[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 17th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 37673 69 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 3977)
---------------------------------------
Vector Time (GMT): 2014/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1445190
11 A = 6793036
69 meter
Y = -6372841
44 meter E =
0017198
Z = 1840999
57 I = 51
29878
XDOT = 4503
555582 Wp = 90
38057
YDOT = 2653
822351 meter/sec RA = 269
73200 deg
ZDOT = 5605
556120 TA = 289
95216
MA = 290
13732
Ha = 226
013 n
mi
Hp = 215
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4741437
38 X = 1507402
25
Y = -20908272
45 feet Y = -6356332
63 meter
Z = 6040024
82 Z = 1848170
96
XDOT = 14775
444824 XDOT = 4446
314989
YDOT = 8706
766244 feet/sec YDOT = 2703
863711 meter/sec
ZDOT = 18390
932151 ZDOT = 5627
295035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20441449
41 X = 6230553
78
Y = 6434248
63 feet Y = 1961158
98 meter
Z = 6071785
24 Z = 1850680
14
XDOT = -9434
036876 XDOT = -2875
494440
YDOT = 12389
153881 feet/sec YDOT = 3776
214103 meter/sec
ZDOT = 18483
127926 ZDOT = 5633
657392
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
56073791
00016717 00000-0 10270-3 0 9009
2 25544 51
6460 270
2430 0007236 142
4564 217
7094 15
52357720 39780
Satellite: ISS
Catalog Number: 25544
Epoch time: 14351
56073791 = yrday
fracday
Element set: 900
Inclination: 51
6460 deg
RA of node: 270
2430 deg
Eccentricity:
0007236
Arg of perigee: 142
4564 deg
Mean anomaly: 217
7094 deg
Mean motion: 15
52357720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3978
Checksum: 303
Coasting Arc #2 (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 = -1781920
20 A = 6790709
73 meter
Y = 5880731
85 meter E =
0011433
Z = -2886957
76 I = 51
29380
XDOT = -4386
118888 Wp = 134
42487
YDOT = -3782
500713 meter/sec RA = 264
74134 deg
ZDOT = -5017
896206 TA = 78
59387
MA = 78
46546
Ha = 225
795 n
mi
Hp = 215
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5846194
90 X = -1833523
45
Y = 19293739
67 feet Y = 5860516
93 meter
Z = -9471646
20 Z = -2895739
10
XDOT = -14390
153833 XDOT = -4319
120555
YDOT = -12409
779243 feet/sec YDOT = -3831
174196 meter/sec
ZDOT = -16462
914063 ZDOT = -5039
041060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18865872
94 X = -5750318
07
Y = -7055059
68 feet Y = -2150382
19 meter
Z = -9510175
49 Z = -2898701
49
XDOT = 12818
425158 XDOT = 3907
055988
YDOT = -12054
083311 feet/sec YDOT = -3674
084593 meter/sec
ZDOT = -16552
375369 ZDOT = -5045
164013
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
52634385
00016717 00000-0 10270-3 0 9019
2 25544 51
6470 265
4418 0007234 146
3768 213
7844 15
52430452 39930
Satellite: ISS
Catalog Number: 25544
Epoch time: 14352
52634385 = yrday
fracday
Element set: 901
Inclination: 51
6470 deg
RA of node: 265
4418 deg
Eccentricity:
0007234
Arg of perigee: 146
3768 deg
Mean anomaly: 213
7844 deg
Mean motion: 15
52430452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3993
Checksum: 313
Coasting Arc #3 (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 = 2118408
85 A = 6788078
13 meter
Y = -5232591
74 meter E =
0016904
Z = 3763100
24 I = 51
28898
XDOT = 4284
992247 Wp = 116
89690
YDOT = 4772
060576 meter/sec RA = 259
74647 deg
ZDOT = 4201
188722 TA = 288
40544
MA = 288
58916
Ha = 225
664 n
mi
Hp = 215
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6950160
28 X = 2158483
40
Y = -17167295
74 feet Y = -5208678
58 meter
Z = 12346129
40 Z = 3773488
13
XDOT = 14058
373515 XDOT = 4210
903301
YDOT = 15656
366720 feet/sec YDOT = 4819
563518 meter/sec
ZDOT = 13783
427565 ZDOT = 4221
825229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16806826
88 X = 5122720
83
Y = 7709200
81 feet Y = 2349764
41 meter
Z = 12391387
13 Z = 3776894
80
XDOT = -15764
635759 XDOT = -4805
060979
YDOT = 11957
220383 feet/sec YDOT = 3644
560773 meter/sec
ZDOT = 13870
549035 ZDOT = 4227
743346
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
55628255
00016717 00000-0 10270-3 0 9023
2 25544 51
6466 260
3207 0007256 150
2268 209
9298 15
52484392 40099
Satellite: ISS
Catalog Number: 25544
Epoch time: 14353
55628255 = yrday
fracday
Element set: 902
Inclination: 51
6466 deg
RA of node: 260
3207 deg
Eccentricity:
0007256
Arg of perigee: 150
2268 deg
Mean anomaly: 209
9298 deg
Mean motion: 15
52484392 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4009
Checksum: 316
Coasting Arc #4 (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 = -2554334
18 A = 6785191
98 meter
Y = 4384228
06 meter E =
0012632
Z = -4513729
16 I = 51
28740
XDOT = -4139
373182 Wp = 104
24253
YDOT = -5628
495648 meter/sec RA = 254
74628 deg
ZDOT = -3134
976175 TA = 134
16468
MA = 134
06078
Ha = 225
415 n
mi
Hp = 215
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8380361
48 X = -2581243
45
Y = 14383950
33 feet Y = 4355513
85 meter
Z = -14808822
71 Z = -4526202
73
XDOT = -13580
620675 XDOT = -4060
897603
YDOT = -18466
193072 feet/sec YDOT = -5674
345697 meter/sec
ZDOT = -10285
354904 ZDOT = -3154
894733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14109440
43 X = -4300557
44
Y = -8743571
10 feet Y = -2665040
47 meter
Z = -14862818
41 Z = -4530187
05
XDOT = 18253
479371 XDOT = 5563
660512
YDOT = -11887
304795 feet/sec YDOT = -3623
250501 meter/sec
ZDOT = -10369
270804 ZDOT = -3160
553741
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
52181008
00016717 00000-0 10270-3 0 9032
2 25544 51
6474 255
5192 0007189 154
1546 205
9966 15
