[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 26th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24756 99 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 453 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
115/06:40:30
000 0
0 0
0 0
0
N/A 0
0 0
0 215
9
000/00:00:00
000 0
0 0
0 213
5
126/05:15:45
661 -1
8 4
9 4
9
N/A -3
1 -0
1 216
2
000/00:11:31
322 -3
4 -0
0 214
5
Coasting Arc #1 (Orbit 1968)
---------------------------------------
Vector Time (GMT): 2015/114/13:09:52
075
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1930027
54 A = 6773462
23 meter
Y = -4240451
84 meter E =
0007573
Z = -4923556
82 I = 51
58118
XDOT = 7293
717625 Wp = 123
74576
YDOT = 704
617939 meter/sec RA = 351
41872 deg
ZDOT = 2250
643866 TA = 168
27142
MA = 168
25377
Ha = 216
080 n
mi
Hp = 213
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6332111
36 X = 2001218
81
Y = -13912243
56 feet Y = -4218471
05 meter
Z = -16153401
65 Z = -4914008
05
XDOT = 23929
519767 XDOT = 7274
363469
YDOT = 2311
738646 feet/sec YDOT = 786
072887 meter/sec
ZDOT = 7384
002185 ZDOT = 2286
028561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6249732
65 X = -1904918
51
Y = -13997674
67 feet Y = -4266491
24 meter
Z = -16111625
79 Z = -4910823
54
XDOT = 16427
514702 XDOT = 5007
106481
YDOT = -16014
353200 feet/sec YDOT = -4881
174855 meter/sec
ZDOT = 7535
550602 ZDOT = 2296
835823
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 15114
56057506
00016717 00000-0 10270-3 0 9003
2 25544 51
6454 351
9277 0005432 261
9188 98
1349 15
56066373 19691
Satellite: ISS
Catalog Number: 25544
Epoch time: 15114
56057506 = yrday
fracday
Element set: 900
Inclination: 51
6454 deg
RA of node: 351
9277 deg
Eccentricity:
0005432
Arg of perigee: 261
9188 deg
Mean anomaly: 98
1349 deg
Mean motion: 15
56066373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1969
Checksum: 328
Coasting Arc #2 (Orbit 1980)
---------------------------------------
Vector Time (GMT): 2015/115/06:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 909283
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3908732
48 A = 6774129
40 meter
Y = 2954391
14 meter E =
0004534
Z = 4678308
06 I = 51
56030
XDOT = -6137
061332 Wp = 157
87588
YDOT = 3626
173174 meter/sec RA = 347
80751 deg
ZDOT = 2832
555049 TA = 263
96887
MA = 264
02054
Ha = 215
862 n
mi
Hp = 213
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12823925
44 X = 3852679
66
Y = 9692884
31 feet Y = 2997787
86 meter
Z = 15348779
73 Z = 4697159
80
XDOT = -20134
715655 XDOT = -6190
913514
YDOT = 11896
893617 feet/sec YDOT = 3557
243519 meter/sec
ZDOT = 9293
159611 ZDOT = 2802
611317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1382417
75 X = 421360
93
Y = 15938155
25 feet Y = 4857949
72 meter
Z = 15429006
37 Z = 4702761
14
XDOT = -21222
685247 XDOT = -6468
674463
YDOT = -7046
377023 feet/sec YDOT = -2147
735717 meter/sec
ZDOT = 9164
080003 ZDOT = 2793
211585
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 15115
33123466
00016717 00000-0 10270-3 0 9019
2 25544 51
6443 348
0750 0005428 263
4148 96
6388 15
56124781 19818
Satellite: ISS
Catalog Number: 25544
Epoch time: 15115
33123466 = yrday
fracday
Element set: 901
Inclination: 51
6443 deg
RA of node: 348
0750 deg
Eccentricity:
0005428
Arg of perigee: 263
4148 deg
Mean anomaly: 96
6388 deg
Mean motion: 15
56124781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1981
Checksum: 311
Coasting Arc #3 (Orbit 1995)
---------------------------------------
Vector Time (GMT): 2015/116/06:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 909283
