[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 26th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15607 67 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
087/01:36:05
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 211
3
092/18:33:35
099 -0
6 1
4 1
4
N/A 1
1 0
0 220
3
000/00:03:10
197 0
5 -0
0 212
5
Coasting Arc #1 (Orbit 1501)
---------------------------------------
Vector Time (GMT): 2015/084/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5889559
28 A = 6784071
36 meter
Y = 2509132
14 meter E =
0017666
Z = 2231253
53 I = 51
88058
XDOT = -196
950157 Wp = 92
22015
YDOT = -5366
498417 meter/sec RA = 141
05314 deg
ZDOT = 5476
962882 TA = 292
50972
MA = 292
69665
Ha = 221
436 n
mi
Hp = 211
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19322701
06 X = -5928017
89
Y = 8232060
82 feet Y = 2443056
41 meter
Z = 7320385
59 Z = 2202549
48
XDOT = -646
161931 XDOT = -163
531156
YDOT = -17606
622104 feet/sec YDOT = -5368
513472 meter/sec
ZDOT = 17969
038327 ZDOT = 5476
087810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19101290
38 X = -5822073
31
Y = 8835506
36 feet Y = 2693062
34 meter
Z = 7196956
30 Z = 2193632
28
XDOT = -667
043846 XDOT = -203
314964
YDOT = -16179
690708 feet/sec YDOT = -4931
569728 meter/sec
ZDOT = 17966
131181 ZDOT = 5476
076784
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
55990668
00016717 00000-0 10270-3 0 9003
2 25544 51
6434 141
7960 0006816 138
6875 221
4795 15
55236868 15029
Satellite: ISS
Catalog Number: 25544
Epoch time: 15084
55990668 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 141
7960 deg
Eccentricity:
0006816
Arg of perigee: 138
6875 deg
Mean anomaly: 221
4795 deg
Mean motion: 15
55236868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1502
Checksum: 336
Coasting Arc #2 (Orbit 1516)
---------------------------------------
Vector Time (GMT): 2015/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5436336
42 A = 6779489
32 meter
Y = -936995
60 meter E =
0011080
Z = -3946951
33 I = 51
89012
XDOT = -1868
111057 Wp = 109
10229
YDOT = 6223
543588 meter/sec RA = 136
08128 deg
ZDOT = -4063
317251 TA = 118
58897
MA = 118
47744
Ha = 221
347 n
mi
Hp = 211
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17835749
42 X = 5465582
89
Y = -3074132
56 feet Y = -876039
77 meter
Z = -12949315
40 Z = -3920471
56
XDOT = -6128
973283 XDOT = -1917
827289
YDOT = 20418
450091 feet/sec YDOT = 6202
374807 meter/sec
ZDOT = -13331
093342 ZDOT = -4072
513478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17747212
45 X = 5409350
36
Y = -3940998
31 feet Y = -1201216
28 meter
Z = -12835653
48 Z = -3912307
18
XDOT = -5333
913920 XDOT = -1625
776963
YDOT = 19392
343583 feet/sec YDOT = 5910
786324 meter/sec
ZDOT = -13371
502710 ZDOT = -4075
634026
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
52372850
00016717 00000-0 10270-3 0 9019
2 25544 51
6438 136
9824 0006829 142
0530 218
1106 15
55279476 15176
Satellite: ISS
Catalog Number: 25544
Epoch time: 15085
52372850 = yrday
fracday
Element set: 901
Inclination: 51
6438 deg
RA of node: 136
9824 deg
Eccentricity:
0006829
Arg of perigee: 142
0530 deg
Mean anomaly: 218
1106 deg
Mean motion: 15
55279476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1517
Checksum: 309
Coasting Arc #3 (Orbit 1532)
---------------------------------------
Vector Time (GMT): 2015/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 889397
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4469567
69 A = 6775270
69 meter
Y = -857453
60 meter E =
0012602