52569391 40242
Satellite: ISS
Catalog Number: 25544
Epoch time: 14354
52181008 = yrday
fracday
Element set: 903
Inclination: 51
6474 deg
RA of node: 255
5192 deg
Eccentricity:
0007189
Arg of perigee: 154
1546 deg
Mean anomaly: 205
9966 deg
Mean motion: 15
52569391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4024
Checksum: 318
Coasting Arc #5 (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 = 3009480
07 A = 6782997
05 meter
Y = -3439494
64 meter E =
0012429
Z = 5008666
54 I = 51
28926
XDOT = 3959
362343 Wp = 143
33443
YDOT = 6280
231351 meter/sec RA = 249
74202 deg
ZDOT = 1921
412497 TA = 287
86894
MA = 288
00446
Ha = 225
229 n
mi
Hp = 215
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9873622
26 X = 3023387
13
Y = -11284431
25 feet Y = -3405763
49 meter
Z = 16432633
01 Z = 5023319
57
XDOT = 12990
033934 XDOT = 3879
507454
YDOT = 20604
433566 feet/sec YDOT = 6324
060799 meter/sec
ZDOT = 6303
846775 ZDOT = 1940
453269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11136371
54 X = 3394366
05
Y = 9936276
77 feet Y = 3028577
16 meter
Z = 16495752
96 Z = 5027905
50
XDOT = -20070
763419 XDOT = -6117
568690
YDOT = 11829
998938 feet/sec YDOT = 3605
783676 meter/sec
ZDOT = 6383
916514 ZDOT = 1945
817753
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
55166576
00016717 00000-0 10270-3 0 9040
2 25544 51
6469 250
3976 0007230 158
6518 201
4937 15
52622062 40406
Satellite: ISS
Catalog Number: 25544
Epoch time: 14355
55166576 = yrday
fracday
Element set: 904
Inclination: 51
6469 deg
RA of node: 250
3976 deg
Eccentricity:
0007230
Arg of perigee: 158
6518 deg
Mean anomaly: 201
4937 deg
Mean motion: 15
52622062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4040
Checksum: 310
Coasting Arc #6 (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 = -3555202
88 A = 6781649
03 meter
Y = 2375335
87 meter E =
0017713
Z = -5278055
71 I = 51
29720
XDOT = -3657
621947 Wp = 108
77690
YDOT = -6700
454292 meter/sec RA = 244
73390 deg
ZDOT = -558
901631 TA = 155
89582
MA = 155
81282
Ha = 225
034 n
mi
Hp = 215
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11664051
44 X = -3555861
24
Y = 7793096
68 feet Y = 2335576
18 meter
Z = -17316455
73 Z = -5295327
64
XDOT = -12000
072003 XDOT = -3579
709107
YDOT = -21983
117755 feet/sec YDOT = -6740
920495 meter/sec
ZDOT = -1833
666770 ZDOT = -576
481252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7818392
08 X = -2383045
91
Y = -11536175
84 feet Y = -3516226
40 meter
Z = -17390557
31 Z = -5300641
87
XDOT = 21114
067142 XDOT = 6435
567665
YDOT = -11469
310980 feet/sec YDOT = -3495
845987 meter/sec
ZDOT = -1907
447309 ZDOT = -581
389940
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
51711758
00016717 00000-0 10270-3 0 9056
2 25544 51
6469 245
5955 0007125 162
5790 197
5608 15
52693209 40555
Satellite: ISS
Catalog Number: 25544
Epoch time: 14356
51711758 = yrday
fracday
Element set: 905
Inclination: 51
6469 deg
RA of node: 245
5955 deg
Eccentricity:
0007125
Arg of perigee: 162
5790 deg
Mean anomaly: 197
5608 deg
Mean motion: 15
52693209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4055
Checksum: 335
Coasting Arc #7 (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 = 4098923
59 A = 6781524
01 meter
Y = -1300778
54 meter E =
0006895
Z = 5239215
19 I = 51
31137
XDOT = 3251
101585 Wp = 140
86424
YDOT = 6897
006043 meter/sec RA = 239
72578 deg
ZDOT = -835
796075 TA = 317
13335
MA = 317
18708
Ha = 224
700 n
mi
Hp = 215
799
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13447912
05 X = 4087714
39
Y = -4267646
14 feet Y = -1255004
92 meter
Z = 17189026
23 Z = 5259099
64
XDOT = 10666
343784 XDOT = 3177
796011
YDOT = 22627
972582 feet/sec YDOT = 6932
952178 meter/sec
ZDOT = -2742
113108 ZDOT = -820
180201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4525762
83 X = 1379452
51
Y = 13253119
80 feet Y = 4039550
92 meter
Z = 17274086
12 Z = 5265141
45
XDOT = -21448
314888 XDOT = -6537
446378
YDOT = 10793
350381 feet/sec YDOT = 3289
813196 meter/sec
ZDOT = -2676
723973 ZDOT = -815
865467
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
54689280
00016717 00000-0 10270-3 0 9065
2 25544 51
6464 240
4733 0007088 167
6301 192
5026 15
52767918 40716
Satellite: ISS
Catalog Number: 25544
Epoch time: 14357
54689280 = yrday
fracday
Element set: 906
Inclination: 51
6464 deg
RA of node: 240
4733 deg
Eccentricity:
0007088
Arg of perigee: 167
6301 deg
Mean anomaly: 192
5026 deg
Mean motion: 15
52767918 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4071
Checksum: 325
Coasting Arc #8 (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 = -4673712
36 A = 6782826
64 meter
Y = 218655
27 meter E =
0016561
Z = -4925540
45 I = 51
33220
XDOT = -2659
077405 Wp = 129
04816
YDOT = -6826
729234 meter/sec RA = 234
71851 deg
ZDOT = 2214
876677 TA = 162
73465
MA = 162
67826
Ha = 224
642 n
mi
Hp = 215
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15333701
95 X = -4651883
67
Y = 717372
94 feet Y = 166513
25 meter
Z = -16159909
63 Z = -4948191
36
XDOT = -8724
007234 XDOT = -2593
300711
YDOT = -22397
405622 feet/sec YDOT = -6856
097166 meter/sec
ZDOT = 7266
655765 ZDOT = 2202
118625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1274778
41 X = -388552
46
Y = -15194668
85 feet Y = -4631335
07 meter
Z = -16256589
35 Z = -4955008
43
XDOT = 20951
535416 XDOT = 6386
027995
YDOT = -9493
448143 feet/sec YDOT = -2893
602994 meter/sec
ZDOT = 7213
425878 ZDOT = 2198
652208
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