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1513913
74 A = 6771517
97 meter
Y = -3942405
99 meter E =
0009480
Z = -5301503
19 I = 51
52082
XDOT = 7257
171461 Wp = 87
99524
YDOT = -2454
630034 meter/sec RA = 342
78158 deg
ZDOT = -247
078736 TA = 179
64518
MA = 179
64450
Ha = 215
871 n
mi
Hp = 213
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4966908
58 X = -1443963
45
Y = -12934402
86 feet Y = -3958944
66 meter
Z = -17393383
17 Z = -5308687
46
XDOT = 23809
617653 XDOT = 7285
280569
YDOT = -8053
248143 feet/sec YDOT = -2373
318442 meter/sec
ZDOT = -810
625773 ZDOT = -211
756252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6096541
01 X = 1858225
70
Y = -12399841
29 feet Y = -3779471
63 meter
Z = -17423399
79 Z = -5310652
25
XDOT = 21276
945298 XDOT = 6485
212927
YDOT = 11386
418261 feet/sec YDOT = 3470
580286 meter/sec
ZDOT = -658
728847 ZDOT = -200
780552
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 15116
29453118
00016717 00000-0 10270-3 0 9026
2 25544 51
6444 343
2579 0005398 268
4955 91
5581 15
56138739 19965
Satellite: ISS
Catalog Number: 25544
Epoch time: 15116
29453118 = yrday
fracday
Element set: 902
Inclination: 51
6444 deg
RA of node: 343
2579 deg
Eccentricity:
0005398
Arg of perigee: 268
4955 deg
Mean anomaly: 91
5581 deg
Mean motion: 15
56138739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1996
Checksum: 345
Coasting Arc #4 (Orbit 2011)
---------------------------------------
Vector Time (GMT): 2015/117/06:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 909283
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1049167
56 A = 6773333
31 meter
Y = 4603740
28 meter E =
0003835
Z = 4857109
94 I = 51
49775
XDOT = -7229
617262 Wp = 9
36651
YDOT = 891
893666 meter/sec RA = 337
75314 deg
ZDOT = -2403
036810 TA = 104
25271
MA = 104
21012
Ha = 215
807 n
mi
Hp = 213
414
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3442150
80 X = -1124163
86
Y = 15104134
77 feet Y = 4591588
72 meter
Z = 15935400
06 Z = 4851830
86
XDOT = -23719
216740 XDOT = -7227
380187
YDOT = 2926
160322 feet/sec YDOT = 811
059744 meter/sec
ZDOT = -7883
979034 ZDOT = -2438
151697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13295807
36 X = -4052562
08
Y = 7997143
22 feet Y = 2437529
25 meter
Z = 15911865
74 Z = 4849936
68
XDOT = -18022
125991 XDOT = -5493
144002
YDOT = -13950
513843 feet/sec YDOT = -4252
116619 meter/sec
ZDOT = -8034
669199 ZDOT = -2448
967172
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 15117
32201150
00016717 00000-0 10270-3 0 9039
2 25544 51
6449 338
1209 0005424 272
5613 87
4919 15
56192463 20123
Satellite: ISS
Catalog Number: 25544
Epoch time: 15117
32201150 = yrday
fracday
Element set: 903
Inclination: 51
6449 deg
RA of node: 338
1209 deg
Eccentricity:
0005424
Arg of perigee: 272
5613 deg
Mean anomaly: 87
4919 deg
Mean motion: 15
56192463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2012
Checksum: 286
Coasting Arc #5 (Orbit 2026)
---------------------------------------
Vector Time (GMT): 2015/118/06:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 909283
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3346481
03 A = 6778255
06 meter
Y = -4794102
12 meter E =
0000943
Z = -3428373
67 I = 51
48542
XDOT = 6076
292613 Wp = 315
61756
YDOT = 967
485327 meter/sec RA = 332
73563 deg
ZDOT = 4578
154251 TA = 4
10576
MA = 4
10499
Ha = 215
759 n
mi
Hp = 213
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10979268
48 X = 3416494
99
Y = -15728681
51 feet Y = -4756288
32 meter
Z = -11247945
12 Z = -3411946
66
XDOT = 19935
343217 XDOT = 6042
