[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 8th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17760 45 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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
314/00:30:30
000 0
0 0
0 0
0
N/A 0
0 0
0 226
9
000/00:00:00
000 0
0 0
0 218
8
317/02:00:11
832 0
5 1
1 1
1
N/A 0
9 -0
1 227
0
000/00:02:23
664 -0
3 -0
0 219
0
Coasting Arc #1 (Orbit 3357)
---------------------------------------
Vector Time (GMT): 2014/311/13:39:19
087
Vector Time (MET): N/A
Weight (LBS) : 930906
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3979797
19 A = 6794451
26 meter
Y = 4575440
67 meter E =
0014632
Z = 3045821
22 I = 51
99305
XDOT = -2346
475911 Wp = 67
08662
YDOT = -5354
157247 meter/sec RA = 107
90626 deg
ZDOT = 4963
660651 TA = 327
63813
MA = 327
72779
Ha = 226
640 n
mi
Hp = 219
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13057077
39 X = -4045461
07
Y = 15011288
29 feet Y = 4530568
90 meter
Z = 9992851
77 Z = 3026327
83
XDOT = -7698
411780 XDOT = -2310
542615
YDOT = -17566
132700 feet/sec YDOT = -5380
196075 meter/sec
ZDOT = 16284
975890 ZDOT = 4952
348847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9825683
04 X = -2994868
19
Y = -17347953
80 feet Y = -5287656
32 meter
Z = 9908964
84 Z = 3020252
48
XDOT = 17891
457038 XDOT = 5453
316105
YDOT = -833
484926 feet/sec YDOT = -254
046206 meter/sec
ZDOT = 16237
655201 ZDOT = 4949
237305
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 14311
62722186
00016717 00000-0 10270-3 0 9001
2 25544 51
6436 108
5157 0004246 6
3807 353
7397 15
51045624 33583
Satellite: ISS
Catalog Number: 25544
Epoch time: 14311
62722186 = yrday
fracday
Element set: 900
Inclination: 51
6436 deg
RA of node: 108
5157 deg
Eccentricity:
0004246
Arg of perigee: 6
3807 deg
Mean anomaly: 353
7397 deg
Mean motion: 15
51045624 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3358
Checksum: 298
Coasting Arc #2 (Orbit 3372)
---------------------------------------
Vector Time (GMT): 2014/312/13:39:19
087
Vector Time (MET): N/A
Weight (LBS) : 930906
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3870287
07 A = 6792927
65 meter
Y = -4276113
58 meter E =
0007728
Z = -3598633
89 I = 51
99706
XDOT = 2248
345878 Wp = 50
65821
YDOT = 5793
884846 meter/sec RA = 102
96948 deg
ZDOT = -4468
218100 TA = 171
54722
MA = 171
53420
Ha = 226
663 n
mi
Hp = 219
181
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12697792
22 X = 3935297
36
Y = -14029244
02 feet Y = -4232470
01 meter
Z = -11806541
64 Z = -3579674
21
XDOT = 7376
462853 XDOT = 2205
095923
YDOT = 19008
808549 feet/sec YDOT = 5818
785498 meter/sec
ZDOT = -14659
508203 ZDOT = -4457
400710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9300033
07 X = 2834650
08
Y = 16537310
49 feet Y = 5040572
24 meter
Z = -11724964
27 Z = -3573769
11
XDOT = -19186
133496 XDOT = -5847
933490
YDOT = 431
887390 feet/sec YDOT = 131
639277 meter/sec
ZDOT = -14614
380845 ZDOT = -4454
463282
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 14312
59368042
00016717 00000-0 10270-3 0 9016
2 25544 51
6439 103
7203 0004392 9
8677 350
2559 15
51042721 33734
Satellite: ISS
Catalog Number: 25544
Epoch time: 14312
59368042 = yrday
fracday
Element set: 901
Inclination: 51
6439 deg
RA of node: 103
7203 deg
Eccentricity:
0004392
