[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 18th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 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 3757)
---------------------------------------
Vector Time (GMT): 2015/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3530533
68 A = 6784280
84 meter
Y = 5440881
31 meter E =
0008092
Z = -1981589
51 I = 51
90395
XDOT = -5078
542192 Wp = 42
87585
YDOT = -1261
166095 meter/sec RA = 136
83757 deg
ZDOT = 5604
657442 TA = 295
32975
MA = 295
41354
Ha = 219
609 n
mi
Hp = 212
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11583115
76 X = -3581486
86
Y = 17850660
46 feet Y = 5401115
54 meter
Z = -6501277
92 Z = -1998864
01
XDOT = -16661
883833 XDOT = -5091
287009
YDOT = -4137
684038 feet/sec YDOT = -1318
028592 meter/sec
ZDOT = 18387
983735 ZDOT = 5579
956361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19732899
19 X = 6014587
67
Y = -7902000
09 feet Y = -2408529
63 meter
Z = -6576651
76 Z = -2004563
46
XDOT = 10729
693008 XDOT = 3270
410429
YDOT = 11630
578848 feet/sec YDOT = 3545
000433 meter/sec
ZDOT = 18281
699583 ZDOT = 5572
262033
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 15229
50395665
00016717 00000-0 10270-3 0 9005
2 25544 51
6438 137
8896 0001397 54
1601 305
9682 15
55277350 37584
Satellite: ISS
Catalog Number: 25544
Epoch time: 15229
50395665 = yrday
fracday
Element set: 900
Inclination: 51
6438 deg
RA of node: 137
8896 deg
Eccentricity:
0001397
Arg of perigee: 54
1601 deg
Mean anomaly: 305
9682 deg
Mean motion: 15
55277350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3758
Checksum: 333
Coasting Arc #2 (Orbit 3773)
---------------------------------------
Vector Time (GMT): 2015/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4587689
26 A = 6785993
24 meter
Y = -4992057
98 meter E =
0012387
Z = -106232
54 I = 51
93233
XDOT = 3423
608899 Wp = 129
51598
YDOT = 3264
656892 meter/sec RA = 131
87981 deg
ZDOT = -6037
397579 TA = 51
62427
MA = 51
51306
Ha = 219
649 n
mi
Hp = 212
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15051473
95 X = 4643686
72
Y = -16378142
97 feet Y = -4940442
33 meter
Z = -348531
94 Z = -83810
34
XDOT = 11232
312660 XDOT = 3416
175351
YDOT = 10710
816574 feet/sec YDOT = 3302
899961 meter/sec
ZDOT = -19807
734839 ZDOT = -6020
784821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21665556
95 X = -6603661
76
Y = 5045050
69 feet Y = 1537731
45 meter
Z = -251028
12 Z = -76513
37
XDOT = -2979
108515 XDOT = -908
032275
YDOT = -13667
909243 feet/sec YDOT = -4165
978737 meter/sec
ZDOT = -19736
651120 ZDOT = -6015
731261
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 15230
53202313
00016717 00000-0 10270-3 0 9018
2 25544 51
6440 132
7554 0001325 60
6407 299
4878 15
55275815 37745
Satellite: ISS
Catalog Number: 25544
Epoch time: 15230
53202313 = yrday
fracday
Element set: 901
Inclination: 51
6440 deg
RA of node: 132
7554 deg
Eccentricity:
0001325
Arg of perigee: 60
6407 deg
Mean anomaly: 299
4878 deg
Mean motion: 15
55275815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3774
Checksum: 297
Coasting Arc #3 (Orbit 3789)
---------------------------------------
Vector Time (GMT): 2015/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5070789
89 A = 6783992
82 meter
Y = 3949293
01 meter E =
0015316
Z = 2147888
11 I = 51
94633
XDOT = -1599
774025 Wp = 68
98135
YDOT = -5075
218877 meter/sec RA = 126
92255 deg
ZDOT = 5528
645550 TA = 314
75411
MA = 314
87864
Ha = 219
644 n
mi
Hp = 212
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16636449
76 X = -5125008
51
Y = 12956998
06 feet Y = 3892285
09 meter
Z = 7046876
99 Z = 2123123
44
XDOT = -5248
602443 XDOT = -1569
758670
YDOT = -16650
