[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 31st 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 124 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 730 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 3493)
---------------------------------------
Vector Time (GMT): 2015/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5749171
04 A = 6782704
45 meter
Y = 1803499
08 meter E =
0013289
Z = 3102991
06 I = 51
39921
XDOT = 783
195747 Wp = 89
56106
YDOT = 5888
206331 meter/sec RA = 221
69159 deg
ZDOT = -4855
263184 TA = 54
57676
MA = 54
45274
Ha = 219
800 n
mi
Hp = 213
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18862109
70 X = 5713503
77
Y = 5916991
73 feet Y = 1867590
52 meter
Z = 10180416
86 Z = 3130832
22
XDOT = 2569
539851 XDOT = 740
878703
YDOT = 19318
262241 feet/sec YDOT = 5896
728140 meter/sec
ZDOT = -15929
341154 ZDOT = -4851
561187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6894203
17 X = -2101353
13
Y = -18461110
25 feet Y = -5626946
40 meter
Z = 10299914
18 Z = 3139413
84
XDOT = 12242
450781 XDOT = 3731
498998
YDOT = -13483
735483 feet/sec YDOT = -4109
842575 meter/sec
ZDOT = -15914
421644 ZDOT = -4850
715717
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 15212
53863689
00016717 00000-0 10270-3 0 9006
2 25544 51
6406 222
5769 0001285 18
2485 341
8714 15
54968923 34941
Satellite: ISS
Catalog Number: 25544
Epoch time: 15212
53863689 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 222
5769 deg
Eccentricity:
0001285
Arg of perigee: 18
2485 deg
Mean anomaly: 341
8714 deg
Mean motion: 15
54968923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3494
Checksum: 331
Coasting Arc #2 (Orbit 3508)
---------------------------------------
Vector Time (GMT): 2015/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5897026
00 A = 6786010
42 meter
Y = -3075238
45 meter E =
0009826
Z = -1327130
61 I = 51
43533
XDOT = 1232
080413 Wp = 36
77960
YDOT = -4855
525897 meter/sec RA = 216
69595 deg
ZDOT = 5806
613613 TA = 308
72678
MA = 308
81459
Ha = 219
812 n
mi
Hp = 213
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19347198
18 X = -5855753
12
Y = -10089364
98 feet Y = -3140952
06 meter
Z = -4354103
05 Z = -1355676
37
XDOT = 4042
258572 XDOT = 1258
078808
YDOT = -15930
203075 feet/sec YDOT = -4841
602714 meter/sec
ZDOT = 19050
569598 ZDOT = 5812
661732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4294057
77 X = 1308828
81
Y = 21367971
04 feet Y = 6512957
57 meter
Z = -4476433
59 Z = -1364416
96
XDOT = -13295
303277 XDOT = -4052
408439
YDOT = 6648
302108 feet/sec YDOT = 2026
402483 meter/sec
ZDOT = 19077
422372 ZDOT = 5814
798339
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 15213
50265733
00016717 00000-0 10270-3 0 9011
2 25544 51
6411 217
7653 0001145 27
0467 333
0746 15
54997484 35097
Satellite: ISS
Catalog Number: 25544
Epoch time: 15213
50265733 = yrday
fracday
Element set: 901
Inclination: 51
6411 deg
RA of node: 217
7653 deg
Eccentricity:
0001145
Arg of perigee: 27
0467 deg
Mean anomaly: 333
0746 deg
Mean motion: 15
54997484 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3509
Checksum: 302
Coasting Arc #3 (Orbit 3524)
---------------------------------------
Vector Time (GMT): 2015/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5440748
86 A = 6786726
30 meter
Y = 3993360
91 meter E =
0010228
Z = -675133
96 I = 51
46252
XDOT = -3315
663081 Wp = 133
11449
YDOT = 3522
284425 meter/sec RA = 211
70757 deg
ZDOT = -5950
015893 TA = 54
19645
MA = 54
10143
Ha = 219
951 n
mi
Hp = 213
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17850225
91 X = 5398969
25
Y = 13101577
78 feet Y = 4053969
33 meter
Z = -2215006
43 Z = -648805
90
XDOT = -10878
