[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 17th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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
077/23:47:09
147 -1
9 1
9 1
9
N/A 0
1 -0
2 222
2
000/00:04:18
294 0
4 0
1 211
0
Coasting Arc #1 (Orbit 1361)
---------------------------------------
Vector Time (GMT): 2015/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6707853
04 A = 6786184
87 meter
Y = -946011
82 meter E =
0018510
Z = 316647
38 I = 51
62212
XDOT = 956
502411 Wp = 72
24914
YDOT = -4678
824949 meter/sec RA = 185
90602 deg
ZDOT = 6000
807180 TA = 291
16548
MA = 291
36318
Ha = 222
404 n
mi
Hp = 209
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22007391
85 X = -6698314
10
Y = -3103713
33 feet Y = -1020970
04 meter
Z = 1038869
34 Z = 284085
61
XDOT = 3138
131269 XDOT = 979
601739
YDOT = -15350
475553 feet/sec YDOT = -4667
998904 meter/sec
ZDOT = 19687
687600 ZDOT = 6005
510240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21463646
23 X = -6542119
37
Y = -5791395
56 feet Y = -1765217
37 meter
Z = 899561
09 Z = 274186
22
XDOT = 4458
454258 XDOT = 1358
936858
YDOT = -13295
581778 feet/sec YDOT = -4052
493326 meter/sec
ZDOT = 19708
542258 ZDOT = 6007
163680
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 15075
56373285
00016717 00000-0 10270-3 0 9004
2 25544 51
6455 186
7060 0008600 108
0717 252
1374 15
55200152 13626
Satellite: ISS
Catalog Number: 25544
Epoch time: 15075
56373285 = yrday
fracday
Element set: 900
Inclination: 51
6455 deg
RA of node: 186
7060 deg
Eccentricity:
0008600
Arg of perigee: 108
0717 deg
Mean anomaly: 252
1374 deg
Mean motion: 15
55200152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1362
Checksum: 284
Coasting Arc #2 (Orbit 1376)
---------------------------------------
Vector Time (GMT): 2015/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6048949
11 A = 6783801
54 meter
Y = 1964130
98 meter E =
0014077
Z = -2358028
17 I = 51
64626
XDOT = -3457
652665 Wp = 121
58113
YDOT = 4211
578036 meter/sec RA = 180
92850 deg
ZDOT = -5392
622054 TA = 84
73422
MA = 84
57361
Ha = 222
354 n
mi
Hp = 209
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19845633
57 X = 6037990
43
Y = 6443999
29 feet Y = 2031712
71 meter
Z = -7736312
91 Z = -2328670
82
XDOT = -11344
004806 XDOT = -3478
295554
YDOT = 13817
513241 feet/sec YDOT = 4172
796197 meter/sec
ZDOT = -17692
329573 ZDOT = -5409
469110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19098529
17 X = 5821231
69
Y = 8517377
54 feet Y = 2596096
67 meter
Z = -7610867
18 Z = -2319792
32
XDOT = -12012
712976 XDOT = -3661
474915
YDOT = 11153
856492 feet/sec YDOT = 3399
695459 meter/sec
ZDOT = -17765
127130 ZDOT = -5414
810749
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 15076
52758230
00016717 00000-0 10270-3 0 9019
2 25544 51
6457 181
8934 0008566 111
8344 248
3721 15
55242736 13776
Satellite: ISS
Catalog Number: 25544
Epoch time: 15076
52758230 = yrday
fracday
Element set: 901
Inclination: 51
6457 deg
RA of node: 181
8934 deg
Eccentricity:
0008566
Arg of perigee: 111
8344 deg
Mean anomaly: 248
3721 deg
Mean motion: 15
55242736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1377
Checksum: 319
Coasting Arc #3 (Orbit 1392)
---------------------------------------
Vector Time (GMT): 2015/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4688433
95 A = 6779260
45 meter
Y = -2827392
79 meter E =
0019395
Z = 3986170
78 I = 51
66384
XDOT = 5531
314889 Wp = 107
16130
YDOT = -3541
559240 meter/sec RA = 175
94088 deg
ZDOT = 3972