980566 feet/sec YDOT = -5092
940402 meter/sec
ZDOT = 18138
600887 ZDOT = 5520
947471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21056757
25 X = 6418099
61
Y = -1664616
03 feet Y = -507374
96 meter
Z = 6939435
32 Z = 2115139
88
XDOT = -4784
561822 XDOT = -1458
334443
YDOT = 15323
639574 feet/sec YDOT = 4670
645342 meter/sec
ZDOT = 18106
258552 ZDOT = 5518
787607
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
56007139
00016717 00000-0 10270-3 0 9022
2 25544 51
6438 127
6210 0001425 57
1687 302
9604 15
55312977 37902
Satellite: ISS
Catalog Number: 25544
Epoch time: 15231
56007139 = yrday
fracday
Element set: 902
Inclination: 51
6438 deg
RA of node: 127
6210 deg
Eccentricity:
0001425
Arg of perigee: 57
1687 deg
Mean anomaly: 302
9604 deg
Mean motion: 15
55312977 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3790
Checksum: 298
Coasting Arc #4 (Orbit 3804)
---------------------------------------
Vector Time (GMT): 2015/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5043992
59 A = 6779447
90 meter
Y = -2326003
60 meter E =
0007513
Z = -3895016
58 I = 51
95026
XDOT = -212
473514 Wp = 72
20842
YDOT = 6450
057237 meter/sec RA = 121
95540 deg
ZDOT = -4131
261624 TA = 154
60201
MA = 154
56507
Ha = 219
488 n
mi
Hp = 212
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16548532
11 X = 5088548
06
Y = -7631245
40 feet Y = -2269349
47 meter
Z = -12778925
80 Z = -3870405
63
XDOT = -697
091583 XDOT = -264
515816
YDOT = 21161
605108 feet/sec YDOT = 6447
389976 meter/sec
ZDOT = -13554
007952 ZDOT = -4132
420578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18133405
31 X = -5527061
94
Y = -2445492
39 feet Y = -745386
08 meter
Z = -12672408
80 Z = -3862550
20
XDOT = 11655
292178 XDOT = 3552
533056
YDOT = -16230
463857 feet/sec YDOT = -4947
045384 meter/sec
ZDOT = -13560
095937 ZDOT = -4133
117242
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
52384948
00016717 00000-0 10270-3 0 9036
2 25544 51
6442 122
8076 0001242 56
7737 303
3536 15
55351647 38055
Satellite: ISS
Catalog Number: 25544
Epoch time: 15232
52384948 = yrday
fracday
Element set: 903
Inclination: 51
6442 deg
RA of node: 122
8076 deg
Eccentricity:
0001242
Arg of perigee: 56
7737 deg
Mean anomaly: 303
3536 deg
Mean motion: 15
55351647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3805
Checksum: 305
Coasting Arc #5 (Orbit 3820)
---------------------------------------
Vector Time (GMT): 2015/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4553935
47 A = 6775183
28 meter
Y = 317391
06 meter E =
0006901
Z = 5001842
50 I = 51
95229
XDOT = 1805
449636 Wp = 113
66808
YDOT = -7158
936448 meter/sec RA = 116
97351 deg
ZDOT = 2093
069105 TA = 316
04052
MA = 316
09539
Ha = 219
627 n
mi
Hp = 212
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14940733
17 X = -4581443
13
Y = 1041309
24 feet Y = 266312
41 meter
Z = 16410244
42 Z = 4979653
63
XDOT = 5923
391193 XDOT = 1875
201106
YDOT = -23487
324304 feet/sec YDOT = -7138
356610 meter/sec
ZDOT = 6867
024623 ZDOT = 2102
009384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13391335
80 X = 4081679
15
Y = 6936498
96 feet Y = 2114244
88 meter
Z = 16314504
66 Z = 4972661
02
XDOT = -16734
070464 XDOT = -5100
544677
YDOT = 16022
881253 feet/sec YDOT = 4883
774206 meter/sec
ZDOT = 6906
800879 ZDOT = 2105
192908
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
55186392
00016717 00000-0 10270-3 0 9044
2 25544 51
6442 117
6729 0001318 62
2461 297
8826 15
55376206 38217
Satellite: ISS
Catalog Number: 25544
Epoch time: 15233
55186392 = yrday
fracday
Element set: 904
Inclination: 51
6442 deg
RA of node: 117
6729 deg
Eccentricity:
0001318
Arg of perigee: 62
2461 deg
Mean anomaly: 297
8826 deg