159715 XDOT = -3325
901359
YDOT = 11556
051263 feet/sec YDOT = 3485
149253 meter/sec
ZDOT = -19521
049517 ZDOT = -5966
147266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1417589
55 X = -432081
29
Y = -22107887
54 feet Y = -6738484
12 meter
Z = -2102357
59 Z = -640798
59
XDOT = 14150
064724 XDOT = 4312
939728
YDOT = 934
702938 feet/sec YDOT = 284
897455 meter/sec
ZDOT = -19591
071389 ZDOT = -5971
358559
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 15214
53093837
00016717 00000-0 10270-3 0 9020
2 25544 51
6402 212
6314 0001311 25
3776 334
7442 15
54963530 35258
Satellite: ISS
Catalog Number: 25544
Epoch time: 15214
53093837 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 212
6314 deg
Eccentricity:
0001311
Arg of perigee: 25
3776 deg
Mean anomaly: 334
7442 deg
Mean motion: 15
54963530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3525
Checksum: 282
Coasting Arc #4 (Orbit 3540)
---------------------------------------
Vector Time (GMT): 2015/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4393619
85 A = 6784074
29 meter
Y = -4484962
17 meter E =
0014428
Z = 2551189
02 I = 51
48161
XDOT = 5186
137715 Wp = 72
29452
YDOT = -2076
868735 meter/sec RA = 206
71886 deg
ZDOT = 5260
142055 TA = 316
46551
MA = 316
57930
Ha = 219
853 n
mi
Hp = 213
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14414763
29 X = -4355533
88
Y = -14714442
82 feet Y = -4533881
52 meter
Z = 8370042
73 Z = 2529938
62
XDOT = 17014
887516 XDOT = 5183
424976
YDOT = -6813
873801 feet/sec YDOT = -2018
889029 meter/sec
ZDOT = 17257
683909 ZDOT = 5285
328295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1644875
23 X = -501357
97
Y = 20569519
90 feet Y = 6269589
67 meter
Z = 8279316
39 Z = 2523535
64
XDOT = -14718
753025 XDOT = -4486
275922
YDOT = -8194
087933 feet/sec YDOT = -2497
558002 meter/sec
ZDOT = 17366
442818 ZDOT = 5293
291771
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 15215
55920983
00016717 00000-0 10270-3 0 9035
2 25544 51
6403 207
4988 0001198 22
0096 338
1108 15
55007721 35417
Satellite: ISS
Catalog Number: 25544
Epoch time: 15215
55920983 = yrday
fracday
Element set: 903
Inclination: 51
6403 deg
RA of node: 207
4988 deg
Eccentricity:
0001198
Arg of perigee: 22
0096 deg
Mean anomaly: 338
1108 deg
Mean motion: 15
55007721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3541
Checksum: 296
Coasting Arc #5 (Orbit 3555)
---------------------------------------
Vector Time (GMT): 2015/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2794683
92 A = 6779786
45 meter
Y = 4626180
15 meter E =
0008392
Z = -4102239
34 I = 51
49566
XDOT = -6618
786455 Wp = 65
24451
YDOT = 624
299428 meter/sec RA = 201
71906 deg
ZDOT = -3807
760368 TA = 165
34017
MA = 165
31582
Ha = 219
952 n
mi
Hp = 213
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9168910
50 X = 2762672
02
Y = 15177756
41 feet Y = 4657253
08 meter
Z = -13458790
48 Z = -4088741
33
XDOT = -21715
178659 XDOT = -6606
779185
YDOT = 2048
226470 feet/sec YDOT = 550
350878 meter/sec
ZDOT = -12492
652127 ZDOT = -3839
883547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5116688
86 X = 1559566
76
Y = -17023305
77 feet Y = -5188703
60 meter
Z = -13401447
93 Z = -4084761
33
XDOT = 14729
955013 XDOT = 4489
690288
YDOT = 14364
066276 feet/sec YDOT = 4378
167401 meter/sec
ZDOT = -12631
040833 ZDOT = -3849
941246
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 15216
52321010
00016717 00000-0 10270-3 0 9040
2 25544 51
6401 202
6858 0001381 28
2257 331
8971 15
54979083 35561
Satellite: ISS
Catalog Number: 25544
Epoch time: 15216
52321010 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 202
6858 deg
Eccentricity:
0001381
Arg of perigee: 28
2257 deg
Mean anomaly: 331
