[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 14th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22604 21 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 3899)
---------------------------------------
Vector Time (GMT): 2014/346/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 135498
85 A = 6790814
18 meter
Y = 5947221
35 meter E =
0019331
Z = 3253933
86 I = 51
32320
XDOT = -5405
047842 Wp = 103
41941
YDOT = 2716
354439 meter/sec RA = 294
66228 deg
ZDOT = -4720
336768 TA = 38
64991
MA = 38
51172
Ha = 226
694 n
mi
Hp = 215
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 444550
04 X = 53179
02
Y = 19511881
06 feet Y = 5948276
15 meter
Z = 10675636
03 Z = 3254392
42
XDOT = -17733
096596 XDOT = -5412
091189
YDOT = 8911
924011 feet/sec YDOT = 2655
872524 meter/sec
ZDOT = -15486
669185 ZDOT = -4746
610676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19296278
05 X = -5881505
55
Y = -2923619
85 feet Y = -891119
33 meter
Z = 10676442
86 Z = 3254179
78
XDOT = -6017
553895 XDOT = -1834
150427
YDOT = -17479
291427 feet/sec YDOT = -5327
688027 meter/sec
ZDOT = -15599
211243 ZDOT = -4754
639587
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 14346
53899603
00016717 00000-0 10270-3 0 9008
2 25544 51
6452 295
2014 0007261 123
1142 237
0708 15
52077618 39009
Satellite: ISS
Catalog Number: 25544
Epoch time: 14346
53899603 = yrday
fracday
Element set: 900
Inclination: 51
6452 deg
RA of node: 295
2014 deg
Eccentricity:
0007261
Arg of perigee: 123
1142 deg
Mean anomaly: 237
0708 deg
Mean motion: 15
52077618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3900
Checksum: 291
Coasting Arc #2 (Orbit 3914)
---------------------------------------
Vector Time (GMT): 2014/347/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 231657
66 A = 6792796
43 meter
Y = -6354209
28 meter E =
0009865
Z = -2399455
77 I = 51
31753
XDOT = 5184
435801 Wp = 92
73324
YDOT = -1817
766350 meter/sec RA = 289
67397 deg
ZDOT = 5332
929597 TA = 240
37638
MA = 240
47469
Ha = 226
634 n
mi
Hp = 215
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 760031
68 X = 314350
48
Y = -20847143
31 feet Y = -6351156
28 meter
Z = -7872230
23 Z = -2398129
80
XDOT = 17009
303809 XDOT = 5178
471511
YDOT = -5963
800360 feet/sec YDOT = -1759
824173 meter/sec
ZDOT = 17496
488179 ZDOT = 5358
100303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20482944
94 X = 6243201
62
Y = 3967127
29 feet Y = 1209180
40 meter
Z = -7865361
32 Z = -2397362
13
XDOT = 3615
436286 XDOT = 1101
984980
YDOT = 16114
342699 feet/sec YDOT = 4911
651655 meter/sec
ZDOT = 17604
150400 ZDOT = 5365
745042
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 14347
50479214
00016717 00000-0 10270-3 0 9019
2 25544 51
6449 290
4020 0007234 126
8477 233
3339 15
52100092 39158
Satellite: ISS
Catalog Number: 25544
Epoch time: 14347
50479214 = yrday
fracday
Element set: 901
Inclination: 51
6449 deg
RA of node: 290
4020 deg
Eccentricity:
0007234
Arg of perigee: 126
8477 deg
Mean anomaly: 233
3339 deg
Mean motion: 15
52100092 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3915
Checksum: 291
Coasting Arc #3 (Orbit 3930)
---------------------------------------
Vector Time (GMT): 2014/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -583566
87 A = 6794303
89 meter
Y = 6614103
49 meter E =
0021016
Z = 1389311
45 I = 51
31401
XDOT = -4987
159528 Wp = 123
32587
YDOT = 784
235016 meter/sec RA = 284
68752 deg
ZDOT = -5776
279419 TA = 41
46315
MA = 41
30389
Ha = 226
514 n
mi
Hp = 215
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1914589
48 X = -664232
79
Y = 21699814
61 feet Y = 6607126
60 meter
Z = 4558108
44 Z = 1386280
84
XDOT = -16362
071943 XDOT = -4967
499003
YDOT = 2572
