[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 19th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 819 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 3788)
---------------------------------------
Vector Time (GMT): 2015/231/10:58:05
436
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1259922
16 A = 6781524
99 meter
Y = -5832986
26 meter E =
0014003
Z = 3209349
89 I = 51
93682
XDOT = 5799
937893 Wp = 90
25484
YDOT = -1410
121471 meter/sec RA = 127
09484 deg
ZDOT = -4821
779443 TA = 52
76128
MA = 52
63361
Ha = 219
617 n
mi
Hp = 212
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4133602
89 X = 1309464
69
Y = -19137094
04 feet Y = -5818619
76 meter
Z = 10529363
15 Z = 3215591
02
XDOT = 19028
667627 XDOT = 5838
697350
YDOT = -4626
382780 feet/sec YDOT = -1345
046362 meter/sec
ZDOT = -15819
486360 ZDOT = -4793
510473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17083314
66 X = -5206994
31
Y = 9533485
90 feet Y = 2905806
50 meter
Z = 10557250
42 Z = 3217849
93
XDOT = -15379
257438 XDOT = -4687
597667
YDOT = -10110
086439 feet/sec YDOT = -3081
554347 meter/sec
ZDOT = -15697
360559 ZDOT = -4784
555498
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 15231
49582833
00016717 00000-0 10270-3 0 9001
2 25544 51
6433 127
9436 0001435 59
0558 301
0736 15
55301316 37898
Satellite: ISS
Catalog Number: 25544
Epoch time: 15231
49582833 = yrday
fracday
Element set: 900
Inclination: 51
6433 deg
RA of node: 127
9436 deg
Eccentricity:
0001435
Arg of perigee: 59
0558 deg
Mean anomaly: 301
0736 deg
Mean motion: 15
55301316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3789
Checksum: 303
Coasting Arc #2 (Orbit 3803)
---------------------------------------
Vector Time (GMT): 2015/232/10:58:05
436
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2617230
67 A = 6785067
75 meter
Y = 6113999
71 meter E =
0010081
Z = -1324009
49 I = 51
96772
XDOT = -4884
984605 Wp = 40
67385
YDOT = -830
579567 meter/sec RA = 122
13291 deg
ZDOT = 5853
359946 TA = 304
97385
MA = 305
06847
Ha = 219
548 n
mi
Hp = 212
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8586714
81 X = -2678972
87
Y = 20059054
18 feet Y = 6084386
82 meter
Z = -4343863
17 Z = -1336873
76
XDOT = -16026
852380 XDOT = -4903
767064
YDOT = -2724
998581 feet/sec YDOT = -885
311331 meter/sec
ZDOT = 19203
936831 ZDOT = 5829
584213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20615356
59 X = 6283560
69
Y = -7114092
30 feet Y = -2168375
33 meter
Z = -4400367
76 Z = -1341232
09
XDOT = 8298
541308 XDOT = 2529
395391
YDOT = 12297
518005 feet/sec YDOT = 3748
283488 meter/sec
ZDOT = 19101
555168 ZDOT = 5822
154015
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 15232
45961836
00016717 00000-0 10270-3 0 9013
2 25544 51
6437 123
1299 0001388 58
1222 302
0066 15
55331091 38040
Satellite: ISS
Catalog Number: 25544
Epoch time: 15232
45961836 = yrday
fracday
Element set: 901
Inclination: 51
6437 deg
RA of node: 123
1299 deg
Eccentricity:
0001388
Arg of perigee: 58
1222 deg
Mean anomaly: 302
0066 deg
Mean motion: 15
55331091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3804
Checksum: 287
Coasting Arc #3 (Orbit 3819)
---------------------------------------
Vector Time (GMT): 2015/233/10:58:05
436
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3628187
11 A = 6785582
55 meter
Y = -5670913
99 meter E =
0010710
Z = -815119
10 I = 51
98593
XDOT = 3621
464176 Wp = 133
83469
YDOT = 3167
366256 meter/sec RA = 117
17985 deg
ZDOT = -5972
226110 TA = 54
94087
MA = 54
84046
Ha = 219
577 n
mi
Hp = 212
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11903501
01 X = 3695290
51
Y = -18605360
86 feet Y = -5629966
06 meter
Z = -2674275
26 Z = -797330
86
XDOT = 11881
444146 XDOT = 3614
787476