Arg of perigee: 9
8677 deg
Mean anomaly: 350
2559 deg
Mean motion: 15
51042721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3373
Checksum: 294
Coasting Arc #3 (Orbit 3388)
---------------------------------------
Vector Time (GMT): 2014/313/13:39:19
087
Vector Time (MET): N/A
Weight (LBS) : 930906
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3764537
54 A = 6791181
94 meter
Y = 3908082
49 meter E =
0011655
Z = 4072150
21 I = 51
99923
XDOT = -2210
545269 Wp = 79
81856
YDOT = -6214
178274 meter/sec RA = 98
03130 deg
ZDOT = 3912
764903 TA = 329
79646
MA = 329
86360
Ha = 226
745 n
mi
Hp = 218
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12350844
96 X = -3827740
47
Y = 12821792
96 feet Y = 3865631
54 meter
Z = 13360072
87 Z = 4053708
76
XDOT = -7252
445109 XDOT = -2159
899962
YDOT = -20387
723996 feet/sec YDOT = -6238
614911 meter/sec
ZDOT = 12837
155192 ZDOT = 3902
149067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8531282
64 X = -2600334
95
Y = -15693058
83 feet Y = -4783244
33 meter
Z = 13280753
52 Z = 4047973
67
XDOT = 20501
502715 XDOT = 6248
858027
YDOT = -297
953863 feet/sec YDOT = -90
816338 meter/sec
ZDOT = 12792
970254 ZDOT = 3899
297333
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 14313
62454612
00016717 00000-0 10270-3 0 9021
2 25544 51
6451 98
6050 0004422 13
1657 346
9609 15
51110793 33890
Satellite: ISS
Catalog Number: 25544
Epoch time: 14313
62454612 = yrday
fracday
Element set: 902
Inclination: 51
6451 deg
RA of node: 98
6050 deg
Eccentricity:
0004422
Arg of perigee: 13
1657 deg
Mean anomaly: 346
9609 deg
Mean motion: 15
51110793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3389
Checksum: 295
Coasting Arc #4 (Orbit 3395)
---------------------------------------
Vector Time (GMT): 2014/314/00:30:30
000
Vector Time (MET): N/A
Weight (LBS) : 915473
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3840225
24 A = 6789769
60 meter
Y = 3384473
21 meter E =
0009932
Z = 4451474
68 I = 51
99497
XDOT = -1953
339186 Wp = 80
80989
YDOT = -6619
714993 meter/sec RA = 95
80063 deg
ZDOT = 3343
081405 TA = 335
57731
MA = 335
62434
Ha = 226
872 n
mi
Hp = 218
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12599164
17 X = -3899410
06
Y = 11103914
73 feet Y = 3341198
32 meter
Z = 14604575
73 Z = 4432675
33
XDOT = -6408
593129 XDOT = -1895
410763
YDOT = -21718
225044 feet/sec YDOT = -6641
234663 meter/sec
ZDOT = 10968
114846 ZDOT = 3333
732748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2078025
55 X = 633382
19
Y = 16735294
51 feet Y = 5100917
77 meter
Z = 14523815
61 Z = 4426859
00
XDOT = -20393
375869 XDOT = -6215
900965
YDOT = -6966
624010 feet/sec YDOT = -2123
426998 meter/sec
ZDOT = 10929
409094 ZDOT = 3331
283892
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 14314
07554355
00016717 00000-0 10270-3 0 9037
2 25544 51
6435 96
3710 0004923 13
0863 347
0415 15
51128042 33965
Satellite: ISS
Catalog Number: 25544
Epoch time: 14314
07554355 = yrday
fracday
Element set: 903
Inclination: 51
6435 deg
RA of node: 96
3710 deg
Eccentricity:
0004923
Arg of perigee: 13
0863 deg
Mean anomaly: 347
0415 deg
Mean motion: 15
51128042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3396
Checksum: 286
Coasting Arc #5 (Orbit 3410)
---------------------------------------
Vector Time (GMT): 2014/315/00:30:30