8971 deg
Mean motion: 15
54979083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3556
Checksum: 295
Coasting Arc #6 (Orbit 3571)
---------------------------------------
Vector Time (GMT): 2015/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -825273
08 A = 6775975
66 meter
Y = -4438776
60 meter E =
0005538
Z = 5048754
72 I = 51
51301
XDOT = 7417
929652 Wp = 110
17254
YDOT = 707
064312 meter/sec RA = 196
70885 deg
ZDOT = 1830
675439 TA = 322
06180
MA = 322
10080
Ha = 219
907 n
mi
Hp = 213
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2707588
86 X = -800100
98
Y = -14562915
35 feet Y = -4447864
53 meter
Z = 16564155
91 Z = 5044806
95
XDOT = 24337
039540 XDOT = 7400
579130
YDOT = 2319
764802 feet/sec YDOT = 789
919483 meter/sec
ZDOT = 6006
153016 ZDOT = 1866
667771
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8755663
52 X = -2668726
24
Y = 11970232
75 feet Y = 3648526
94 meter
Z = 16547890
69 Z = 5043797
08
XDOT = -13961
576232 XDOT = -4255
488436
YDOT = -18745
222657 feet/sec YDOT = -5713
543866 meter/sec
ZDOT = 6160
992708 ZDOT = 1877
870577
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 15217
55146748
00016717 00000-0 10270-3 0 9058
2 25544 51
6400 197
5531 0001418 24
5748 335
5472 15
55000754 35721
Satellite: ISS
Catalog Number: 25544
Epoch time: 15217
55146748 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 197
5531 deg
Eccentricity:
0001418
Arg of perigee: 24
5748 deg
Mean anomaly: 335
5472 deg
Mean motion: 15
55000754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3572
Checksum: 303
Coasting Arc #7 (Orbit 3586)
---------------------------------------
Vector Time (GMT): 2015/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1317071
13 A = 6774870
70 meter
Y = 4026599
98 meter E =
0015546
Z = -5300270
26 I = 51
54021
XDOT = -7413
726402 Wp = 88
56431
YDOT = -1874
549059 meter/sec RA = 191
69178 deg
ZDOT = 419
604221 TA = 185
43945
MA = 185
45636
Ha = 219
952 n
mi
Hp = 212
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4321099
50 X = -1336253
14
Y = 13210629
86 feet Y = 4011764
37 meter
Z = -17389338
14 Z = -5306714
88
XDOT = -24323
249351 XDOT = -7394
252002
YDOT = -6150
095338 feet/sec YDOT = -1957
345328 meter/sec
ZDOT = 1376
654268 ZDOT = 383
637383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12440568
54 X = 3791885
29
Y = -6118496
09 feet Y = -1864917
61 meter
Z = -17417749
08 Z = -5308929
92
XDOT = 11981
620773 XDOT = 3651
998012
YDOT = 20896
393711 feet/sec YDOT = 6369
220803 meter/sec
ZDOT = 1222
099953 ZDOT = 372
496066
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 15218
51545161
00016717 00000-0 10270-3 0 9068
2 25544 51
6402 192
7407 0001462 30
6666 329
4572 15
54998848 35876
Satellite: ISS
Catalog Number: 25544
Epoch time: 15218
51545161 = yrday
fracday
Element set: 906
Inclination: 51
6402 deg
RA of node: 192
7407 deg
Eccentricity:
0001462
Arg of perigee: 30
6666 deg
Mean anomaly: 329
4572 deg
Mean motion: 15
54998848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3587
Checksum: 328
Coasting Arc #8 (Orbit 3602)
---------------------------------------
Vector Time (GMT): 2015/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3378694
40 A = 6776937
00 meter
Y = -3417182
32 meter E =
0008657
Z = 4774306
52 I = 51
57874
XDOT = 6616
079052 Wp = 56
19358
YDOT = 2868
047535 meter/sec RA = 186
67897 deg
ZDOT = -2621
162989 TA = 59
70117
MA = 59
61555
Ha = 219
809 n
mi
Hp = 212
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11084955
38 X = 3393463
44
Y = -11211228
10 feet Y = -3379317
03 meter
Z = 15663735
30 Z = 4790755
25
XDOT = 21706
296101 XDOT = 6596
248656
YDOT = 9409
604775 feet/sec YDOT = 2941
922033 meter/sec
ZDOT = -8599
616106 ZDOT = -2589
