[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 13th 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) : 128 5 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 578)
---------------------------------------
Vector Time (GMT): 2014/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3482143
13 A = 6791569
67 meter
Y = -3406259
36 meter E =
0009984
Z = -4741689
76 I = 51
27708
XDOT = 2812
380469 Wp = 95
81193
YDOT = -6595
915605 meter/sec RA = 275
67535 deg
ZDOT = 2676
841604 TA = 200
80110
MA = 200
84176
Ha = 227
377 n
mi
Hp = 221
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11424354
10 X = -3420760
66
Y = -11175391
60 feet Y = -3444855
71 meter
Z = -15556724
92 Z = -4758456
78
XDOT = 9226
970044 XDOT = 2872
924952
YDOT = -21640
143062 feet/sec YDOT = -6564
127237 meter/sec
ZDOT = 8782
288728 ZDOT = 2690
651110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15858273
76 X = -4833601
84
Y = 1314406
85 feet Y = 400631
21 meter
Z = -15627041
38 Z = -4763122
21
XDOT = -10349
538054 XDOT = -3154
539199
YDOT = -19897
771276 feet/sec YDOT = -6064
840685 meter/sec
ZDOT = 8841
775452 ZDOT = 2694
973158
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 14132
51135136
00016717 00000-0 10270-3 0 9003
2 25544 51
6459 276
4319 0002609 347
6280 12
4806 15
50079427 5793
Satellite: ISS
Catalog Number: 25544
Epoch time: 14132
51135136 = yrday
fracday
Element set: 900
Inclination: 51
6459 deg
RA of node: 276
4319 deg
Eccentricity:
0002609
Arg of perigee: 347
6280 deg
Mean anomaly: 12
4806 deg
Mean motion: 15
50079427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 579
Checksum: 300
Coasting Arc #2 (Orbit 594)
---------------------------------------
Vector Time (GMT): 2014/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3604105
52 A = 6792287
42 meter
Y = 3525727
10 meter E =
0009689
Z = 4547872
08 I = 51
27739
XDOT = -2533
912625 Wp = 51
56997
YDOT = 6552
315898 meter/sec RA = 270
69293 deg
ZDOT = -3061
223184 TA = 69
28050
MA = 69
17668
Ha = 227
403 n
mi
Hp = 221
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11824493
17 X = 3542319
56
Y = 11567346
14 feet Y = 3565684
96 meter
Z = 14920840
15 Z = 4565230
72
XDOT = -8313
361630 XDOT = -2592
122994
YDOT = 21497
099403 feet/sec YDOT = 6523
654653 meter/sec
ZDOT = -10043
383148 ZDOT = -3073
674112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16392938
37 X = 4996567
61
Y = -1647993
86 feet Y = -502308
53 meter
Z = 14993641
80 Z = 4570062
02
XDOT = 11163
718462 XDOT = 3402
701387
YDOT = 18875
204406 feet/sec YDOT = 5753
162303 meter/sec
ZDOT = -10097
115991 ZDOT = -3077
600954
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 14133
54286059
00016717 00000-0 10270-3 0 9019
2 25544 51
6459 271
3201 0002617 352
8145 7
2968 15
50086254 5959
Satellite: ISS
Catalog Number: 25544
Epoch time: 14133
54286059 = yrday
fracday
Element set: 901
Inclination: 51
6459 deg
RA of node: 271
3201 deg
Eccentricity:
0002617
Arg of perigee: 352
8145 deg
Mean anomaly: 7
2968 deg
Mean motion: 15
50086254 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 595
Checksum: 302
Coasting Arc #3 (Orbit 609)
---------------------------------------
Vector Time (GMT): 2014/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3767644
60 A = 6792885
95 meter
Y = -3618755
21 meter E =
0007928
Z = -4349051
35 I = 51
28153
XDOT = 2265
248934 Wp = 92
08202
YDOT = -6462
987891 meter/sec RA = 265
71236 deg
ZDOT = 3420
446861 TA = 212
83031
MA = 212
87959
Ha = 227
397 n
mi
Hp = 220
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12361038
72 X = -3705772
06
Y = -11872556
45 feet Y = -3660541
28 meter
Z = -14268541
17 Z = -4367204
34
XDOT = 7431
919074 XDOT = 2320
735353
YDOT = -21204
