[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 5th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25833 39 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 124 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 3 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
097/13:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
8
000/00:00:00
000 0
0 0
0 220
3
099/21:16:36
000 0
0 0
0 0
0
N/A 0
0 0
0 226
7
000/00:00:00
000 0
0 0
0 220
1
102/15:22:48
553 3
6 5
5 5
6
N/A 4
0 -0
4 226
7
000/00:13:37
106 -1
2 -0
0 223
1
106/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
9
000/00:00:00
000 0
0 0
0 222
8
Coasting Arc #1 (Orbit 3990)
---------------------------------------
Vector Time (GMT): 2014/094/13:24:19
566
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3543615
06 A = 6788762
49 meter
Y = -2584340
95 meter E =
0006058
Z = 5180273
48 I = 51
97459
XDOT = 2876
033498 Wp = 30
99615
YDOT = -6945
388138 meter/sec RA = 103
56695 deg
ZDOT = -1491
718131 TA = 73
34251
MA = 73
27601
Ha = 226
864 n
mi
Hp = 220
649
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11626033
67 X = -3539617
31
Y = -8478808
91 feet Y = -2623945
20 meter
Z = 16995647
89 Z = 5163068
86
XDOT = 9435
805439 XDOT = 2960
730984
YDOT = -22786
706491 feet/sec YDOT = -6912
753024 meter/sec
ZDOT = -4894
088356 ZDOT = -1477
540431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14457080
43 X = -4406518
11
Y = -709284
60 feet Y = -216189
95 meter
Z = 16923257
59 Z = 5158208
91
XDOT = -4541
336067 XDOT = -1384
199233
YDOT = -23209
022915 feet/sec YDOT = -7074
110185 meter/sec
ZDOT = -4833
072306 ZDOT = -1473
120439
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 14094
60438280
00016717 00000-0 10270-3 0 9006
2 25544 51
6447 104
2450 0002630 344
9066 15
2006 15
50462663 39912
Satellite: ISS
Catalog Number: 25544
Epoch time: 14094
60438280 = yrday
fracday
Element set: 900
Inclination: 51
6447 deg
RA of node: 104
2450 deg
Eccentricity:
0002630
Arg of perigee: 344
9066 deg
Mean anomaly: 15
2006 deg
Mean motion: 15
50462663 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3991
Checksum: 282
Coasting Arc #2 (Orbit 4005)
---------------------------------------
Vector Time (GMT): 2014/095/13:24:19
566
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3555874
75 A = 6789340
40 meter
Y = 2848783
38 meter E =
0011870
Z = -5043846
09 I = 51
98325
XDOT = -2648
302500 Wp = 93
27738
YDOT = 6888
640811 meter/sec RA = 98
62938 deg
ZDOT = 2027
146371 TA = 196
34869
MA = 196
38701
Ha = 226
845 n
mi
Hp = 220
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11666255
73 X = 3548256
24
Y = 9346402
18 feet Y = 2888504
52 meter
Z = -16548051
47 Z = -5026590
76
XDOT = -8688
656497 XDOT = -2734
983284
YDOT = 22600
527594 feet/sec YDOT = 6858
541271 meter/sec
ZDOT = 6650
742686 ZDOT = 2014
070215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14983681
03 X = 4567025
98
Y = 1158615
45 feet Y = 353145
99 meter
Z = -16475487
15 Z = -5021728
48
XDOT = 5496
780334 XDOT = 1675
418646
YDOT = 22523
685732 feet/sec YDOT = 6865
219411 meter/sec
ZDOT = 6594
378258 ZDOT = 2009
966493
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 14095
57118303
00016717 00000-0 10270-3 0 9015
2 25544 51
6449 99
4522 0002655 349
7909 10
3187 15
50477666 40068
Satellite: ISS
Catalog Number: 25544
Epoch time: 14095
57118303 = yrday
fracday
Element set: 901
Inclination: 51
6449 deg
RA of node: 99
4522 deg
Eccentricity:
0002655
Arg of perigee: 349
7909 deg
Mean anomaly: 10