Mean motion: 15
55376206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3821
Checksum: 315
Coasting Arc #6 (Orbit 3835)
---------------------------------------
Vector Time (GMT): 2015/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3746600
24 A = 6773618
18 meter
Y = 1873247
69 meter E =
0015878
Z = -5336802
97 I = 51
96105
XDOT = -3079
580049 Wp = 89
94965
YDOT = 7006
216248 meter/sec RA = 111
98189 deg
ZDOT = 298
038333 TA = 182
87782
MA = 182
88697
Ha = 219
358 n
mi
Hp = 212
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12291995
54 X = 3751298
76
Y = 6145825
77 feet Y = 1915170
70 meter
Z = -17509196
09 Z = -5318591
45
XDOT = -10103
609084 XDOT = -3159
144123
YDOT = 22986
273780 feet/sec YDOT = 6971
333503 meter/sec
ZDOT = 977
816054 ZDOT = 282
884861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7596480
78 X = -2315407
34
Y = -11571113
95 feet Y = -3526875
53 meter
Z = -17430980
41 Z = -5312962
83
XDOT = 19498
216131 XDOT = 5943
056277
YDOT = -14169
529409 feet/sec YDOT = -4318
872564 meter/sec
ZDOT = 911
255248 ZDOT = 277
750600
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
51561049
00016717 00000-0 10270-3 0 9058
2 25544 51
6441 112
8588 0001210 59
1252 301
0020 15
55422166 38367
Satellite: ISS
Catalog Number: 25544
Epoch time: 15234
51561049 = yrday
fracday
Element set: 905
Inclination: 51
6441 deg
RA of node: 112
8588 deg
Eccentricity:
0001210
Arg of perigee: 59
1252 deg
Mean anomaly: 301
0020 deg
Mean motion: 15
55422166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3836
Checksum: 269
Coasting Arc #7 (Orbit 3851)
---------------------------------------
Vector Time (GMT): 2015/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2712854
21 A = 6775723
95 meter
Y = -3942408
76 meter E =
0008613
Z = 4791990
48 I = 51
98006
XDOT = 3999
385195 Wp = 60
81629
YDOT = -5987
245485 meter/sec RA = 106
99300 deg
ZDOT = -2653
939502 TA = 55
26486
MA = 55
18378
Ha = 219
328 n
mi
Hp = 212
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8900440
33 X = -2691845
19
Y = -12934411
95 feet Y = -3972628
08 meter
Z = 15721753
56 Z = 4778863
18
XDOT = 13121
342502 XDOT = 4078
930550
YDOT = -19643
193849 feet/sec YDOT = -5942
077041 meter/sec
ZDOT = -8707
150597 ZDOT = -2634
317999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1498831
99 X = 456843
99
Y = 15685210
37 feet Y = 4780852
12 meter
Z = 15665824
71 Z = 4774943
37
XDOT = -19974
916505 XDOT = -6088
354551
YDOT = 10544
799248 feet/sec YDOT = 3214
054811 meter/sec
ZDOT = -8621
479782 ZDOT = -2627
827037
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
54358967
00016717 00000-0 10270-3 0 9066
2 25544 51
6444 107
7243 0001130 55
8062 304
3198 15
55473137 38528
Satellite: ISS
Catalog Number: 25544
Epoch time: 15235
54358967 = yrday
fracday
Element set: 906
Inclination: 51
6444 deg
RA of node: 107
7243 deg
Eccentricity:
0001130
Arg of perigee: 55
8062 deg
Mean anomaly: 304
3198 deg
Mean motion: 15
55473137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3852
Checksum: 308
Coasting Arc #8 (Orbit 3866)
---------------------------------------
Vector Time (GMT): 2015/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1598707
69 A = 6780328
57 meter
Y = 5590956
11 meter E =
0005936
Z = -3491668
27 I = 52
00322
XDOT = -4537
488731 Wp = 87
16383
YDOT = 4150
323841 meter/sec RA = 102
01647 deg
ZDOT = 4575
034153 TA = 232
04985
MA = 232
10350
Ha = 219
268 n
mi
Hp = 212
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5245103
96 X = 1553030
52
Y = 18343031
87 feet Y = 5608578
45 meter
Z = -11455604
56 Z = -3484013
18
XDOT = -14886
774053 XDOT = -4605
785044
YDOT = 13616
548035 feet/sec YDOT = 4099
200883 meter/sec
ZDOT = 15009
954569 ZDOT = 4552