51227202
00016717 00000-0 10270-3 0 9076
2 25544 51
6459 235
6702 0007028 171
4574 188
6699 15
52803001 40863
Satellite: ISS
Catalog Number: 25544
Epoch time: 14358
51227202 = yrday
fracday
Element set: 907
Inclination: 51
6459 deg
RA of node: 235
6702 deg
Eccentricity:
0007028
Arg of perigee: 171
4574 deg
Mean anomaly: 188
6699 deg
Mean motion: 15
52803001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4086
Checksum: 313
Coasting Arc #9 (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 = 5177623
34 A = 6784950
46 meter
Y = 788820
16 meter E =
0010421
Z = 4302596
06 I = 51
35901
XDOT = 1903
477346 Wp = 112
00052
YDOT = 6561
930564 meter/sec RA = 229
71670 deg
ZDOT = -3490
661423 TA = 13
63862
MA = 13
61048
Ha = 224
219 n
mi
Hp = 215
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16986953
22 X = 5147517
43
Y = 2587992
64 feet Y = 846551
10 meter
Z = 14116128
79 Z = 4327674
79
XDOT = 6245
004416 XDOT = 1846
915099
YDOT = 21528
643584 feet/sec YDOT = 6582
900444 meter/sec
ZDOT = -11452
301255 ZDOT = -3481
551704
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1674588
15 X = -510414
47
Y = 17012387
69 feet Y = 5185375
77 meter
Z = 14223002
40 Z = 4335171
13
XDOT = -19915
154145 XDOT = -6070
138983
YDOT = 7590
776355 feet/sec YDOT = 2313
668633 meter/sec
ZDOT = -11414
573196 ZDOT = -3479
161910
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
54196962
00016717 00000-0 10270-3 0 9089
2 25544 51
6458 230
5472 0006896 175
8815 184
2395 15
52891952 41024
Satellite: ISS
Catalog Number: 25544
Epoch time: 14359
54196962 = yrday
fracday
Element set: 908
Inclination: 51
6458 deg
RA of node: 230
5472 deg
Eccentricity:
0006896
Arg of perigee: 175
8815 deg
Mean anomaly: 184
2395 deg
Mean motion: 15
52891952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4102
Checksum: 347
Coasting Arc #10 (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 = -5611286
22 A = 6787795
71 meter
Y = -1699371
88 meter E =
0008665
Z = -3432089
51 I = 51
38900
XDOT = -953
015033 Wp = 145
56684
YDOT = -6073
255141 meter/sec RA = 224
72038 deg
ZDOT = 4563
914744 TA = 174
15344
MA = 174
14332
Ha = 224
223 n
mi
Hp = 216
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18409731
70 X = -5575194
65
Y = -5575367
07 feet Y = -1761918
97 meter
Z = -11260136
20 Z = -3459260
40
XDOT = -3126
689742 XDOT = -907
201373
YDOT = -19925
377759 feet/sec YDOT = -6083
656418 meter/sec
ZDOT = 14973
473571 ZDOT = 4559
396200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4258848
87 X = 1298097
14
Y = -18688155
45 feet Y = -5696149
78 meter
Z = -11375792
65 Z = -3467341
60
XDOT = 18281
880404 XDOT = 5572
317147
YDOT = -4939
887319 feet/sec YDOT = -1505
677655 meter/sec
ZDOT = 14955
237897 ZDOT = 4558
356511
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
50727656
00016717 00000-0 10270-3 0 9098
2 25544 51
6451 225
7432 0006926 180
3327 179
7821 15
52908671 41178
Satellite: ISS
Catalog Number: 25544
Epoch time: 14360
50727656 = yrday
fracday
Element set: 909
Inclination: 51
6451 deg
RA of node: 225
7432 deg
Eccentricity:
0006926
Arg of perigee: 180
3327 deg
Mean anomaly: 179
7821 deg
Mean motion: 15
52908671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4117
Checksum: 320
Coasting Arc #11 (Orbit 4132)
---------------------------------------
Vector Time (GMT): 2014/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5870752
20 A = 6790335
29 meter
Y = 2477656
77 meter E =
0016766
Z = 2315690
23 I = 51
42129
XDOT = -168
562263 Wp = 130
59415
YDOT = 5454
961655 meter/sec RA = 219
73235 deg
ZDOT = -5394
162633 TA = 23
49918
MA = 23
42266
Ha = 223
912 n
mi
Hp = 216
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19260998
04 X = 5831361
39
Y = 8128795
19 feet Y = 2543087
01 meter
Z = 7597408
89 Z = 2344113
60
XDOT = -553
025797 XDOT = -203
345578
YDOT = 17896
855824 feet/sec YDOT = 5452
882375 meter/sec
ZDOT = -17697
383968 ZDOT = -5395
065782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6402747
25 X = -1951557
36
Y = 19854893
51 feet Y = 6051771
54 meter
Z = 7718290
63 Z = 2352534
99
XDOT = -16416
523614 XDOT = -5003
756398
YDOT = 1606
325858 feet/sec YDOT = 489
608122 meter/sec
ZDOT = -17702
170380 ZDOT = -5395
621532
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
53689873
00016717 00000-0 10270-3 0 9102
2 25544 51
6453 220
6197 0006862 183
5541 176
5564 15
52977483 41338
Satellite: ISS
Catalog Number: 25544
Epoch time: 14361
53689873 = yrday
fracday
Element set: 910
Inclination: 51
6453 deg
RA of node: 220
6197 deg
Eccentricity:
0006862
Arg of perigee: 183
5541 deg
Mean anomaly: 176
5564 deg
Mean motion: 15
52977483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4133
Checksum: 334
Coasting Arc #12 (Orbit 4147)
---------------------------------------
Vector Time (GMT): 2014/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5950292
48 A = 6792039
17 meter
Y = -3098965
97 meter E =
0004883
Z = -1060849
25 I = 51
45121
XDOT = 1412
496896 Wp = 82
54991
YDOT = -4713
710544 meter/sec RA = 214
74933 deg
ZDOT = 5870
961727 TA = 265
93039
MA = 265
98621
Ha = 223
783 n
mi
Hp = 216
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19521956
97 X = -5910043
66
Y = -10167211
19 feet Y = -3165280
93 meter
Z = -3480476
54 Z = -1089657
03
XDOT = 4634
176169 XDOT = 1436
582717
YDOT = -15464
929606 feet/sec YDOT = -4697
780594 meter/sec
ZDOT = 19261
685456 ZDOT = 5877
881741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8056733
65 X = 2455692
42
Y = -20462179