783232
YDOT = 3174
164458 feet/sec YDOT = 1035
247312 meter/sec
ZDOT = 15020
191111 ZDOT = 4607
590469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18924015
55 X = 5768039
94
Y = -3378954
96 feet Y = -1029905
47 meter
Z = -11176597
27 Z = -3406626
85
XDOT = 11597
171255 XDOT = 3534
817799
YDOT = 14850
345223 feet/sec YDOT = 4526
385224 meter/sec
ZDOT = 15146
168300 ZDOT = 4616
552098
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 15118
28524077
00016717 00000-0 10270-3 0 9042
2 25544 51
6446 333
3038 0005563 276
9594 83
0927 15
56242922 20270
Satellite: ISS
Catalog Number: 25544
Epoch time: 15118
28524077 = yrday
fracday
Element set: 904
Inclination: 51
6446 deg
RA of node: 333
3038 deg
Eccentricity:
0005563
Arg of perigee: 276
9594 deg
Mean anomaly: 83
0927 deg
Mean motion: 15
56242922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2027
Checksum: 316
Coasting Arc #6 (Orbit 2042)
---------------------------------------
Vector Time (GMT): 2015/119/06:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 909283
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5023810
33 A = 6782380
57 meter
Y = 4367959
80 meter E =
0008786
Z = 1270660
60 I = 51
47270
XDOT = -4034
027219 Wp = 133
89104
YDOT = -2939
291070 meter/sec RA = 327
73599 deg
ZDOT = -5826
203891 TA = 32
24265
MA = 32
18896
Ha = 215
763 n
mi
Hp = 213
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16482317
36 X = -5078452
97
Y = 14330576
77 feet Y = 4311474
82 meter
Z = 4168833
99 Z = 1246122
66
XDOT = -13234
997439 XDOT = -3972
557747
YDOT = -9643
343407 feet/sec YDOT = -2984
058872 meter/sec
ZDOT = -19114
842162 ZDOT = -5845
651116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21834174
76 X = -6655056
47
Y = -1083391
86 feet Y = -330217
84 meter
Z = 4062815
21 Z = 1238346
08
XDOT = -2867
440332 XDOT = -873
995813
YDOT = -14445
674464 feet/sec YDOT = -4403
041577 meter/sec
ZDOT = -19197
616421 ZDOT = -5851
433485
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 15119
31265117
00016717 00000-0 10270-3 0 9055
2 25544 51
6453 328
1657 0005553 280
8600 79
1929 15
56297380 20432
Satellite: ISS
Catalog Number: 25544
Epoch time: 15119
31265117 = yrday
fracday
Element set: 905
Inclination: 51
6453 deg
RA of node: 328
1657 deg
Eccentricity:
0005553
Arg of perigee: 280
8600 deg
Mean anomaly: 79
1929 deg
Mean motion: 15
56297380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2043
Checksum: 311
Coasting Arc #7 (Orbit 2058)
---------------------------------------
Vector Time (GMT): 2015/120/06:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 909283
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5820528
80 A = 6782278
18 meter
Y = -3270236
42 meter E =
0010733
Z = 1155383
34 I = 51
44615
XDOT = 1491
227734 Wp = 34
80926
YDOT = 4729
611082 meter/sec RA = 322
74314 deg
ZDOT = 5856
181159 TA = 337
78547
MA = 337
83194
Ha = 215
782 n
mi
Hp = 213
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19096223
09 X = 5851052
27
Y = -10729122
13 feet Y = -3204976
73 meter
Z = 3790627
77 Z = 1183733
06
XDOT = 4892
479441 XDOT = 1409
781756
YDOT = 15517
096726 feet/sec YDOT = 4745
831941 meter/sec
ZDOT = 19213
192780 ZDOT = 5863
227225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21281660
44 X = 6486650
10
Y = 5092141
04 feet Y = 1552084
59 meter
Z = 3912759
29 Z = 1192609
03
XDOT = -6676
757664 XDOT = -2035
075736
YDOT = 13073
960688 feet/sec YDOT = 3984
943218 meter/sec
ZDOT = 19242
469890 ZDOT = 5865
104822
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 15120
34002516
00016717 00000-0 10270-3 0 9063