826125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4043073
69 X = 1232328
86
Y = -18664521
62 feet Y = -5688946
19 meter
Z = -11423572
00 Z = -3481904
75
XDOT = 18294
344893 XDOT = 5576
116324
YDOT = -5150
804574 feet/sec YDOT = -1569
965234 meter/sec
ZDOT = 14913
434669 ZDOT = 4545
614887
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
50730633
00016717 00000-0 10270-3 0 9078
2 25544 51
6439 102
9101 0001069 57
5676 302
5580 15
55454870 38677
Satellite: ISS
Catalog Number: 25544
Epoch time: 15236
50730633 = yrday
fracday
Element set: 907
Inclination: 51
6439 deg
RA of node: 102
9101 deg
Eccentricity:
0001069
Arg of perigee: 57
5676 deg
Mean anomaly: 302
5580 deg
Mean motion: 15
55454870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3867
Checksum: 309
Coasting Arc #9 (Orbit 3882)
---------------------------------------
Vector Time (GMT): 2015/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -431149
35 A = 6784360
87 meter
Y = -6576256
54 meter E =
0014654
Z = 1583058
99 I = 52
02274
XDOT = 4753
789355 Wp = 113
68980
YDOT = -1710
408360 meter/sec RA = 97
05691 deg
ZDOT = -5774
244999 TA = 49
07439
MA = 48
94761
Ha = 219
284 n
mi
Hp = 212
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1414532
00 X = -365269
84
Y = -21575644
80 feet Y = -6580709
55 meter
Z = 5193763
09 Z = 1581124
71
XDOT = 15596
421768 XDOT = 4800
611048
YDOT = -5611
575984 feet/sec YDOT = -1656
986677 meter/sec
ZDOT = -18944
373357 ZDOT = -5751
038516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8645679
69 X = -2635203
17
Y = 19820091
87 feet Y = 6041164
00 meter
Z = 5186588
98 Z = 1580872
32
XDOT = -15091
472542 XDOT = -4599
880831
YDOT = -1620
627172 feet/sec YDOT = -493
967162 meter/sec
ZDOT = -18843
967244 ZDOT = -5743
641216
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
53525364
00016717 00000-0 10270-3 0 9086
2 25544 51
6441 97
7755 0001147 64
9495 295
1777 15
55474626 38838
Satellite: ISS
Catalog Number: 25544
Epoch time: 15237
53525364 = yrday
fracday
Element set: 908
Inclination: 51
6441 deg
RA of node: 97
7755 deg
Eccentricity:
0001147
Arg of perigee: 64
9495 deg
Mean anomaly: 295
1777 deg
Mean motion: 15
55474626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3883
Checksum: 348
Coasting Arc #10 (Orbit 3898)
---------------------------------------
Vector Time (GMT): 2015/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -682963
35 A = 6785153
44 meter
Y = 6720893
91 meter E =
0014016
Z = 558116
41 I = 52
02793
XDOT = -4661
259948 Wp = 51
83507
YDOT = -980
877959 meter/sec RA = 92
10523 deg
ZDOT = 6014
274296 TA = 314
16019
MA = 314
27533
Ha = 219
153 n
mi
Hp = 212
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2240693
42 X = -760778
34
Y = 22050176
88 feet Y = 6712821
49 meter
Z = 1831090
59 Z = 554609
56
XDOT = -15292
847600 XDOT = -4679
159768
YDOT = -3218
103540 feet/sec YDOT = -1033
103147 meter/sec
ZDOT = 19731
871051 ZDOT = 5991
587681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11828422
63 X = 3605303
22
Y = -18745105
19 feet Y = -5713508
06 meter
Z = 1814758
93 Z = 553138
52
XDOT = 11010
030610 XDOT = 3355
857330
YDOT = 8878
313817 feet/sec YDOT = 2706
110051 meter/sec
ZDOT = 19634
180994 ZDOT = 5984
498367
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
56318146
00016717 00000-0 10270-3 0 9099
2 25544 51
6432 92
6397 0000994 63
5845 296
5410 15
55522527 38997
Satellite: ISS
Catalog Number: 25544
Epoch time: 15238
56318146 = yrday
fracday
Element set: 909
Inclination: 51
6432 deg
RA of node: 92
6397 deg
Eccentricity:
0000994
Arg of perigee: 63
5845 deg
Mean anomaly: 296
5410 deg
Mean motion: 15
55522527 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3899