000
Vector Time (MET): N/A
Weight (LBS) : 915473
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3808581
38 A = 6788388
91 meter
Y = -2916919
45 meter E =
0014870
Z = -4817054
77 I = 51
99301
XDOT = 1956
516800 Wp = 55
19123
YDOT = 6911
587817 meter/sec RA = 90
85865 deg
ZDOT = -2635
852725 TA = 188
87008
MA = 188
89638
Ha = 226
891 n
mi
Hp = 218
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12495345
72 X = 3864316
09
Y = -9569945
69 feet Y = -2874017
70 meter
Z = -15803985
47 Z = -4798417
58
XDOT = 6419
018374 XDOT = 1891
888748
YDOT = 22675
813049 feet/sec YDOT = 6933
105548 meter/sec
ZDOT = -8647
810776 ZDOT = -2626
504932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1133580
04 X = -345515
20
Y = -15778297
98 feet Y = -4809225
22 meter
Z = -15723987
76 Z = -4792671
47
XDOT = 21377
039721 XDOT = 6515
721707
YDOT = 7051
868091 feet/sec YDOT = 2149
409394 meter/sec
ZDOT = -8609
170522 ZDOT = -2624
075175
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 14315
04195377
00016717 00000-0 10270-3 0 9041
2 25544 51
6439 91
5747 0005150 17
2258 342
9067 15
51129458 34110
Satellite: ISS
Catalog Number: 25544
Epoch time: 14315
04195377 = yrday
fracday
Element set: 904
Inclination: 51
6439 deg
RA of node: 91
5747 deg
Eccentricity:
0005150
Arg of perigee: 17
2258 deg
Mean anomaly: 342
9067 deg
Mean motion: 15
51129458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3411
Checksum: 305
Coasting Arc #6 (Orbit 3426)
---------------------------------------
Vector Time (GMT): 2014/316/00:30:30
000
Vector Time (MET): N/A
Weight (LBS) : 915473
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3808549
01 A = 6787056
92 meter
Y = 2389774
66 meter E =
0006492
Z = 5078224
67 I = 51
98938
XDOT = -1985
832899 Wp = 74
89868
YDOT = -7163
920015 meter/sec RA = 85
91639 deg
ZDOT = 1881
606320 TA = 356
95438
MA = 356
95833
Ha = 226
956 n
mi
Hp = 218
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12495239
55 X = -3859657
71
Y = 7840468
04 feet Y = 2346899
17 meter
Z = 16660842
10 Z = 5059598
89
XDOT = -6515
199800 XDOT = -1914
717058
YDOT = -23503
674589 feet/sec YDOT = -7185
729274 meter/sec
ZDOT = 6173
249080 ZDOT = 1872
131944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -62406
89 X = -19021
62
Y = 14840986
70 feet Y = 4523532
74 meter
Z = 16580977
93 Z = 5053882
07
XDOT = -22305
992039 XDOT = -6798
866374
YDOT = -6948
400340 feet/sec YDOT = -2117
872424 meter/sec
ZDOT = 6134
123745 ZDOT = 1869
680917
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 14316
07276690
00016717 00000-0 10270-3 0 9054
2 25544 51
6445 86
4598 0005110 19
2012 340
9331 15
51193787 34275
Satellite: ISS
Catalog Number: 25544
Epoch time: 14316
07276690 = yrday
fracday
Element set: 905
Inclination: 51
6445 deg
RA of node: 86
4598 deg
Eccentricity:
0005110
Arg of perigee: 19
2012 deg
Mean anomaly: 340
9331 deg
Mean motion: 15
51193787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3427
Checksum: 303
Coasting Arc #7 (Orbit 3441)
---------------------------------------
Vector Time (GMT): 2014/317/00:30:30
000
Vector Time (MET): N/A
Weight (LBS) : 915473
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3877480
28 A = 6786300
33 meter
Y = -1846933
44 meter E =
0017604
Z = -5269353
28 I = 51
98374
XDOT = 2011
715529 Wp = 66
88081
YDOT = 7302