2 25544 51
6448 323
0270 0005672 285
6641 74
3886 15
56349848 20594
Satellite: ISS
Catalog Number: 25544
Epoch time: 15120
34002516 = yrday
fracday
Element set: 906
Inclination: 51
6448 deg
RA of node: 323
0270 deg
Eccentricity:
0005672
Arg of perigee: 285
6641 deg
Mean anomaly: 74
3886 deg
Mean motion: 15
56349848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2059
Checksum: 311
Coasting Arc #8 (Orbit 2073)
---------------------------------------
Vector Time (GMT): 2015/121/06:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 909283
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5681960
74 A = 6777765
00 meter
Y = 1538973
78 meter E =
0001965
Z = -3360809
92 I = 51
40784
XDOT = 1114
311244 Wp = 343
25642
YDOT = -6007
926848 meter/sec RA = 317
73949 deg
ZDOT = -4632
524819 TA = 236
11463
MA = 236
13333
Ha = 215
911 n
mi
Hp = 213
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18641603
46 X = -5682421
79
Y = 5049126
56 feet Y = 1475431
61 meter
Z = -11026279
28 Z = -3388413
44
XDOT = 3655
876784 XDOT = 1203
913933
YDOT = -19711
046090 feet/sec YDOT = -5994
965157 meter/sec
ZDOT = -15198
572241 ZDOT = -4626
893641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17204537
85 X = -5243943
14
Y = -8624249
03 feet Y = -2628671
10 meter
Z = -11144868
76 Z = -3396956
00
XDOT = 15313
827122 XDOT = 4667
654507
YDOT = -10931
023787 feet/sec YDOT = -3331
776050 meter/sec
ZDOT = -15173
276700 ZDOT = -4624
814738
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 15121
30315475
00016717 00000-0 10270-3 0 9072
2 25544 51
6455 318
2096 0005734 289
7630 70
2906 15
56422236 20744
Satellite: ISS
Catalog Number: 25544
Epoch time: 15121
30315475 = yrday
fracday
Element set: 907
Inclination: 51
6455 deg
RA of node: 318
2096 deg
Eccentricity:
0005734
Arg of perigee: 289
7630 deg
Mean anomaly: 70
2906 deg
Mean motion: 15
56422236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2074
Checksum: 300
Coasting Arc #9 (Orbit 2089)
---------------------------------------
Vector Time (GMT): 2015/122/06:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 909283
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4691167
45 A = 6772412
25 meter
Y = 626187
08 meter E =
0001379
Z = 4844210
67 I = 51
36702
XDOT = -3351
339251 Wp = 156
18052
YDOT = 6467
358766 meter/sec RA = 312
71288 deg
ZDOT = 2407
977498 TA = 270
12057
MA = 270
13638
Ha = 215
833 n
mi
Hp = 213
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15390969
33 X = 4660284
80
Y = 2054419
54 feet Y = 678474
32 meter
Z = 15893079
61 Z = 4866924
84
XDOT = -10995
207517 XDOT = -3435
106994
YDOT = 21218
368654 feet/sec YDOT = 6429
413636 meter/sec
ZDOT = 7900
188642 ZDOT = 2391
493268
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10221859
05 X = 3115622
64
Y = 11554942
13 feet Y = 3521946
36 meter
Z = 15990292
87 Z = 4873841
27
XDOT = -21390
435949 XDOT = -6519
804877
YDOT = 8082
778325 feet/sec YDOT = 2463
630833 meter/sec
ZDOT = 7828
302020 ZDOT = 2386
066456
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 15122
33045824
00016717 00000-0 10270-3 0 9085
2 25544 51
6450 313
0702 0005806 293
1692 66
8850 15
56473689 20908
Satellite: ISS
Catalog Number: 25544
Epoch time: 15122
33045824 = yrday
fracday
Element set: 908
Inclination: 51
6450 deg
RA of node: 313
0702 deg
Eccentricity:
0005806
Arg of perigee: 293
1692 deg
Mean anomaly: 66
8850 deg
Mean motion: 15
56473689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2090
Checksum: 307
Coasting Arc #10 (Orbit 2104)
---------------------------------------