95 feet Y = -6236872
45 meter
Z = -3602906
97 Z = -1098166
04
XDOT = 14360
346509 XDOT = 4377
033616
YDOT = 2270
674753 feet/sec YDOT = 692
101665 meter/sec
ZDOT = 19292
021364 ZDOT = 5880
208112
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
50213316
00016717 00000-0 10270-3 0 9116
2 25544 51
6444 215
8151 0006842 188
6418 171
4618 15
53018705 41485
Satellite: ISS
Catalog Number: 25544
Epoch time: 14362
50213316 = yrday
fracday
Element set: 911
Inclination: 51
6444 deg
RA of node: 215
8151 deg
Eccentricity:
0006842
Arg of perigee: 188
6418 deg
Mean anomaly: 171
4618 deg
Mean motion: 15
53018705 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4148
Checksum: 295
Coasting Arc #13 (Orbit 4163)
---------------------------------------
Vector Time (GMT): 2014/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5754827
30 A = 6792414
58 meter
Y = 3575801
60 meter E =
0016488
Z = -309367
37 I = 51
47894
XDOT = -2752
065949 Wp = 157
43145
YDOT = 3921
151357 meter/sec RA = 209
77199 deg
ZDOT = -5992
352439 TA = 25
91086
MA = 25
82839
Ha = 223
633 n
mi
Hp = 216
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18880667
00 X = 5715916
94
Y = 11731632
55 feet Y = 3639938
27 meter
Z = -1014984
80 Z = -281505
75
XDOT = -9029
087758 XDOT = -2766
599873
YDOT = 12864
669806 feet/sec YDOT = 3890
294928 meter/sec
ZDOT = -19659
948946 ZDOT = -6005
756673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9330842
02 X = -2844040
65
Y = 20180990
33 feet Y = 6151165
85 meter
Z = -896660
03 Z = -273301
98
XDOT = -12384
717024 XDOT = -3774
861749
YDOT = -6582
288369 feet/sec YDOT = -2006
281495 meter/sec
ZDOT = -19717
828775 ZDOT = -6009
994211
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
53167959
00016717 00000-0 10270-3 0 9122
2 25544 51
6442 210
6913 0006934 192
4050 167
6932 15
53058476 41642
Satellite: ISS
Catalog Number: 25544
Epoch time: 14363
53167959 = yrday
fracday
Element set: 912
Inclination: 51
6442 deg
RA of node: 210
6913 deg
Eccentricity:
0006934
Arg of perigee: 192
4050 deg
Mean anomaly: 167
6932 deg
Mean motion: 15
53058476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4164
Checksum: 318
Coasting Arc #14 (Orbit 4179)
---------------------------------------
Vector Time (GMT): 2014/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5309294
38 A = 6791041
46 meter
Y = -3896898
58 meter E =
0010410
Z = 1648554
36 I = 51
50200
XDOT = 4066
288296 Wp = 92
36478
YDOT = -3115
450610 meter/sec RA = 204
79376 deg
ZDOT = 5699
785126 TA = 285
71044
MA = 285
82525
Ha = 223
333 n
mi
Hp = 216
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17418944
82 X = -5273331
87
Y = -12785100
34 feet Y = -3956069
57 meter
Z = 5408642
91 Z = 1622849
80
XDOT = 13340
840865 XDOT = 4073
136157
YDOT = -10221
294653 feet/sec YDOT = -3069
940733 meter/sec
ZDOT = 18700
082434 ZDOT = 5719
554986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10225106
87 X = 3116612
57
Y = -19065508
82 feet Y = -5811167
09 meter
Z = 5299567
01 Z = 1615308
02
XDOT = 10573
774613 XDOT = 3222
886502
YDOT = 10921
890458 feet/sec YDOT = 3328
992212 meter/sec
ZDOT = 18785
006081 ZDOT = 5725
669854
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
56118430
00016717 00000-0 10270-3 0 9137
2 25544 51
6432 205
5657 0006920 197
2101 162
8817 15
53160181 41808
Satellite: ISS
Catalog Number: 25544
Epoch time: 14364
56118430 = yrday
fracday
Element set: 913
Inclination: 51
6432 deg
RA of node: 205
5657 deg
Eccentricity:
0006920
Arg of perigee: 197
2101 deg
Mean anomaly: 162
8817 deg
Mean motion: 15
53160181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4180
Checksum: 289
Coasting Arc #15 (Orbit 4194)
---------------------------------------
Vector Time (GMT): 2014/365/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4541574
23 A = 6788492
70 meter
Y = 4105845
74 meter E =
0008502
Z = -2923029
43 I = 51
52174
XDOT = -5317
114553 Wp = 168
64045
YDOT = 2319
769772 meter/sec RA = 199
81452 deg
ZDOT = -5013
487549 TA = 44
75127
MA = 44
68271
Ha = 223
153 n
mi
Hp = 216
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14900177
92 X = 4509523
24
Y = 13470622
51 feet Y = 4156453
56 meter
Z = -9589991
56 Z = -2901044
76
XDOT = -17444
601551 XDOT = -5318
305765
YDOT = 7610
793215 feet/sec YDOT = 2260
304013 meter/sec
ZDOT = -16448
449963 ZDOT = -5039
319986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10962384
43 X = -3341334
78
Y = 16884237
02 feet Y = 5146315
44 meter
Z = -9496819
41 Z = -2894630
56
XDOT = -8998
098026 XDOT = -2742
620278
YDOT = -15136
293115 feet/sec YDOT = -4613
542141 meter/sec
ZDOT = -16559
133725 ZDOT = -5047
223959
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 14365
52631125
00016717 00000-0 10270-3 0 9146
2 25544 51
6422 200
7614 0006776 200
9664 159
1212 15
53194499 41955
Satellite: ISS
Catalog Number: 25544
Epoch time: 14365
52631125 = yrday
fracday
Element set: 914
Inclination: 51
6422 deg
RA of node: 200
7614 deg
Eccentricity:
0006776
Arg of perigee: 200
9664 deg
Mean anomaly: 159
1212 deg
Mean motion: 15
53194499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4195
Checksum: 305
Coasting Arc #16 (Orbit 4210)
---------------------------------------
Vector Time (GMT): 2014/366/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3534305
39 A = 6785225
50 meter
Y = -4206628
66 meter E =
0011313
Z = 3980914
82 I = 51
54075
XDOT = 6364
502460 Wp = 136
08309
YDOT = -1576
617605 meter/sec RA = 194
82935 deg
ZDOT = 3969
708632 TA = 272
44586
MA = 272