3187 deg
Mean motion: 15
50477666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4006
Checksum: 317
Coasting Arc #3 (Orbit 4021)
---------------------------------------
Vector Time (GMT): 2014/096/13:24:19
566
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3584954
29 A = 6789982
56 meter
Y = -3137139
86 meter E =
0008653
Z = 4835785
39 I = 51
98978
XDOT = 2454
804355 Wp = 43
88171
YDOT = -6788
197869 meter/sec RA = 93
69191 deg
ZDOT = -2575
074405 TA = 71
40746
MA = 71
31349
Ha = 226
850 n
mi
Hp = 220
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11761661
05 X = -3573098
40
Y = -10292453
63 feet Y = -3177162
49 meter
Z = 15865437
65 Z = 4818399
17
XDOT = 8053
820063 XDOT = 2543
037988
YDOT = -22270
990383 feet/sec YDOT = -6760
253512 meter/sec
ZDOT = -8448
406839 ZDOT = -2562
934482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15618883
83 X = -4760635
79
Y = -1623290
57 feet Y = -494778
97 meter
Z = 15792364
60 Z = 4813512
73
XDOT = -6257
818072 XDOT = -1907
382948
YDOT = -21753
211735 feet/sec YDOT = -6630
378937 meter/sec
ZDOT = -8396
003913 ZDOT = -2559
101993
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 14096
60241041
00016717 00000-0 10270-3 0 9027
2 25544 51
6449 94
3392 0002710 351
9176 8
1931 15
50542907 40221
Satellite: ISS
Catalog Number: 25544
Epoch time: 14096
60241041 = yrday
fracday
Element set: 902
Inclination: 51
6449 deg
RA of node: 94
3392 deg
Eccentricity:
0002710
Arg of perigee: 351
9176 deg
Mean anomaly: 8
1931 deg
Mean motion: 15
50542907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4022
Checksum: 282
Coasting Arc #4 (Orbit 4036)
---------------------------------------
Vector Time (GMT): 2014/097/13:24:19
566
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3668594
37 A = 6790903
45 meter
Y = 3403507
31 meter E =
0009214
Z = -4598919
32 I = 51
99435
XDOT = -2273
433521 Wp = 94
41806
YDOT = 6623
161840 meter/sec RA = 88
75536 deg
ZDOT = 3092
685444 TA = 206
40441
MA = 206
45139
Ha = 226
854 n
mi
Hp = 220
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12036070
76 X = 3652603
02
Y = 11166362
55 feet Y = 3444442
11 meter
Z = -15088317
98 Z = -4581136
90
XDOT = -7458
771393 XDOT = -2362
349536
YDOT = 21729
533597 feet/sec YDOT = 6597
241935 meter/sec
ZDOT = 10146
605789 ZDOT = 3081
424917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16376262
55 X = 4991484
82
Y = 1903020
06 feet Y = 580040
51 meter
Z = -15013611
53 Z = -4576148
79
XDOT = 6825
711419 XDOT = 2080
476840
YDOT = 20807
551512 feet/sec YDOT = 6342
141701 meter/sec
ZDOT = 10097
936424 ZDOT = 3077
851022
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 14097
56916196
00016717 00000-0 10270-3 0 9034
2 25544 51
6452 89
5460 0002727 356
7481 3
3652 15
50557161 40378
Satellite: ISS
Catalog Number: 25544
Epoch time: 14097
56916196 = yrday
fracday
Element set: 903
Inclination: 51
6452 deg
RA of node: 89
5460 deg
Eccentricity:
0002727
Arg of perigee: 356
7481 deg
Mean anomaly: 3
3652 deg
Mean motion: 15
50557161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4037
Checksum: 316
Coasting Arc #5 (Orbit 4037)
---------------------------------------
Vector Time (GMT): 2014/097/13:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 886346
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3011232
84 A = 6792909
34 meter
Y = 4594673
20 meter E =
0010528
Z = 3986100
69 I = 52
00224
XDOT = -3272
789294 Wp = 86
65872
YDOT = -5644
540404 meter/sec RA = 88
70844 deg
ZDOT = 4025
394584 TA = 321
52235
MA = 321