817033 meter/sec RA = 80
97117 deg
ZDOT = -1075
479423 TA = 192
81865
MA = 192
86346
Ha = 226
956 n
mi
Hp = 218
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12721392
01 X = 3923442
09
Y = -6059492
93 feet Y = -1803315
96 meter
Z = -17287904
45 Z = -5250405
14
XDOT = 6600
116565 XDOT = 1935
128616
YDOT = 23959
373467 feet/sec YDOT = 7324
885117 meter/sec
ZDOT = -3528
475796 ZDOT = -1065
892696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1450254
23 X = 442037
49
Y = -14115495
28 feet Y = -4302402
96 meter
Z = -17206756
38 Z = -5244619
34
XDOT = 22900
519355 XDOT = 6980
078299
YDOT = 6621
330524 feet/sec YDOT = 2018
181544 meter/sec
ZDOT = -3488
905862 ZDOT = -1063
418507
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 14317
03913632
00016717 00000-0 10270-3 0 9066
2 25544 51
6446 81
6632 0005289 23
2634 336
8756 15
51191695 34422
Satellite: ISS
Catalog Number: 25544
Epoch time: 14317
03913632 = yrday
fracday
Element set: 906
Inclination: 51
6446 deg
RA of node: 81
6632 deg
Eccentricity:
0005289
Arg of perigee: 23
2634 deg
Mean anomaly: 336
8756 deg
Mean motion: 15
51191695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3442
Checksum: 312
Coasting Arc #8 (Orbit 3442)
---------------------------------------
Vector Time (GMT): 2014/317/02:01:23
664
Vector Time (MET): N/A
Weight (LBS) : 915369
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3605715
51 A = 6787551
61 meter
Y = -2672173
87 meter E =
0016076
Z = -5106351
37 I = 51
98691
XDOT = 2585
301987 Wp = 61
74674
YDOT = 6967
924902 meter/sec RA = 80
66529 deg
ZDOT = -1817
758639 TA = 190
68560
MA = 190
71980
Ha = 226
959 n
mi
Hp = 219
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11829775
30 X = 3660133
73
Y = -8766974
63 feet Y = -2631548
16 meter
Z = -16753121
29 Z = -5088702
90
XDOT = 8481
961900 XDOT = 2516
023085
YDOT = 22860
646004 feet/sec YDOT = 6996
448061 meter/sec
ZDOT = -5963
775062 ZDOT = -1805
367728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6938520
34 X = -2114861
00
Y = -13084069
14 feet Y = -3988024
27 meter
Z = -16677367
03 Z = -5083261
47
XDOT = 22902
338045 XDOT = 6980
632636
YDOT = -4596
544176 feet/sec YDOT = -1401
026665 meter/sec
ZDOT = -5912
185241 ZDOT = -1802
034061
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 14317
10356116
00016717 00000-0 10270-3 0 9073
2 25544 51
6457 81
3437 0004721 17
0233 343
1075 15
51003222 34434
Satellite: ISS
Catalog Number: 25544
Epoch time: 14317
10356116 = yrday
fracday
Element set: 907
Inclination: 51
6457 deg
RA of node: 81
3437 deg
Eccentricity:
0004721
Arg of perigee: 17
0233 deg
Mean anomaly: 343
1075 deg
Mean motion: 15
51003222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3443
Checksum: 261
Coasting Arc #9 (Orbit 3458)
---------------------------------------
Vector Time (GMT): 2014/318/02:01:23
664
Vector Time (MET): N/A
Weight (LBS) : 915369
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3686972
99 A = 6786696
13 meter
Y = 2183498
02 meter E =
0005236
Z = 5258493
68 I = 51
97831
XDOT = -2675
752070 Wp = 62
49161
YDOT = -7104
581518 meter/sec RA = 75
72206 deg
ZDOT = 1075
496467 TA = 17
26094
MA = 17
24314
Ha = 227
051 n
mi
Hp = 218
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12096368
06 X = -3736659
74
Y = 7163707
41 feet Y = 2141990
15 meter