57538
Ha = 222
886 n
mi
Hp = 216
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11595490
14 X = -3506341
10
Y = -13801275
12 feet Y = -4245995
51 meter
Z = 13060744
14 Z = 3963813
34
XDOT = 20880
913583 XDOT = 6362
376086
YDOT = -5172
629939 feet/sec YDOT = -1505
457811 meter/sec
ZDOT = 13023
978453 ZDOT = 4000
621024
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11565097
18 X = 3525041
62
Y = -13894707
22 feet Y = -4235106
76 meter
Z = 12988428
02 Z = 3958872
86
XDOT = 7687
648966 XDOT = 2343
195405
YDOT = 18742
390020 feet/sec YDOT = 5712
680478 meter/sec
ZDOT = 13156
243844 ZDOT = 4010
023124
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 14366
55574005
00016717 00000-0 10270-3 0 9154
2 25544 51
6416 195
6354 0006795 205
7308 154
3507 15
53258720 42111
Satellite: ISS
Catalog Number: 25544
Epoch time: 14366
55574005 = yrday
fracday
Element set: 915
Inclination: 51
6416 deg
RA of node: 195
6354 deg
Eccentricity:
0006795
Arg of perigee: 205
7308 deg
Mean anomaly: 154
3507 deg
Mean motion: 15
53258720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4211
Checksum: 309
Coasting Arc #17 (Orbit 4225)
---------------------------------------
Vector Time (GMT): 2014/367/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2254258
18 A = 6782030
77 meter
Y = 4247819
33 meter E =
0007881
Z = -4787782
32 I = 51
56046
XDOT = -7152
340923 Wp = 107
77525
YDOT = 861
429933 meter/sec RA = 189
83902 deg
ZDOT = -2609
194614 TA = 136
48537
MA = 136
42315
Ha = 222
666 n
mi
Hp = 216
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7395860
16 X = 2229847
83
Y = 13936415
12 feet Y = 4272891
85 meter
Z = -15707947
25 Z = -4776890
46
XDOT = -23465
685444 XDOT = -7148
767541
YDOT = 2826
213692 feet/sec YDOT = 781
468027 meter/sec
ZDOT = -8560
349783 ZDOT = -2643
930617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12253145
18 X = -3734758
65
Y = 10010974
41 feet Y = 3051345
00 meter
Z = -15662146
89 Z = -4773822
37
XDOT = -6500
836767 XDOT = -1981
455047
YDOT = -21551
448932 feet/sec YDOT = -6568
881634 meter/sec
ZDOT = -8708
843682 ZDOT = -2654
455554
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 14367
52079339
00016717 00000-0 10270-3 0 9163
2 25544 51
6407 190
8299 0006693 207
7862 152
2934 15
53320839 42268
Satellite: ISS
Catalog Number: 25544
Epoch time: 14367
52079339 = yrday
fracday
Element set: 916
Inclination: 51
6407 deg
RA of node: 190
8299 deg
Eccentricity:
0006693
Arg of perigee: 207
7862 deg
Mean anomaly: 152
2934 deg
Mean motion: 15
53320839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4226
Checksum: 335
Coasting Arc #18 (Orbit 4241)
---------------------------------------
Vector Time (GMT): 2014/368/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -839266
78 A = 6780081
22 meter
Y = -4233722
42 meter E =
0007716
Z = 5230313
08 I = 51
58501
XDOT = 7591
014454 Wp = 182
48038
YDOT = -194
686767 meter/sec RA = 184
84431 deg
ZDOT = 1052
993839 TA = 257
38014
MA = 257
46643
Ha = 222
502 n
mi
Hp = 216
875
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2753499
93 X = -817268
78
Y = -13890165
44 feet Y = -4242985
14 meter
Z = 17159819
82 Z = 5226289
13
XDOT = 24904
903064 XDOT = 7587
512266
YDOT = -638
736113 feet/sec YDOT = -109
818797 meter/sec
ZDOT = 3454
704197 ZDOT = 1089
860932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12993925
48 X = 3960548
49
Y = -5678159
52 feet Y = -1730703
02 meter
Z = 17143345
04 Z = 5225291
57
XDOT = 5367
232444 XDOT = 1635
932449
YDOT = 23262
502537 feet/sec YDOT = 7090
410773 meter/sec
ZDOT = 3612
211302 ZDOT = 1101
002005
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 14368
55014507
00016717 00000-0 10270-3 0 9174
2 25544 51
6404 185
7035 0006600 211
9145 148
1608 15
53329702 42423
Satellite: ISS
Catalog Number: 25544
Epoch time: 14368
55014507 = yrday
fracday
Element set: 917
Inclination: 51
6404 deg
RA of node: 185
7035 deg
Eccentricity:
0006600
Arg of perigee: 211
9145 deg
Mean anomaly: 148
1608 deg
Mean motion: 15
53329702 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4242
Checksum: 291
Coasting Arc #19 (Orbit 4256)
---------------------------------------
Vector Time (GMT): 2014/369/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -694606
45 A = 6779479
37 meter
Y = 4193437
61 meter E =
0012693
Z = -5291415
96 I = 51
61557
XDOT = -7619
241079 Wp = 121
69725
YDOT = -471
699319 meter/sec RA = 179
84825 deg
ZDOT = 620
940779 TA = 154
27093
MA = 154
20774
Ha = 222
168 n
mi
Hp = 216
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2278892
55 X = -715743
25
Y = 13757997
40 feet Y = 4185552
38 meter
Z = -17360288
59 Z = -5294841
16
XDOT = -24997
510103 XDOT = -7616
416430
YDOT = -1547
569943 feet/sec YDOT = -556
886883 meter/sec
ZDOT = 2037
207281 ZDOT = 583
935000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13892654
99 X = -4234481
24
Y = 968089
97 feet Y = 295073
82 meter
Z = -17375626
69 Z = -5296091
02
XDOT = -4024
580019 XDOT = -1226
691990
YDOT = -23707
750162 feet/sec YDOT = -7226
122250 meter/sec
ZDOT = 1879
195329 ZDOT = 572
778736
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 14369
51512223
00016717 00000-0 10270-3 0 9180
2 25544 51
6404 180
8973 0006637 214
9970 145
0752 15
53437080 42570
Satellite: ISS
Catalog Number: 25544
Epoch time: 14369
51512223 = yrday
fracday
Element set: 918
Inclination: 51
6404 deg
RA of node: 180
8973 deg
Eccentricity:
0006637
Arg of perigee: 214
9970 deg
Mean anomaly: 145
0752 deg
Mean motion: 15