59737
Ha = 226
757 n
mi
Hp = 220
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9879372
82 X = -3081750
93
Y = 15074387
13 feet Y = 4560605
69 meter
Z = 13077758
18 Z = 3971300
88
XDOT = -10737
497684 XDOT = -3228
981626
YDOT = -18518
833346 feet/sec YDOT = -5680
893572 meter/sec
ZDOT = 13206
675145 ZDOT = 4009
602671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2976681
21 X = 907292
43
Y = 17822202
76 feet Y = 5432207
40 meter
Z = 13014429
35 Z = 3966798
07
XDOT = -19235
832970 XDOT = -5863
081889
YDOT = -6403
634936 feet/sec YDOT = -1951
827929 meter/sec
ZDOT = 13140
738014 ZDOT = 4005
296947
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 14097
63360997
00016717 00000-0 10270-3 0 9045
2 25544 51
6458 89
2268 0002603 353
8959 6
2160 15
50615677 40382
Satellite: ISS
Catalog Number: 25544
Epoch time: 14097
63360997 = yrday
fracday
Element set: 904
Inclination: 51
6458 deg
RA of node: 89
2268 deg
Eccentricity:
0002603
Arg of perigee: 353
8959 deg
Mean anomaly: 6
2160 deg
Mean motion: 15
50615677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4038
Checksum: 331
Coasting Arc #6 (Orbit 4052)
---------------------------------------
Vector Time (GMT): 2014/098/13:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 886346
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2937165
27 A = 6791664
70 meter
Y = -4332408
89 meter E =
0009797
Z = -4338251
99 I = 51
99682
XDOT = 3420
488360 Wp = 54
35357
YDOT = 5861
576334 meter/sec RA = 83
77243 deg
ZDOT = -3537
933956 TA = 179
72687
MA = 179
72633
Ha = 226
765 n
mi
Hp = 220
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9636369
00 X = 3006466
80
Y = -14213939
93 feet Y = -4299176
52 meter
Z = -14233110
22 Z = -4323814
94
XDOT = 11222
074671 XDOT = 3371
874829
YDOT = 19230
893485 feet/sec YDOT = 5899
554300 meter/sec
ZDOT = -11607
394868 ZDOT = -3521
436299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2855813
48 X = -870451
95
Y = -16985120
55 feet Y = -5177064
74 meter
Z = -14171348
97 Z = -4319427
17
XDOT = 20236
105005 XDOT = 6167
964805
YDOT = 6224
454740 feet/sec YDOT = 1897
213805 meter/sec
ZDOT = -11538
511553 ZDOT = -3516
938321
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 14098
60033662
00016717 00000-0 10270-3 0 9050
2 25544 51
6461 84
4327 0002750
2570 359
8582 15
50627737 40536
Satellite: ISS
Catalog Number: 25544
Epoch time: 14098
60033662 = yrday
fracday
Element set: 905
Inclination: 51
6461 deg
RA of node: 84
4327 deg
Eccentricity:
0002750
Arg of perigee:
2570 deg
Mean anomaly: 359
8582 deg
Mean motion: 15
50627737 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4053
Checksum: 300
Coasting Arc #7 (Orbit 4068)
---------------------------------------
Vector Time (GMT): 2014/099/13:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 886346
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2893615
03 A = 6790322
81 meter
Y = 4029613
28 meter E =
0007729
Z = 4630362
22 I = 51
98915
XDOT = -3599
885053 Wp = 96
30843
YDOT = -6058
702002 meter/sec RA = 78
83629 deg
ZDOT = 3017
852129 TA = 323
69081
MA = 323
74323
Ha = 226
743 n
mi
Hp = 220
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9493487
64 X = -2960952
85
Y = 13220516
02 feet Y = 3996878
98 meter
Z = 15191477
11 Z = 4616141
47
XDOT = -11810
646499 XDOT = -3546
527499
YDOT = -19877
631239 feet/sec YDOT = -6098
659586 meter/sec
ZDOT = 9901
089662 ZDOT = 3000
494587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2543229
73 X = 775176
42
Y = 16133321
63 feet Y = 4917436