211756 TA = 301
46262
MA = 301
65205
Ha = 222
269 n
mi
Hp = 209
918
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15382001
16 X = -4675832
02
Y = -9276223
06 feet Y = -2879750
87 meter
Z = 13077988
11 Z = 3963426
57
XDOT = 18147
358560 XDOT = 5551
211054
YDOT = -11619
288845 feet/sec YDOT = -3479
592632 meter/sec
ZDOT = 13032
190801 ZDOT = 3999
130336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14578196
02 X = -4443434
15
Y = -10614057
74 feet Y = -3235164
80 meter
Z = 12980987
10 Z = 3956604
87
XDOT = 18252
292155 XDOT = 5563
298649
YDOT = -8901
994950 feet/sec YDOT = -2713
328061 meter/sec
ZDOT = 13148
034436 ZDOT = 4007
520896
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 15077
55566411
00016717 00000-0 10270-3 0 9022
2 25544 51
6463 176
7599 0008542 115
1116 245
0925 15
55303804 13933
Satellite: ISS
Catalog Number: 25544
Epoch time: 15077
55566411 = yrday
fracday
Element set: 902
Inclination: 51
6463 deg
RA of node: 176
7599 deg
Eccentricity:
0008542
Arg of perigee: 115
1116 deg
Mean anomaly: 245
0925 deg
Mean motion: 15
55303804 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1393
Checksum: 309
Coasting Arc #4 (Orbit 1399)
---------------------------------------
Vector Time (GMT): 2015/077/23:49:18
294
Vector Time (MET): N/A
Weight (LBS) : 889206
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1687933
84 A = 6776155
76 meter
Y = 4213230
50 meter E =
0019886
Z = -5049618
79 I = 51
66506
XDOT = -7382
353320 Wp = 108
25710
YDOT = -670
496776 meter/sec RA = 173
44375 deg
ZDOT = 1908
354552 TA = 180
27471
MA = 180
27580
Ha = 222
155 n
mi
Hp = 210
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5537840
68 X = -1710392
82
Y = 13822934
71 feet Y = 4194228
56 meter
Z = -16566990
80 Z = -5057873
57
XDOT = -24220
319292 XDOT = -7383
576973
YDOT = -2199
792573 feet/sec YDOT = -753
057616 meter/sec
ZDOT = 6261
005747 ZDOT = 1872
490022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7143058
08 X = 2177204
10
Y = -13020134
62 feet Y = -3968537
03 meter
Z = -16602987
78 Z = -5060590
67
XDOT = 22834
734808 XDOT = 6960
027169
YDOT = 4739
807847 feet/sec YDOT = 1444
693432 meter/sec
ZDOT = 6107
469702 ZDOT = 1861
556765
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 15078
00544479
00016717 00000-0 10270-3 0 9034
2 25544 51
6457 174
5161 0006894 115
1974 244
9895 15
54936868 14001
Satellite: ISS
Catalog Number: 25544
Epoch time: 15078
00544479 = yrday
fracday
Element set: 903
Inclination: 51
6457 deg
RA of node: 174
5161 deg
Eccentricity:
0006894
Arg of perigee: 115
1974 deg
Mean anomaly: 244
9895 deg
Mean motion: 15
54936868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1400
Checksum: 339
Coasting Arc #5 (Orbit 1415)
---------------------------------------
Vector Time (GMT): 2015/078/23:49:18
294
Vector Time (MET): N/A
Weight (LBS) : 889206
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3639068
07 A = 6779797
98 meter
Y = -4015181
28 meter E =
0016435
Z = 4059526
48 I = 51
70876
XDOT = 6365
115668 Wp = 93
65528
YDOT = 1828
981999 meter/sec RA = 168
44690 deg
ZDOT = -3884
344172 TA = 36
53579
MA = 36
42378
Ha = 222
026 n
mi
Hp = 211
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11939199
71 X = 3663976
77
Y = -13173166
92 feet Y = -3974346
89 meter
Z = 13318656
44 Z = 4077265
43
XDOT = 20882
925419 XDOT = 6363
059070
YDOT = 6000
597108 feet/sec YDOT = 1900
148730 meter/sec
ZDOT = -12743
911324 ZDOT = -3853
429166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13229662
25 X = -4032401
05
Y = 11790103