53437080 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4257
Checksum: 314
Coasting Arc #20 (Orbit 4272)
---------------------------------------
Vector Time (GMT): 2014/370/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2187869
97 A = 6780895
60 meter
Y = -4110798
52 meter E =
0002105
Z = 4927330
42 I = 51
65202
XDOT = 7237
774011 Wp = 143
50130
YDOT = 1143
987394 meter/sec RA = 174
85591 deg
ZDOT = -2260
516826 TA = 328
57094
MA = 328
58352
Ha = 221
942 n
mi
Hp = 216
998
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7178051
08 X = 2209740
36
Y = -13486871
78 feet Y = -4086210
47 meter
Z = 16165782
21 Z = 4938011
35
XDOT = 23745
977725 XDOT = 7235
424396
YDOT = 3753
239481 feet/sec YDOT = 1224
911935 meter/sec
ZDOT = -7416
393785 ZDOT = -2225
363042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14792275
76 X = 4508685
65
Y = 3620599
62 feet Y = 1103558
76 meter
Z = 16212109
01 Z = 4941450
83
XDOT = 2350
382662 XDOT = 716
396635
YDOT = 22917
328104 feet/sec YDOT = 6985
201606 meter/sec
ZDOT = -7266
383608 ZDOT = -2214
793724
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 14370
54439241
00016717 00000-0 10270-3 0 9194
2 25544 51
6403 175
7708 0006602 219
3778 140
6895 15
53466924 42731
Satellite: ISS
Catalog Number: 25544
Epoch time: 14370
54439241 = yrday
fracday
Element set: 919
Inclination: 51
6403 deg
RA of node: 175
7708 deg
Eccentricity:
0006602
Arg of perigee: 219
3778 deg
Mean anomaly: 140
6895 deg
Mean motion: 15
53466924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4273
Checksum: 329
Coasting Arc #21 (Orbit 4287)
---------------------------------------
Vector Time (GMT): 2014/371/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3583832
99 A = 6783552
41 meter
Y = 3984014
42 meter E =
0008012
Z = -4167030
14 I = 51
69429
XDOT = -6420
777815 Wp = 158
64778
YDOT = -1856
021049 meter/sec RA = 169
87028 deg
ZDOT = 3742
632634 TA = 149
88329
MA = 149
83720
Ha = 221
664 n
mi
Hp = 216
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11757982
26 X = -3607875
18
Y = 13070913
46 feet Y = 3943803
54 meter
Z = -13671358
72 Z = -4184497
62
XDOT = -21065
544014 XDOT = -6417
726249
YDOT = -6089
307903 feet/sec YDOT = -1927
805557 meter/sec
ZDOT = 12278
978458 ZDOT = 3711
449373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15633703
80 X = -4765152
92
Y = -7913363
95 feet Y = -2411993
33 meter
Z = -13746670
55 Z = -4189985
18
XDOT = -136
874540 XDOT = -41
719360
YDOT = -20857
477973 feet/sec YDOT = -6357
359286 meter/sec
ZDOT = 12146
032948 ZDOT = 3702
110843
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 14371
50929403
00016717 00000-0 10270-3 0 9207
2 25544 51
6414 170
9642 0006514 222
6541 137
4107 15
53560932 42884
Satellite: ISS
Catalog Number: 25544
Epoch time: 14371
50929403 = yrday
fracday
Element set: 920
Inclination: 51
6414 deg
RA of node: 170
9642 deg
Eccentricity:
0006514
Arg of perigee: 222
6541 deg
Mean anomaly: 137
4107 deg
Mean motion: 15
53560932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4288
Checksum: 295
Coasting Arc #22 (Orbit 4303)
---------------------------------------
Vector Time (GMT): 2014/372/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4747414
06 A = 6786848
34 meter
Y = -3766312
46 meter E =
0009973
Z = 3041685
46 I = 51
73621
XDOT = 5248
984758 Wp = 125
34578
YDOT = 2620
537433 meter/sec RA = 164
89495 deg
ZDOT = -4941
923534 TA = 19
81080
MA = 19
77209
Ha = 221
343 n
mi
Hp = 217
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15575505
46 X = 4774401
83
Y = -12356668
18 feet Y = -3713073
06 meter
Z = 9979283
00 Z = 3064812
54
XDOT = 17221
078601 XDOT = 5243
296890
YDOT = 8597
563756 feet/sec YDOT = 2679
203450 meter/sec
ZDOT = -16213
659890 ZDOT = -4916
438980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16133366
01 X = 4917449
96
Y = 11532688
12 feet Y = 3515163
34 meter
Z = 10078755
58 Z = 3072004
70
XDOT = -2679
251619 XDOT = -816
635893
YDOT = 17839
256106 feet/sec YDOT = 5437
405261 meter/sec
ZDOT = -16105
179663 ZDOT = -4908
858761
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 14372
53848160
00016717 00000-0 10270-3 0 9212
2 25544 51
6411 165
8374 0006500 227
5263 132
5341 15
53605502 43044
Satellite: ISS
Catalog Number: 25544
Epoch time: 14372
53848160 = yrday
fracday
Element set: 921
Inclination: 51
6411 deg
RA of node: 165
8374 deg
Eccentricity:
0006500
Arg of perigee: 227
5263 deg
Mean anomaly: 132
5341 deg
Mean motion: 15
53605502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4304
Checksum: 280
Coasting Arc #23 (Orbit 4318)
---------------------------------------
Vector Time (GMT): 2014/373/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5616831
93 A = 6789406
91 meter
Y = 3435888
86 meter E =
0002081
Z = -1650217
02 I = 51
77734
XDOT = -3774
602839 Wp = 354
84862
YDOT = -3421
453954 meter/sec RA = 159
92934 deg
ZDOT = 5725
298678 TA = 347
12535
MA = 347
13066
Ha = 221
108 n
mi
Hp = 217
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18427926
29 X = -5646819
36
Y = 11272601
26 feet Y = 3372910
19 meter
Z = -5414097
84 Z = -1677574
87
XDOT = -12383
867581 XDOT = -3763
873812
YDOT = -11225
242631 feet/sec YDOT = -3463
604233 meter/sec
ZDOT = 18783
788315 ZDOT = 5706
988554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16129497
67 X = -4916270
89
Y = -14325259
24 feet Y = -4366339
02 meter
Z = -5531610
47 Z = -1686034
87
XDOT = 6062
658311 XDOT = 1847
898253
YDOT = -14047
669669 feet/sec YDOT = -4281
729715 meter/sec
ZDOT = 18706