YDOT = 10391
621576 feet/sec YDOT = 3207
826202 meter/sec
ZDOT = -19593
917684 ZDOT = -5954
650204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21727705
72 X = -6622604
70
Y = 4021071
65 feet Y = 1225622
64 meter
Z = -2596598
57 Z = -791443
24
XDOT = -332
871991 XDOT = -101
459383
YDOT = -14280
830177 feet/sec YDOT = -4352
797038 meter/sec
ZDOT = -19518
665612 ZDOT = -5949
289278
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 15233
48764851
00016717 00000-0 10270-3 0 9026
2 25544 51
6441 117
9954 0001296 64
9186 295
2102 15
55325831 38203
Satellite: ISS
Catalog Number: 25544
Epoch time: 15233
48764851 = yrday
fracday
Element set: 902
Inclination: 51
6441 deg
RA of node: 117
9954 deg
Eccentricity:
0001296
Arg of perigee: 64
9186 deg
Mean anomaly: 295
2102 deg
Mean motion: 15
55325831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3820
Checksum: 313
Coasting Arc #4 (Orbit 3835)
---------------------------------------
Vector Time (GMT): 2015/234/10:58:05
436
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4204884
25 A = 6782504
66 meter
Y = 4519244
38 meter E =
0014816
Z = 2793484
07 I = 51
98970
XDOT = -2204
054960 Wp = 77
87503
YDOT = -5245
843473 meter/sec RA = 112
22289 deg
ZDOT = 5149
051706 TA = 313
67717
MA = 313
79986
Ha = 219
601 n
mi
Hp = 212
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13795552
01 X = -4268676
66
Y = 14826917
27 feet Y = 4471866
03 meter
Z = 9164973
97 Z = 2772902
51
XDOT = -7231
151442 XDOT = -2170
242919
YDOT = -17210
772549 feet/sec YDOT = -5270
301400 meter/sec
ZDOT = 16893
214258 ZDOT = 5138
427220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20289070
22 X = 6184108
60
Y = -376304
64 feet Y = -114697
65 meter
Z = 9075434
05 Z = 2766192
30
XDOT = -7273
413110 XDOT = -2216
936316
YDOT = 15769
021788 feet/sec YDOT = 4806
397841 meter/sec
ZDOT = 16848
300431 ZDOT = 5135
361971
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 15234
51566455
00016717 00000-0 10270-3 0 9032
2 25544 51
6442 112
8608 0001426 61
4286 298
7011 15
55359908 38368
Satellite: ISS
Catalog Number: 25544
Epoch time: 15234
51566455 = yrday
fracday
Element set: 903
Inclination: 51
6442 deg
RA of node: 112
8608 deg
Eccentricity:
0001426
Arg of perigee: 61
4286 deg
Mean anomaly: 298
7011 deg
Mean motion: 15
55359908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3836
Checksum: 314
Coasting Arc #5 (Orbit 3850)
---------------------------------------
Vector Time (GMT): 2015/235/10:58:05
436
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4419910
56 A = 6777659
75 meter
Y = -2726127
28 meter E =
0009907
Z = -4365521
24 I = 51
98565
XDOT = 745
163857 Wp = 68
40998
YDOT = 6782
693254 meter/sec RA = 107
25310 deg
ZDOT = -3483
911505 TA = 166
35120
MA = 166
32439
Ha = 219
424 n
mi
Hp = 212
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14501018
89 X = 4471272
22
Y = -8943987
12 feet Y = -2676413
88 meter
Z = -14322576
24 Z = -4343925
46
XDOT = 2444
763311 XDOT = 686
186205
YDOT = 22252
930622 feet/sec YDOT = 6790
696303 meter/sec
ZDOT = -11430
155857 ZDOT = -3480
435108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16650602
86 X = -5075103
75
Y = -3962922
97 feet Y = -1207898
92 meter
Z = -14228960
27 Z = -4336987
09
XDOT = 13633
681080 XDOT = 4155
545993
YDOT = -16325
624641 feet/sec YDOT = -4976
050391 meter/sec
ZDOT = -11416
345669 ZDOT = -3479
702160
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 15235
47941598
00016717 00000-0 10270-3 0 9044
2 25544 51
6447 108
0473 0001271 59
7946 300
3333 15
55400787 38517
Satellite: ISS
Catalog Number: 25544
Epoch time: 15235
47941598 = yrday
fracday
Element set: 904
Inclination: 51
6447 deg
RA of node: 108
0473 deg
Eccentricity:
0001271
Arg of perigee: 59
7946 deg
Mean anomaly: 300