028515 feet/sec YDOT = -6437
346335 meter/sec
ZDOT = 11221
938520 ZDOT = 3431
585862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16938226
59 X = -5162771
47
Y = 2161124
39 feet Y = 658710
71 meter
Z = -14344691
12 Z = -4372261
85
XDOT = -11796
370663 XDOT = -3595
533778
YDOT = -17761
254993 feet/sec YDOT = -5413
630522 meter/sec
ZDOT = 11270
108372 ZDOT = 3435
129032
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 14134
50987738
00016717 00000-0 10270-3 0 9029
2 25544 51
6469 266
5293 0002805 353
8559 6
2557 15
50141962 6105
Satellite: ISS
Catalog Number: 25544
Epoch time: 14134
50987738 = yrday
fracday
Element set: 902
Inclination: 51
6469 deg
RA of node: 266
5293 deg
Eccentricity:
0002805
Arg of perigee: 353
8559 deg
Mean anomaly: 6
2557 deg
Mean motion: 15
50141962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 610
Checksum: 318
Coasting Arc #4 (Orbit 625)
---------------------------------------
Vector Time (GMT): 2014/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3932524
88 A = 6793734
65 meter
Y = 3727163
10 meter E =
0011432
Z = 4093422
54 I = 51
28805
XDOT = -2045
303214 Wp = 62
95161
YDOT = 6337
366204 meter/sec RA = 260
73110 deg
ZDOT = -3792
102089 TA = 66
46679
MA = 66
34673
Ha = 227
431 n
mi
Hp = 220
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12901984
51 X = 3870669
67
Y = 12228225
40 feet Y = 3770793
00 meter
Z = 13429863
96 Z = 4112376
59
XDOT = -6710
312381 XDOT = -2097
595865
YDOT = 20791
883870 feet/sec YDOT = 6314
202174 meter/sec
ZDOT = -12441
279821 ZDOT = -3802
164698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17513863
54 X = 5338225
61
Y = -2667001
74 feet Y = -812902
13 meter
Z = 13509390
52 Z = 4117662
23
XDOT = 12204
049723 XDOT = 3719
794356
YDOT = 16681
723666 feet/sec YDOT = 5084
589374 meter/sec
ZDOT = -12484
876701 ZDOT = -3805
390418
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 14135
54134163
00016717 00000-0 10270-3 0 9031
2 25544 51
6472 261
4178 0002782 359
6165
4983 15
50159576 6262
Satellite: ISS
Catalog Number: 25544
Epoch time: 14135
54134163 = yrday
fracday
Element set: 903
Inclination: 51
6472 deg
RA of node: 261
4178 deg
Eccentricity:
0002782
Arg of perigee: 359
6165 deg
Mean anomaly:
4983 deg
Mean motion: 15
50159576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 626
Checksum: 307
Coasting Arc #5 (Orbit 640)
---------------------------------------
Vector Time (GMT): 2014/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4133875
42 A = 6794478
35 meter
Y = -3794758
99 meter E =
0006231
Z = -3835021
70 I = 51
29740
XDOT = 1845
584930 Wp = 77
00900
YDOT = -6177
409946 meter/sec RA = 255
75158 deg
ZDOT = 4130
217113 TA = 236
68738
MA = 236
74706
Ha = 227
432 n
mi
Hp = 220
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13562583
40 X = -4072504
70
Y = -12449996
70 feet Y = -3840643
19 meter
Z = -12582092
21 Z = -3854955
08
XDOT = 6055
068667 XDOT = 1894
461345
YDOT = -20267
092999 feet/sec YDOT = -6156
498478 meter/sec
ZDOT = 13550
581081 ZDOT = 4139
301086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18041113
48 X = -5498931
39
Y = 3369259
45 feet Y = 1026950
28 meter
Z = -12665758
80 Z = -3860523
28
XDOT = -12434
836305 XDOT = -3790
138106
YDOT = -15582
734412 feet/sec YDOT = -4749
617449 meter/sec
ZDOT = 13590
011775 ZDOT = 4142
235589
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 14136
50831664
00016717 00000-0 10270-3 0 9049
2 25544 51
6477 256
6267 0003018
0389
0761 15
50202985 6410
Satellite: ISS
Catalog Number: 25544
Epoch time: 14136
50831664 = yrday
fracday
Element set: 904
Inclination: 51
6477 deg
RA of node: 256
6267 deg
Eccentricity:
0003018
Arg of perigee:
0389 deg
Mean anomaly:
0761 deg
Mean motion: 15
