[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 29th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22604 21 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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 2237)
---------------------------------------
Vector Time (GMT): 2014/239/09:14:47
654
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3900425
41 A = 6796997
19 meter
Y = 4524544
59 meter E =
0015859
Z = 3225677
50 I = 51
99624
XDOT = -2359
597224 Wp = 78
83735
YDOT = -5479
462322 meter/sec RA = 105
80633 deg
ZDOT = 4815
650273 TA = 318
24684
MA = 318
36775
Ha = 228
706 n
mi
Hp = 220
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12796671
29 X = -3966399
16
Y = 14844306
38 feet Y = 4480558
94 meter
Z = 10582931
43 Z = 3206569
29
XDOT = -7741
460710 XDOT = -2321
541886
YDOT = -17977
238590 feet/sec YDOT = -5505
635609 meter/sec
ZDOT = 15799
377536 ZDOT = 4804
280775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18733025
77 X = 5709826
25
Y = 5908598
19 feet Y = 1800940
73 meter
Z = 10500898
94 Z = 3200674
00
XDOT = -12952
063389 XDOT = -3947
788921
YDOT = 12969
503205 feet/sec YDOT = 3953
104577 meter/sec
ZDOT = 15751
867957 ZDOT = 4801
169353
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 14239
44313729
00016717 00000-0 10270-3 0 9009
2 25544 51
6450 106
4047 0003599 50
7667 309
3803 15
50012572 22381
Satellite: ISS
Catalog Number: 25544
Epoch time: 14239
44313729 = yrday
fracday
Element set: 900
Inclination: 51
6450 deg
RA of node: 106
4047 deg
Eccentricity:
0003599
Arg of perigee: 50
7667 deg
Mean anomaly: 309
3803 deg
Mean motion: 15
50012572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2238
Checksum: 294
Coasting Arc #2 (Orbit 2252)
---------------------------------------
Vector Time (GMT): 2014/240/09:14:47
654
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3667337
62 A = 6796053
42 meter
Y = -4518978
54 meter E =
0008180
Z = -3518524
53 I = 52
00172
XDOT = 2543
779302 Wp = 72
86841
YDOT = 5602
682980 meter/sec RA = 100
87603 deg
ZDOT = -4550
765109 TA = 148
16796
MA = 148
11849
Ha = 228
555 n
mi
Hp = 220
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12031947
56 X = 3734689
05
Y = -14826045
08 feet Y = -4477591
78 meter
Z = -11543715
65 Z = -3500545
19
XDOT = 8345
732619 XDOT = 2503
045757
YDOT = 18381
505841 feet/sec YDOT = 5630
900945 meter/sec
ZDOT = -14930
331721 ZDOT = -4538
507384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18502071
86 X = -5639431
50
Y = -4902032
36 feet Y = -1494139
46 meter
Z = -11466479
89 Z = -3494983
07
XDOT = 12897
907854 XDOT = 3931
282314
YDOT = -13926
746122 feet/sec YDOT = -4244
872218 meter/sec
ZDOT = -14879
068927 ZDOT = -4535
140209
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 14240
41021608
00016717 00000-0 10270-3 0 9011
2 25544 51
6456 101
6130 0003510 52
5600 307
5869 15
50053528 22532
Satellite: ISS
Catalog Number: 25544
Epoch time: 14240
41021608 = yrday
fracday
Element set: 901
Inclination: 51
6456 deg
RA of node: 101
6130 deg
Eccentricity:
0003510
Arg of perigee: 52
5600 deg
Mean anomaly: 307
5869 deg
Mean motion: 15
50053528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2253
Checksum: 257
Coasting Arc #3 (Orbit 2268)
---------------------------------------
Vector Time (GMT): 2014/241/09:14:47
654
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3425622
53 A = 6795234
16 meter
Y = 4489502
85 meter E =
0014527
Z = 3766329
52 I = 52
00382
XDOT = -2770
750045 Wp = 86
93906
YDOT = -5721
432790 meter/sec RA = 95
94535 deg
ZDOT = 4286
436389 TA = 317
81690
MA = 317
92859
Ha = 228
660 n
mi
Hp = 219
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11238919
06 X = -3493866
14
Y = 14729340
05 feet Y = 4450814
13 meter
Z = 12356724
14 Z = 3749522
18