949529 feet/sec YDOT = 728
575476 meter/sec
ZDOT = -18951
047963 ZDOT = -5800
458610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21239839
17 X = -6473902
98
Y = -4852408
09 feet Y = -1479013
99 meter
Z = 4543933
02 Z = 1384990
78
XDOT = -710
915315 XDOT = -216
686988
YDOT = -14891
556901 feet/sec YDOT = -4538
946543 meter/sec
ZDOT = -19054
284254 ZDOT = -5807
745841
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 14348
53494896
00016717 00000-0 10270-3 0 9027
2 25544 51
6457 285
2817 0007290 130
8753 229
3031 15
52142477 39312
Satellite: ISS
Catalog Number: 25544
Epoch time: 14348
53494896 = yrday
fracday
Element set: 902
Inclination: 51
6457 deg
RA of node: 285
2817 deg
Eccentricity:
0007290
Arg of perigee: 130
8753 deg
Mean anomaly: 229
3031 deg
Mean motion: 15
52142477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3931
Checksum: 323
Coasting Arc #4 (Orbit 3945)
---------------------------------------
Vector Time (GMT): 2014/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 853667
13 A = 6794917
93 meter
Y = -6729500
46 meter E =
0013231
Z = -365431
97 I = 51
30897
XDOT = 4797
015589 Wp = 75
53505
YDOT = 294
614373 meter/sec RA = 279
70241 deg
ZDOT = 5965
899277 TA = 280
51305
MA = 280
66209
Ha = 226
392 n
mi
Hp = 215
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2800745
16 X = 930629
68
Y = -22078413
58 feet Y = -6719523
87 meter
Z = -1198923
79 Z = -361098
23
XDOT = 15738
240123 XDOT = 4764
384067
YDOT = 966
582587 feet/sec YDOT = 348
075076 meter/sec
ZDOT = 19573
160356 ZDOT = 5989
123356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21593924
80 X = 6581828
28
Y = 5389794
34 feet Y = 1642809
31 meter
Z = -1179180
49 Z = -359414
21
XDOT = -2408
138039 XDOT = -734
000474
YDOT = 13816
778675 feet/sec YDOT = 4211
354140 meter/sec
ZDOT = 19672
121198 ZDOT = 5996
062541
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 14349
50069559
00016717 00000-0 10270-3 0 9030
2 25544 51
6452 280
4819 0007210 134
6115 225
5626 15
52186851 39460
Satellite: ISS
Catalog Number: 25544
Epoch time: 14349
50069559 = yrday
fracday
Element set: 903
Inclination: 51
6452 deg
RA of node: 280
4819 deg
Eccentricity:
0007210
Arg of perigee: 134
6115 deg
Mean anomaly: 225
5626 deg
Mean motion: 15
52186851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3946
Checksum: 314
Coasting Arc #5 (Orbit 3961)
---------------------------------------
Vector Time (GMT): 2014/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1145336
04 A = 6794650
22 meter
Y = 6648038
13 meter E =
0017648
Z = -742490
96 I = 51
30498
XDOT = -4643
860628 Wp = 139
41726
YDOT = -1451
647689 meter/sec RA = 274
71716 deg
ZDOT = -5926
918001 TA = 48
64065
MA = 48
48900
Ha = 226
264 n
mi
Hp = 215
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3757664
19 X = -1215984
03
Y = 21811148
73 feet Y = 6634835
25 meter
Z = -2435993
95 Z = -748226
24
XDOT = -15235
763214 XDOT = -4598
491565
YDOT = -4762
623651 feet/sec YDOT = -1503
324466 meter/sec
ZDOT = -19445
269031 ZDOT = -5949
367227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21323145
40 X = -6499294
72
Y = -5919786
54 feet Y = -1804350
94 meter
Z = -2461689
10 Z = -750322
84
XDOT = 5830
530037 XDOT = 1777
145555
YDOT = -13001
014127 feet/sec YDOT = -3962
709106 meter/sec
ZDOT = -19540
712095 ZDOT = -5956
009046
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 14350
53080025
00016717 00000-0 10270-3 0 9047
2 25544 51
6462 275
3612 0007247 138
7331 221
4370 15
52218304 39628
Satellite: ISS
Catalog Number: 25544
Epoch time: 14350
53080025 = yrday
fracday
Element set: 904
Inclination: 51
6462 deg
RA of node: 275
3612 deg
Eccentricity:
0007247
Arg of perigee: 138
7331 deg
Mean anomaly: 221
4370 deg
Mean motion: 15