50202985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 641
Checksum: 283
Coasting Arc #6 (Orbit 656)
---------------------------------------
Vector Time (GMT): 2014/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4332214
98 A = 6795389
49 meter
Y = 3873235
02 meter E =
0012908
Z = 3514878
25 I = 51
30920
XDOT = -1706
899482 Wp = 74
75754
YDOT = 5983
721851 meter/sec RA = 250
77248 deg
ZDOT = -4472
845883 TA = 63
70856
MA = 63
57600
Ha = 227
480 n
mi
Hp = 220
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14213303
75 X = 4271507
24
Y = 12707463
99 feet Y = 3921340
89 meter
Z = 11531752
80 Z = 3535776
69
XDOT = -5600
063916 XDOT = -1751
956032
YDOT = 19631
633368 feet/sec YDOT = 5964
382666 meter/sec
ZDOT = -14674
691218 ZDOT = -4481
246791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18573157
76 X = 5661098
49
Y = -4062509
94 feet Y = -1238253
03 meter
Z = 11619500
46 Z = 3541623
74
XDOT = 12426
780740 XDOT = 3787
682770
YDOT = 14577
152946 feet/sec YDOT = 4443
116218 meter/sec
ZDOT = -14711
198461 ZDOT = -4483
973291
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 14137
53973635
00016717 00000-0 10270-3 0 9059
2 25544 51
6477 251
5156 0002971 6
6301 353
4889 15
50231359 6574
Satellite: ISS
Catalog Number: 25544
Epoch time: 14137
53973635 = yrday
fracday
Element set: 905
Inclination: 51
6477 deg
RA of node: 251
5156 deg
Eccentricity:
0002971
Arg of perigee: 6
6301 deg
Mean anomaly: 353
4889 deg
Mean motion: 15
50231359 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 657
Checksum: 317
Coasting Arc #7 (Orbit 671)
---------------------------------------
Vector Time (GMT): 2014/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4557603
45 A = 6796200
70 meter
Y = -3898692
93 meter E =
0006282
Z = -3196097
64 I = 51
32348
XDOT = 1595
929275 Wp = 51
26794
YDOT = -5771
407572 meter/sec RA = 245
79460 deg
ZDOT = 4774
577949 TA = 271
69005
MA = 271
76201
Ha = 227
484 n
mi
Hp = 220
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14952767
21 X = -4498142
90
Y = -12790987
30 feet Y = -3949326
25 meter
Z = -10485884
64 Z = -3218093
92
XDOT = 5235
988434 XDOT = 1637
154294
YDOT = -18935
064213 feet/sec YDOT = -5753
330761 meter/sec
ZDOT = 15664
625817 ZDOT = 4782
430468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18994101
10 X = -5789402
02
Y = 4946955
26 feet Y = 1507831
96 meter
Z = -10578286
12 Z = -3224261
61
XDOT = -12272
855237 XDOT = -3740
766276
YDOT = -13624
043620 feet/sec YDOT = -4152
608495 meter/sec
ZDOT = 15698
774487 ZDOT = 4784
986464
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 14138
50667010
00016717 00000-0 10270-3 0 9065
2 25544 51
6479 246
7240 0003228 6
5629 353
5563 15
50262782 6725
Satellite: ISS
Catalog Number: 25544
Epoch time: 14138
50667010 = yrday
fracday
Element set: 906
Inclination: 51
6479 deg
RA of node: 246
7240 deg
Eccentricity:
0003228
Arg of perigee: 6
5629 deg
Mean anomaly: 353
5563 deg
Mean motion: 15
50262782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 672
Checksum: 304
Coasting Arc #8 (Orbit 687)
---------------------------------------
Vector Time (GMT): 2014/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4772288
79 A = 6797072
70 meter
Y = 3931430
83 meter E =
0013926
Z = 2812043
83 I = 51
33978
XDOT = -1556
266804 Wp = 86
58624
YDOT = 5531
511933 meter/sec RA = 240
81809 deg
ZDOT = -5069
695694 TA = 61
39684
MA = 61
25681
Ha = 227
543 n
mi
Hp = 220
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15657115
44 X = 4714311
87
Y = 12898395
10 feet Y = 3984473
26 meter
Z = 9225865
58 Z = 2835086
51
XDOT = -5105
862218 XDOT = -1593
378682
YDOT = 18148
005030 feet/sec YDOT = 5513
901612 meter/sec
ZDOT = -16632
859888 ZDOT = -5077