XDOT = -9090
387287 XDOT = -2727
387796
YDOT = -18771
104953 feet/sec YDOT = -5752
174229 meter/sec
ZDOT = 14063
111512 ZDOT = 4273
082417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18158715
55 X = 5534776
50
Y = 3912568
22 feet Y = 1192550
79 meter
Z = 12284471
94 Z = 3744307
05
XDOT = -12740
662768 XDOT = -3883
354012
YDOT = 15012
390946 feet/sec YDOT = 4575
776760 meter/sec
ZDOT = 14007
211435 ZDOT = 4269
398045
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 14241
44174958
00016717 00000-0 10270-3 0 9023
2 25544 51
6453 96
5017 0003573 56
0368 304
1122 15
50069007 22695
Satellite: ISS
Catalog Number: 25544
Epoch time: 14241
44174958 = yrday
fracday
Element set: 902
Inclination: 51
6453 deg
RA of node: 96
5017 deg
Eccentricity:
0003573
Arg of perigee: 56
0368 deg
Mean anomaly: 304
1122 deg
Mean motion: 15
50069007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2269
Checksum: 292
Coasting Arc #4 (Orbit 2283)
---------------------------------------
Vector Time (GMT): 2014/242/09:14:47
654
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3232970
57 A = 6794243
78 meter
Y = -4415377
28 meter E =
0010291
Z = -4037859
45 I = 52
00374
XDOT = 2996
115701 Wp = 67
23932
YDOT = 5817
410344 meter/sec RA = 91
01438 deg
ZDOT = -3966
603434 TA = 161
64738
MA = 161
61022
Ha = 228
467 n
mi
Hp = 219
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10606858
83 X = 3301718
67
Y = -14486145
92 feet Y = -4378840
08 meter
Z = -13247570
37 Z = -4021986
76
XDOT = 9829
775923 XDOT = 2950
109871
YDOT = 19085
991942 feet/sec YDOT = 5850
657252 meter/sec
ZDOT = -13013
790793 ZDOT = -3952
161013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17727353
68 X = -5403297
40
Y = -3146271
71 feet Y = -958983
62 meter
Z = -13179298
34 Z = -4017050
13
XDOT = 12470
484302 XDOT = 3801
003615
YDOT = -16061
923989 feet/sec YDOT = -4895
674432 meter/sec
ZDOT = -12953
284381 ZDOT = -3948
161079
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 14242
40879325
00016717 00000-0 10270-3 0 9031
2 25544 51
6458 91
7099 0003423 56
8925 303
2554 15
50109103 22846
Satellite: ISS
Catalog Number: 25544
Epoch time: 14242
40879325 = yrday
fracday
Element set: 903
Inclination: 51
6458 deg
RA of node: 91
7099 deg
Eccentricity:
0003423
Arg of perigee: 56
8925 deg
Mean anomaly: 303
2554 deg
Mean motion: 15
50109103 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2284
Checksum: 301
Coasting Arc #5 (Orbit 2299)
---------------------------------------
Vector Time (GMT): 2014/243/09:14:47
654
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3041808
26 A = 6793388
94 meter
Y = 4318066
85 meter E =
0012746
Z = 4261935
03 I = 52
00076
XDOT = -3259
520705 Wp = 94
62085
YDOT = -5904
967820 meter/sec RA = 86
08269 deg
ZDOT = 3646
009046 TA = 318
21304
MA = 318
31030
Ha = 228
597 n
mi
Hp = 219
831
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9979685
89 X = -3110570
93
Y = 14166885
99 feet Y = 4283667
24 meter
Z = 13982726
46 Z = 4246990
98
XDOT = -10693
965567 XDOT = -3210
958893
YDOT = -19373
254002 feet/sec YDOT = -5941
146077 meter/sec
ZDOT = 11961
971935 ZDOT = 3630
293159
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17209366
96 X = 5245415
05
Y = 2434524
68 feet Y = 742043
12 meter
Z = 13918412
52 Z = 4242332
13
XDOT = -12083
314130 XDOT = -3682
994147
YDOT = 17209
305450 feet/sec YDOT = 5245
396301 meter/sec
ZDOT = 11896
071200 ZDOT = 3625
922502
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 14243
44028950
00016717 00000-0 10270-3 0 9047
2 25544 51
6459 86
5983 0003530 60
5850 299
5653 15
50123991 23006
Satellite: ISS
Catalog Number: 25544
Epoch time: 14243
44028950 = yrday
fracday
Element set: 904
Inclination: 51
6459 deg
RA of node: 86
5983 deg
Eccentricity:
0003530
Arg of perigee: 60