06 feet Y = 3593623
41 meter
Z = 13395257
84 Z = 4082874
59
XDOT = -19317
691396 XDOT = -5888
032338
YDOT = -7301
227412 feet/sec YDOT = -2225
414115 meter/sec
ZDOT = -12611
742001 ZDOT = -3844
058962
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 15079
03372888
00016717 00000-0 10270-3 0 9042
2 25544 51
6455 169
3843 0006921 118
5160 241
6690 15
54967784 14168
Satellite: ISS
Catalog Number: 25544
Epoch time: 15079
03372888 = yrday
fracday
Element set: 904
Inclination: 51
6455 deg
RA of node: 169
3843 deg
Eccentricity:
0006921
Arg of perigee: 118
5160 deg
Mean anomaly: 241
6690 deg
Mean motion: 15
54967784 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1416
Checksum: 334
Coasting Arc #6 (Orbit 1430)
---------------------------------------
Vector Time (GMT): 2015/079/23:49:18
294
Vector Time (MET): N/A
Weight (LBS) : 889206
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5159390
20 A = 6783944
66 meter
Y = 3612105
17 meter E =
0009867
Z = -2530204
33 I = 51
75444
XDOT = -4669
268919 Wp = 92
60280
YDOT = -2970
180422 meter/sec RA = 163
46473 deg
ZDOT = 5298
388985 TA = 239
06004
MA = 239
15706
Ha = 221
939 n
mi
Hp = 210
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16927133
20 X = -5187107
38
Y = 11850738
73 feet Y = 3554254
10 meter
Z = -8301195
30 Z = -2555335
54
XDOT = -15319
123750 XDOT = -4661
446196
YDOT = -9744
686423 feet/sec YDOT = -3022
350612 meter/sec
ZDOT = 17383
165962 ZDOT = 5275
726107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17900329
78 X = 5456020
52
Y = -10234139
83 feet Y = -3119365
82 meter
Z = -8409415
33 Z = -2563189
79
XDOT = 13712
768362 XDOT = 4179
651797
YDOT = 9826
670774 feet/sec YDOT = 2995
169252 meter/sec
ZDOT = 17286
516075 ZDOT = 5268
930100
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 15079
99772290
00016717 00000-0 10270-3 0 9059
2 25544 51
6460 164
5723 0006857 121
8127 238
3695 15
55020596 14313
Satellite: ISS
Catalog Number: 25544
Epoch time: 15079
99772290 = yrday
fracday
Element set: 905
Inclination: 51
6460 deg
RA of node: 164
5723 deg
Eccentricity:
0006857
Arg of perigee: 121
8127 deg
Mean anomaly: 238
3695 deg
Mean motion: 15
55020596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1431
Checksum: 326
Coasting Arc #7 (Orbit 1446)
---------------------------------------
Vector Time (GMT): 2015/080/23:49:18
294
Vector Time (MET): N/A
Weight (LBS) : 889206
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6100122
81 A = 6786591
25 meter
Y = -2894884
55 meter E =
0020002
Z = 581017
27 I = 51
79298
XDOT = 2518
496966 Wp = 127
86428
YDOT = 4078
310944 meter/sec RA = 158
49644 deg
ZDOT = -5993
510701 TA = 45
87204
MA = 45
70769
Ha = 221
935 n
mi
Hp = 211
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20013526
26 X = 6129218
34
Y = -9497652
73 feet Y = -2826506
22 meter
Z = 1906224
65 Z = 610721
69
XDOT = 8262
785320 XDOT = 2501
819467
YDOT = 13380
285248 feet/sec YDOT = 4106
380242 meter/sec
ZDOT = -19663
749020 ZDOT = -5981
317439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20661747
08 X = -6297700
51
Y = 7958367
75 feet Y = 2425710
49 meter
Z = 2033942
87 Z = 619945
79
XDOT = -6771
672019 XDOT = -2064
005631
YDOT = -12467
630804 feet/sec YDOT = -3800
133869 meter/sec
ZDOT = -19612
123288 ZDOT = -5977
775178
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 15081
02596147
00016717 00000-0 10270-3 0 9062
2 25544 51
6458 159
4395 0006875 125
7940 234
3853 15
55016682 14474
Satellite: ISS
Catalog Number: 25544
Epoch time: 15081
02596147 = yrday
fracday
Element set: 906