Z = 17252275
86 Z = 5240461
94
XDOT = -8778
714139 XDOT = -2601
332600
YDOT = -23308
994482 feet/sec YDOT = -7134
087395 meter/sec
ZDOT = 3528
531715 ZDOT = 1062
678725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5537965
90 X = 1687972
01
Y = 13024330
36 feet Y = 3969815
89 meter
Z = 17174970
12 Z = 5234930
89
XDOT = -23296
392010 XDOT = -7100
740285
YDOT = 5329
708175 feet/sec YDOT = 1624
495052 meter/sec
ZDOT = 3475
155274 ZDOT = 1059
227328
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 14318
13446719
00016717 00000-0 10270-3 0 9087
2 25544 51
6454 76
2287 0004680 19
1058 341
0268 15
51048230 34595
Satellite: ISS
Catalog Number: 25544
Epoch time: 14318
13446719 = yrday
fracday
Element set: 908
Inclination: 51
6454 deg
RA of node: 76
2287 deg
Eccentricity:
0004680
Arg of perigee: 19
1058 deg
Mean anomaly: 341
0268 deg
Mean motion: 15
51048230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3459
Checksum: 306
Coasting Arc #10 (Orbit 3473)
---------------------------------------
Vector Time (GMT): 2014/319/02:01:23
664
Vector Time (MET): N/A
Weight (LBS) : 915369
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3835005
46 A = 6786314
29 meter
Y = -1705003
11 meter E =
0017446
Z = -5347501
55 I = 51
96928
XDOT = 2741
296669 Wp = 73
04410
YDOT = 7136
493557 meter/sec RA = 70
77723 deg
ZDOT = -305
343671 TA = 194
02740
MA = 194
07592
Ha = 227
017 n
mi
Hp = 218
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12582038
91 X = 3879762
97
Y = -5593842
22 feet Y = -1661867
45 meter
Z = -17544296
41 Z = -5328762
62
XDOT = 8993
755475 XDOT = 2662
774279
YDOT = 23413
692772 feet/sec YDOT = 7166
709463 meter/sec
ZDOT = -1001
783696 ZDOT = -292
217539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4146809
67 X = -1263947
59
Y = -13236757
31 feet Y = -4034563
63 meter
Z = -17464058
40 Z = -5323045
00
XDOT = 23305
137517 XDOT = 7103
405915
YDOT = -6033
539124 feet/sec YDOT = -1839
022725 meter/sec
ZDOT = -947
107745 ZDOT = -288
678441
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 14319
10092320
00016717 00000-0 10270-3 0 9091
2 25544 51
6462 71
4331 0004851 23
1715 336
9654 15
51067282 34743
Satellite: ISS
Catalog Number: 25544
Epoch time: 14319
10092320 = yrday
fracday
Element set: 909
Inclination: 51
6462 deg
RA of node: 71
4331 deg
Eccentricity:
0004851
Arg of perigee: 23
1715 deg
Mean anomaly: 336
9654 deg
Mean motion: 15
51067282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3474
Checksum: 288
Coasting Arc #11 (Orbit 3489)
---------------------------------------
Vector Time (GMT): 2014/320/02:01:23
664
Vector Time (MET): N/A
Weight (LBS) : 915369
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4028022
28 A = 6786195
91 meter
Y = 1199826
08 meter E =
0007111
Z = 5324449
69 I = 51
95818
XDOT = -2778
888420 Wp = 40
28413
YDOT = -7129
038865 meter/sec RA = 65
83117 deg
ZDOT = -490
145888 TA = 54
40491
MA = 54
33867
Ha = 227
090 n
mi
Hp = 218
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13215296
19 X = -4067004
50
Y = 3936437
26 feet Y = 1154564
31 meter
Z = 17468666
95 Z = 5304787
10
XDOT = -9117
087991 XDOT = -2696
582305
YDOT = -23389
235122 feet/sec YDOT = -7159
654011 meter/sec
ZDOT = -1608
090183 ZDOT = -503
445421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2664200
94 X = 812048
45