094750 ZDOT = 5701
617680
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 14373
50330574
00016717 00000-0 10270-3 0 9226
2 25544 51
6428 161
0310 0006371 231
0451 129
0134 15
53686151 43191
Satellite: ISS
Catalog Number: 25544
Epoch time: 14373
50330574 = yrday
fracday
Element set: 922
Inclination: 51
6428 deg
RA of node: 161
0310 deg
Eccentricity:
0006371
Arg of perigee: 231
0451 deg
Mean anomaly: 129
0134 deg
Mean motion: 15
53686151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4319
Checksum: 271
Coasting Arc #24 (Orbit 4334)
---------------------------------------
Vector Time (GMT): 2014/374/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6117175
15 A = 6790377
04 meter
Y = -2927804
93 meter E =
0012478
Z = 82356
41 I = 51
81001
XDOT = 2116
056673 Wp = 163
13021
YDOT = 4245
490534 meter/sec RA = 154
97062 deg
ZDOT = -6028
261474 TA = 15
98455
MA = 15
94521
Ha = 220
739 n
mi
Hp = 217
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20069472
27 X = 6149059
86
Y = -9605659
22 feet Y = -2859220
43 meter
Z = 270198
21 Z = 112149
51
XDOT = 6942
443154 XDOT = 2097
708040
YDOT = 13928
774717 feet/sec YDOT = 4269
051196 meter/sec
ZDOT = -19777
760741 ZDOT = -6018
026668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15301317
40 X = 4663841
54
Y = 16150438
27 feet Y = 4922653
58 meter
Z = 398049
12 Z = 121325
37
XDOT = -9907
781887 XDOT = -3019
891919
YDOT = 9885
161695 feet/sec YDOT = 3012
997285 meter/sec
ZDOT = -19734
717440 ZDOT = -6015
141876
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 14374
53240864
00016717 00000-0 10270-3 0 9233
2 25544 51
6423 155
9038 0006293 236
8660 123
1889 15
53766998 43351
Satellite: ISS
Catalog Number: 25544
Epoch time: 14374
53240864 = yrday
fracday
Element set: 923
Inclination: 51
6423 deg
RA of node: 155
9038 deg
Eccentricity:
0006293
Arg of perigee: 236
8660 deg
Mean anomaly: 123
1889 deg
Mean motion: 15
53766998 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4335
Checksum: 338
Coasting Arc #25 (Orbit 4350)
---------------------------------------
Vector Time (GMT): 2014/375/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6229612
16 A = 6789268
39 meter
Y = 2232958
91 meter E =
0007594
Z = 1500718
07 I = 51
83661
XDOT = -400
273104 Wp = 63
25024
YDOT = -5016
431788 meter/sec RA = 150
01417 deg
ZDOT = 5783
300819 TA = 313
08642
MA = 313
14995
Ha = 220
482 n
mi
Hp = 217
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20438360
11 X = -6261408
49
Y = 7325980
67 feet Y = 2163117
53 meter
Z = 4923615
70 Z = 1470378
90
XDOT = -1313
231967 XDOT = -372
241289
YDOT = -16458
109541 feet/sec YDOT = -5020
751239 meter/sec
ZDOT = 18974
084053 ZDOT = 5781
424411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13549895
34 X = -4130008
10
Y = -17001791
85 feet Y = -5182146
16 meter
Z = 4793533
01 Z = 1461068
86
XDOT = 13869
734898 XDOT = 4227
495197
YDOT = -5687
906467 feet/sec YDOT = -1733
673891 meter/sec
ZDOT = 18966
901404 ZDOT = 5781
111548
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 14375
56146790
00016717 00000-0 10270-3 0 9241
2 25544 51
6438 150
7766 0006276 239
6847 120
3685 15
53838470 43513
Satellite: ISS
Catalog Number: 25544
Epoch time: 14375
56146790 = yrday
fracday
Element set: 924
Inclination: 51
6438 deg
RA of node: 150
7766 deg
Eccentricity:
0006276
Arg of perigee: 239
6847 deg
Mean anomaly: 120
3685 deg
Mean motion: 15
53838470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4351
Checksum: 338
Coasting Arc #26 (Orbit 4365)
---------------------------------------
Vector Time (GMT): 2014/376/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5952348
37 A = 6786380
68 meter
Y = -1303546
59 meter E =
0004639
Z = -2980635
83 I = 51
85394
XDOT = -1260
893348 Wp = 198
09250
YDOT = 5673
163720 meter/sec RA = 145
05435 deg
ZDOT = -5001
317433 TA = 15
87530
MA = 15
86077
Ha = 220
272 n
mi
Hp = 217
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19528701
99 X = 5980961
26
Y = -4276727
64 feet Y = -1236823
55 meter
Z = -9778988
95 Z = -2951651
19
XDOT = -4136
789198 XDOT = -1299
943919
YDOT = 18612
741865 feet/sec YDOT = 5658
845283 meter/sec
ZDOT = -16408
521763 ZDOT = -5007
537376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10674220
77 X = 3253502
49
Y = 16974518
78 feet Y = 5173833
33 meter
Z = -9654840
70 Z = -2942795
44
XDOT = -17637
236551 XDOT = -5375
829701
YDOT = 1746
566626 feet/sec YDOT = 532
353508 meter/sec
ZDOT = -16436
069289 ZDOT = -5009
713919
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 14376
52617171
00016717 00000-0 10270-3 0 9255
2 25544 51
6436 145
9697 0006179 245
0866 114
9645 15
53879321 43665
Satellite: ISS
Catalog Number: 25544
Epoch time: 14376
52617171 = yrday
fracday
Element set: 925
Inclination: 51
6436 deg
RA of node: 145
9697 deg
Eccentricity:
0006179
Arg of perigee: 245
0866 deg
Mean anomaly: 114
9645 deg
Mean motion: 15
53879321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4366
Checksum: 344
Coasting Arc #27 (Orbit 4381)
---------------------------------------
Vector Time (GMT): 2014/377/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5334558
14 A = 6782473
54 meter
Y = 180011
42 meter E =
0006358
Z = 4184312
05 I = 51
86794
XDOT = 2731
825094 Wp = 138
20153
YDOT = -6110
634079 meter/sec RA = 140
08706 deg
ZDOT = 3737
787063 TA = 273
45818
MA = 273
53090
Ha = 219
822 n
mi
Hp = 217
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17501831
16 X = -5356500
32
Y = 590588
65 feet Y = 120234
21 meter
Z = 13728057