3333 deg
Mean motion: 15
55400787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3851
Checksum: 315
Coasting Arc #6 (Orbit 3866)
---------------------------------------
Vector Time (GMT): 2015/236/10:58:05
436
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4287064
37 A = 6774133
52 meter
Y = 529859
98 meter E =
0004982
Z = 5214524
65 I = 51
98280
XDOT = 620
866946 Wp = 111
73351
YDOT = -7541
990965 meter/sec RA = 102
26898 deg
ZDOT = 1274
029239 TA = 326
08540
MA = 326
11724
Ha = 219
565 n
mi
Hp = 212
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14065171
83 X = -4318000
78
Y = 1738385
76 feet Y = 481746
34 meter
Z = 17108020
51 Z = 5193623
94
XDOT = 2036
965047 XDOT = 698
968460
YDOT = -24744
064846 feet/sec YDOT = -7534
611306 meter/sec
ZDOT = 4179
885954 ZDOT = 1277
235117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11417911
97 X = 3480179
57
Y = 8576825
05 feet Y = 2614216
27 meter
Z = 17017777
98 Z = 5187018
73
XDOT = -17983
587434 XDOT = -5481
397450
YDOT = 15598
930497 feet/sec YDOT = 4754
554015 meter/sec
ZDOT = 4195
042499 ZDOT = 1278
648954
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 15236
50740567
00016717 00000-0 10270-3 0 9053
2 25544 51
6449 102
9127 0001296 65
2366 294
8922 15
55417845 38674
Satellite: ISS
Catalog Number: 25544
Epoch time: 15236
50740567 = yrday
fracday
Element set: 905
Inclination: 51
6449 deg
RA of node: 102
9127 deg
Eccentricity:
0001296
Arg of perigee: 65
2366 deg
Mean anomaly: 294
8922 deg
Mean motion: 15
55417845 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3867
Checksum: 331
Coasting Arc #7 (Orbit 3881)
---------------------------------------
Vector Time (GMT): 2015/237/10:58:05
436
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3903531
35 A = 6773946
18 meter
Y = 1805788
01 meter E =
0015200
Z = -5246617
84 I = 51
98818
XDOT = -1847
317715 Wp = 96
09669
YDOT = 7343
054826 meter/sec RA = 97
27825 deg
ZDOT = 1154
215007 TA = 184
92240
MA = 184
93737
Ha = 219
328 n
mi
Hp = 212
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12806861
39 X = 3908534
30
Y = 5924501
34 feet Y = 1849467
74 meter
Z = -17213313
12 Z = -5227643
33
XDOT = -6060
753657 XDOT = -1934
898914
YDOT = 24091
387226 feet/sec YDOT = 7321
907232 meter/sec
ZDOT = 3786
794641 ZDOT = 1145
028332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5424099
72 X = -1653265
60
Y = -13133718
79 feet Y = -4003157
49 meter
Z = -17131787
30 Z = -5221768
77
XDOT = 19905
415288 XDOT = 6067
170580
YDOT = -13101
332548 feet/sec YDOT = -3993
286161 meter/sec
ZDOT = 3745
862401 ZDOT = 1141
738860
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 15237
47113304
00016717 00000-0 10270-3 0 9064
2 25544 51
6448 98
0987 0001210 62
0720 298
0556 15
55448621 38829
Satellite: ISS
Catalog Number: 25544
Epoch time: 15237
47113304 = yrday
fracday
Element set: 906
Inclination: 51
6448 deg
RA of node: 98
0987 deg
Eccentricity:
0001210
Arg of perigee: 62
0720 deg
Mean anomaly: 298
0556 deg
Mean motion: 15
55448621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3882
Checksum: 307
Coasting Arc #8 (Orbit 3897)
---------------------------------------
Vector Time (GMT): 2015/238/10:58:05
436
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3284847
70 A = 6777179
51 meter
Y = -3960490
20 meter E =
0010606
Z = 4404408
07 I = 52
00278
XDOT = 2916
572181 Wp = 69
18431
YDOT = -6224
297626 meter/sec RA = 92
29421 deg
ZDOT = -3411
475841 TA = 55
20808
MA = 55
10832
Ha = 219
317 n
mi
Hp = 212
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10777059
37 X = -3261711
06
Y = -12993734
26 feet Y = -3997094
04 meter
Z = 14450157
72 Z = 4388507
45
XDOT = 9568
806368 XDOT = 3002
528450
YDOT = -20420
923970 feet/sec YDOT = -6191
202083 meter/sec