Checksum: 340
Coasting Arc #11 (Orbit 3913)
---------------------------------------
Vector Time (GMT): 2015/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1774972
02 A = 6782326
66 meter
Y = -5985066
28 meter E =
0005487
Z = -2651480
07 I = 52
01778
XDOT = 4281
639738 Wp = 117
50536
YDOT = 3590
175589 meter/sec RA = 87
15120 deg
ZDOT = -5248
448743 TA = 92
22895
MA = 92
16612
Ha = 219
136 n
mi
Hp = 212
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5823399
03 X = 1854646
24
Y = -19636044
24 feet Y = -5964772
02 meter
Z = -8699081
61 Z = -2642663
96
XDOT = 14047
374470 XDOT = 4266
669868
YDOT = 11778
791304 feet/sec YDOT = 3637
971756 meter/sec
ZDOT = -17219
320022 ZDOT = -5227
686253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13742639
67 X = -4188756
57
Y = 15208714
46 feet Y = 4635616
17 meter
Z = -8659970
54 Z = -2639559
02
XDOT = -6617
672900 XDOT = -2017
066700
YDOT = -15713
764408 feet/sec YDOT = -4789
555392 meter/sec
ZDOT = -17130
396802 ZDOT = -5221
344945
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
52684992
00016717 00000-0 10270-3 0 9103
2 25544 51
6422 87
8256 0000930 63
2427 296
8822 15
55519646 39145
Satellite: ISS
Catalog Number: 25544
Epoch time: 15239
52684992 = yrday
fracday
Element set: 910
Inclination: 51
6422 deg
RA of node: 87
8256 deg
Eccentricity:
0000930
Arg of perigee: 63
2427 deg
Mean anomaly: 296
8822 deg
Mean motion: 15
55519646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3914
Checksum: 332
Coasting Arc #12 (Orbit 3929)
---------------------------------------
Vector Time (GMT): 2015/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2757145
30 A = 6777538
39 meter
Y = 4471793
79 meter E =
0010680
Z = 4274619
43 I = 51
99884
XDOT = -3636
283008 Wp = 102
64163
YDOT = -5708
761240 meter/sec RA = 82
18148 deg
ZDOT = 3616
815297 TA = 310
57875
MA = 310
67165
Ha = 219
202 n
mi
Hp = 212
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9045752
30 X = -2827709
19
Y = 14671239
47 feet Y = 4440567
33 meter
Z = 14024341
96 Z = 4261054
29
XDOT = -11930
062362 XDOT = -3589
744819
YDOT = -18729
531628 feet/sec YDOT = -5749
164085 meter/sec
ZDOT = 11866
191920 ZDOT = 3599
264698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14388624
02 X = 4385652
60
Y = -9575962
12 feet Y = -2918753
26 meter
Z = 13965010
49 Z = 4256535
20
XDOT = 2479
308374 XDOT = 755
693192
YDOT = 20968
744766 feet/sec YDOT = 6391
273405 meter/sec
ZDOT = 11791
509094 ZDOT = 3594
051972
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
55474588
00016717 00000-0 10270-3 0 9117
2 25544 51
6417 82
6891 0001003 60
2426 299
8827 15
55534894 39303
Satellite: ISS
Catalog Number: 25544
Epoch time: 15240
55474588 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 82
6891 deg
Eccentricity:
0001003
Arg of perigee: 60
2426 deg
Mean anomaly: 299
8827 deg
Mean motion: 15
55534894 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3930
Checksum: 324
Coasting Arc #13 (Orbit 3944)
---------------------------------------
Vector Time (GMT): 2015/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3633649
36 A = 6773718
27 meter
Y = -2385706
59 meter E =
0014900
Z = -5208167
96 I = 51
97984
XDOT = 2686
090037 Wp = 78
99620
YDOT = 7044
406999 meter/sec RA = 77
19555 deg
ZDOT = -1353
301556 TA = 178
04670
MA = 178
04087
Ha = 219
045 n
mi
Hp = 212
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11921421
79 X = 3685355
76
Y = -7827121
36 feet Y = -2344784
11 meter
Z = -17087165
23 Z = -5190390
89
XDOT = 8812
631354 XDOT = 2613
691860
YDOT = 23111
571520 feet/sec YDOT = 7074
039697 meter/sec
ZDOT = -4439
965735 ZDOT = -1340
429778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14152577
18 X = -4313705
52