Vector Time (GMT): 2015/123/06:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 909283
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3099722
89 A = 6770413
35 meter
Y = -2900296
11 meter E =
0009777
Z = -5282514
37 I = 51
34050
XDOT = 4901
741844 Wp = 78
03541
YDOT = -5882
945443 meter/sec RA = 307
66874 deg
ZDOT = 356
214656 TA = 195
36135
MA = 195
39104
Ha = 216
039 n
mi
Hp = 212
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10169694
53 X = -3041399
69
Y = -9515407
17 feet Y = -2934633
28 meter
Z = -17331083
88 Z = -5297430
79
XDOT = 16081
830197 XDOT = 4965
431635
YDOT = -19301
002110 feet/sec YDOT = -5827
774841 meter/sec
ZDOT = 1168
683255 ZDOT = 380
181743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1622353
35 X = -494493
30
Y = -13752580
21 feet Y = -4191786
45 meter
Z = -17394442
68 Z = -5301826
13
XDOT = 23705
974611 XDOT = 7225
581062
YDOT = -4395
481562 feet/sec YDOT = -1339
742780 meter/sec
ZDOT = 1272
515593 ZDOT = 387
862753
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 15123
29352250
00016717 00000-0 10270-3 0 9096
2 25544 51
6455 308
2519 0005912 297
8228 62
2327 15
56531203 21052
Satellite: ISS
Catalog Number: 25544
Epoch time: 15123
29352250 = yrday
fracday
Element set: 909
Inclination: 51
6455 deg
RA of node: 308
2519 deg
Eccentricity:
0005912
Arg of perigee: 297
8228 deg
Mean anomaly: 62
2327 deg
Mean motion: 15
56531203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2105
Checksum: 292
Coasting Arc #11 (Orbit 2120)
---------------------------------------
Vector Time (GMT): 2015/124/06:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 909283
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1190372
99 A = 6773375
20 meter
Y = 4882440
14 meter E =
0007255
Z = 4542292
36 I = 51
33201
XDOT = -5618
459041 Wp = 22
98975
YDOT = 4228
364175 meter/sec RA = 302
62557 deg
ZDOT = -3064
383272 TA = 97
82664
MA = 97
74427
Ha = 216
206 n
mi
Hp = 212
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3905423
19 X = 1113622
66
Y = 16018504
40 feet Y = 4895322
58 meter
Z = 14902534
00 Z = 4547888
62
XDOT = -18433
264569 XDOT = -5650
438080
YDOT = 13872
585876 feet/sec YDOT = 4165
356058 meter/sec
ZDOT = -10053
750891 ZDOT = -3091
754976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7087398
52 X = -2160239
07
Y = 14863589
48 feet Y = 4530422
07 meter
Z = 14925576
13 Z = 4549315
61
XDOT = -21922
950936 XDOT = -6682
115445
YDOT = -212
194275 feet/sec YDOT = -64
676815 meter/sec
ZDOT = -10171
849023 ZDOT = -3100
379582
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 15124
32075527
00016717 00000-0 10270-3 0 9102
2 25544 51
6452 303
1124 0006075 302
3250 57
7316 15
56592259 21216
Satellite: ISS
Catalog Number: 25544
Epoch time: 15124
32075527 = yrday
fracday
Element set: 910
Inclination: 51
6452 deg
RA of node: 303
1124 deg
Eccentricity:
0006075
Arg of perigee: 302
3250 deg
Mean anomaly: 57
7316 deg
Mean motion: 15
56592259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2121
Checksum: 272
Coasting Arc #12 (Orbit 2135)
---------------------------------------
Vector Time (GMT): 2015/125/06:40:30
000
Vector Time (MET): N/A
Weight (LBS) : 909283
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 693529
36 A = 6778757
05 meter
Y = -6136933
56 meter E =
0006101
Z = -2785134
71 I = 51
33488
XDOT = 5482
897043 Wp = 351
14379
YDOT = -1690
183674 meter/sec RA = 297
59923 deg
ZDOT = 5093
985100 TA = 337
08726
MA = 337
11447
Ha = 216
288 n
mi
Hp = 212
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2275358
80 X = 775631
90
Y = -20134296
45 feet Y = -6128718
97 meter