Inclination: 51
6458 deg
RA of node: 159
4395 deg
Eccentricity:
0006875
Arg of perigee: 125
7940 deg
Mean anomaly: 234
3853 deg
Mean motion: 15
55016682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1447
Checksum: 330
Coasting Arc #8 (Orbit 1462)
---------------------------------------
Vector Time (GMT): 2015/081/23:49:18
294
Vector Time (MET): N/A
Weight (LBS) : 889206
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6348119
08 A = 6785808
57 meter
Y = 1923039
08 meter E =
0017526
Z = 1408722
78 I = 51
81961
XDOT = -211
807402 Wp = 81
26892
YDOT = -5000
032356 meter/sec RA = 153
53284 deg
ZDOT = 5812
007604 TA = 294
05564
MA = 294
23892
Ha = 221
780 n
mi
Hp = 211
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20827162
34 X = -6375994
24
Y = 6309183
32 feet Y = 1851894
59 meter
Z = 4621793
90 Z = 1377816
74
XDOT = -694
906173 XDOT = -184
112812
YDOT = -16404
305630 feet/sec YDOT = -5002
245285 meter/sec
ZDOT = 19068
266418 ZDOT = 5811
046628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21189088
32 X = 6458434
12
Y = -5080190
59 feet Y = -1548442
09 meter
Z = 4489060
47 Z = 1368265
63
XDOT = -514
419420 XDOT = -156
795039
YDOT = 14877
144637 feet/sec YDOT = 4534
553685 meter/sec
ZDOT = 19064
915478 ZDOT = 5810
986238
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 15082
05417569
00016717 00000-0 10270-3 0 9077
2 25544 51
6455 154
3065 0006696 127
8991 232
2768 15
55068075 14632
Satellite: ISS
Catalog Number: 25544
Epoch time: 15082
05417569 = yrday
fracday
Element set: 907
Inclination: 51
6455 deg
RA of node: 154
3065 deg
Eccentricity:
0006696
Arg of perigee: 127
8991 deg
Mean anomaly: 232
2768 deg
Mean motion: 15
55068075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1463
Checksum: 333
Coasting Arc #9 (Orbit 1477)
---------------------------------------
Vector Time (GMT): 2015/082/23:49:18
294
Vector Time (MET): N/A
Weight (LBS) : 889206
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5916687
91 A = 6782110
94 meter
Y = -613905
29 meter E =
0010719
Z = -3259921
80 I = 51
83551
XDOT = -2035
463942 Wp = 119
37724
YDOT = 5641
269237 meter/sec RA = 148
56389 deg
ZDOT = -4773
600838 TA = 98
30286
MA = 98
18131
Ha = 221
687 n
mi
Hp = 211
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19411705
75 X = 5938948
56
Y = -2014124
98 feet Y = -547616
94 meter
Z = -10695281
51 Z = -3231125
41
XDOT = -6678
031306 XDOT = -2075
206190
YDOT = 18508
101170 feet/sec YDOT = 5618
284586 meter/sec
ZDOT = -15661
420073 ZDOT = -4783
585956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19545687
16 X = -5957525
45
Y = 1209847
91 feet Y = 368761
64 meter
Z = -10571775
98 Z = -3222277
32
XDOT = 7424
573890 XDOT = 2263
010122
YDOT = -16794
316586 feet/sec YDOT = -5118
907695 meter/sec
ZDOT = -15705
086511 ZDOT = -4786
910369
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 15083
01810496
00016717 00000-0 10270-3 0 9081
2 25544 51
6456 149
4940 0006594 132
7476 227
4233 15
55094966 14787
Satellite: ISS
Catalog Number: 25544
Epoch time: 15083
01810496 = yrday
fracday
Element set: 908
Inclination: 51
6456 deg
RA of node: 149
4940 deg
Eccentricity:
0006594
Arg of perigee: 132
7476 deg
Mean anomaly: 227
4233 deg
Mean motion: 15
55094966 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1478
Checksum: 332
Coasting Arc #10 (Orbit 1493)
---------------------------------------
Vector Time (GMT): 2015/083/23:49:18
294
Vector Time (MET): N/A
Weight (LBS) : 889206
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4902825
47 A = 6777556