5850 deg
Mean anomaly: 299
5653 deg
Mean motion: 15
50123991 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2300
Checksum: 307
Coasting Arc #6 (Orbit 2314)
---------------------------------------
Vector Time (GMT): 2014/244/09:14:47
654
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2908006
78 A = 6792412
31 meter
Y = -4187202
50 meter E =
0012700
Z = -4501461
97 I = 51
99497
XDOT = 3515
031684 Wp = 67
17066
YDOT = 5956
071926 meter/sec RA = 81
15023 deg
ZDOT = -3272
062770 TA = 169
97052
MA = 169
94515
Ha = 228
370 n
mi
Hp = 219
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9540704
67 X = 2976479
59
Y = -13737541
03 feet Y = -4154300
73 meter
Z = -14768576
00 Z = -4487168
69
XDOT = 11532
256182 XDOT = 3464
062911
YDOT = 19540
918391 feet/sec YDOT = 5995
094089 meter/sec
ZDOT = -10735
114075 ZDOT = -3255
111413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16664870
41 X = -5079452
50
Y = -1959818
17 feet Y = -597352
58 meter
Z = -14707043
32 Z = -4482706
80
XDOT = 11552
037609 XDOT = 3521
061063
YDOT = -18267
871020 feet/sec YDOT = -5568
047087 meter/sec
ZDOT = -10663
974482 ZDOT = -3250
379422
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 14244
40729773
00016717 00000-0 10270-3 0 9056
2 25544 51
6460 81
8063 0003340 60
8984 299
2501 15
50167292 23152
Satellite: ISS
Catalog Number: 25544
Epoch time: 14244
40729773 = yrday
fracday
Element set: 905
Inclination: 51
6460 deg
RA of node: 81
8063 deg
Eccentricity:
0003340
Arg of perigee: 60
8984 deg
Mean anomaly: 299
2501 deg
Mean motion: 15
50167292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2315
Checksum: 302
Coasting Arc #7 (Orbit 2330)
---------------------------------------
Vector Time (GMT): 2014/245/09:14:47
654
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2785186
84 A = 6791606
57 meter
Y = 4036063
96 meter E =
0010621
Z = 4690779
39 I = 51
98690
XDOT = -3801
023007 Wp = 100
99502
YDOT = -5996
421769 meter/sec RA = 76
21691 deg
ZDOT = 2895
069809 TA = 320
32942
MA = 320
40707
Ha = 228
521 n
mi
Hp = 219
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9137752
09 X = -2852898
31
Y = 13241679
64 feet Y = 4004539
84 meter
Z = 15389696
16 Z = 4677084
69
XDOT = -12470
547924 XDOT = -3747
750441
YDOT = -19673
299767 feet/sec YDOT = -6038
629251 meter/sec
ZDOT = 9498
260529 ZDOT = 2876
734700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16068430
63 X = 4897657
66
Y = 1567703
00 feet Y = 477835
88 meter
Z = 15330726
83 Z = 4672805
54
XDOT = -10903
693265 XDOT = -3323
445707
YDOT = 19385
842870 feet/sec YDOT = 5908
804907 meter/sec
ZDOT = 9421
248077 ZDOT = 2871
596414
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 14245
43875631
00016717 00000-0 10270-3 0 9066
2 25544 51
6462 76
6948 0003470 64
8009 295
3501 15
50177493 23313
Satellite: ISS
Catalog Number: 25544
Epoch time: 14245
43875631 = yrday
fracday
Element set: 906
Inclination: 51
6462 deg
RA of node: 76
6948 deg
Eccentricity:
0003470
Arg of perigee: 64
8009 deg
Mean anomaly: 295
3501 deg
Mean motion: 15
50177493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2331
Checksum: 313
Coasting Arc #8 (Orbit 2345)
---------------------------------------
Vector Time (GMT): 2014/246/09:14:47
654
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2724989
91 A = 6790720
59 meter
Y = -3865795
53 meter E =
0014995
Z = -4886903
10 I = 51
97545
XDOT = 4068
696500 Wp = 70
74061
YDOT = 5988
889452 meter/sec RA = 71
28195 deg
ZDOT = -2470
149565 TA = 175
06844
MA = 175
05366
Ha = 228
277 n
mi
Hp = 219
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8940255
60 X = 2791754
51
Y = -12683056
22 feet Y = -3834949
85 meter
Z = -16033146
65 Z = -4873503
20
XDOT = 13348
741797 XDOT = 4013
424107
YDOT = 19648
587441 feet/sec YDOT = 6034