Z = 5014258
45 I = 51
89838
XDOT = 3544
840415 Wp = 135
08563
YDOT = -6494
462667 meter/sec RA = 131
09655 deg
ZDOT = 2037
379457 TA = 295
13243
MA = 295
26311
Ha = 221
270 n
mi
Hp = 211
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14663935
98 X = -4484004
56
Y = -2813167
98 feet Y = -907515
48 meter
Z = 16450979
15 Z = 4992511
24
XDOT = 11630
053854 XDOT = 3607
302779
YDOT = -21307
292216 feet/sec YDOT = -6454
472511 meter/sec
ZDOT = 6684
315803 ZDOT = 2054
751864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14920803
48 X = -4547860
90
Y = -1835486
24 feet Y = -559456
21 meter
Z = 16357880
71 Z = 4985882
04
XDOT = 10028
828186 XDOT = 3056
786831
YDOT = -20933
847841 feet/sec YDOT = -6380
636822 meter/sec
ZDOT = 6759
833607 ZDOT = 2060
397283
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
55178302
00016717 00000-0 10270-3 0 9020
2 25544 51
6435 131
8487 0006769 145
2193 214
9403 15
55327170 15332
Satellite: ISS
Catalog Number: 25544
Epoch time: 15086
55178302 = yrday
fracday
Element set: 902
Inclination: 51
6435 deg
RA of node: 131
8487 deg
Eccentricity:
0006769
Arg of perigee: 145
2193 deg
Mean anomaly: 214
9403 deg
Mean motion: 15
55327170 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1533
Checksum: 306
Coasting Arc #4 (Orbit 1541)
---------------------------------------
Vector Time (GMT): 2015/087/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904314
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4494541
94 A = 6785731
62 meter
Y = 5054563
90 meter E =
0013670
Z = 509363
22 I = 51
94360
XDOT = -3234
661839 Wp = 78
36677
YDOT = -3495
263020 meter/sec RA = 128
26378 deg
ZDOT = 6009
039390 TA = 287
10581
MA = 287
25548
Ha = 220
978 n
mi
Hp = 211
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14745872
49 X = -4553203
51
Y = 16583214
90 feet Y = 5003975
05 meter
Z = 1671139
18 Z = 487386
73
XDOT = -10612
407609 XDOT = -3224
526110
YDOT = -11467
398361 feet/sec YDOT = -3531
377864 meter/sec
ZDOT = 19714
696161 ZDOT = 5993
351060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5113132
54 X = 1558482
80
Y = -21601116
85 feet Y = -6584020
42 meter
Z = 1576104
23 Z = 480396
57
XDOT = 13318
484916 XDOT = 4059
474202
YDOT = 4620
019703 feet/sec YDOT = 1408
182006 meter/sec
ZDOT = 19647
993735 ZDOT = 5988
708491
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
13005376
00016717 00000-0 10270-3 0 9036
2 25544 51
6420 128
9591 0006450 148
0443 212
1102 15
55332884 15429
Satellite: ISS
Catalog Number: 25544
Epoch time: 15087
13005376 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 128
9591 deg
Eccentricity:
0006450
Arg of perigee: 148
0443 deg
Mean anomaly: 212
1102 deg
Mean motion: 15
55332884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1542
Checksum: 279
Coasting Arc #5 (Orbit 1556)
---------------------------------------
Vector Time (GMT): 2015/088/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904314
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4942826
02 A = 6782994
07 meter
Y = -3867508
83 meter E =
0011481
Z = -2564888
02 I = 51
95336
XDOT = 1447
491512 Wp = 141
61057
YDOT = 5350
742659 meter/sec RA = 123
30602 deg
ZDOT = -5300
159330 TA = 67
09972
MA = 66
97857
Ha = 220
931 n
mi
Hp = 211
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16216620
81 X = 4998165
26
Y = -12688677
25 feet Y = -3811925
78 meter
Z = -8414986
94 Z = -2540742
04
XDOT = 4748
987899 XDOT = 1413
296700
YDOT = 17554
929982 feet/sec YDOT = 5366
737684 meter/sec
ZDOT = -17388
974181 ZDOT = -5293