ZDOT = -11192
506041 ZDOT = -3397
098956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -598625
46 X = -182461
04
Y = 16928703
80 feet Y = 5159868
92 meter
Z = 14382274
92 Z = 4383717
40
XDOT = -19585
262664 XDOT = -5969
588060
YDOT = 8791
485019 feet/sec YDOT = 2679
644634 meter/sec
ZDOT = -11129
372505 ZDOT = -3392
232739
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 15238
49909508
00016717 00000-0 10270-3 0 9077
2 25544 51
6449 92
9642 0001181 57
8077 302
3190 15
55497642 38982
Satellite: ISS
Catalog Number: 25544
Epoch time: 15238
49909508 = yrday
fracday
Element set: 907
Inclination: 51
6449 deg
RA of node: 92
9642 deg
Eccentricity:
0001181
Arg of perigee: 57
8077 deg
Mean anomaly: 302
3190 deg
Mean motion: 15
55497642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3898
Checksum: 343
Coasting Arc #9 (Orbit 3912)
---------------------------------------
Vector Time (GMT): 2015/239/10:58:05
436
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2502923
44 A = 6781981
66 meter
Y = 5614070
72 meter E =
0005759
Z = -2866494
44 I = 52
01803
XDOT = -3787
585412 Wp = 61
86199
YDOT = 4288
422031 meter/sec RA = 87
32414 deg
ZDOT = 5102
164949 TA = 265
71183
MA = 265
77763
Ha = 219
275 n
mi
Hp = 212
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8211691
06 X = 2453883
64
Y = 18418867
19 feet Y = 5641785
73 meter
Z = -9404509
30 Z = -2854455
29
XDOT = -12426
461325 XDOT = -3860
042067
YDOT = 14069
626086 feet/sec YDOT = 4245
661863 meter/sec
ZDOT = 16739
386316 ZDOT = 5083
589728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5825306
35 X = 1775553
38
Y = -19331518
77 feet Y = -5892246
92 meter
Z = -9353583
36 Z = -2850972
21
XDOT = 17278
693507 XDOT = 5266
545781
YDOT = -2836
890278 feet/sec YDOT = -864
684157 meter/sec
ZDOT = 16658
480085 ZDOT = 5077
504730
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 15239
46279875
00016717 00000-0 10270-3 0 9083
2 25544 51
6441 88
1498 0001107 59
8825 300
2438 15
55468567 39135
Satellite: ISS
Catalog Number: 25544
Epoch time: 15239
46279875 = yrday
fracday
Element set: 908
Inclination: 51
6441 deg
RA of node: 88
1498 deg
Eccentricity:
0001107
Arg of perigee: 59
8825 deg
Mean anomaly: 300
2438 deg
Mean motion: 15
55468567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3913
Checksum: 342
Coasting Arc #10 (Orbit 3928)
---------------------------------------
Vector Time (GMT): 2015/240/10:58:05
436
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1522590
86 A = 6785143
99 meter
Y = -6554784
91 meter E =
0014038
Z = 818258
23 I = 52
02597
XDOT = 4465
631709 Wp = 122
35803
YDOT = -1791
592992 meter/sec RA = 82
36915 deg
ZDOT = -5975
216297 TA = 48
83388
MA = 48
71286
Ha = 219
295 n
mi
Hp = 212
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4995376
82 X = -1453155
22
Y = -21505199
83 feet Y = -6571423
23 meter
Z = 2684574
24 Z = 811031
01
XDOT = 14651
022666 XDOT = 4514
358677
YDOT = -5877
929763 feet/sec YDOT = -1741
383325 meter/sec
ZDOT = -19603
728007 ZDOT = -5953
405046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9972651
88 X = -3039664
29
Y = 19701110
67 feet Y = 6004898
53 meter
Z = 2654581
09 Z = 809116
32
XDOT = -13664
420451 XDOT = -4164
915353
YDOT = -4258
158918 feet/sec YDOT = -1297
886838 meter/sec
ZDOT = -19509
306628 ZDOT = -5946
436660
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 15240
49073582
00016717 00000-0 10270-3 0 9096
2 25544 51
6438 83
0150 0001150 70
2150 289
9127 15
55474341 39298
Satellite: ISS
Catalog Number: 25544
Epoch time: 15240
49073582 = yrday
fracday
Element set: 909
Inclination: 51
6438 deg
RA of node: 83
0150 deg
Eccentricity:
0001150
Arg of perigee: 70
2150 deg
Mean anomaly: 289
9127 deg
Mean motion: 15