52218304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3962
Checksum: 279
Coasting Arc #6 (Orbit 3977)
---------------------------------------
Vector Time (GMT): 2014/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1391769
11 A = 6793416
12 meter
Y = -6403867
07 meter E =
0017097
Z = 1774752
39 I = 51
29930
XDOT = 4524
891971 Wp = 89
55859
YDOT = 2557
504482 meter/sec RA = 269
73046 deg
ZDOT = 5632
767648 TA = 290
01066
MA = 290
19467
Ha = 226
150 n
mi
Hp = 215
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4566171
61 X = 1454653
96
Y = -21010062
58 feet Y = -6387951
89 meter
Z = 5822678
44 Z = 1781665
90
XDOT = 14845
446100 XDOT = 4468
594655
YDOT = 8390
762736 feet/sec YDOT = 2607
789712 meter/sec
ZDOT = 18480
208820 ZDOT = 5654
612501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20557437
50 X = 6265906
95
Y = 6269477
79 feet Y = 1910936
83 meter
Z = 5853345
08 Z = 1784099
58
XDOT = -9136
966262 XDOT = -2784
947317
YDOT = 12476
300507 feet/sec YDOT = 3802
776395 meter/sec
ZDOT = 18572
874168 ZDOT = 5661
012046
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 14351
56087827
00016717 00000-0 10270-3 0 9059
2 25544 51
6459 270
2409 0007187 142
2656 217
9001 15
52262588 39786
Satellite: ISS
Catalog Number: 25544
Epoch time: 14351
56087827 = yrday
fracday
Element set: 905
Inclination: 51
6459 deg
RA of node: 270
2409 deg
Eccentricity:
0007187
Arg of perigee: 142
2656 deg
Mean anomaly: 217
9001 deg
Mean motion: 15
52262588 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3978
Checksum: 329
Coasting Arc #7 (Orbit 3992)
---------------------------------------
Vector Time (GMT): 2014/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1703342
53 A = 6791282
91 meter
Y = 5947345
84 meter E =
0011586
Z = -2797101
41 I = 51
29472
XDOT = -4425
608133 Wp = 135
57897
YDOT = -3648
004821 meter/sec RA = 264
74071 deg
ZDOT = -5082
463356 TA = 76
28654
MA = 76
15759
Ha = 225
973 n
mi
Hp = 215
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5588394
11 X = -1756133
00
Y = 19512289
50 feet Y = 5928002
98 meter
Z = -9176841
88 Z = -2805503
91
XDOT = -14519
711722 XDOT = -4359
797179
YDOT = -11968
519754 feet/sec YDOT = -3697
126533 meter/sec
ZDOT = -16674
748543 ZDOT = -5103
802919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19100968
73 X = -5821975
27
Y = -6814212
22 feet Y = -2076971
88 meter
Z = -9213768
11 Z = -2808356
52
XDOT = 12404
240130 XDOT = 3780
812392
YDOT = -12194
184676 feet/sec YDOT = -3716
787489 meter/sec
ZDOT = -16765
064921 ZDOT = -5109
991788
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 14352
52655217
00016717 00000-0 10270-3 0 9061
2 25544 51
6469 265
4401 0007175 146
0479 214
1133 15
52308684 39937
Satellite: ISS
Catalog Number: 25544
Epoch time: 14352
52655217 = yrday
fracday
Element set: 906
Inclination: 51
6469 deg
RA of node: 265
4401 deg
Eccentricity:
0007175
Arg of perigee: 146
0479 deg
Mean anomaly: 214
1133 deg
Mean motion: 15
52308684 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3993
Checksum: 312
Coasting Arc #8 (Orbit 4008)
---------------------------------------
Vector Time (GMT): 2014/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2009443
77 A = 6788846
87 meter
Y = -5351211
45 meter E =
0016999
Z = 3655749
78 I = 51
29033
XDOT = 4351
389495 Wp = 114
91121
YDOT = 4601
509442 meter/sec RA = 259
74727 deg
ZDOT = 4320
889501 TA = 288
75596
MA = 288
94033
Ha = 225
881 n
mi
Hp = 215
801
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6592663
28 X = 2051374
33
Y = -17556468
00 feet Y = -5328506
41 meter
Z = 11993929
72 Z = 3665612
83
XDOT = 14276
212253 XDOT = 4278
621284
YDOT = 15096
815753 feet/sec YDOT = 4649
762255 meter/sec
ZDOT = 14176
146658 ZDOT = 4341