43 meter
Z = 15130672
29 Z = 4611828
91
XDOT = -21264
486099 XDOT = -6481
415363
YDOT = -5881
558884 feet/sec YDOT = -1792
699148 meter/sec
ZDOT = 9828
605945 ZDOT = 2995
759092
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 14099
63148151
00016717 00000-0 10270-3 0 9065
2 25544 51
6465 79
3200 0002621
5716 359
5437 15
50698830 40690
Satellite: ISS
Catalog Number: 25544
Epoch time: 14099
63148151 = yrday
fracday
Element set: 906
Inclination: 51
6465 deg
RA of node: 79
3200 deg
Eccentricity:
0002621
Arg of perigee:
5716 deg
Mean anomaly: 359
5437 deg
Mean motion: 15
50698830 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4069
Checksum: 309
Coasting Arc #8 (Orbit 4072)
---------------------------------------
Vector Time (GMT): 2014/099/21:16:36
000
Vector Time (MET): N/A
Weight (LBS) : 904195
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2522923
09 A = 6798571
45 meter
Y = 6145978
12 meter E =
0010807
Z = -1417942
79 I = 52
01358
XDOT = -3991
437530 Wp = 28
69672
YDOT = 2976
056974 meter/sec RA = 77
27593 deg
ZDOT = 5825
185276 TA = 315
94646
MA = 316
03252
Ha = 226
713 n
mi
Hp = 220
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8277306
74 X = 2460897
79
Y = 20163970
21 feet Y = 6173844
11 meter
Z = -4652043
28 Z = -1405838
06
XDOT = -13095
267486 XDOT = -4052
716735
YDOT = 9763
966449 feet/sec YDOT = 2931
080128 meter/sec
ZDOT = 19111
500249 ZDOT = 5805
646261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 475337
60 X = 144882
90
Y = -21802258
90 feet Y = -6645328
51 meter
Z = -4601800
65 Z = -1402628
84
XDOT = 14431
585857 XDOT = 4398
747369
YDOT = -3682
375041 feet/sec YDOT = -1122
387913 meter/sec
ZDOT = 19028
358594 ZDOT = 5799
843700
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 14099
88926302
00016717 00000-0 10270-3 0 9075
2 25544 51
6456 78
0399 0002692 359
2517
8629 15
50668706 40739
Satellite: ISS
Catalog Number: 25544
Epoch time: 14099
88926302 = yrday
fracday
Element set: 907
Inclination: 51
6456 deg
RA of node: 78
0399 deg
Eccentricity:
0002692
Arg of perigee: 359
2517 deg
Mean anomaly:
8629 deg
Mean motion: 15
50668706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4073
Checksum: 338
Coasting Arc #9 (Orbit 4088)
---------------------------------------
Vector Time (GMT): 2014/100/21:16:36
000
Vector Time (MET): N/A
Weight (LBS) : 904195
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2657386
17 A = 6798861
75 meter
Y = -6196966
63 meter E =
0012031
Z = 835805
20 I = 52
00794
XDOT = 4073
422386 Wp = 114
76319
YDOT = -2559
471774 meter/sec RA = 72
34533 deg
ZDOT = -5963
423416 TA = 56
25668
MA = 56
14209
Ha = 226
622 n
mi
Hp = 219
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8718458
56 X = -2591952
87
Y = -20331255
34 feet Y = -6226317
27 meter
Z = 2742143
03 Z = 823055
59
XDOT = 13364
246674 XDOT = 4130
708716
YDOT = -8397
217106 feet/sec YDOT = -2513
600522 meter/sec
ZDOT = -19565
037453 ZDOT = -5943
495811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 231353
49 X = 70516
54
Y = 22127032
17 feet Y = 6744319
41 meter
Z = 2689188
47 Z = 819664
65
XDOT = -14067
261553 XDOT = -4287
701321
YDOT = 2539
922680 feet/sec YDOT = 774
168433 meter/sec
ZDOT = -19480
314712 ZDOT = -5937
599924
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 14100
92037270
00016717 00000-0 10270-3 0 9081
2 25544 51
6458 72
9263 0002810 3
1487 356
9681 15
50757665 40890
Satellite: ISS
Catalog Number: 25544
Epoch time: 14100
92037270 = yrday
fracday
Element set: 908
Inclination: 51