071750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15694332
17 X = -4783632
45
Y = 118817
95 feet Y = 36215
71 meter
Z = 15735129
33 Z = 4796067
42
XDOT = -8668
891017 XDOT = -2642
277982
YDOT = -20918
046526 feet/sec YDOT = -6375
820581 meter/sec
ZDOT = -8461
895991 ZDOT = -2579
185898
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 15219
54369286
00016717 00000-0 10270-3 0 9075
2 25544 51
6400 187
6078 0001484 28
9394 331
1841 15
55028034 36033
Satellite: ISS
Catalog Number: 25544
Epoch time: 15219
54369286 = yrday
fracday
Element set: 907
Inclination: 51
6400 deg
RA of node: 187
6078 deg
Eccentricity:
0001484
Arg of perigee: 28
9394 deg
Mean anomaly: 331
1841 deg
Mean motion: 15
55028034 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3603
Checksum: 312
Coasting Arc #9 (Orbit 3617)
---------------------------------------
Vector Time (GMT): 2015/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5090113
16 A = 6781185
02 meter
Y = 2692110
16 meter E =
0006229
Z = -3586497
53 I = 51
62465
XDOT = -5060
388923 Wp = 85
53155
YDOT = -3664
546536 meter/sec RA = 181
67920 deg
ZDOT = 4438
352199 TA = 232
06245
MA = 232
11876
Ha = 219
925 n
mi
Hp = 212
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16699846
34 X = -5102416
99
Y = 8832382
42 feet Y = 2635120
47 meter
Z = -11766724
18 Z = -3611253
89
XDOT = -16602
325862 XDOT = -5040
594624
YDOT = -12022
790474 feet/sec YDOT = -3721
024563 meter/sec
ZDOT = 14561
522963 ZDOT = 4413
818036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18078679
77 X = 5510381
59
Y = 5246536
78 feet Y = 1599144
41 meter
Z = -11873787
71 Z = -3619130
49
XDOT = 3984
043006 XDOT = 1214
336308
YDOT = 18936
627944 feet/sec YDOT = 5771
884197 meter/sec
ZDOT = 14456
462713 ZDOT = 4406
329835
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 15220
50766151
00016717 00000-0 10270-3 0 9086
2 25544 51
6401 182
7956 0001562 32
6574 327
4676 15
55018592 36182
Satellite: ISS
Catalog Number: 25544
Epoch time: 15220
50766151 = yrday
fracday
Element set: 908
Inclination: 51
6401 deg
RA of node: 182
7956 deg
Eccentricity:
0001562
Arg of perigee: 32
6574 deg
Mean anomaly: 327
4676 deg
Mean motion: 15
55018592 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3618
Checksum: 312
Coasting Arc #10 (Orbit 3633)
---------------------------------------
Vector Time (GMT): 2015/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6262251
42 A = 6785141
05 meter
Y = -1824468
35 meter E =
0014348
Z = 1847288
37 I = 51
67040
XDOT = 2925
551163 Wp = 107
54739
YDOT = 4298
026971 meter/sec RA = 176
69538 deg
ZDOT = -5640
740980 TA = 52
12617
MA = 51
99647
Ha = 219
896 n
mi
Hp = 212
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20545444
28 X = 6273214
32
Y = -5985788
56 feet Y = -1754378
51 meter
Z = 6060657
39 Z = 1877735
36
XDOT = 9598
264969 XDOT = 2904
672417
YDOT = 14101
138357 feet/sec YDOT = 4330
625839 meter/sec
ZDOT = -18506
368044 ZDOT = -5626
579978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19049778
68 X = -5806372
54
Y = -9666451
32 feet Y = -2946334
36 meter
Z = 6192105
01 Z = 1887353
61
XDOT = 1856
928582 XDOT = 565
991832
YDOT = -15541
128745 feet/sec YDOT = -4736
936041 meter/sec
ZDOT = -18446
078756 ZDOT = -5622
364805
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 15221
53588648
00016717 00000-0 10270-3 0 9094
2 25544 51
6405 177
6620 0001562 34
5866 325
5388 15
55050641 36340
Satellite: ISS
Catalog Number: 25544
Epoch time: 15221
53588648 = yrday
fracday
Element set: 909
Inclination: 51
6405 deg
RA of node: 177
6620 deg
Eccentricity:
0001562
Arg of perigee: 34
5866 deg
Mean anomaly: 325
5388 deg
Mean motion: 15
55050641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3634