55474341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3929
Checksum: 298
Coasting Arc #11 (Orbit 3944)
---------------------------------------
Vector Time (GMT): 2015/241/10:58:05
436
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 413096
29 A = 6784484
22 meter
Y = 6632007
95 meter E =
0014815
Z = 1334099
01 I = 52
01814
XDOT = -4880
500850 Wp = 60
20693
YDOT = -882
027584 meter/sec RA = 77
41701 deg
ZDOT = 5854
594261 TA = 314
25496
MA = 314
37646
Ha = 219
144 n
mi
Hp = 212
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1355302
79 X = 332424
43
Y = 21758556
26 feet Y = 6636176
52 meter
Z = 4376965
27 Z = 1335909
17
XDOT = -16012
141895 XDOT = -4898
714021
YDOT = -2893
791286 feet/sec YDOT = -936
705849 meter/sec
ZDOT = 19207
986419 ZDOT = 5830
841985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12656587
65 X = 3857727
92
Y = -17748931
06 feet Y = -5409874
19 meter
Z = 4383568
92 Z = 1336111
81
XDOT = 9428
112607 XDOT = 2873
688723
YDOT = 11475
175996 feet/sec YDOT = 3497
633644 meter/sec
ZDOT = 19105
674834 ZDOT = 5823
409689
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 15241
51865615
00016717 00000-0 10270-3 0 9108
2 25544 51
6427 77
8786 0001004 67
6054 292
5206 15
55537019 39451
Satellite: ISS
Catalog Number: 25544
Epoch time: 15241
51865615 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 77
8786 deg
Eccentricity:
0001004
Arg of perigee: 67
6054 deg
Mean anomaly: 292
5206 deg
Mean motion: 15
55537019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3945
Checksum: 313
Coasting Arc #12 (Orbit 3959)
---------------------------------------
Vector Time (GMT): 2015/242/10:58:05
436
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 856960
99 A = 6780635
00 meter
Y = -5860282
84 meter E =
0005587
Z = -3306281
05 I = 51
99638
XDOT = 4964
914734 Wp = 89
98505
YDOT = 3400
233159 meter/sec RA = 72
45736 deg
ZDOT = -4746
848689 TA = 128
22879
MA = 128
17848
Ha = 219
150 n
mi
Hp = 212
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2811551
81 X = 938488
86
Y = -19226649
75 feet Y = -5850244
25 meter
Z = -10847378
79 Z = -3301919
50
XDOT = 16289
090336 XDOT = 4949
581605
YDOT = 11155
620601 feet/sec YDOT = 3455
667850 meter/sec
ZDOT = -15573
650553 ZDOT = -4722
768042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14107163
53 X = -4299863
44
Y = 13378635
29 feet Y = 4077808
04 meter
Z = -10827491
20 Z = -3300219
32
XDOT = -5072
031349 XDOT = -1545
955155
YDOT = -17850
231290 feet/sec YDOT = -5440
750497 meter/sec
ZDOT = -15470
384930 ZDOT = -4715
373327
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 15242
48232130
00016717 00000-0 10270-3 0 9116
2 25544 51
6417 73
0639 0001020 66
1638 293
9622 15
55529487 39609
Satellite: ISS
Catalog Number: 25544
Epoch time: 15242
48232130 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 73
0639 deg
Eccentricity:
0001020
Arg of perigee: 66
1638 deg
Mean anomaly: 293
9622 deg
Mean motion: 15
55529487 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3960
Checksum: 299
Coasting Arc #13 (Orbit 3975)
---------------------------------------
Vector Time (GMT): 2015/243/10:58:05
436
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2165804
59 A = 6775947
83 meter
Y = 4370176
44 meter E =
0008752
Z = 4698021
09 I = 51
97010
XDOT = -4655
557917 Wp = 110
57323
YDOT = -5389
113772 meter/sec RA = 67
48019 deg
ZDOT = 2859
528191 TA = 311
15671
MA = 311
23219
Ha = 219
267 n
mi
Hp = 212
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7105658
11 X = -2237333
02
Y = 14337849
20 feet Y = 4345557
59 meter
Z = 15413455
04 Z = 4687325
89
XDOT = -15274
140149 XDOT = -4608
839927
YDOT = -17680
819462 feet/sec YDOT = -5440
913737 meter/sec
ZDOT = 9381
654170 ZDOT = 2837
026697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14384311