6458 deg
RA of node: 72
9263 deg
Eccentricity:
0002810
Arg of perigee: 3
1487 deg
Mean anomaly: 356
9681 deg
Mean motion: 15
50757665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4089
Checksum: 315
Coasting Arc #10 (Orbit 4103)
---------------------------------------
Vector Time (GMT): 2014/101/21:16:36
000
Vector Time (MET): N/A
Weight (LBS) : 904195
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2798806
66 A = 6799139
32 meter
Y = 6182719
90 meter E =
0013722
Z = -267987
86 I = 51
99750
XDOT = -4207
083686 Wp = 37
18344
YDOT = 2158
516162 meter/sec RA = 67
41265 deg
ZDOT = 6032
395273 TA = 319
94641
MA = 320
04751
Ha = 226
678 n
mi
Hp = 219
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9182436
54 X = 2730763
88
Y = 20284514
10 feet Y = 6213637
47 meter
Z = -879225
25 Z = -254557
59
XDOT = -13802
767999 XDOT = -4260
211630
YDOT = 7081
745937 feet/sec YDOT = 2111
173528 meter/sec
ZDOT = 19791
323075 ZDOT = 6011
828432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1049486
09 X = -319883
36
Y = -22243477
34 feet Y = -6779811
89 meter
Z = -823398
40 Z = -250971
83
XDOT = 13935
645085 XDOT = 4247
584622
YDOT = -1364
677655 feet/sec YDOT = -415
953749 meter/sec
ZDOT = 19703
958434 ZDOT = 6005
766531
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 14101
88701397
00016717 00000-0 10270-3 0 9096
2 25544 51
6448 68
1308 0002536 8
1963 351
9228 15
50750664 41047
Satellite: ISS
Catalog Number: 25544
Epoch time: 14101
88701397 = yrday
fracday
Element set: 909
Inclination: 51
6448 deg
RA of node: 68
1308 deg
Eccentricity:
0002536
Arg of perigee: 8
1963 deg
Mean anomaly: 351
9228 deg
Mean motion: 15
50750664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4104
Checksum: 307
Coasting Arc #11 (Orbit 4115)
---------------------------------------
Vector Time (GMT): 2014/102/15:29:37
106
Vector Time (MET): N/A
Weight (LBS) : 903571
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4117835
60 A = 6790478
86 meter
Y = -1043555
99 meter E =
0010754
Z = -5306958
51 I = 51
95230
XDOT = 2811
178520 Wp = 92
15305
YDOT = 7074
296735 meter/sec RA = 63
66246 deg
ZDOT = 791
187961 TA = 185
38434
MA = 185
39591
Ha = 226
727 n
mi
Hp = 223
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13509959
32 X = 4154978
55
Y = -3423740
11 feet Y = -997300
68 meter
Z = -17411281
20 Z = -5286864
13
XDOT = 9223
026639 XDOT = 2728
019832
YDOT = 23209
634958 feet/sec YDOT = 7105
268269 meter/sec
ZDOT = 2595
761026 ZDOT = 804
641518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 868681
50 X = 264774
12
Y = -14015901
76 feet Y = -4272046
86 meter
Z = -17326095
94 Z = -5280994
04
XDOT = 23887
103022 XDOT = 7280
789001
YDOT = -1793
239397 feet/sec YDOT = -546
579368 meter/sec
ZDOT = 2651
533299 ZDOT = 808
187350
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 14102
66031421
00016717 00000-0 10270-3 0 9109
2 25544 51
6482 64
2973 0003845 287
2137 72
8592 15
49705098 41162
Satellite: ISS
Catalog Number: 25544
Epoch time: 14102
66031421 = yrday
fracday
Element set: 910
Inclination: 51
6482 deg
RA of node: 64
2973 deg
Eccentricity:
0003845
Arg of perigee: 287
2137 deg
Mean anomaly: 72
8592 deg
Mean motion: 15
49705098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4116
Checksum: 305
Coasting Arc #12 (Orbit 4131)
---------------------------------------
Vector Time (GMT): 2014/103/15:29:37
106
Vector Time (MET): N/A
Weight (LBS) : 903571
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4147460
67 A = 6790446
89 meter
Y = 1108584