Checksum: 318
Coasting Arc #11 (Orbit 3649)
---------------------------------------
Vector Time (GMT): 2015/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6721915
30 A = 6786587
31 meter
Y = 875622
81 meter E =
0013779
Z = 128101
58 I = 51
70708
XDOT = -494
028949 Wp = 45
92624
YDOT = -4730
442041 meter/sec RA = 171
72330 deg
ZDOT = 6018
971436 TA = 315
45321
MA = 315
56389
Ha = 219
887 n
mi
Hp = 212
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22053527
88 X = -6731829
40
Y = 2872778
23 feet Y = 800398
50 meter
Z = 420280
77 Z = 95424
29
XDOT = -1620
829884 XDOT = -470
332728
YDOT = -15519
822970 feet/sec YDOT = -4735
834281 meter/sec
ZDOT = 19747
281613 ZDOT = 6016
628993
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18270933
77 X = 5568980
61
Y = 12683947
27 feet Y = 3866067
13 meter
Z = 279362
39 Z = 85149
66
XDOT = -8202
647936 XDOT = -2500
167091
YDOT = 11338
378980 feet/sec YDOT = 3455
937913 meter/sec
ZDOT = 19737
969135 ZDOT = 6016
132992
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 15222
56410215
00016717 00000-0 10270-3 0 9104
2 25544 51
6406 172
5289 0001512 38
6215 321
5046 15
55072134 36500
Satellite: ISS
Catalog Number: 25544
Epoch time: 15222
56410215 = yrday
fracday
Element set: 910
Inclination: 51
6406 deg
RA of node: 172
5289 deg
Eccentricity:
0001512
Arg of perigee: 38
6215 deg
Mean anomaly: 321
5046 deg
Mean motion: 15
55072134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3650
Checksum: 268
Coasting Arc #12 (Orbit 3664)
---------------------------------------
Vector Time (GMT): 2015/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6438027
55 A = 6784705
77 meter
Y = 208838
92 meter E =
0006370
Z = -2128013
48 I = 51
73335
XDOT = -1979
391722 Wp = 125
29988
YDOT = 4938
420054 meter/sec RA = 166
75262 deg
ZDOT = -5518
984081 TA = 78
24921
MA = 78
17775
Ha = 219
932 n
mi
Hp = 212
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21122137
63 X = 6445550
67
Y = 685167
06 feet Y = 280875
28 meter
Z = -6981671
53 Z = -2096721
11
XDOT = -6494
067331 XDOT = -2007
658568
YDOT = 16202
165533 feet/sec YDOT = 4916
127265 meter/sec
ZDOT = -18106
903152 ZDOT = -5528
667950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15473774
50 X = -4716406
47
Y = -14458230
91 feet Y = -4406868
78 meter
Z = -6846878
93 Z = -2086928
70
XDOT = 14416
648503 XDOT = 4394
194464
YDOT = -6858
516009 feet/sec YDOT = -2090
475680 meter/sec
ZDOT = -18149
439702 ZDOT = -5531
949221
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 15223
52804703
00016717 00000-0 10270-3 0 9111
2 25544 51
6418 167
7163 0001579 38
1233 322
0031 15
55082205 36654
Satellite: ISS
Catalog Number: 25544
Epoch time: 15223
52804703 = yrday
fracday
Element set: 911
Inclination: 51
6418 deg
RA of node: 167
7163 deg
Eccentricity:
0001579
Arg of perigee: 38
1233 deg
Mean anomaly: 322
0031 deg
Mean motion: 15
55082205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3665
Checksum: 279
Coasting Arc #13 (Orbit 3680)
---------------------------------------
Vector Time (GMT): 2015/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5452366
60 A = 6780511
19 meter
Y = -1348439
19 meter E =
0012549
Z = 3787924
87 I = 51
75070
XDOT = 4151
781336 Wp = 91
27747
YDOT = -4876
101594 meter/sec RA = 161
77423 deg
ZDOT = 4227
938503 TA = 314
11902
MA = 314
22219
Ha = 219
984 n
mi
Hp = 212
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17888341
87 X = -5455282
73
Y = -4424013
10 feet Y = -1409427
47 meter
Z = 12427575
04 Z = 3761431
80
XDOT = 13621
329844 XDOT = 4185
461206
YDOT = -15997
708642 feet/sec YDOT = -4829
485367 meter/sec
ZDOT = 13871
189313 ZDOT = 4248
188389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10863603