83 meter
Y = -865848
39 meter E =
0015032
Z = 4591926
66 I = 51
84705
XDOT = 3905
862223 Wp = 122
90698
YDOT = -5859
299478 meter/sec RA = 143
58259 deg
ZDOT = 3050
291761 TA = 296
65385
MA = 296
80771
Ha = 221
672 n
mi
Hp = 211
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16085385
41 X = -4915084
90
Y = -2840709
95 feet Y = -920743
08 meter
Z = 15065376
19 Z = 4568079
92
XDOT = 12814
508606 XDOT = 3956
274780
YDOT = -19223
423483 feet/sec YDOT = -5815
339400 meter/sec
ZDOT = 10007
518901 ZDOT = 3069
388772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16107626
37 X = 4909604
52
Y = 3227811
00 feet Y = 983836
79 meter
Z = 14963302
62 Z = 4560814
64
XDOT = -12974
130915 XDOT = -3954
515103
YDOT = 17735
651767 feet/sec YDOT = 5405
826659 meter/sec
ZDOT = 10090
287084 ZDOT = 3075
519503
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 15084
04627510
00016717 00000-0 10270-3 0 9099
2 25544 51
6455 144
3606 0006637 134
5620 225
6076 15
55136491 14941
Satellite: ISS
Catalog Number: 25544
Epoch time: 15084
04627510 = yrday
fracday
Element set: 909
Inclination: 51
6455 deg
RA of node: 144
3606 deg
Eccentricity:
0006637
Arg of perigee: 134
5620 deg
Mean anomaly: 225
6076 deg
Mean motion: 15
55136491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1494
Checksum: 304
Coasting Arc #11 (Orbit 1508)
---------------------------------------
Vector Time (GMT): 2015/084/23:49:18
294
Vector Time (MET): N/A
Weight (LBS) : 889206
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3449949
54 A = 6774491
44 meter
Y = 2491875
75 meter E =
0018956
Z = -5286573
88 I = 51
86211
XDOT = -5252
169979 Wp = 99
90453
YDOT = 5508
262210 meter/sec RA = 138
58930 deg
ZDOT = -836
851859 TA = 162
14121
MA = 162
07450
Ha = 221
350 n
mi
Hp = 211
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11318732
08 X = 3447508
61
Y = 8175445
36 feet Y = 2530441
21 meter
Z = -17344402
50 Z = -5269820
84
XDOT = -17231
528803 XDOT = -5309
309202
YDOT = 18071
726412 feet/sec YDOT = 5449
209456 meter/sec
ZDOT = -2745
576966 ZDOT = -862
505186
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11372205
34 X = -3466248
19
Y = -8252084
48 feet Y = -2515235
35 meter
Z = -17272983
19 Z = -5264805
28
XDOT = 16735
511834 XDOT = 5100
984007
YDOT = -17123
755739 feet/sec YDOT = -5219
320749 meter/sec
ZDOT = -2856
411285 ZDOT = -870
634160
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 15085
01016229
00016717 00000-0 10270-3 0 9108
2 25544 51
6453 139
5474 0006471 138
4702 221
6944 15
55199122 15095
Satellite: ISS
Catalog Number: 25544
Epoch time: 15085
01016229 = yrday
fracday
Element set: 910
Inclination: 51
6453 deg
RA of node: 139
5474 deg
Eccentricity:
0006471
Arg of perigee: 138
4702 deg
Mean anomaly: 221
6944 deg
Mean motion: 15
55199122 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1509
Checksum: 297
Coasting Arc #12 (Orbit 1524)
---------------------------------------
Vector Time (GMT): 2015/085/23:49:18
294
Vector Time (MET): N/A
Weight (LBS) : 889206
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1774696
79 A = 6774799
16 meter
Y = -4006207
76 meter E =
0008046
Z = 5159939
63 I = 51
88715
XDOT = 5978
811870 Wp = 108
01613
YDOT = -4576
290095 meter/sec RA = 133
59431 deg
ZDOT = -1497
238883 TA = 356
33361
MA = 356
33950
Ha = 221
277 n
mi
Hp = 211
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5822496
02 X = -1754831
53
Y = -13143726
26 feet Y = -4025942
05 meter
Z = 16928935
78 Z = 5151367
12
XDOT = 19615
524509 XDOT = 6036
813685
YDOT = -15014