99 meter E =
0003483
Z = 5262190
54 I = 51
93838
XDOT = -3198
431017 Wp = 350
42140
YDOT = -6878
563690 meter/sec RA = 58
72989 deg
ZDOT = -1068
536895 TA = 109
80148
MA = 109
76393
Ha = 226
759 n
mi
Hp = 222
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13607154
42 X = -4185111
21
Y = 3637089
85 feet Y = 1061995
53 meter
Z = 17264404
67 Z = 5241950
94
XDOT = -10493
540082 XDOT = -3116
084975
YDOT = -22567
466176 feet/sec YDOT = -6913
870305 meter/sec
ZDOT = -3505
698475 ZDOT = -1083
873769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -450727
09 X = -137381
62
Y = 14182222
55 feet Y = 4322741
43 meter
Z = 17178595
72 Z = 5236035
98
XDOT = -23589
444748 XDOT = -7190
062759
YDOT = 3586
840375 feet/sec YDOT = 1093
268946 meter/sec
ZDOT = -3569
456437 ZDOT = -1087
970322
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 14103
69207608
00016717 00000-0 10270-3 0 9116
2 25544 51
6483 59
1881 0003986 290
2561 69
8160 15
49774570 41321
Satellite: ISS
Catalog Number: 25544
Epoch time: 14103
69207608 = yrday
fracday
Element set: 911
Inclination: 51
6483 deg
RA of node: 59
1881 deg
Eccentricity:
0003986
Arg of perigee: 290
2561 deg
Mean anomaly: 69
8160 deg
Mean motion: 15
49774570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4132
Checksum: 321
Coasting Arc #13 (Orbit 4146)
---------------------------------------
Vector Time (GMT): 2014/104/15:29:37
106
Vector Time (MET): N/A
Weight (LBS) : 903571
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4196542
38 A = 6790642
06 meter
Y = -1183694
83 meter E =
0010091
Z = -5214685
72 I = 51
92321
XDOT = 3551
441445 Wp = 95
06028
YDOT = 6643
988445 meter/sec RA = 53
79573 deg
ZDOT = 1351
286795 TA = 187
89234
MA = 187
90823
Ha = 226
723 n
mi
Hp = 222
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13768183
65 X = 4234798
49
Y = -3883513
21 feet Y = -1136553
06 meter
Z = -17108548
94 Z = -5194206
14
XDOT = 11651
710777 XDOT = 3470
318691
YDOT = 21797
862353 feet/sec YDOT = 6683
249506 meter/sec
ZDOT = 4433
355628 ZDOT = 1368
341705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12769
19 X = 3892
05
Y = -14408612
11 feet Y = -4391744
97 meter
Z = -17021713
68 Z = -5188218
33
XDOT = 23078
999531 XDOT = 7034
479057
YDOT = -5295
466278 feet/sec YDOT = -1614
058121 meter/sec
ZDOT = 4504
405103 ZDOT = 1372
942675
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 14104
65933001
00016717 00000-0 10270-3 0 9127
2 25544 51
6492 54
3980 0003922 293
8175 66
2564 15
49788300 41479
Satellite: ISS
Catalog Number: 25544
Epoch time: 14104
65933001 = yrday
fracday
Element set: 912
Inclination: 51
6492 deg
RA of node: 54
3980 deg
Eccentricity:
0003922
Arg of perigee: 293
8175 deg
Mean anomaly: 66
2564 deg
Mean motion: 15
49788300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4147
Checksum: 310
Coasting Arc #14 (Orbit 4162)
---------------------------------------
Vector Time (GMT): 2014/105/15:29:37
106
Vector Time (MET): N/A
Weight (LBS) : 903571
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4261816
83 A = 6790741
96 meter
Y = 1244905
37 meter E =
0004791
Z = 5138913
04 I = 51
90546
XDOT = -3870
086498 Wp = 6
64676
YDOT = -6401
176555 meter/sec RA = 48
86045 deg
ZDOT = -1654
073875 TA = 99
30368
MA = 99
24950
Ha = 226
758 n
mi
Hp = 222
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13982338
67 X = -4300384
54
Y = 4084335
20 feet Y = 1197031
81 meter
Z = 16859950
92 Z = 5118115
56
XDOT = -12697
134180 XDOT = -3790
184351
YDOT = -21001
235417 feet/sec YDOT = -6444