Z = -9137581
07 Z = -2781566
24
XDOT = 17988
507358 XDOT = 5476
644370
YDOT = -5545
222028 feet/sec YDOT = -1628
905343 meter/sec
ZDOT = 16712
549541 ZDOT = 5120
605321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14206909
55 X = 4330266
03
Y = -14457922
02 feet Y = -4406774
63 meter
Z = -9121115
67 Z = -2780116
06
XDOT = 16462
909986 XDOT = 5017
894964
YDOT = 5570
609598 feet/sec YDOT = 1697
921805 meter/sec
ZDOT = 16826
939065 ZDOT = 5128
851027
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 15125
28375295
00016717 00000-0 10270-3 0 9114
2 25544 51
6460 298
2932 0006168 305
8682 54
1899 15
56636647 21369
Satellite: ISS
Catalog Number: 25544
Epoch time: 15125
28375295 = yrday
fracday
Element set: 911
Inclination: 51
6460 deg
RA of node: 298
2932 deg
Eccentricity:
0006168
Arg of perigee: 305
8682 deg
Mean anomaly: 54
1899 deg
Mean motion: 15
56636647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2136
Checksum: 337
Coasting Arc #13 (Orbit 2150)
---------------------------------------
Vector Time (GMT): 2015/126/05:21:31
322
Vector Time (MET): N/A
Weight (LBS) : 908777
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4670530
14 A = 6777939
14 meter
Y = 2911500
77 meter E =
0002478
Z = -3957915
04 I = 51
30986
XDOT = -698
080807 Wp =
71805
YDOT = -6521
591400 meter/sec RA = 292
89643 deg
ZDOT = -3971
202803 TA = 227
69949
MA = 227
72049
Ha = 216
164 n
mi
Hp = 214
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15323261
61 X = -4683513
66
Y = 9552167
88 feet Y = 2859199
35 meter
Z = -12985285
55 Z = -3980635
48
XDOT = -2290
291361 XDOT = -605
811939
YDOT = -21396
297245 feet/sec YDOT = -6528
881795 meter/sec
ZDOT = -13028
880588 ZDOT = -3974
370052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16350016
40 X = -4983485
00
Y = -7494717
53 feet Y = -2284389
90 meter
Z = -13083198
05 Z = -3987758
77
XDOT = 16125
930189 XDOT = 4915
183522
YDOT = -12400
194291 feet/sec YDOT = -3779
579220 meter/sec
ZDOT = -13041
208583 ZDOT = -3974
960376
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 15126
24673201
00016717 00000-0 10270-3 0 9120
2 25544 51
6456 293
4744 0006547 273
6836 86
3568 15
55724847 21512
Satellite: ISS
Catalog Number: 25544
Epoch time: 15126
24673201 = yrday
fracday
Element set: 912
Inclination: 51
6456 deg
RA of node: 293
4744 deg
Eccentricity:
0006547
Arg of perigee: 273
6836 deg
Mean anomaly: 86
3568 deg
Mean motion: 15
55724847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2151
Checksum: 326
Coasting Arc #14 (Orbit 2166)
---------------------------------------
Vector Time (GMT): 2015/127/05:21:31
322
Vector Time (MET): N/A
Weight (LBS) : 908777
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4467315
02 A = 6773590
08 meter
Y = -662137
63 meter E =
0003094
Z = 5050868
65 I = 51
28414
XDOT = -900
373005 Wp = 224
88373
YDOT = 7408
408691 meter/sec RA = 287
86438 deg
ZDOT = 1766
052918 TA = 207
94216
MA = 207
95877
Ha = 216
081 n
mi
Hp = 214
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14656545
34 X = 4449851
54
Y = -2172367
57 feet Y = -612279
02 meter
Z = 16571091
37 Z = 5072527
92
XDOT = -2953
979675 XDOT = -991
727644
YDOT = 24305
802792 feet/sec YDOT = 7397
829276 meter/sec
ZDOT = 5794
136869 ZDOT = 1761
457371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9990297
30 X = 3045042
62
Y = 10799936
72 feet Y = 3291820
71 meter
Z = 16664030
07 Z = 5079196
37
XDOT = -20980
245525 XDOT = -6394
778836
YDOT = 10492
255129 feet/sec YDOT = 3198
039363 meter/sec
ZDOT = 5773
039000 ZDOT = 1759
622287
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 15127