075115 feet/sec YDOT = -4509
106945 meter/sec
ZDOT = -4912
201060 ZDOT = -1468
053739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6065409
37 X = 1848736
78
Y = 13080183
43 feet Y = 3986839
91 meter
Z = 16892823
24 Z = 5148932
52
XDOT = -18536
077299 XDOT = -5649
796361
YDOT = 14774
654490 feet/sec YDOT = 4503
314689 meter/sec
ZDOT = -4786
355072 ZDOT = -1458
881026
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 15086
03828709
00016717 00000-0 10270-3 0 9116
2 25544 51
6456 134
4141 0006417 142
6821 217
4780 15
55243079 15252
Satellite: ISS
Catalog Number: 25544
Epoch time: 15086
03828709 = yrday
fracday
Element set: 911
Inclination: 51
6456 deg
RA of node: 134
4141 deg
Eccentricity:
0006417
Arg of perigee: 142
6821 deg
Mean anomaly: 217
4780 deg
Mean motion: 15
55243079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1525
Checksum: 302
Coasting Arc #13 (Orbit 1539)
---------------------------------------
Vector Time (GMT): 2015/086/23:49:18
294
Vector Time (MET): N/A
Weight (LBS) : 889206
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 77414
29 A = 6778319
06 meter
Y = 5271678
13 meter E =
0013979
Z = -4275225
62 I = 51
91954
XDOT = -6037
023464 Wp = 126
03490
YDOT = 3020
543218 meter/sec RA = 128
60644 deg
ZDOT = 3615
486605 TA = 180
81996
MA = 180
82226
Ha = 221
100 n
mi
Hp = 211
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 253983
90 X = 39226
74
Y = 17295531
91 feet Y = 5272329
89 meter
Z = -14026330
79 Z = -4274942
82
XDOT = -19806
507428 XDOT = -6087
913816
YDOT = 9909
918695 feet/sec YDOT = 2952
749084 meter/sec
ZDOT = 11861
832692 ZDOT = 3586
036145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -819187
96 X = -249688
49
Y = -17278285
57 feet Y = -5266421
44 meter
Z = -14025964
00 Z = -4275113
83
XDOT = 18340
861752 XDOT = 5590
294662
YDOT = -10395
083794 feet/sec YDOT = -3168
421541 meter/sec
ZDOT = 11735
080814 ZDOT = 3576
852632
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 15087
00213476
00016717 00000-0 10270-3 0 9124
2 25544 51
6449 129
6005 0006377 146
1240 214
0321 15
55254785 15405
Satellite: ISS
Catalog Number: 25544
Epoch time: 15087
00213476 = yrday
fracday
Element set: 912
Inclination: 51
6449 deg
RA of node: 129
6005 deg
Eccentricity:
0006377
Arg of perigee: 146
1240 deg
Mean anomaly: 214
0321 deg
Mean motion: 15
55254785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1540
Checksum: 283
Coasting Arc #14 (Orbit 1555)
---------------------------------------
Vector Time (GMT): 2015/087/23:49:18
294
Vector Time (MET): N/A
Weight (LBS) : 889206
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1477253
49 A = 6782790
62 meter
Y = -6033233
34 meter E =
0018372
Z = 2698665
33 I = 51
95428
XDOT = 5551
521192 Wp = 116
30151
YDOT = -980
751147 meter/sec RA = 123
63525 deg
ZDOT = -5212
108745 TA = 33
30098
MA = 33
18553
Ha = 220
952 n
mi
Hp = 211
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4846632
20 X = 1531499
72
Y = -19794072
65 feet Y = -6016410
13 meter
Z = 8853888
89 Z = 2705973
91
XDOT = 18213
652204 XDOT = 5587
393912
YDOT = -3217
687491 feet/sec YDOT = -918
470397 meter/sec
ZDOT = -17100
094309 ZDOT = -5185
053455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3900112
71 X = -1188754
35
Y = 19987772
54 feet Y = 6092273
07 meter
Z = 8886201
31 Z = 2708514
16
XDOT = -16701
875154 XDOT = -5090
731547
YDOT = 4319
995232 feet/sec YDOT = 1316
734547 meter/sec
ZDOT = -16983
927568 ZDOT = -5176
701123
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 15088
03021606