851752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17213058
40 X = 5246540
20
Y = 7373538
66 feet Y = 2247454
59 meter
Z = 12036971
21 Z = 3668868
83
XDOT = -15240
884638 XDOT = -4645
421638
YDOT = 12170
248361 feet/sec YDOT = 3709
491700 meter/sec
ZDOT = 14264
688507 ZDOT = 4347
877057
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 14353
55658017
00016717 00000-0 10270-3 0 9077
2 25544 51
6466 260
3196 0007179 149
6996 210
4572 15
52337890 40092
Satellite: ISS
Catalog Number: 25544
Epoch time: 14353
55658017 = yrday
fracday
Element set: 907
Inclination: 51
6466 deg
RA of node: 260
3196 deg
Eccentricity:
0007179
Arg of perigee: 149
6996 deg
Mean anomaly: 210
4572 deg
Mean motion: 15
52337890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4009
Checksum: 333
Coasting Arc #9 (Orbit 4023)
---------------------------------------
Vector Time (GMT): 2014/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2411517
90 A = 6786112
60 meter
Y = 4573247
48 meter E =
0012095
Z = -4403886
51 I = 51
28902
XDOT = -4246
728719 Wp = 105
29116
YDOT = -5434
227921 meter/sec RA = 254
74915 deg
ZDOT = -3328
555909 TA = 130
91105
MA = 130
80625
Ha = 225
670 n
mi
Hp = 215
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7911804
14 X = -2441085
03
Y = 15004092
79 feet Y = 4546115
46 meter
Z = -14448446
57 Z = -4415672
73
XDOT = -13932
837004 XDOT = -4169
477156
YDOT = -17828
831762 feet/sec YDOT = -5481
285313 meter/sec
ZDOT = -10920
459019 ZDOT = -3348
998941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14744250
11 X = -4494047
43
Y = -8297428
60 feet Y = -2529056
24 meter
Z = -14499545
55 Z = -4419461
48
XDOT = 17660
204080 XDOT = 5382
830204
YDOT = -12209
467559 feet/sec YDOT = -3721
445712 meter/sec
ZDOT = -11006
647070 ZDOT = -3354
826027
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 14354
52220713
00016717 00000-0 10270-3 0 9084
2 25544 51
6474 255
5188 0007103 153
5254 206
6262 15
52397141 40241
Satellite: ISS
Catalog Number: 25544
Epoch time: 14354
52220713 = yrday
fracday
Element set: 908
Inclination: 51
6474 deg
RA of node: 255
5188 deg
Eccentricity:
0007103
Arg of perigee: 153
5254 deg
Mean anomaly: 206
6262 deg
Mean motion: 15
52397141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4024
Checksum: 289
Coasting Arc #10 (Orbit 4039)
---------------------------------------
Vector Time (GMT): 2014/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2830630
66 A = 6783970
76 meter
Y = -3713523
56 meter E =
0012968
Z = 4917675
85 I = 51
29078
XDOT = 4124
194329 Wp = 140
84527
YDOT = 6077
937872 meter/sec RA = 249
74741 deg
ZDOT = 2202
707292 TA = 287
48457
MA = 287
62627
Ha = 225
537 n
mi
Hp = 215
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9286845
99 X = 2848057
27
Y = -12183476
23 feet Y = -3681772
72 meter
Z = 16134107
12 Z = 4931468
57
XDOT = 13530
821288 XDOT = 4045
222842
YDOT = 19940
741049 feet/sec YDOT = 6123
615486 meter/sec
ZDOT = 7226
729959 ZDOT = 2222
550917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12044042
96 X = 3671024
29
Y = 9364834
08 feet Y = 2854401
43 meter
Z = 16193607
57 Z = 4935811
59
XDOT = -19456
855538 XDOT = -5930
449568
YDOT = 12308
563676 feet/sec YDOT = 3751
650208 meter/sec
ZDOT = 7310
260600 ZDOT = 2228
167431
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 14355
55218554
00016717 00000-0 10270-3 0 9099
2 25544 51
6469 250
3980 0007134 157
7358 202
4105 15
52422687 40405
Satellite: ISS
Catalog Number: 25544
Epoch time: 14355
55218554 = yrday
fracday
Element set: 909
Inclination: 51
6469 deg
RA of node: 250
3980 deg
Eccentricity:
0007134
Arg of perigee: 157
7358 deg
Mean anomaly: 202
4105 deg
Mean motion: 15
52422687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4040