Y = 13637166
19 feet Y = 4156608
25 meter
Z = 17384580
76 Z = 5298820
22
XDOT = -23149
319955 XDOT = -7055
912722
YDOT = 6666
868127 feet/sec YDOT = 2032
061405 meter/sec
ZDOT = -1663
495905 ZDOT = -507
033552
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 14320
13178590
00016717 00000-0 10270-3 0 9102
2 25544 51
6460 66
3175 0004848 25
0312 335
1074 15
51122434 34906
Satellite: ISS
Catalog Number: 25544
Epoch time: 14320
13178590 = yrday
fracday
Element set: 910
Inclination: 51
6460 deg
RA of node: 66
3175 deg
Eccentricity:
0004848
Arg of perigee: 25
0312 deg
Mean anomaly: 335
1074 deg
Mean motion: 15
51122434 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3490
Checksum: 272
Coasting Arc #12 (Orbit 3504)
---------------------------------------
Vector Time (GMT): 2014/321/02:01:23
664
Vector Time (MET): N/A
Weight (LBS) : 915369
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4275775
60 A = 6786653
32 meter
Y = -739542
96 meter E =
0016285
Z = -5231743
83 I = 51
94670
XDOT = 2767
228019 Wp = 82
87437
YDOT = 7019
281769 meter/sec RA = 60
88439 deg
ZDOT = 1274
725206 TA = 199
30832
MA = 199
37010
Ha = 227
062 n
mi
Hp = 218
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14028135
18 X = 4309142
14
Y = -2426322
03 feet Y = -691542
07 meter
Z = -17164513
88 Z = -5210891
27
XDOT = 9078
832084 XDOT = 2682
338792
YDOT = 23029
139661 feet/sec YDOT = 7049
752105 meter/sec
ZDOT = 4182
169311 ZDOT = 1287
961828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1330190
61 X = -405442
10
Y = -14281322
29 feet Y = -4352947
04 meter
Z = -17075437
87 Z = -5204593
46
XDOT = 22617
757490 XDOT = 6893
892483
YDOT = -7151
858958 feet/sec YDOT = -2179
886611 meter/sec
ZDOT = 4237
314618 ZDOT = 1291
533495
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 14321
09820170
00016717 00000-0 10270-3 0 9117
2 25544 51
6467 61
5217 0004964 28
7530 331
3894 15
51129040 35053
Satellite: ISS
Catalog Number: 25544
Epoch time: 14321
09820170 = yrday
fracday
Element set: 911
Inclination: 51
6467 deg
RA of node: 61
5217 deg
Eccentricity:
0004964
Arg of perigee: 28
7530 deg
Mean anomaly: 331
3894 deg
Mean motion: 15
51129040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3505
Checksum: 284
Coasting Arc #13 (Orbit 3520)
---------------------------------------
Vector Time (GMT): 2014/322/02:01:23
664
Vector Time (MET): N/A
Weight (LBS) : 915369
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4559873
93 A = 6787352
96 meter
Y = 269314
23 meter E =
0010845
Z = 5016099
66 I = 51
93384
XDOT = -2692
431617 Wp = 44
85294
YDOT = -6874
119131 meter/sec RA = 55
93694 deg
ZDOT = -2068
270719 TA = 65
24188
MA = 65
12907
Ha = 227
121 n
mi
Hp = 218
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14960216
30 X = -4586913
66
Y = 883576
87 feet Y = 218171
73 meter
Z = 16457019
89 Z = 4993882
29
XDOT = -8833
437063 XDOT = -2605
316305
YDOT = -22552
884289 feet/sec YDOT = -6903
740622 meter/sec
ZDOT = -6785
665088 ZDOT = -2081
138628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20011
87 X = -6099
62
Y = 15089727
67 feet Y = 4599348
99 meter
Z = 16362212
62 Z = 4987202
41
XDOT = -21939
749239 XDOT = -6687
235568
YDOT = 7423
416090 feet/sec YDOT = 2262
657224 meter/sec
ZDOT = -6839
251395 ZDOT = -2084
603825
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 14322