00016717 00000-0 10270-3 0 9131
2 25544 51
6452 124
4670 0006291 148
9166 211
2360 15
55306962 15566
Satellite: ISS
Catalog Number: 25544
Epoch time: 15088
03021606 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 124
4670 deg
Eccentricity:
0006291
Arg of perigee: 148
9166 deg
Mean anomaly: 211
2360 deg
Mean motion: 15
55306962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1556
Checksum: 291
Coasting Arc #15 (Orbit 1570)
---------------------------------------
Vector Time (GMT): 2015/088/23:49:18
294
Vector Time (MET): N/A
Weight (LBS) : 889206
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2723770
43 A = 6785655
95 meter
Y = 6171091
75 meter E =
0009812
Z = -731148
67 I = 51
97938
XDOT = -4603
351937 Wp = 76
31828
YDOT = -1331
228022 meter/sec RA = 118
67699 deg
ZDOT = 5982
510893 TA = 275
81971
MA = 275
93156
Ha = 220
866 n
mi
Hp = 211
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8936254
68 X = -2789022
97
Y = 20246364
03 feet Y = 6140267
84 meter
Z = -2398781
74 Z = -744539
37
XDOT = -15102
860687 XDOT = -4617
184325
YDOT = -4367
546003 feet/sec YDOT = -1382
782331 meter/sec
ZDOT = 19627
660409 ZDOT = 5960
115403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7650245
36 X = 2331794
78
Y = -20759622
84 feet Y = -6327533
04 meter
Z = -2457206
41 Z = -748956
51
XDOT = 13954
342101 XDOT = 4253
283472
YDOT = 2856
832422 feet/sec YDOT = 870
762522 meter/sec
ZDOT = 19531
842028 ZDOT = 5953
305450
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 15088
99402207
00016717 00000-0 10270-3 0 9147
2 25544 51
6440 119
6532 0006310 153
2938 206
8542 15
55308401 15713
Satellite: ISS
Catalog Number: 25544
Epoch time: 15088
99402207 = yrday
fracday
Element set: 914
Inclination: 51
6440 deg
RA of node: 119
6532 deg
Eccentricity:
0006310
Arg of perigee: 153
2938 deg
Mean anomaly: 206
8542 deg
Mean motion: 15
55308401 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1571
Checksum: 294
Coasting Arc #16 (Orbit 1586)
---------------------------------------
Vector Time (GMT): 2015/089/23:49:18
294
Vector Time (MET): N/A
Weight (LBS) : 889206
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3636541
56 A = 6785040
22 meter
Y = -5544564
85 meter E =
0014913
Z = -1405402
28 I = 51
99125
XDOT = 3364
933386 Wp = 148
99131
YDOT = 3675
639593 meter/sec RA = 113
72500 deg
ZDOT = -5833
975662 TA = 46
26621
MA = 46
14283
Ha = 220
841 n
mi
Hp = 211
603
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11930910
63 X = 3705098
81
Y = -18190829
55 feet Y = -5503515
52 meter
Z = -4610899
87 Z = -1387569
51
XDOT = 11039
807698 XDOT = 3351
920554
YDOT = 12059
185017 feet/sec YDOT = 3713
194945 meter/sec
ZDOT = -19140
340100 ZDOT = -5817
661647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10484055
13 X = -3195540
00
Y = 19079966
10 feet Y = 5815573
67 meter
Z = -4533518
20 Z = -1381816
35
XDOT = -10688
141771 XDOT = -3257
745612
YDOT = -10372
719570 feet/sec YDOT = -3161
604925 meter/sec
ZDOT = -19070
981485 ZDOT = -5812
835157
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 15090
02205988
00016717 00000-0 10270-3 0 9152
2 25544 51
6434 114
5191 0006395 157
6050 202
5384 15
55325437 15879
Satellite: ISS
Catalog Number: 25544
Epoch time: 15090
02205988 = yrday
fracday
Element set: 915
Inclination: 51
6434 deg
RA of node: 114
5191 deg
Eccentricity:
0006395
Arg of perigee: 157
6050 deg
Mean anomaly: 202
5384 deg
Mean motion: 15
55325437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1587
Checksum: 305
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