211376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7967780
29 X = -2428579
43
Y = 19032549
66 feet Y = 5801121
14 meter
Z = -8310827
68 Z = -2533140
28
XDOT = -11447
160767 XDOT = -3489
094602
YDOT = -12341
653643 feet/sec YDOT = -3761
736030 meter/sec
ZDOT = -17360
047084 ZDOT = -5291
342351
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
09382416
00016717 00000-0 10270-3 0 9046
2 25544 51
6417 124
1456 0006440 150
9408 209
2105 15
55369611 15579
Satellite: ISS
Catalog Number: 25544
Epoch time: 15088
09382416 = yrday
fracday
Element set: 904
Inclination: 51
6417 deg
RA of node: 124
1456 deg
Eccentricity:
0006440
Arg of perigee: 150
9408 deg
Mean anomaly: 209
2105 deg
Mean motion: 15
55369611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1557
Checksum: 299
Coasting Arc #6 (Orbit 1572)
---------------------------------------
Vector Time (GMT): 2015/089/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904314
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4878069
09 A = 6778326
16 meter
Y = 2162331
09 meter E =
0015287
Z = 4175077
66 I = 51
95425
XDOT = 266
144657 Wp = 123
66000
YDOT = -6684
979533 meter/sec RA = 118
33523 deg
ZDOT = 3755
092019 TA = 287
83022
MA = 287
99693
Ha = 220
816 n
mi
Hp = 211
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16004163
68 X = -4922167
09
Y = 7094262
11 feet Y = 2107535
28 meter
Z = 13697761
36 Z = 4151273
72
XDOT = 873
178010 XDOT = 322
637180
YDOT = -21932
347548 feet/sec YDOT = -6681
687005 meter/sec
ZDOT = 12319
855704 ZDOT = 3756
522915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10308510
18 X = 3142033
90
Y = -14247525
03 feet Y = -4342645
63 meter
Z = 13595334
67 Z = 4143858
01
XDOT = 9345
418327 XDOT = 2848
483506
YDOT = 18581
611219 feet/sec YDOT = 5663
675100 meter/sec
ZDOT = 12327
079281 ZDOT = 3757
293765
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 15089
12182476
00016717 00000-0 10270-3 0 9056
2 25544 51
6413 119
0103 0006465 155
6828 204
4632 15
55405145 15735
Satellite: ISS
Catalog Number: 25544
Epoch time: 15089
12182476 = yrday
fracday
Element set: 905
Inclination: 51
6413 deg
RA of node: 119
0103 deg
Eccentricity:
0006465
Arg of perigee: 155
6828 deg
Mean anomaly: 204
4632 deg
Mean motion: 15
55405145 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1573
Checksum: 295
Coasting Arc #7 (Orbit 1587)
---------------------------------------
Vector Time (GMT): 2015/090/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904314
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4406157
21 A = 6774383
57 meter
Y = -21570
22 meter E =
0016194
Z = -5158488
27 I = 51
95526
XDOT = -1799
262559 Wp = 101
96613
YDOT = 7276
876330 meter/sec RA = 113
35014 deg
ZDOT = -1574
711385 TA = 152
94368
MA = 152
85918
Ha = 220
738 n
mi
Hp = 211
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14455896
36 X = 4431128
82
Y = -70768
44 feet Y = 27841
24 meter
Z = -16924174
11 Z = -5137023
47
XDOT = -5903
092386 XDOT = -1872
851270
YDOT = 23874
266176 feet/sec YDOT = 7256
344133 meter/sec
ZDOT = -5166
375935 ZDOT = -1583
631517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12405533
68 X = -3781206
66
Y = 7628108
93 feet Y = 2325047
60 meter
Z = -16832121
25 Z = -5130430
56
XDOT = -6832
002775 XDOT = -2082
394446
YDOT = -22543
863758 feet/sec YDOT = -6871
369674 meter/sec
ZDOT = -5205
821418 ZDOT = -1586
734368
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
08555640
00016717 00000-0 10270-3 0 9061
2 25544 51
6410 114
1961 0006644 157
3553 202
7895 15
55435099 15882
Satellite: ISS