007737 meter/sec
ZDOT = -5426
751557 ZDOT = -1672
679898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 375332
56 X = 114401
36
Y = 14663310
61 feet Y = 4469377
07 meter
Z = 16771761
42 Z = 5112032
88
XDOT = -22459
163399 XDOT = -6845
553004
YDOT = 6888
806375 feet/sec YDOT = 2099
708183 meter/sec
ZDOT = -5504
387381 ZDOT = -1677
737274
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 14105
69103873
00016717 00000-0 10270-3 0 9139
2 25544 51
6495 49
2887 0004055 296
9443 63
1293 15
49858820 41639
Satellite: ISS
Catalog Number: 25544
Epoch time: 14105
69103873 = yrday
fracday
Element set: 913
Inclination: 51
6495 deg
RA of node: 49
2887 deg
Eccentricity:
0004055
Arg of perigee: 296
9443 deg
Mean anomaly: 63
1293 deg
Mean motion: 15
49858820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4163
Checksum: 332
Coasting Arc #15 (Orbit 4174)
---------------------------------------
Vector Time (GMT): 2014/106/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925957
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5633223
57 A = 6797684
03 meter
Y = 2090642
87 meter E =
0003207
Z = -3176014
00 I = 51
90860
XDOT = 542
343699 Wp = 17
51563
YDOT = 5901
867155 meter/sec RA = 44
83813 deg
ZDOT = 4851
153146 TA = 306
05984
MA = 306
08954
Ha = 226
861 n
mi
Hp = 222
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18481704
64 X = 5624855
21
Y = 6859064
53 feet Y = 2153590
17 meter
Z = -10419993
44 Z = -3148668
54
XDOT = 1779
342845 XDOT = 452
741571
YDOT = 19363
081216 feet/sec YDOT = 5907
431351 meter/sec
ZDOT = 15915
856778 ZDOT = 4853
569753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19369809
89 X = 5903918
05
Y = 3977521
91 feet Y = 1212348
68 meter
Z = -10304669
82 Z = -3140863
36
XDOT = 4875
973836 XDOT = 1486
196825
YDOT = 17475
902838 feet/sec YDOT = 5326
655185 meter/sec
ZDOT = 15925
079231 ZDOT = 4853
964150
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 14106
46480461
00016717 00000-0 10270-3 0 9147
2 25544 51
6468 45
4556 0003956 300
2487 59
8272 15
49832326 41751
Satellite: ISS
Catalog Number: 25544
Epoch time: 14106
46480461 = yrday
fracday
Element set: 914
Inclination: 51
6468 deg
RA of node: 45
4556 deg
Eccentricity:
0003956
Arg of perigee: 300
2487 deg
Mean anomaly: 59
8272 deg
Mean motion: 15
49832326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4175
Checksum: 322
Coasting Arc #16 (Orbit 4190)
---------------------------------------
Vector Time (GMT): 2014/107/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925957
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5835523
40 A = 6798160
15 meter
Y = -1894089
15 meter E =
0009809
Z = 2919956
58 I = 51
88906
XDOT = -674
618217 Wp = 88
76864
YDOT = -5724
518892 meter/sec RA = 39
90326 deg
ZDOT = -5046
705186 TA = 58
12596
MA = 58
03055
Ha = 226
808 n
mi
Hp = 222
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19145417
99 X = -5828094
05
Y = -6214203
26 feet Y = -1959304
03 meter
Z = 9579910
06 Z = 2891626
03
XDOT = -2213
314361 XDOT = -586
039463
YDOT = -18781
229959 feet/sec YDOT = -5731
567897 meter/sec
ZDOT = -16557
431714 ZDOT = -5049
766995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19976078
02 X = -6088708
58
Y = -2897466
53 feet Y = -883147
80 meter
Z = 9460392
37 Z = 2883527
59
XDOT = -5447
494176 XDOT = -1660
396225
YDOT = -16704
239844 feet/sec YDOT = -5091
452304 meter/sec
ZDOT = -16569
401777 ZDOT = -5050
353662
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 14107
49646684
00016717 00000-0 10270-3 0 9153