12902178
00016717 00000-0 10270-3 0 9122
2 25544 51
6469 56
4060 0005018 30
8266 329
3179 15
51192377 35219
Satellite: ISS
Catalog Number: 25544
Epoch time: 14322
12902178 = yrday
fracday
Element set: 912
Inclination: 51
6469 deg
RA of node: 56
4060 deg
Eccentricity:
0005018
Arg of perigee: 30
8266 deg
Mean anomaly: 329
3179 deg
Mean motion: 15
51192377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3521
Checksum: 295
Coasting Arc #14 (Orbit 3535)
---------------------------------------
Vector Time (GMT): 2014/323/02:01:23
664
Vector Time (MET): N/A
Weight (LBS) : 915369
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4874771
60 A = 6788559
88 meter
Y = 125127
76 meter E =
0012976
Z = -4733732
34 I = 51
91979
XDOT = 2551
020490 Wp = 86
94813
YDOT = 6646
940941 meter/sec RA = 50
98946 deg
ZDOT = 2810
039557 TA = 210
81468
MA = 210
89091
Ha = 227
099 n
mi
Hp = 218
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15993345
13 X = 4896005
57
Y = 410524
15 feet Y = 179759
24 meter
Z = -15530617
90 Z = -4709999
26
XDOT = 8369
489797 XDOT = 2462
852661
YDOT = 21807
549019 feet/sec YDOT = 6674
975193 meter/sec
ZDOT = 9219
289886 ZDOT = 2822
218041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1097405
11 X = 334489
08
Y = -16058776
30 feet Y = -4894715
02 meter
Z = -15429423
74 Z = -4702888
35
XDOT = 20973
062957 XDOT = 6392
589589
YDOT = -7450
235113 feet/sec YDOT = -2270
831662 meter/sec
ZDOT = 9269
964456 ZDOT = 2825
485166
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 14323
09539784
00016717 00000-0 10270-3 0 9139
2 25544 51
6471 51
6099 0005055 34
2600 325
8877 15
51189860 35367
Satellite: ISS
Catalog Number: 25544
Epoch time: 14323
09539784 = yrday
fracday
Element set: 913
Inclination: 51
6471 deg
RA of node: 51
6099 deg
Eccentricity:
0005055
Arg of perigee: 34
2600 deg
Mean anomaly: 325
8877 deg
Mean motion: 15
51189860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3536
Checksum: 320
Coasting Arc #15 (Orbit 3551)
---------------------------------------
Vector Time (GMT): 2014/324/02:01:23
664
Vector Time (MET): N/A
Weight (LBS) : 915369
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5205419
25 A = 6789913
54 meter
Y = -516189
15 meter E =
0014345
Z = 4322673
62 I = 51
90486
XDOT = -2315
651362 Wp = 60
26318
YDOT = -6395
697531 meter/sec RA = 46
04207 deg
ZDOT = -3536
550304 TA = 65
69685
MA = 65
54710
Ha = 227
138 n
mi
Hp = 217
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17078147
14 X = -5220258
91
Y = -1693533
96 feet Y = -574482
48 meter
Z = 14182000
08 Z = 4297349
75
XDOT = -7597
281370 XDOT = -2226
781215
YDOT = -20983
259617 feet/sec YDOT = -6421
095762 meter/sec
ZDOT = -11602
855328 ZDOT = -3547
583802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2131275
57 X = -649612
80
Y = 17118343
05 feet Y = 5217670
96 meter
Z = 14074099
94 Z = 4289785
66
XDOT = -19921
784072 XDOT = -6072
159785
YDOT = 7139
565759 feet/sec YDOT = 2176
139643 meter/sec
ZDOT = -11648
680324 ZDOT = -3550
517763
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 14324
12617623
00016717 00000-0 10270-3 0 9144
2 25544 51
6475 46
4942 0005168 36
7767 323
3738 15
51255118 35523
Satellite: ISS
Catalog Number: 25544
Epoch time: 14324
12617623 = yrday
fracday
Element set: 914
Inclination: 51
6475 deg