Catalog Number: 25544
Epoch time: 15090
08555640 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 114
1961 deg
Eccentricity:
0006644
Arg of perigee: 157
3553 deg
Mean anomaly: 202
7895 deg
Mean motion: 15
55435099 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1588
Checksum: 317
Coasting Arc #8 (Orbit 1603)
---------------------------------------
Vector Time (GMT): 2015/091/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904314
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3621014
90 A = 6773800
73 meter
Y = -2201583
55 meter E =
0006881
Z = 5279579
21 I = 51
96456
XDOT = 3024
336227 Wp = 133
09833
YDOT = -7002
992806 meter/sec RA = 108
35766 deg
ZDOT = -849
882836 TA = 324
96076
MA = 325
00601
Ha = 220
795 n
mi
Hp = 211
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11879970
14 X = -3621773
30
Y = -7223043
16 feet Y = -2242079
60 meter
Z = 17321454
10 Z = 5261987
55
XDOT = 9922
362949 XDOT = 3106
548980
YDOT = -22975
698184 feet/sec YDOT = -6968
713145 meter/sec
ZDOT = -2788
329514 ZDOT = -834
990555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13993265
70 X = 4265147
39
Y = -299799
57 feet Y = -91378
91 meter
Z = 17246374
99 Z = 5256695
10
XDOT = 3848
658706 XDOT = 1173
071173
YDOT = 23712
436456 feet/sec YDOT = 7227
550632 meter/sec
ZDOT = -2723
306391 ZDOT = -830
063788
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 15091
11351567
00016717 00000-0 10270-3 0 9079
2 25544 51
6405 109
0606 0006674 161
0259 199
1144 15
55423415 16047
Satellite: ISS
Catalog Number: 25544
Epoch time: 15091
11351567 = yrday
fracday
Element set: 907
Inclination: 51
6405 deg
RA of node: 109
0606 deg
Eccentricity:
0006674
Arg of perigee: 161
0259 deg
Mean anomaly: 199
1144 deg
Mean motion: 15
55423415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1604
Checksum: 290
Coasting Arc #9 (Orbit 1618)
---------------------------------------
Vector Time (GMT): 2015/092/01:36:05
000
Vector Time (MET): N/A
Weight (LBS) : 904314
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2645359
33 A = 6776624
71 meter
Y = 4276670
07 meter E =
0014830
Z = -4557281
70 I = 51
98421
XDOT = -3908
281203 Wp = 132
06368
YDOT = 5781
611906 meter/sec RA = 103
36949 deg
ZDOT = 3153
881947 TA = 169
46746
MA = 169
43636
Ha = 220
496 n
mi
Hp = 211
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8679000
43 X = 2619477
56
Y = 14031069
78 feet Y = 4306106
82 meter
Z = -14951711
60 Z = -4544494
55
XDOT = -12822
444892 XDOT = -3987
962471
YDOT = 18968
542998 feet/sec YDOT = 5737
461895 meter/sec
ZDOT = 10347
381715 ZDOT = 3134
701877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15032645
13 X = -4581950
24
Y = -6916010
32 feet Y = -2107999
95 meter
Z = -14897584
67 Z = -4540783
81
XDOT = -136
892561 XDOT = -41
724853
YDOT = -21834
153586 feet/sec YDOT = -6655
050013 meter/sec
ZDOT = 10264
161195 ZDOT = 3128
516332
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 15092
07720548
00016717 00000-0 10270-3 0 9085
2 25544 51
6410 104
2457 0006762 164
2981 195
8383 15
55496620 16191
Satellite: ISS
Catalog Number: 25544
Epoch time: 15092
07720548 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 104
2457 deg
Eccentricity:
0006762
Arg of perigee: 164
2981 deg
Mean anomaly: 195
8383 deg
Mean motion: 15
55496620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1619
Checksum: 320
Coasting Arc #10 (Orbit 1629)
---------------------------------------
Vector Time (GMT): 2015/092/18:35:10
197
Vector Time (MET): N/A
Weight (LBS) : 904173