27449901
00016717 00000-0 10270-3 0 9133
2 25544 51
6455 288
3382 0006610 277
5841 82
4562 15
55772962 21671
Satellite: ISS
Catalog Number: 25544
Epoch time: 15127
27449901 = yrday
fracday
Element set: 913
Inclination: 51
6455 deg
RA of node: 288
3382 deg
Eccentricity:
0006610
Arg of perigee: 277
5841 deg
Mean anomaly: 82
4562 deg
Mean motion: 15
55772962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2167
Checksum: 328
Coasting Arc #15 (Orbit 2181)
---------------------------------------
Vector Time (GMT): 2015/128/05:21:31
322
Vector Time (MET): N/A
Weight (LBS) : 908777
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3905830
07 A = 6772600
58 meter
Y = -1786359
24 meter E =
0007946
Z = -5243466
26 I = 51
27304
XDOT = 2290
998991 Wp = 90
62203
YDOT = -7274
369411 meter/sec RA = 282
82147 deg
ZDOT = 772
632673 TA = 186
79580
MA = 186
80658
Ha = 216
358 n
mi
Hp = 214
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12814403
12 X = -3860093
16
Y = -5860758
66 feet Y = -1829780
85 meter
Z = -17202973
28 Z = -5262329
25
XDOT = 7516
400888 XDOT = 2368
419240
YDOT = -23866
041374 feet/sec YDOT = -7248
317112 meter/sec
ZDOT = 2534
884097 ZDOT = 783
949809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2549980
10 X = -777233
93
Y = -13757868
48 feet Y = -4193398
31 meter
Z = -17283470
88 Z = -5268001
92
XDOT = 22812
550395 XDOT = 6953
265361
YDOT = -7471
536038 feet/sec YDOT = -2277
324184 meter/sec
ZDOT = 2584
752024 ZDOT = 787
832417
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 15128
23799833
00016717 00000-0 10270-3 0 9143
2 25544 51
6460 283
5231 0006706 282
4752 77
5651 15
55831596 21829
Satellite: ISS
Catalog Number: 25544
Epoch time: 15128
23799833 = yrday
fracday
Element set: 914
Inclination: 51
6460 deg
RA of node: 283
5231 deg
Eccentricity:
0006706
Arg of perigee: 282
4752 deg
Mean anomaly: 77
5651 deg
Mean motion: 15
55831596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2182
Checksum: 326
Coasting Arc #16 (Orbit 2197)
---------------------------------------
Vector Time (GMT): 2015/129/05:21:31
322
Vector Time (MET): N/A
Weight (LBS) : 908777
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3061299
52 A = 6775623
40 meter
Y = 4070182
68 meter E =
0005683
Z = 4470283
34 I = 51
27749
XDOT = -3413
956872 Wp = 18
60330
YDOT = 6080
320383 meter/sec RA = 277
78249 deg
ZDOT = -3191
781759 TA = 103
66769
MA = 103
60440
Ha = 216
649 n
mi
Hp = 214
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10043633
61 X = 2993843
08
Y = 13353617
72 feet Y = 4104038
80 meter
Z = 14666283
91 Z = 4484990
98
XDOT = -11200
645906 XDOT = -3466
190102
YDOT = 19948
557687 feet/sec YDOT = 6041
851350 meter/sec
ZDOT = -10471
724931 ZDOT = -3208
492906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4884735
21 X = -1488867
29
Y = 15921765
85 feet Y = 4852954
23 meter
Z = 14728553
90 Z = 4489263
23
XDOT = -21508
900559 XDOT = -6555
912890
YDOT = 3174
807889 feet/sec YDOT = 967
681445 meter/sec
ZDOT = -10544
476648 ZDOT = -3213
956482
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 15129
26569583
00016717 00000-0 10270-3 0 9155
2 25544 51
6458 278
3871 0006851 287
5406 72
4999 15
55899532 21981
Satellite: ISS
Catalog Number: 25544
Epoch time: 15129
26569583 = yrday
fracday
Element set: 915
Inclination: 51
6458 deg
RA of node: 278
3871 deg
Eccentricity:
0006851
Arg of perigee: 287
5406 deg
Mean anomaly: 72
4999 deg
Mean motion: 15
55899532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2198
Checksum: 370
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