87 X = 3311226
46
Y = 14978846
58 feet Y = 4565552
44 meter
Z = 12313632
86 Z = 3753195
29
XDOT = -19570
018173 XDOT = -5964
941539
YDOT = 2684
328386 feet/sec YDOT = 818
183292 meter/sec
ZDOT = 13959
251314 ZDOT = 4254
779801
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 15224
55624584
00016717 00000-0 10270-3 0 9123
2 25544 51
6422 162
5836 0001497 43
0261 317
1009 15
55103453 36811
Satellite: ISS
Catalog Number: 25544
Epoch time: 15224
55624584 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 162
5836 deg
Eccentricity:
0001497
Arg of perigee: 43
0261 deg
Mean anomaly: 317
1009 deg
Mean motion: 15
55103453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3681
Checksum: 288
Coasting Arc #14 (Orbit 3695)
---------------------------------------
Vector Time (GMT): 2015/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3910582
84 A = 6776292
79 meter
Y = 2545716
44 meter E =
0013484
Z = -4926316
43 I = 51
76728
XDOT = -5792
303892 Wp = 70
20868
YDOT = 4453
894925 meter/sec RA = 156
78262 deg
ZDOT = -2297
086671 TA = 177
34938
MA = 177
34223
Ha = 219
902 n
mi
Hp = 212
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12829996
21 X = 3905755
06
Y = 8352088
04 feet Y = 2589420
11 meter
Z = -16162455
49 Z = -4907331
75
XDOT = -19003
621694 XDOT = -5830
519786
YDOT = 14612
516158 feet/sec YDOT = 4388
907881 meter/sec
ZDOT = -7536
373593 ZDOT = -2325
316796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4735897
67 X = -1443501
61
Y = -14647938
22 feet Y = -4464691
57 meter
Z = -16081054
82 Z = -4901505
51
XDOT = 22855
767454 XDOT = 6966
437920
YDOT = 1016
086532 feet/sec YDOT = 309
703175 meter/sec
ZDOT = -7658
768656 ZDOT = -2334
392686
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 15225
52017521
00016717 00000-0 10270-3 0 9139
2 25544 51
6429 157
7709 0001611 44
3003 315
8279 15
55114113 36964
Satellite: ISS
Catalog Number: 25544
Epoch time: 15225
52017521 = yrday
fracday
Element set: 913
Inclination: 51
6429 deg
RA of node: 157
7709 deg
Eccentricity:
0001611
Arg of perigee: 44
3003 deg
Mean anomaly: 315
8279 deg
Mean motion: 15
55114113 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3696
Checksum: 287
Coasting Arc #15 (Orbit 3711)
---------------------------------------
Vector Time (GMT): 2015/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2017198
51 A = 6774375
57 meter
Y = -3671206
38 meter E =
0003547
Z = 5321068
52 I = 51
79056
XDOT = 6747
346017 Wp = 75
40319
YDOT = -3654
016350 meter/sec RA = 151
78391 deg
ZDOT = 37
703194 TA = 14
24352
MA = 14
23353
Ha = 219
872 n
mi
Hp = 212
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6618105
33 X = -2001843
46
Y = -12044640
36 feet Y = -3693678
03 meter
Z = 17457573
88 Z = 5311306
97
XDOT = 22136
961999 XDOT = 6787
521491
YDOT = -11988
242617 feet/sec YDOT = -3578
338458 meter/sec
ZDOT = 123
698143 ZDOT = 70
577452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2170555
80 X = -661585
41
Y = 13623789
26 feet Y = 4152530
97 meter
Z = 17416102
30 Z = 5308427
98
XDOT = -23812
108804 XDOT = -7257
930764
YDOT = -4130
220820 feet/sec YDOT = -1258
891306 meter/sec
ZDOT = 265
991841 ZDOT = 81
074313
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 15226
54835641
00016717 00000-0 10270-3 0 9144
2 25544 51
6432 152
6384 0001486 43
4673 316
6597 15
55149011 37120
Satellite: ISS
Catalog Number: 25544
Epoch time: 15226
54835641 = yrday
fracday
Element set: 914
Inclination: 51
6432 deg
RA of node: 152
6384 deg
Eccentricity:
0001486
Arg of perigee: 43
4673 deg
Mean anomaly: 316
6597 deg
Mean motion: 15
55149011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3712
Checksum: 308
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