345610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19391052
22 X = 5910392
72
Y = -5805578
81 feet Y = -1769540
42 meter
Z = 9322703
69 Z = 2841560
09
XDOT = 11887
679711 XDOT = 3623
364776
YDOT = 12825
061492 feet/sec YDOT = 3909
078743 meter/sec
ZDOT = -16666
107010 ZDOT = -5079
829417
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 14139
53804605
00016717 00000-0 10270-3 0 9073
2 25544 51
6473 241
6126 0003173 13
7375 346
3862 15
50301286 6885
Satellite: ISS
Catalog Number: 25544
Epoch time: 14139
53804605 = yrday
fracday
Element set: 907
Inclination: 51
6473 deg
RA of node: 241
6126 deg
Eccentricity:
0003173
Arg of perigee: 13
7375 deg
Mean anomaly: 346
3862 deg
Mean motion: 15
50301286 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 688
Checksum: 302
Coasting Arc #9 (Orbit 702)
---------------------------------------
Vector Time (GMT): 2014/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5001092
86 A = 6797848
93 meter
Y = -3902871
50 meter E =
0008440
Z = -2435433
71 I = 51
35877
XDOT = 1547
603557 Wp = 35
17600
YDOT = -5291
769374 meter/sec RA = 235
84255 deg
ZDOT = 5318
288676 TA = 297
51019
MA = 297
59595
Ha = 227
548 n
mi
Hp = 220
230
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16407784
96 X = -4945247
77
Y = -12804696
52 feet Y = -3958484
55 meter
Z = -7990268
09 Z = -2459592
98
XDOT = 5077
439491 XDOT = 1580
827661
YDOT = -17361
448076 feet/sec YDOT = -5274
277592 meter/sec
ZDOT = 17448
453660 ZDOT = 5325
887165
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19619803
53 X = -5980116
12
Y = 6826808
99 feet Y = 2080811
38 meter
Z = -8091849
79 Z = -2466395
82
XDOT = -11412
950064 XDOT = -3478
667180
YDOT = -12140
656849 feet/sec YDOT = -3700
472208 meter/sec
ZDOT = 17481
438769 ZDOT = 5328
342537
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 14140
50493942
00016717 00000-0 10270-3 0 9081
2 25544 51
6476 236
8203 0003424 13
3090 346
8151 15
50320790 7034
Satellite: ISS
Catalog Number: 25544
Epoch time: 14140
50493942 = yrday
fracday
Element set: 908
Inclination: 51
6476 deg
RA of node: 236
8203 deg
Eccentricity:
0003424
Arg of perigee: 13
3090 deg
Mean anomaly: 346
8151 deg
Mean motion: 15
50320790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 703
Checksum: 279
Coasting Arc #10 (Orbit 718)
---------------------------------------
Vector Time (GMT): 2014/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5208624
49 A = 6798548
43 meter
Y = 3880100
95 meter E =
0014244
Z = 1992332
11 I = 51
37904
XDOT = -1616
308037 Wp = 97
93798
YDOT = 5034
064962 meter/sec RA = 230
86909 deg
ZDOT = -5546
143285 TA = 60
01578
MA = 59
87448
Ha = 227
606 n
mi
Hp = 220
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17088663
02 X = 5155171
04
Y = 12729989
99 feet Y = 3938048
18 meter
Z = 6536522
66 Z = 2017505
31
XDOT = -5302
847892 XDOT = -1645
538447
YDOT = 16515
961161 feet/sec YDOT = 5015
827132 meter/sec
ZDOT = -18196
008153 ZDOT = -5554
065939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19799164
00 X = 6034785
19
Y = -7789264
72 feet Y = -2374167
89 meter
Z = 6642412
01 Z = 2024607
18
XDOT = 10739
395185 XDOT = 3273
367652
YDOT = 11663
095755 feet/sec YDOT = 3554
911586 meter/sec
ZDOT = -18230
318474 ZDOT = -5556
601071
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 14141
53627285
00016717 00000-0 10270-3 0 9095
2 25544 51
6469 231
7085 0003383 20
3488 339
7797 15
50370436 7197
Satellite: ISS
Catalog Number: 25544
Epoch time: 14141
53627285 = yrday
fracday
Element set: 909
Inclination: 51
6469 deg
RA of node: 231
7085 deg
Eccentricity:
0003383
Arg of perigee: 20
3488 deg
Mean anomaly: 339
7797 deg
Mean motion: 15
50370436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 719