079090 meter/sec
ZDOT = -8104
165240 ZDOT = -2450
519010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15513164
27 X = -4728412
47
Y = -1405890
02 feet Y = -428515
28 meter
Z = -15975452
55 Z = -4869317
94
XDOT = 10100
353341 XDOT = 3078
587698
YDOT = -20351
033595 feet/sec YDOT = -6202
995040 meter/sec
ZDOT = -8021
645683 ZDOT = -2444
997604
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 14246
40572851
00016717 00000-0 10270-3 0 9073
2 25544 51
6456 71
9023 0003276 65
2713 294
8778 15
50227074 23466
Satellite: ISS
Catalog Number: 25544
Epoch time: 14246
40572851 = yrday
fracday
Element set: 907
Inclination: 51
6456 deg
RA of node: 71
9023 deg
Eccentricity:
0003276
Arg of perigee: 65
2713 deg
Mean anomaly: 294
8778 deg
Mean motion: 15
50227074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2346
Checksum: 313
Coasting Arc #9 (Orbit 2361)
---------------------------------------
Vector Time (GMT): 2014/247/09:14:47
654
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2683700
92 A = 6790056
79 meter
Y = 3680122
58 meter E =
0008362
Z = 5029443
96 I = 51
96250
XDOT = -4356
714331 Wp = 104
11635
YDOT = -5970
445144 meter/sec RA = 66
34612 deg
ZDOT = 2039
115904 TA = 326
12171
MA = 326
17509
Ha = 228
433 n
mi
Hp = 219
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8804793
03 X = -2749084
67
Y = 12073892
97 feet Y = 3649746
35 meter
Z = 16500800
39 Z = 5016248
04
XDOT = -14293
682189 XDOT = -4299
532931
YDOT = -19588
074618 feet/sec YDOT = -6018
844925 meter/sec
ZDOT = 6690
012810 ZDOT = 2018
090926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14945694
47 X = 4555447
68
Y = 1341931
23 feet Y = 409020
64 meter
Z = 16443999
58 Z = 5012131
07
XDOT = -9196
273086 XDOT = -2803
024036
YDOT = 21333
275100 feet/sec YDOT = 6502
382251 meter/sec
ZDOT = 6601
560777 ZDOT = 2012
155725
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 14247
43714841
00016717 00000-0 10270-3 0 9085
2 25544 51
6457 66
7906 0003387 69
2391 290
9122 15
50231205 23627
Satellite: ISS
Catalog Number: 25544
Epoch time: 14247
43714841 = yrday
fracday
Element set: 908
Inclination: 51
6457 deg
RA of node: 66
7906 deg
Eccentricity:
0003387
Arg of perigee: 69
2391 deg
Mean anomaly: 290
9122 deg
Mean motion: 15
50231205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2362
Checksum: 306
Coasting Arc #10 (Orbit 2376)
---------------------------------------
Vector Time (GMT): 2014/248/09:14:47
654
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2706116
76 A = 6789353
64 meter
Y = -3492156
59 meter E =
0016815
Z = -5170317
44 I = 51
94596
XDOT = 4612
847215 Wp = 76
58501
YDOT = 5896
819207 meter/sec RA = 61
40767 deg
ZDOT = -1569
010758 TA = 178
31875
MA = 178
31309
Ha = 228
190 n
mi
Hp = 219
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8878335
84 X = 2770081
20
Y = -11457206
67 feet Y = -3461537
70 meter
Z = -16962983
74 Z = -5157016
09
XDOT = 15134
013173 XDOT = 4554
186453
YDOT = 19346
519709 feet/sec YDOT = 5948
074964 meter/sec
ZDOT = -5147
673091 ZDOT = -1546
745267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14486004
95 X = -4415334
31
Y = -1478553
45 feet Y = -450663
09 meter
Z = -16905762
03 Z = -5152876
27
XDOT = 8151
598918 XDOT = 2484
607350
YDOT = -22096
731058 feet/sec YDOT = -6735
083627 meter/sec
ZDOT = -5053
932264 ZDOT = -1540
438554
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 14248
40408368
00016717 00000-0 10270-3 0 9098
2 25544 51
6444 61
9973 0003231 70
4678 289
6822 15
50286890 23772
Satellite: ISS
Catalog Number: 25544
Epoch time: 14248
40408368 = yrday
fracday
Element set: 909
Inclination: 51
6444 deg
RA of node: 61
9973 deg
Eccentricity:
0003231
Arg of perigee: 70
4678 deg
Mean anomaly: 289
6822 deg
Mean motion: 15
