT = -7020
816223 meter/sec
ZDOT = -4443
664328 ZDOT = -1354
428887
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 14360
57206950
00016717 00000-0 10270-3 0 9027
2 25544 51
6428 225
4292 0006828 178
6209 181
4963 15
52753561 1183
Satellite: ISS
Catalog Number: 25544
Epoch time: 14360
57206950 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 225
4292 deg
Eccentricity:
0006828
Arg of perigee: 178
6209 deg
Mean anomaly: 181
4963 deg
Mean motion: 15
52753561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 118
Checksum: 314
Coasting Arc #4 (Orbit 133)
---------------------------------------
Vector Time (GMT): 2014/361/13:17:12
615
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2768678
57 A = 6781311
66 meter
Y = -3200148
76 meter E =
0007080
Z = 5297105
99 I = 51
38828
XDOT = 5869
448107 Wp = 162
70597
YDOT = 4934
176523 meter/sec RA = 219
49403 deg
ZDOT = -93
538909 TA = 288
14994
MA = 288
22702
Ha = 224
305 n
mi
Hp = 216
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9083591
12 X = 2778526
26
Y = -10499175
73 feet Y = -3169132
71 meter
Z = 17378956
65 Z = 5310579
51
XDOT = 19256
719512 XDOT = 5814
291138
YDOT = 16188
243185 feet/sec YDOT = 4999
504105 meter/sec
ZDOT = -306
886186 ZDOT = -65
160081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13268110
51 X = 4044120
08
Y = 3831517
82 feet Y = 1167846
63 meter
Z = 17437005
70 Z = 5314799
34
XDOT = -6500
092827 XDOT = -1981
228294
YDOT = 23260
109422 feet/sec YDOT = 7089
681352 meter/sec
ZDOT = -186
613411 ZDOT = -56
879768
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 14361
60180327
00016717 00000-0 10270-3 0 9032
2 25544 51
6432 220
3064 0006860 182
3708 177
7412 15
52767346 1342
Satellite: ISS
Catalog Number: 25544
Epoch time: 14361
60180327 = yrday
fracday
Element set: 903
Inclination: 51
6432 deg
RA of node: 220
3064 deg
Eccentricity:
0006860
Arg of perigee: 182
3708 deg
Mean anomaly: 177
7412 deg
Mean motion: 15
52767346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 134
Checksum: 288
Coasting Arc #5 (Orbit 148)
---------------------------------------
Vector Time (GMT): 2014/362/13:17:12
615
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3751386
72 A = 6781876
07 meter
Y = 2390883
09 meter E =
0015894
Z = -5132240
88 I = 51
41449
XDOT = -5410
178873 Wp = 127
19011
YDOT = -5195
911737 meter/sec RA = 214
48980 deg
ZDOT = 1527
864474 TA = 157
63769
MA = 157
56832
Ha = 224
141 n
mi
Hp = 216
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12307699
20 X = -3752912
74
Y = 7844104
64 feet Y = 2348924
28 meter
Z = -16838060
62 Z = -5150468
07
XDOT = -17749
930685 XDOT = -5359
096691
YDOT = -17046
954519 feet/sec YDOT = -5256
126301 meter/sec
ZDOT = 5012
678720 ZDOT = 1501
706709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12318233
80 X = -3754597
66
Y = -7657079
44 feet Y = -2333877
81 meter
Z = -16916263
57 Z = -5156077
13
XDOT = 7212
274066 XDOT = 2198
301135
YDOT = -22476
386330 feet/sec YDOT = -6850
802554 meter/sec
ZDOT = 4901
914226 ZDOT = 1494
103456
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 14362
56715351
00016717 00000-0 10270-3 0 9040
2 25544 51
6421 215
5018 0006861 185
9421 174
1650 15
52833104 1494
Satellite: ISS
Catalog Number: 25544
Epoch time: 14362
56715351 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 215
5018 deg
Eccentricity:
0006861
Arg of perigee: 185
9421 deg
Mean anomaly: 174
1650 deg
Mean motion: 15
52833104 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 149
Checksum: 288
Coasting Arc #6 (Orbit 164)
---------------------------------------
Vector Time (GMT): 2014/363/13:17:12
615
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4659823
51 A = 6783731
84 meter
Y = -1621051
35 meter E =
0006753
Z = 4649206
63 I = 51
44785
XDOT = 4724
027526 Wp = 118
59925
YDOT = 5311
335616 meter/sec RA = 209
49229 deg
ZDOT = -2882
881243 TA =
12437
MA =
12420
Ha = 223
857 n
mi
Hp = 216
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15288134
87 X = 4655019
92
Y = -5318409
93 feet Y = -1568969
21 meter
Z = 15253302
60 Z = 4671831
55
XDOT = 15498
777974 XDOT = 4678
287866
YDOT = 17425
641784 feet/sec YDOT = 5363
907123 meter/sec
ZDOT = -9458
271794 ZDOT = -2860
043597
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11514808
65 X = 3509713
68
Y = 11245344
26 feet Y = 3427580
93 meter
Z = 15350153
30 Z = 4678726
73
XDOT = -7874
263931 XDOT = -2400
075646
YDOT = 20841
937466 feet/sec YDOT = 6352
622540 meter/sec
ZDOT = -9361
684971 ZDOT = -2853
441579
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 14363
59683550
00016717 00000-0 10270-3 0 9050
2 25544 51
6424 210
3789 0006859 190
8790 169
2214 15
52860180 1659
Satellite: ISS
Catalog Number: 25544
Epoch time: 14363
59683550 = yrday
fracday
Element set: 905
Inclination: 51
6424 deg
RA of node: 210
3789 deg
Eccentricity:
0006859
Arg of perigee: 190
8790 deg
Mean anomaly: 169
2214 deg
Mean motion: 15
52860180 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 165
Checksum: 323
Coasting Arc #7 (Orbit 179)
---------------------------------------
Vector Time (GMT): 2014/364/13:17:12
615
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5490310
97 A = 6786362
96 meter
Y = 905375
89 meter E =
0009772
Z = -3895753
72 I = 51
48398
XDOT = -3764
058502 Wp = 151
34278
YDOT = -5278
483606 meter/sec RA = 204
49938 deg
ZDOT = 4073
849535 TA = 161
51867
MA = 161
48315
Ha = 223
830 n
mi
Hp = 216
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18012831
28 X = -5481102
80
Y = 2970393
33 feet Y = 844031
35 meter
Z = -12781344
24 Z = -3922402
37
XDOT = -12349
273300 XDOT = -3724
542887
YDOT = -17317
859600 feet/sec YDOT = -5320
355016 meter/sec
ZDOT = 13365
648081 ZDOT = 4055
660045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10881599
75 X = -3316711
60
Y = -14558540
65 feet Y = -4437443
19 meter
Z = -12895261
49 Z = -3930475
70
XDOT = 8599
121237 XDOT = 2621
012153
YDOT = -18209
890953 feet/sec YDOT = -5550
374763 meter/sec
ZDOT = 13288
886743 ZDOT = 4050
452679
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 14364
56213905
00016717 00000-0 10270-3 0 9062
2 25544 51
6415 205
5744 0006873 193
2716 166
8256 15
52904402 1809
Satellite: ISS
Catalog Number: 25544
Epoch time: 14364
56213905 = yrday
fracday
Element set: 906
Inclination: 51
6415 deg
RA of node: 205
5744 deg
Eccentricity:
0006873
Arg of perigee: 193
2716 deg
Mean anomaly: 166
8256 deg
Mean motion: 15
52904402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 180
Checksum: 305
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