91 Z = 4158344
62
XDOT = 8962
680754 XDOT = 2781
795909
YDOT = -20048
012071 feet/sec YDOT = -6079
805657 meter/sec
ZDOT = 12263
080916 ZDOT = 3751
179017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6807891
53 X = -2075045
34
Y = -16228144
71 feet Y = -4946338
51 meter
Z = 13616989
20 Z = 4150458
31
XDOT = 20712
708241 XDOT = 6313
233472
YDOT = 1671
501521 feet/sec YDOT = 509
473663 meter/sec
ZDOT = 12321
377981 ZDOT = 3755
556009
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 14377
55514392
00016717 00000-0 10270-3 0 9261
2 25544 51
6444 140
8418 0006182 249
6911 110
3577 15
53975390 43829
Satellite: ISS
Catalog Number: 25544
Epoch time: 14377
55514392 = yrday
fracday
Element set: 926
Inclination: 51
6444 deg
RA of node: 140
8418 deg
Eccentricity:
0006182
Arg of perigee: 249
6911 deg
Mean anomaly: 110
3577 deg
Mean motion: 15
53975390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4382
Checksum: 324
Coasting Arc #28 (Orbit 4396)
---------------------------------------
Vector Time (GMT): 2014/378/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4436335
92 A = 6779176
74 meter
Y = 1125913
55 meter E =
0006477
Z = -5006780
30 I = 51
88086
XDOT = -3937
405446 Wp = 74
27982
YDOT = 6233
876075 meter/sec RA = 135
11206 deg
ZDOT = -2087
471647 TA = 175
46472
MA = 175
45885
Ha = 219
521 n
mi
Hp = 217
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14554907
89 X = 4447736
99
Y = 3693942
08 feet Y = 1175587
34 meter
Z = -16426444
56 Z = -4985201
79
XDOT = -12917
996871 XDOT = -3996
681341
YDOT = 20452
349327 feet/sec YDOT = 6189
514041 meter/sec
ZDOT = -6848
660259 ZDOT = -2106
742661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2019771
57 X = 615626
37
Y = 14980918
96 feet Y = 4566184
10 meter
Z = -16334357
13 Z = -4978712
05
XDOT = -22679
132539 XDOT = -6912
599598
YDOT = -4498
828192 feet/sec YDOT = -1371
242833 meter/sec
ZDOT = -6932
132322 ZDOT = -2112
913932
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 14378
51976656
00016717 00000-0 10270-3 0 9274
2 25544 51
6444 136
0349 0006083 255
0506 104
9974 15
54008786 43973
Satellite: ISS
Catalog Number: 25544
Epoch time: 14378
51976656 = yrday
fracday
Element set: 927
Inclination: 51
6444 deg
RA of node: 136
0349 deg
Eccentricity:
0006083
Arg of perigee: 255
0506 deg
Mean anomaly: 104
9974 deg
Mean motion: 15
54008786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4397
Checksum: 341
Coasting Arc #29 (Orbit 4412)
---------------------------------------
Vector Time (GMT): 2014/379/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3352393
83 A = 6777431
56 meter
Y = -2509948
14 meter E =
0003814
Z = 5331770
95 I = 51
89824
XDOT = 4809
599452 Wp = 246
39722
YDOT = -5965
995814 meter/sec RA = 130
13058 deg
ZDOT = 214
196186 TA = 201
55998
MA = 201
57604
Ha = 219
181 n
mi
Hp = 216
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10998667
41 X = -3349977
56
Y = -8234737
98 feet Y = -2547423
39 meter
Z = 17492686
84 Z = 5315491
50
XDOT = 15779
525762 XDOT = 4874
914673
YDOT = -19573
477080 feet/sec YDOT = -5911
846553 meter/sec
ZDOT = 702
743393 ZDOT = 237
718777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3284258
63 X = 1001042
03
Y = -13431723
81 feet Y = -4093989
42 meter
Z = 17423493
57 Z = 5310680
84
XDOT = 23177
824863 XDOT = 7064
601018
YDOT = 6716
586035 feet/sec YDOT = 2047
215423 meter/sec
ZDOT = 804
369496 ZDOT = 245
171822
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 14379
54865217
00016717 00000-0 10270-3 0 9289
2 25544 51
6450 130
9060 0006024 260
1360 99
9113 15
54106841 44131
Satellite: ISS
Catalog Number: 25544
Epoch time: 14379
54865217 = yrday
fracday
Element set: 928
Inclination: 51
6450 deg
RA of node: 130
9060 deg
Eccentricity:
0006024
Arg of perigee: 260
1360 deg
Mean anomaly: 99
9113 deg
Mean motion: 15
54106841 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4413
Checksum: 294
Coasting Arc #30 (Orbit 4427)
---------------------------------------
Vector Time (GMT): 2014/380/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952853
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2174068
17 A = 6778152
62 meter
Y = 3881506
23 meter E =
0008083
Z = -5120933
75 I = 51
92106
XDOT = -5325
151453 Wp = 115
98964
YDOT = 5238
112948 meter/sec RA = 125
15025 deg
ZDOT = 1708
197115 TA = 170
46985
MA = 170
45450
Ha = 218
855 n
mi
Hp = 216
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7132769
58 X = 2155378
22
Y = 12734600
50 feet Y = 3905713
76 meter
Z = -16800963
76 Z = -5110417
82
XDOT = -17470
969334 XDOT = -5391
627254
YDOT = 17185
409934 feet/sec YDOT = 5178
191893 meter/sec
ZDOT = 5604
321244 ZDOT = 1682
167325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8731419
33 X = -2661336
61
Y = 11759913
92 feet Y = 3584421
76 meter
Z = -16756657
67 Z = -5107429
26
XDOT = -21929
499633 XDOT = -6684
111488
YDOT = -8450
049625 feet/sec YDOT = -2575
575126 meter/sec
ZDOT = 5492
077792 ZDOT = 1673
985311
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 14380
51319303
00016717 00000-0 10270-3 0 9299
2 25544 51
6451 126
0987 0005845 264
4045 95
6441 15
54172233 44284
Satellite: ISS
Catalog Number: 25544
Epoch time: 14380
51319303 = yrday
fracday
Element set: 929
Inclination: 51
6451 deg
RA of node: 126
0987 deg
Eccentricity:
0005845
Arg of perigee: 264
4045 deg
Mean anomaly: 95
6441 deg
Mean motion: 15
54172233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4428
Checksum: 307
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