Y = 2391341
84 feet Y = 728880
99 meter
Z = -17010037
79 Z = -5184659
52
XDOT = 1266
622795 XDOT = 386
066628
YDOT = -23688
273287 feet/sec YDOT = -7220
185698 meter/sec
ZDOT = -4385
715383 ZDOT = -1336
766049
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
51838055
00016717 00000-0 10270-3 0 9128
2 25544 51
6403 77
8735 0000958 68
9005 291
2250 15
55582749 39451
Satellite: ISS
Catalog Number: 25544
Epoch time: 15241
51838055 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 77
8735 deg
Eccentricity:
0000958
Arg of perigee: 68
9005 deg
Mean anomaly: 291
2250 deg
Mean motion: 15
55582749 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3945
Checksum: 323
Coasting Arc #14 (Orbit 3960)
---------------------------------------
Vector Time (GMT): 2015/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4291154
74 A = 6773530
40 meter
Y = 34272
89 meter E =
0004797
Z = 5237623
15 I = 51
97158
XDOT = -1454
665503 Wp = 59
12349
YDOT = -7448
055732 meter/sec RA = 72
20238 deg
ZDOT = -1139
893599 TA = 41
76444
MA = 41
72783
Ha = 219
173 n
mi
Hp = 212
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14078591
68 X = -4316661
14
Y = 112443
86 feet Y = -13855
66 meter
Z = 17183803
00 Z = 5216715
88
XDOT = -4772
524615 XDOT = -1365
734325
YDOT = -24435
878385 feet/sec YDOT = -7463
825641 meter/sec
ZDOT = -3739
808395 ZDOT = -1146
743163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13153648
53 X = 4009232
07
Y = 5319101
28 feet Y = 1621262
07 meter
Z = 17093600
11 Z = 5210129
31
XDOT = -4566
909024 XDOT = -1391
993871
YDOT = 23436
058642 feet/sec YDOT = 7143
310674 meter/sec
ZDOT = -3767
996371 ZDOT = -1148
485294
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
54624139
00016717 00000-0 10270-3 0 9139
2 25544 51
6406 72
7374 0000909 72
4092 287
7160 15
55589916 39610
Satellite: ISS
Catalog Number: 25544
Epoch time: 15242
54624139 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 72
7374 deg
Eccentricity:
0000909
Arg of perigee: 72
4092 deg
Mean anomaly: 287
7160 deg
Mean motion: 15
55589916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3961
Checksum: 323
Coasting Arc #15 (Orbit 3975)
---------------------------------------
Vector Time (GMT): 2015/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 892870
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4662906
96 A = 6776878
64 meter
Y = 2232970
84 meter E =
0009611
Z = -4391067
75 I = 51
97192
XDOT = -42
165596 Wp = 107
29462
YDOT = 6846
399271 meter/sec RA = 67
21326 deg
ZDOT = 3440
206206 TA = 197
43799
MA = 197
47101
Ha = 218
988 n
mi
Hp = 212
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15298251
17 X = 4658920
76
Y = 7326019
82 feet Y = 2285091
74 meter
Z = -14406390
24 Z = -4368426
39
XDOT = -138
338569 XDOT = -135
431645
YDOT = 22461
939865 feet/sec YDOT = 6845
406665 meter/sec
ZDOT = 11286
765769 ZDOT = 3439
774049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11636182
83 X = -3546708
53
Y = -12453886
09 feet Y = -3795944
48 meter
Z = -14309126
65 Z = -4361421
80
XDOT = 7517
433149 XDOT = 2291
313624
YDOT = -19975
451223 feet/sec YDOT = -6088
517533 meter/sec
ZDOT = 11283
640521 ZDOT = 3439
253631
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
50984387
00016717 00000-0 10270-3 0 9141
2 25544 51
6399 67
9210 0000955 78
0695 282
0565 15
55637429 39764
Satellite: ISS
Catalog Number: 25544
Epoch time: 15243
50984387 = yrday
fracday
Element set: 914
Inclination: 51
6399 deg
RA of node: 67
9210 deg
Eccentricity:
0000955
Arg of perigee: 78
0695 deg
Mean anomaly: 282
0565 deg
Mean motion: 15
55637429 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3976
Checksum: 349
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