Checksum: 326
Coasting Arc #11 (Orbit 733)
---------------------------------------
Vector Time (GMT): 2014/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5415257
60 A = 6799176
58 meter
Y = -3793127
06 meter E =
0011470
Z = -1564434
45 I = 51
40197
XDOT = 1714
432877 Wp = 32
64719
YDOT = -4796
478713 meter/sec RA = 225
89674 deg
ZDOT = 5724
189121 TA = 310
21771
MA = 310
31802
Ha = 227
622 n
mi
Hp = 219
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17766593
16 X = -5364839
93
Y = -12444642
59 feet Y = -3853402
01 meter
Z = -5132658
96 Z = -1590618
86
XDOT = 5624
779779 XDOT = 1740
134274
YDOT = -15736
478716 feet/sec YDOT = -4777
163270 meter/sec
ZDOT = 18780
148036 ZDOT = 5732
579963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19768510
53 X = -6025442
01
Y = 8864740
92 feet Y = 2701973
03 meter
Z = -5242853
18 Z = -1598021
65
XDOT = -10052
174880 XDOT = -3063
902903
YDOT = -11343
290069 feet/sec YDOT = -3457
434813 meter/sec
ZDOT = 18816
398179 ZDOT = 5735
238165
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 14142
50312719
00016717 00000-0 10270-3 0 9108
2 25544 51
6474 226
9158 0003613 20
0632 340
0660 15
50376455 7342
Satellite: ISS
Catalog Number: 25544
Epoch time: 14142
50312719 = yrday
fracday
Element set: 910
Inclination: 51
6474 deg
RA of node: 226
9158 deg
Eccentricity:
0003613
Arg of perigee: 20
0632 deg
Mean anomaly: 340
0660 deg
Mean motion: 15
50376455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 734
Checksum: 274
Coasting Arc #12 (Orbit 749)
---------------------------------------
Vector Time (GMT): 2014/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5588324
00 A = 6799557
63 meter
Y = 3713884
11 meter E =
0013673
Z = 1071851
33 I = 51
42546
XDOT = -1889
749594 Wp = 108
09497
YDOT = 4552
908956 meter/sec RA = 220
92683 deg
ZDOT = -5865
249526 TA = 60
26460
MA = 60
12862
Ha = 227
665 n
mi
Hp = 219
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18334396
32 X = 5541172
39
Y = 12184659
15 feet Y = 3776112
67 meter
Z = 3516572
61 Z = 1098884
52
XDOT = -6199
965861 XDOT = -1912
028969
YDOT = 14937
365342 feet/sec YDOT = 4531
652150 meter/sec
ZDOT = -19242
944638 ZDOT = -5874
483765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19674608
09 X = 5996820
55
Y = -9834246
94 feet Y = -2997478
47 meter
Z = 3630382
00 Z = 1106540
43
XDOT = 9221
924469 XDOT = 2810
842578
YDOT = 11263
621391 feet/sec YDOT = 3433
151800 meter/sec
ZDOT = -19282
723891 ZDOT = -5877
374242
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 14143
53441958
00016717 00000-0 10270-3 0 9111
2 25544 51
6467 221
8036 0003603 26
4327 333
7007 15
50439628 7507
Satellite: ISS
Catalog Number: 25544
Epoch time: 14143
53441958 = yrday
fracday
Element set: 911
Inclination: 51
6467 deg
RA of node: 221
8036 deg
Eccentricity:
0003603
Arg of perigee: 26
4327 deg
Mean anomaly: 333
7007 deg
Mean motion: 15
50439628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 750
Checksum: 292
Coasting Arc #13 (Orbit 764)
---------------------------------------
Vector Time (GMT): 2014/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5745252
42 A = 6799925
98 meter
Y = -3573638
40 meter E =
0014407
Z = -603534
38 I = 51
45090
XDOT = 2088
110567 Wp = 37
45322
YDOT = -4348
301882 meter/sec RA = 215
95821 deg
ZDOT = 5955
857417 TA = 316
02357
MA = 316
13811
Ha = 227
713 n
mi
Hp = 219
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18849253
36 X = -5701932
36
Y = -11724535
44 feet Y = -3637643
27 meter
Z = -1980099
66 Z = -631339
34
XDOT = 6850
756452 XDOT = 2107
646986
YDOT = -14266
082291 feet/sec YDOT = -4324
842275 meter/sec
ZDOT = 19540
214624 ZDOT = 5966
048613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19352072