34 X = 4384338
10
Y = -7113424
67 feet Y = -2168171
84 meter
Z = 15366511
31 Z = 4683712
65
XDOT = 1082
381199 XDOT = 329
909789
YDOT = 22299
328876 feet/sec YDOT = 6796
835442 meter/sec
ZDOT = 9285
574608 ZDOT = 2830
243141
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 15243
51021736
00016717 00000-0 10270-3 0 9120
2 25544 51
6417 67
9272 0001112 65
7380 294
3889 15
55522086 39760
Satellite: ISS
Catalog Number: 25544
Epoch time: 15243
51021736 = yrday
fracday
Element set: 912
Inclination: 51
6417 deg
RA of node: 67
9272 deg
Eccentricity:
0001112
Arg of perigee: 65
7380 deg
Mean anomaly: 294
3889 deg
Mean motion: 15
55522086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3976
Checksum: 314
Coasting Arc #14 (Orbit 3990)
---------------------------------------
Vector Time (GMT): 2015/244/10:58:05
436
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3452097
31 A = 6773205
50 meter
Y = -2396385
54 meter E =
0015820
Z = -5325592
88 I = 51
94744
XDOT = 3854
762145 Wp = 85
44585
YDOT = 6601
656629 meter/sec RA = 62
48841 deg
ZDOT = -471
873206 TA = 180
06673
MA = 180
06694
Ha = 219
094 n
mi
Hp = 212
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11325778
58 X = 3504507
33
Y = -7862157
29 feet Y = -2357489
47 meter
Z = -17472417
58 Z = -5308695
77
XDOT = 12646
857430 XDOT = 3782
946501
YDOT = 21658
978442 feet/sec YDOT = 6644
361519 meter/sec
ZDOT = -1548
140440 ZDOT = -453
322773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13874776
99 X = -4229032
03
Y = -367017
62 feet Y = -111866
97 meter
Z = -17399080
87 Z = -5303239
85
XDOT = 2476
137618 XDOT = 754
726746
YDOT = -23948
756275 feet/sec YDOT = -7299
580913 meter/sec
ZDOT = -1469
342544 ZDOT = -447
855607
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 15244
47385448
00016717 00000-0 10270-3 0 9130
2 25544 51
6408 63
1116 0001061 73
5537 286
5733 15
55578580 39917
Satellite: ISS
Catalog Number: 25544
Epoch time: 15244
47385448 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 63
1116 deg
Eccentricity:
0001061
Arg of perigee: 73
5537 deg
Mean anomaly: 286
5733 deg
Mean motion: 15
55578580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3991
Checksum: 321
Coasting Arc #15 (Orbit 4006)
---------------------------------------
Vector Time (GMT): 2015/245/10:58:05
436
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4527942
75 A = 6774455
10 meter
Y = 223724
25 meter E =
0006868
Z = 5029990
95 I = 51
93677
XDOT = -2570
870330 Wp = 58
85568
YDOT = -6948
518284 meter/sec RA = 57
49416 deg
ZDOT = -1999
739653 TA = 50
50261
MA = 50
44189
Ha = 219
205 n
mi
Hp = 212
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14855455
22 X = -4554541
74
Y = 734003
46 feet Y = 172941
59 meter
Z = 16502594
97 Z = 5007930
49
XDOT = -8434
613945 XDOT = -2483
265273
YDOT = -22796
975997 feet/sec YDOT = -6976
777815 meter/sec
ZDOT = -6560
825633 ZDOT = -2012
014955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12671079
10 X = 3862144
91
Y = 7987505
40 feet Y = 2434591
64 meter
Z = 16407390
51 Z = 5000972
63
XDOT = -5635
574785 XDOT = -1717
723194
YDOT = 22560
058280 feet/sec YDOT = 6876
305764 meter/sec
ZDOT = -6612
474473 ZDOT = -2015
482219
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 15245
50172140
00016717 00000-0 10270-3 0 9149
2 25544 51
6414 57
9761 0000973 76
1179 284
0083 15
55585036 40077
Satellite: ISS
Catalog Number: 25544
Epoch time: 15245
50172140 = yrday
fracday
Element set: 914
Inclination: 51
6414 deg
RA of node: 57
9761 deg
Eccentricity:
0000973
Arg of perigee: 76
1179 deg
Mean anomaly: 284
0083 deg
Mean motion: 15
55585036 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4007
Checksum: 300
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