RA of node: 46
4942 deg
Eccentricity:
0005168
Arg of perigee: 36
7767 deg
Mean anomaly: 323
3738 deg
Mean motion: 15
51255118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3552
Checksum: 311
Coasting Arc #16 (Orbit 3566)
---------------------------------------
Vector Time (GMT): 2014/325/02:01:23
664
Vector Time (MET): N/A
Weight (LBS) : 915369
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5534163
19 A = 6791544
45 meter
Y = 810735
79 meter E =
0009560
Z = -3858277
25 I = 51
88743
XDOT = 2009
100051 Wp = 74
89099
YDOT = 6097
065359 meter/sec RA = 41
09467 deg
ZDOT = 4173
991159 TA = 238
91536
MA = 239
00922
Ha = 227
130 n
mi
Hp = 217
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18156703
38 X = 5543428
80
Y = 2659894
34 feet Y = 872674
27 meter
Z = -12658389
93 Z = -3831369
84
XDOT = 6591
535601 XDOT = 1920
495486
YDOT = 20003
495272 feet/sec YDOT = 6119
036931 meter/sec
ZDOT = 13694
196717 ZDOT = 4183
536222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2811947
00 X = 857081
45
Y = -18213232
90 feet Y = -5551393
39 meter
Z = -12543797
36 Z = -3823349
44
XDOT = 18730
571450 XDOT = 5709
078178
YDOT = -6541
664539 feet/sec YDOT = -1993
899351 meter/sec
ZDOT = 13733
717974 ZDOT = 4186
037238
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 14325
09251317
00016717 00000-0 10270-3 0 9156
2 25544 51
6470 41
6979 0005121 40
0621 320
0907 15
51247297 35678
Satellite: ISS
Catalog Number: 25544
Epoch time: 14325
09251317 = yrday
fracday
Element set: 915
Inclination: 51
6470 deg
RA of node: 41
6979 deg
Eccentricity:
0005121
Arg of perigee: 40
0621 deg
Mean anomaly: 320
0907 deg
Mean motion: 15
51247297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3567
Checksum: 288
Coasting Arc #17 (Orbit 3582)
---------------------------------------
Vector Time (GMT): 2014/326/02:01:23
664
Vector Time (MET): N/A
Weight (LBS) : 915369
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5848248
80 A = 6793127
61 meter
Y = -1096063
19 meter E =
0016629
Z = 3267215
71 I = 51
86931
XDOT = -1589
150921 Wp = 78
71307
YDOT = -5791
780281 meter/sec RA = 36
14793 deg
ZDOT = -4763
836764 TA = 63
56055
MA = 63
39001
Ha = 227
136 n
mi
Hp = 217
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19187167
99 X = -5851429
20
Y = -3596007
83 feet Y = -1161480
00 meter
Z = 10719211
64 Z = 3238797
25
XDOT = -5213
749740 XDOT = -1501
126001
YDOT = -19001
903808 feet/sec YDOT = -5809
058839 meter/sec
ZDOT = -15629
385708 ZDOT = -4771
343240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3425531
91 X = -1044102
13
Y = 19285314
28 feet Y = 5878163
79 meter
Z = 10598234
29 Z = 3230341
81
XDOT = -17551
280471 XDOT = -5349
630288
YDOT = 5531
775749 feet/sec YDOT = 1686
085248 meter/sec
ZDOT = -15660
260638 ZDOT = -4773
247443
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 14326
12325079
00016717 00000-0 10270-3 0 9169
2 25544 51
6472 36
5820 0005269 43
1241 317
0322 15
51309994 35831
Satellite: ISS
Catalog Number: 25544
Epoch time: 14326
12325079 = yrday
fracday
Element set: 916
Inclination: 51
6472 deg
RA of node: 36
5820 deg
Eccentricity:
0005269
Arg of perigee: 43
1241 deg
Mean anomaly: 317
0322 deg
Mean motion: 15
51309994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3583
Checksum: 294
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