64 X = -5898511
74
Y = 10852598
03 feet Y = 3307871
88 meter
Z = -2097207
35 Z = -639228
80
XDOT = -8463
662205 XDOT = -2579
724240
YDOT = -11359
280021 feet/sec YDOT = -3462
308550 meter/sec
ZDOT = 19584
012460 ZDOT = 5969
206998
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 14144
50123633
00016717 00000-0 10270-3 0 9127
2 25544 51
6470 217
0108 0003814 27
0432 333
0917 15
50430840 7652
Satellite: ISS
Catalog Number: 25544
Epoch time: 14144
50123633 = yrday
fracday
Element set: 912
Inclination: 51
6470 deg
RA of node: 217
0108 deg
Eccentricity:
0003814
Arg of perigee: 27
0432 deg
Mean anomaly: 333
0917 deg
Mean motion: 15
50430840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 765
Checksum: 263
Coasting Arc #14 (Orbit 780)
---------------------------------------
Vector Time (GMT): 2014/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5856374
12 A = 6799868
57 meter
Y = 3447457
37 meter E =
0012169
Z = 75675
82 I = 51
47666
XDOT = -2355
872626 Wp = 115
74001
YDOT = 4150
014455 meter/sec RA = 210
99189 deg
ZDOT = -5992
501377 TA = 63
44448
MA = 63
31980
Ha = 227
727 n
mi
Hp = 219
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19213825
86 X = 5817020
99
Y = 11310555
66 feet Y = 3512727
06 meter
Z = 248280
24 Z = 104030
36
XDOT = -7729
240899 XDOT = -2372
993776
YDOT = 13615
532989 feet/sec YDOT = 4123
574162 meter/sec
ZDOT = -19660
437590 ZDOT = -6003
987445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18971572
11 X = 5782535
18
Y = -11709211
45 feet Y = -3568967
65 meter
Z = 367744
15 Z = 112088
42
XDOT = 7634
414288 XDOT = 2326
969475
YDOT = 11698
401940 feet/sec YDOT = 3565
672911 meter/sec
ZDOT = -19709
687853 ZDOT = -6007
512858
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 14145
53248890
00016717 00000-0 10270-3 0 9135
2 25544 51
6465 211
8983 0003830 32
6554 327
4833 15
50507225 7818
Satellite: ISS
Catalog Number: 25544
Epoch time: 14145
53248890 = yrday
fracday
Element set: 913
Inclination: 51
6465 deg
RA of node: 211
8983 deg
Eccentricity:
0003830
Arg of perigee: 32
6554 deg
Mean anomaly: 327
4833 deg
Mean motion: 15
50507225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 781
Checksum: 307
Coasting Arc #15 (Orbit 796)
---------------------------------------
Vector Time (GMT): 2014/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5937953
23 A = 6799875
46 meter
Y = -3269412
35 meter E =
0016681
Z = 417835
00 I = 51
50319
XDOT = 2636
262403 Wp = 46
12102
YDOT = -4006
079480 meter/sec RA = 206
02689 deg
ZDOT = 5980
535375 TA = 318
38770
MA = 318
51452
Ha = 227
820 n
mi
Hp = 219
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19481473
84 X = -5902982
34
Y = -10726418
46 feet Y = -3335618
85 meter
Z = 1370849
75 Z = 389073
44
XDOT = 8649
154866 XDOT = 2651
811309
YDOT = -13143
305381 feet/sec YDOT = -3976
512588 meter/sec
ZDOT = 19621
179051 ZDOT = 5993
379685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18371486
04 X = -5599628
95
Y = 12545518
98 feet Y = 3823874
18 meter
Z = 1249623
63 Z = 380885
28
XDOT = -6960
345835 XDOT = -2121
513410
YDOT = -12201
941979 feet/sec YDOT = -3719
151915 meter/sec
ZDOT = 19676
161168 ZDOT = 5997
293924
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 14146
56372234
00016717 00000-0 10270-3 0 9140
2 25544 51
6462 206
7857 0004034 34
7805 325
3609 15
50488129 7973
Satellite: ISS
Catalog Number: 25544
Epoch time: 14146
56372234 = yrday
fracday
Element set: 914
Inclination: 51
6462 deg
RA of node: 206
7857 deg
Eccentricity:
0004034
Arg of perigee: 34
7805 deg
Mean anomaly: 325
3609 deg
Mean motion: 15
50488129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 797
Checksum: 317
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