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2582060
52 A = 6778393
01 meter
Y = 4604711
11 meter E =
0011720
Z = -4264120
59 I = 51
99582
XDOT = -3848
546872 Wp = 135
83275
YDOT = 5531
750979 meter/sec RA = 99
85383 deg
ZDOT = 3641
006234 TA = 171
28188
MA = 171
26150
Ha = 220
268 n
mi
Hp = 212
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8471327
18 X = 2551091
21
Y = 15107319
91 feet Y = 4633411
60 meter
Z = -13989896
94 Z = -4251653
31
XDOT = -12626
466114 XDOT = -3927
804888
YDOT = 18148
789300 feet/sec YDOT = 5488
271399 meter/sec
ZDOT = 11945
558510 ZDOT = 3622
117353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11554435
12 X = 3521791
82
Y = -12959983
12 feet Y = -3950202
85 meter
Z = -13937201
36 Z = -4248058
98
XDOT = 20323
766010 XDOT = 6194
683880
YDOT = 5353
745659 feet/sec YDOT = 1631
821677 meter/sec
ZDOT = 11863
620975 ZDOT = 3616
031673
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 15092
78389967
00016717 00000-0 10270-3 0 9090
2 25544 51
6441 100
7197 0005612 174
7811 185
3402 15
55261733 16302
Satellite: ISS
Catalog Number: 25544
Epoch time: 15092
78389967 = yrday
fracday
Element set: 909
Inclination: 51
6441 deg
RA of node: 100
7197 deg
Eccentricity:
0005612
Arg of perigee: 174
7811 deg
Mean anomaly: 185
3402 deg
Mean motion: 15
55261733 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1630
Checksum: 316
Coasting Arc #11 (Orbit 1645)
---------------------------------------
Vector Time (GMT): 2015/093/18:35:10
197
Vector Time (MET): N/A
Weight (LBS) : 904173
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1587685
43 A = 6782977
52 meter
Y = -6013747
82 meter E =
0015916
Z = 2681980
03 I = 52
01545
XDOT = 4397
492390 Wp = 122
33800
YDOT = -3499
504638 meter/sec RA = 94
88698 deg
ZDOT = -5229
396771 TA = 27
50496
MA = 27
42082
Ha = 220
254 n
mi
Hp = 212
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5208941
70 X = -1533348
42
Y = -19730143
77 feet Y = -6031198
15 meter
Z = 8799147
09 Z = 2674400
18
XDOT = 14427
468470 XDOT = 4461
700470
YDOT = -11481
314429 feet/sec YDOT = -3449
970762 meter/sec
ZDOT = -17156
813553 ZDOT = -5207
878001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16794068
48 X = -5118832
07
Y = 11615680
89 feet Y = 3540459
53 meter
Z = 8767659
76 Z = 2672382
70
XDOT = -14868
681062 XDOT = -4531
973988
YDOT = -8581
855183 feet/sec YDOT = -2615
749460 meter/sec
ZDOT = -17063
930924 ZDOT = -5201
086146
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 15093
81197434
00016717 00000-0 10270-3 0 9103
2 25544 51
6438 95
5857 0005685 178
1319 181
9856 15
55270925 16468
Satellite: ISS
Catalog Number: 25544
Epoch time: 15093
81197434 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 95
5857 deg
Eccentricity:
0005685
Arg of perigee: 178
1319 deg
Mean anomaly: 181
9856 deg
Mean motion: 15
55270925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1646
Checksum: 345
Coasting Arc #12 (Orbit 1660)
---------------------------------------
Vector Time (GMT): 2015/094/18:35:10
197
Vector Time (MET): N/A
Weight (LBS) : 904173
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 554374
31 A = 6785624
20 meter
Y = 6725509
96 meter E =
0006988
Z = -700134
81 I = 52
02734
XDOT = -4675
156044 Wp = 69
31932
YDOT = 1003
810211 meter/sec RA = 89
93264 deg
ZDOT = 5991
323360 TA = 283
15860
MA = 283
23657
Ha = 219
959 n
mi
Hp = 212
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1818813
37 X = 482527
89
Y = 22065321
40 feet Y = 6731307
53 meter
Z = -2297030
21 Z = -697617
18
XDOT = -15338
438466 XDOT = -4715