2 25544 51
6476 40
3461 0003975 303
6884 56
3887 15
49894357 41912
Satellite: ISS
Catalog Number: 25544
Epoch time: 14107
49646684 = yrday
fracday
Element set: 915
Inclination: 51
6476 deg
RA of node: 40
3461 deg
Eccentricity:
0003975
Arg of perigee: 303
6884 deg
Mean anomaly: 56
3887 deg
Mean motion: 15
49894357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4191
Checksum: 349
Coasting Arc #17 (Orbit 4205)
---------------------------------------
Vector Time (GMT): 2014/108/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925957
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6026606
47 A = 6798694
69 meter
Y = 1662162
01 meter E =
0005478
Z = -2664482
70 I = 51
86652
XDOT = 776
749466 Wp = 7
90193
YDOT = 5548
104643 meter/sec RA = 34
96674 deg
ZDOT = 5224
459495 TA = 322
19949
MA = 322
23795
Ha = 226
897 n
mi
Hp = 222
553
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19772330
95 X = 6020515
32
Y = 5453287
44 feet Y = 1729521
24 meter
Z = -8741741
14 Z = -2635220
63
XDOT = 2548
390635 XDOT = 689
272385
YDOT = 18202
443055 feet/sec YDOT = 5556
301819 meter/sec
ZDOT = 17140
615142 ZDOT = 5228
020233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20493139
64 X = 6246308
96
Y = 1690706
08 feet Y = 515327
21 meter
Z = -8618247
73 Z = -2626841
91
XDOT = 5889
746395 XDOT = 1795
194701
YDOT = 15943
724396 feet/sec YDOT = 4859
647196 meter/sec
ZDOT = 17154
715805 ZDOT = 5228
757377
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 14108
46362543
00016717 00000-0 10270-3 0 9161
2 25544 51
6475 35
5558 0004047 306
6298 53
4481 15
49913909 42067
Satellite: ISS
Catalog Number: 25544
Epoch time: 14108
46362543 = yrday
fracday
Element set: 916
Inclination: 51
6475 deg
RA of node: 35
5558 deg
Eccentricity:
0004047
Arg of perigee: 306
6298 deg
Mean anomaly: 53
4481 deg
Mean motion: 15
49913909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4206
Checksum: 322
Coasting Arc #18 (Orbit 4221)
---------------------------------------
Vector Time (GMT): 2014/109/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925957
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6205275
05 A = 6799160
53 meter
Y = -1439817
07 meter E =
0010207
Z = 2365760
27 I = 51
84349
XDOT = -818
799733 Wp = 98
03653
YDOT = -5373
110395 meter/sec RA = 30
02863 deg
ZDOT = -5399
242412 TA = 55
68371
MA = 55
58715
Ha = 226
843 n
mi
Hp = 222
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20358513
94 X = -6200205
76
Y = -4723809
29 feet Y = -1509180
04 meter
Z = 7761680
68 Z = 2335627
84
XDOT = -2686
350829 XDOT = -732
427389
YDOT = -17628
314944 feet/sec YDOT = -5381
783918 meter/sec
ZDOT = -17714
049908 ZDOT = -5403
010172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20940045
52 X = -6382525
87
Y = -506474
15 feet Y = -154373
32 meter
Z = 7634469
77 Z = 2326986
39
XDOT = -6118
203885 XDOT = -1864
828544
YDOT = -15219
982923 feet/sec YDOT = -4639
050795 meter/sec
ZDOT = -17729
048657 ZDOT = -5403
814031
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 14109
49523548
00016717 00000-0 10270-3 0 9170
2 25544 51
6483 30
4458 0004014 310
1264 49
9535 15
49970532 42229
Satellite: ISS
Catalog Number: 25544
Epoch time: 14109
49523548 = yrday
fracday
Element set: 917
Inclination: 51
6483 deg
RA of node: 30
4458 deg
Eccentricity:
0004014
Arg of perigee: 310
1264 deg
Mean anomaly: 49
9535 deg
Mean motion: 15
49970532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4222
Checksum: 303
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