Checksum: 308
Coasting Arc #11 (Orbit 4054)
---------------------------------------
Vector Time (GMT): 2014/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3344118
47 A = 6782477
81 meter
Y = 2745332
89 meter E =
0017186
Z = -5236880
22 I = 51
29805
XDOT = -3901
924614 Wp = 106
46402
YDOT = -6518
567121 meter/sec RA = 244
74208 deg
ZDOT = -932
909989 TA = 154
59324
MA = 154
50864
Ha = 225
364 n
mi
Hp = 215
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10971517
30 X = -3349129
93
Y = 9006997
68 feet Y = 2707909
35 meter
Z = -17181365
54 Z = -5253137
27
XDOT = -12801
589940 XDOT = -3824
210719
YDOT = -21386
375070 feet/sec YDOT = -6561
766347 meter/sec
ZDOT = -3060
728311 ZDOT = -951
676855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9030690
89 X = -2752554
58
Y = -10841682
50 feet Y = -3304544
83 meter
Z = -17251204
70 Z = -5258167
19
XDOT = 20566
233636 XDOT = 6268
588012
YDOT = -12173
262129 feet/sec YDOT = -3710
410297 meter/sec
ZDOT = -3139
605805 ZDOT = -956
951849
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 14356
51776736
00016717 00000-0 10270-3 0 9109
2 25544 51
6469 245
5968 0007020 161
6070 198
5337 15
52474031 40554
Satellite: ISS
Catalog Number: 25544
Epoch time: 14356
51776736 = yrday
fracday
Element set: 910
Inclination: 51
6469 deg
RA of node: 245
5968 deg
Eccentricity:
0007020
Arg of perigee: 161
6070 deg
Mean anomaly: 198
5337 deg
Mean motion: 15
52474031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4055
Checksum: 317
Coasting Arc #12 (Orbit 4070)
---------------------------------------
Vector Time (GMT): 2014/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3863465
67 A = 6782074
38 meter
Y = -1770989
32 meter E =
0007379
Z = 5281327
67 I = 51
31099
XDOT = 3600
495008 Wp = 146
03437
YDOT = 6761
912410 meter/sec RA = 239
73649 deg
ZDOT = -372
167545 TA = 307
49627
MA = 307
56333
Ha = 225
103 n
mi
Hp = 216
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12675412
30 X = 3857327
41
Y = -5810332
40 feet Y = -1727820
38 meter
Z = 17327190
52 Z = 5300080
58
XDOT = 11812
647664 XDOT = 3526
421979
YDOT = 22184
752002 feet/sec YDOT = 6801
761352 meter/sec
ZDOT = -1221
022128 ZDOT = -354
856260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6053037
85 X = 1844965
94
Y = 12449779
29 feet Y = 3794692
73 meter
Z = 17407506
99 Z = 5305808
13
XDOT = -21041
700104 XDOT = -6413
510192
YDOT = 11809
774643 feet/sec YDOT = 3599
619311 meter/sec
ZDOT = -1148
376238 ZDOT = -350
025077
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 14357
54769749
00016717 00000-0 10270-3 0 9110
2 25544 51
6465 240
4756 0006999 166
4294 193
7047 15
52518057 40714
Satellite: ISS
Catalog Number: 25544
Epoch time: 14357
54769749 = yrday
fracday
Element set: 911
Inclination: 51
6465 deg
RA of node: 240
4756 deg
Eccentricity:
0006999
Arg of perigee: 166
4294 deg
Mean anomaly: 193
7047 deg
Mean motion: 15
52518057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4071
Checksum: 348
Coasting Arc #13 (Orbit 4085)
---------------------------------------
Vector Time (GMT): 2014/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4433092
17 A = 6782919
43 meter
Y = 784178
73 meter E =
0017278
Z = -5088410
61 I = 51
33012
XDOT = -3138
724056 Wp = 124
56871
YDOT = -6773
593973 meter/sec RA = 234
73100 deg
ZDOT = 1685
103943 TA = 161
84230
MA = 161
78052
Ha = 225
052 n
mi
Hp = 216
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14544265
65 X = -4416814
03
Y = 2572764
87 feet Y = 734696
46 meter
Z = -16694260
54 Z = -5109906
07
XDOT = -10297
651102 XDOT = -3070
932453
YDOT = -22223
077339 feet/sec YDOT = -6808
314316 meter/sec
ZDOT = 5528
556243 ZDOT = 1670
020763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3099753