50286890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2377
Checksum: 334
Coasting Arc #11 (Orbit 2392)
---------------------------------------
Vector Time (GMT): 2014/249/09:14:47
654
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2752845
51 A = 6788921
89 meter
Y = 3295097
98 meter E =
0006397
Z = 5253409
37 I = 51
92891
XDOT = -4877
014733 Wp = 99
80864
YDOT = -5814
793938 meter/sec RA = 56
46848 deg
ZDOT = 1089
416951 TA = 339
78037
MA = 339
80570
Ha = 228
334 n
mi
Hp = 219
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9031645
37 X = -2815006
50
Y = 10810688
90 feet Y = 3263966
73 meter
Z = 17235595
05 Z = 5239885
37
XDOT = -16000
704504 XDOT = -4816
921864
YDOT = -19077
407933 feet/sec YDOT = -5868
995786 meter/sec
ZDOT = 3574
202596 ZDOT = 1065
871832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14053710
03 X = 4283570
82
Y = 1713341
68 feet Y = 522226
54 meter
Z = 17177457
44 Z = 5235689
03
XDOT = -7040
207426 XDOT = -2145
855223
YDOT = 22835
824023 feet/sec YDOT = 6960
359162 meter/sec
ZDOT = 3475
004382 ZDOT = 1059
181335
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 14249
43546350
00016717 00000-0 10270-3 0 9108
2 25544 51
6444 56
8851 0003289 74
2845 285
8668 15
50287226 23939
Satellite: ISS
Catalog Number: 25544
Epoch time: 14249
43546350 = yrday
fracday
Element set: 910
Inclination: 51
6444 deg
RA of node: 56
8851 deg
Eccentricity:
0003289
Arg of perigee: 74
2845 deg
Mean anomaly: 285
8668 deg
Mean motion: 15
50287226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2393
Checksum: 331
Coasting Arc #12 (Orbit 2407)
---------------------------------------
Vector Time (GMT): 2014/250/09:14:47
654
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2859235
86 A = 6788495
01 meter
Y = -3113714
09 meter E =
0017860
Z = -5327097
09 I = 51
90855
XDOT = 5094
343792 Wp = 83
78276
YDOT = 5675
864768 meter/sec RA = 51
52612 deg
ZDOT = -583
060668 TA = 180
65803
MA = 180
66038
Ha = 228
109 n
mi
Hp = 219
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9380695
07 X = 2919718
61
Y = -10215597
39 feet Y = -3081402
63 meter
Z = -17477352
65 Z = -5313060
28
XDOT = 16713
726351 XDOT = 5033
328625
YDOT = 18621
603570 feet/sec YDOT = 5732
491799 meter/sec
ZDOT = -1912
928701 ZDOT = -558
462179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13786457
06 X = -4202112
11
Y = -2096002
74 feet Y = -638861
64 meter
Z = -17417063
47 Z = -5308720
95
XDOT = 5828
799737 XDOT = 1776
618160
YDOT = -23299
381231 feet/sec YDOT = -7101
651399 meter/sec
ZDOT = -1809
227222 ZDOT = -551
452457
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 14250
40236086
00016717 00000-0 10270-3 0 9110
2 25544 51
6430 52
0909 0003210 76
5252 283
6256 15
50346583 24085
Satellite: ISS
Catalog Number: 25544
Epoch time: 14250
40236086 = yrday
fracday
Element set: 911
Inclination: 51
6430 deg
RA of node: 52
0909 deg
Eccentricity:
0003210
Arg of perigee: 76
5252 deg
Mean anomaly: 283
6256 deg
Mean motion: 15
50346583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2408
Checksum: 279
Coasting Arc #13 (Orbit 2423)
---------------------------------------
Vector Time (GMT): 2014/251/09:14:47
654
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2991973
95 A = 6788375
58 meter
Y = 2930135
38 meter E =
0005593
Z = 5337891
75 I = 51
88849
XDOT = -5305
887682 Wp = 84
56267
YDOT = -5534
169207 meter/sec RA = 46
58337 deg
ZDOT = 64
301664 TA = 4
82929
MA = 4
82389
Ha = 228
232 n
mi
Hp = 219
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9816187
51 X = -3050446
52
Y = 9613305
05 feet Y = 2896350
91 meter
Z = 17512768
22 Z = 5323214
94
XDOT = -17407
767985 XDOT = -5243
921334
YDOT = -18156
723119 feet/sec YDOT = -5593
156593 meter/sec
ZDOT = 210
963465 ZDOT = 38
677889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13579831