137319
YDOT = 3293
340586 feet/sec YDOT = 951
306839 meter/sec
ZDOT = 19656
572704 ZDOT = 5968
514886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19990226
11 X = 6093020
92
Y = -9519535
34 feet Y = -2901554
37 meter
Z = -2287388
39 Z = -697195
98
XDOT = 7857
269200 XDOT = 2394
895652
YDOT = 11840
010558 feet/sec YDOT = 3608
835218 meter/sec
ZDOT = 19558
579984 ZDOT = 5961
455179
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 15094
77577223
00016717 00000-0 10270-3 0 9118
2 25544 51
6445 90
7719 0005599 182
8445 177
2678 15
55330525 16616
Satellite: ISS
Catalog Number: 25544
Epoch time: 15094
77577223 = yrday
fracday
Element set: 911
Inclination: 51
6445 deg
RA of node: 90
7719 deg
Eccentricity:
0005599
Arg of perigee: 182
8445 deg
Mean anomaly: 177
2678 deg
Mean motion: 15
55330525 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1661
Checksum: 338
Coasting Arc #13 (Orbit 1676)
---------------------------------------
Vector Time (GMT): 2015/095/18:35:10
197
Vector Time (MET): N/A
Weight (LBS) : 904173
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 543755
84 A = 6784987
85 meter
Y = -6601972
96 meter E =
0013209
Z = -1433578
69 I = 52
02466
XDOT = 4711
297120 Wp = 160
21358
YDOT = 1647
500180 meter/sec RA = 84
98285 deg
ZDOT = -5827
833906 TA = 35
35110
MA = 35
26359
Ha = 219
924 n
mi
Hp = 212
756
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1783975
86 X = 624504
13
Y = -21660016
27 feet Y = -6595441
01 meter
Z = -4703342
15 Z = -1430740
24
XDOT = 15457
011549 XDOT = 4720
834022
YDOT = 5405
184316 feet/sec YDOT = 1700
237580 meter/sec
ZDOT = -19120
189980 ZDOT = -5804
924094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20796032
37 X = -6338630
67
Y = 6323690
41 feet Y = 1927460
84 meter
Z = -4690019
13 Z = -1429517
83
XDOT = -278
255710 XDOT = -84
812341
YDOT = -14955
483582 feet/sec YDOT = -4558
431396 meter/sec
ZDOT = -19022
221757 ZDOT = -5797
973191
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 15095
80380258
00016717 00000-0 10270-3 0 9124
2 25544 51
6450 85
6375 0005741 187
3400 172
7670 15
55324116 16771
Satellite: ISS
Catalog Number: 25544
Epoch time: 15095
80380258 = yrday
fracday
Element set: 912
Inclination: 51
6450 deg
RA of node: 85
6375 deg
Eccentricity:
0005741
Arg of perigee: 187
3400 deg
Mean anomaly: 172
7670 deg
Mean motion: 15
55324116 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1677
Checksum: 309
Coasting Arc #14 (Orbit 1692)
---------------------------------------
Vector Time (GMT): 2015/096/18:35:10
197
Vector Time (MET): N/A
Weight (LBS) : 904173
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1630517
41 A = 6781064
27 meter
Y = 5682832
30 meter E =
0012690
Z = 3316461
18 I = 52
00855
XDOT = -4467
645480 Wp = 113
16490
YDOT = -4055
815592 meter/sec RA = 80
02430 deg
ZDOT = 4734
052958 TA = 285
20840
MA = 285
34869
Ha = 219
677 n
mi
Hp = 212
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5349466
57 X = -1710053
36
Y = 18644462
93 feet Y = 5664154
44 meter
Z = 10880778
13 Z = 3308346
53
XDOT = -14657
629527 XDOT = -4444
956924
YDOT = -13306
481600 feet/sec YDOT = -4105
648352 meter/sec
ZDOT = 15531
669811 ZDOT = 4712
405247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19292645
58 X = 5880398
37
Y = -2191919
62 feet Y = -668097
10 meter
Z = 10844972
95 Z = 3305547
76
XDOT = -6744
590914 XDOT = -2055
751310
YDOT = 17338
900295 feet/sec YDOT = 5284
896810 meter/sec
ZDOT = 15439
543106 ZDOT = 4705
972739
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 15096
83180956