15 X = -944804
76
Y = -14334265
04 feet Y = -4369083
98 meter
Z = -16786110
13 Z = -5116406
37
XDOT = 20782
837993 XDOT = 6334
609020
YDOT = -10915
542659 feet/sec YDOT = -3327
057402 meter/sec
ZDOT = 5465
396756 ZDOT = 1665
852931
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
51323638
00016717 00000-0 10270-3 0 9122
2 25544 51
6460 235
6735 0006918 170
2244 189
9043 15
52537063 40868
Satellite: ISS
Catalog Number: 25544
Epoch time: 14358
51323638 = yrday
fracday
Element set: 912
Inclination: 51
6460 deg
RA of node: 235
6735 deg
Eccentricity:
0006918
Arg of perigee: 170
2244 deg
Mean anomaly: 189
9043 deg
Mean motion: 15
52537063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4086
Checksum: 314
Coasting Arc #14 (Orbit 4101)
---------------------------------------
Vector Time (GMT): 2014/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4958628
66 A = 6784591
18 meter
Y = 138387
14 meter E =
0008662
Z = 4620000
69 I = 51
35520
XDOT = 2542
374845 Wp = 112
27682
YDOT = 6620
253722 meter/sec RA = 229
73001 deg
ZDOT = -2925
843227 TA = 6
95918
MA = 6
94716
Ha = 224
674 n
mi
Hp = 216
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16268466
75 X = 4934270
50
Y = 454026
04 feet Y = 193701
26 meter
Z = 15157482
57 Z = 4644029
51
XDOT = 8341
124818 XDOT = 2482
369265
YDOT = 21719
992527 feet/sec YDOT = 6648
348880 meter/sec
ZDOT = -9599
223187 ZDOT = -2913
638239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 417091
53 X = 127129
50
Y = 16173347
90 feet Y = 4929636
44 meter
Z = 15259989
51 Z = 4651244
80
XDOT = -20055
210737 XDOT = -6112
828233
YDOT = 9529
905589 feet/sec YDOT = 2904
715223 meter/sec
ZDOT = -9548
297797 ZDOT = -2910
321168
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
54311999
00016717 00000-0 10270-3 0 9134
2 25544 51
6459 230
5518 0006800 174
7977 185
3246 15
52602195 41024
Satellite: ISS
Catalog Number: 25544
Epoch time: 14359
54311999 = yrday
fracday
Element set: 913
Inclination: 51
6459 deg
RA of node: 230
5518 deg
Eccentricity:
0006800
Arg of perigee: 174
7977 deg
Mean anomaly: 185
3246 deg
Mean motion: 15
52602195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4102
Checksum: 322
Coasting Arc #15 (Orbit 4116)
---------------------------------------
Vector Time (GMT): 2014/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5454476
92 A = 6787147
07 meter
Y = -985550
04 meter E =
0010976
Z = -3929628
12 I = 51
38399
XDOT = -1765
820475 Wp = 143
46585
YDOT = -6270
361876 meter/sec RA = 224
73332 deg
ZDOT = 4020
804725 TA = 168
78507
MA = 168
76059
Ha = 224
721 n
mi
Hp = 216
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17895265
47 X = -5423962
27
Y = -3233431
90 feet Y = -1046374
75 meter
Z = -12892480
72 Z = -3956050
77
XDOT = -5793
374262 XDOT = -1715
104093
YDOT = -20572
053398 feet/sec YDOT = -6289
825034 meter/sec
ZDOT = 13191
616551 ZDOT = 4012
349639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1960287
19 X = 597495
53
Y = -17998254
61 feet Y = -5485868
00 meter
Z = -13005067
18 Z = -3963944
48
XDOT = 18788
652887 XDOT = 5726
781400
YDOT = -7466
899701 feet/sec YDOT = -2275
911029 meter/sec
ZDOT = 13156
616039 ZDOT = 4010
136569
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
50861635
00016717 00000-0 10270-3 0 9140
2 25544 51
6452 225
7491 0006828 178
8396 181
2773 15
52598208 41178
Satellite: ISS
Catalog Number: 25544
Epoch time: 14360
50861635 = yrday
fracday
Element set: 914
Inclination: 51
6452 deg
RA of node: 225
7491 deg
Eccentricity:
0006828
Arg of perigee: 178
8396 deg
Mean anomaly: 181
2773 deg
Mean motion: 15
52598208 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4117
Checksum: 332
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