98 X = 4139132
79
Y = 2561890
27 feet Y = 780864
16 meter
Z = 17449788
06 Z = 5318695
40
XDOT = -4602
079882 XDOT = -1402
713948
YDOT = 23703
818787 feet/sec YDOT = 7224
923966 meter/sec
ZDOT = 102
880311 ZDOT = 31
357919
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 14251
43369924
00016717 00000-0 10270-3 0 9123
2 25544 51
6434 46
9784 0003211 80
0826 280
0687 15
50346990 24249
Satellite: ISS
Catalog Number: 25544
Epoch time: 14251
43369924 = yrday
fracday
Element set: 912
Inclination: 51
6434 deg
RA of node: 46
9784 deg
Eccentricity:
0003211
Arg of perigee: 80
0826 deg
Mean anomaly: 280
0687 deg
Mean motion: 15
50346990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2424
Checksum: 306
Coasting Arc #14 (Orbit 2438)
---------------------------------------
Vector Time (GMT): 2014/252/09:14:47
654
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3174690
23 A = 6788299
37 meter
Y = -2779672
22 meter E =
0017896
Z = -5332977
62 I = 51
86575
XDOT = 5456
608864 Wp = 91
61065
YDOT = 5340
203939 meter/sec RA = 41
63753 deg
ZDOT = 465
709885 TA = 182
82370
MA = 182
83382
Ha = 228
035 n
mi
Hp = 219
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10415650
36 X = 3231442
94
Y = -9119659
50 feet Y = -2743854
18 meter
Z = -17496645
73 Z = -5317417
30
XDOT = 17902
260051 XDOT = 5394
225669
YDOT = 17520
354129 feet/sec YDOT = 5400
874528 meter/sec
ZDOT = 1527
919571 ZDOT = 492
064896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13577722
19 X = -4138489
72
Y = -3103135
64 feet Y = -945835
74 meter
Z = -17429933
53 Z = -5312643
74
XDOT = 3338
146442 XDOT = 1017
467035
YDOT = -23796
916035 feet/sec YDOT = -7253
300008 meter/sec
ZDOT = 1639
138974 ZDOT = 499
609559
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 14252
40055784
00016717 00000-0 10270-3 0 9138
2 25544 51
6425 42
1839 0003229 83
2164 276
9354 15
50407252 24397
Satellite: ISS
Catalog Number: 25544
Epoch time: 14252
40055784 = yrday
fracday
Element set: 913
Inclination: 51
6425 deg
RA of node: 42
1839 deg
Eccentricity:
0003229
Arg of perigee: 83
2164 deg
Mean anomaly: 276
9354 deg
Mean motion: 15
50407252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2439
Checksum: 299
Coasting Arc #15 (Orbit 2454)
---------------------------------------
Vector Time (GMT): 2014/253/09:14:47
654
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3381869
54 A = 6788551
49 meter
Y = 2633250
21 meter E =
0006672
Z = 5259253
24 I = 51
84327
XDOT = -5587
173513 Wp = 70
39820
YDOT = -5152
577555 meter/sec RA = 36
69149 deg
ZDOT = -1009
670456 TA = 29
26140
MA = 29
22405
Ha = 228
138 n
mi
Hp = 219
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11095372
50 X = -3436611
53
Y = 8639272
33 feet Y = 2595126
59 meter
Z = 17254767
84 Z = 5242691
29
XDOT = -18330
621761 XDOT = -5524
236301
YDOT = -16904
782005 feet/sec YDOT = -5214
705180 meter/sec
ZDOT = -3312
567113 ZDOT = -1036
658537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13656475
72 X = 4162493
80
Y = 3699770
79 feet Y = 1127690
14 meter
Z = 17183820
80 Z = 5237628
58
XDOT = -2125
354733 XDOT = -647
808123
YDOT = 23808
968361 feet/sec YDOT = 7256
973557 meter/sec
ZDOT = -3426
501379 ZDOT = -1044
397620
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 14253
43185366
00016717 00000-0 10270-3 0 9143
2 25544 51
6431 37
0714 0003189 86
4867 273
6649 15
50410740 24554
Satellite: ISS
Catalog Number: 25544
Epoch time: 14253
43185366 = yrday
fracday
Element set: 914
Inclination: 51
6431 deg
RA of node: 37
0714 deg
Eccentricity:
0003189
Arg of perigee: 86
4867 deg
Mean anomaly: 273
6649 deg
Mean motion: 15
50410740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2455
Checksum: 311
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