00016717 00000-0 10270-3 0 9132
2 25544 51
6452 80
5027 0005492 190
4051 169
6989 15
55377704 16938
Satellite: ISS
Catalog Number: 25544
Epoch time: 15096
83180956 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 80
5027 deg
Eccentricity:
0005492
Arg of perigee: 190
4051 deg
Mean anomaly: 169
6989 deg
Mean motion: 15
55377704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1693
Checksum: 334
Coasting Arc #15 (Orbit 1707)
---------------------------------------
Vector Time (GMT): 2015/097/18:35:10
197
Vector Time (MET): N/A
Weight (LBS) : 904173
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2724584
78 A = 6776210
26 meter
Y = -4052033
94 meter E =
0008770
Z = -4704957
65 I = 51
98670
XDOT = 3903
260923 Wp = 101
44101
YDOT = 5942
186648 meter/sec RA = 75
05024 deg
ZDOT = -2863
430432 TA = 140
28462
MA = 140
22038
Ha = 219
474 n
mi
Hp = 212
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8938926
44 X = 2792548
33
Y = -13294074
61 feet Y = -4021186
28 meter
Z = -15436212
75 Z = -4691556
51
XDOT = 12805
974158 XDOT = 3850
433554
YDOT = 19495
363020 feet/sec YDOT = 5985
539827 meter/sec
ZDOT = -9394
456798 ZDOT = -2844
597734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15804941
93 X = -4817346
30
Y = -2938372
17 feet Y = -895615
84 meter
Z = -15378012
52 Z = -4687218
22
XDOT = 12474
759822 XDOT = 3802
306794
YDOT = -18457
226501 feet/sec YDOT = -5625
762638 meter/sec
ZDOT = -9314
749734 ZDOT = -2839
135719
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 15097
79554361
00016717 00000-0 10270-3 0 9144
2 25544 51
6454 75
6891 0005532 195
9834 164
1146 15
55435315 17083
Satellite: ISS
Catalog Number: 25544
Epoch time: 15097
79554361 = yrday
fracday
Element set: 914
Inclination: 51
6454 deg
RA of node: 75
6891 deg
Eccentricity:
0005532
Arg of perigee: 195
9834 deg
Mean anomaly: 164
1146 deg
Mean motion: 15
55435315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1708
Checksum: 331
Coasting Arc #16 (Orbit 1723)
---------------------------------------
Vector Time (GMT): 2015/098/18:35:10
197
Vector Time (MET): N/A
Weight (LBS) : 904173
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3699626
41 A = 6773546
87 meter
Y = 1988931
91 meter E =
0006378
Z = 5313718
32 I = 51
96940
XDOT = -3001
561952 Wp = 172
68275
YDOT = -7039
172203 meter/sec RA = 70
06268 deg
ZDOT = 538
729761 TA = 272
16570
MA = 272
23874
Ha = 219
402 n
mi
Hp = 212
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12137881
93 X = -3747404
55
Y = 6525367
16 feet Y = 1947293
53 meter
Z = 17433459
06 Z = 5295629
82
XDOT = -9847
644199 XDOT = -2925
242155
YDOT = -23094
396991 feet/sec YDOT = -7072
310860 meter/sec
ZDOT = 1767
486092 ZDOT = 524
334478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11041579
68 X = 3365473
49
Y = 8408541
16 feet Y = 2562923
35 meter
Z = 17355519
09 Z = 5289962
22
XDOT = -16262
502587 XDOT = -4956
810788
YDOT = 17789
171704 feet/sec YDOT = 5422
139535 meter/sec
ZDOT = 1707
022123 ZDOT = 520
300343
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 15098
82350546
00016717 00000-0 10270-3 0 9159
2 25544 51
6458 70
5547 0005580 198
8489 161
2458 15
55465222 17242
Satellite: ISS
Catalog Number: 25544
Epoch time: 15098
82350546 = yrday
fracday
Element set: 915
Inclination: 51
6458 deg
RA of node: 70
5547 deg
Eccentricity:
0005580
Arg of perigee: 198
8489 deg
Mean anomaly: 161
2458 deg
Mean motion: 15
55465222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1724
Checksum: 335
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