[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 29th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 132 3 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
There are no maneuvers
Coasting Arc #1 (Orbit 3681)
---------------------------------------
Vector Time (GMT): 2014/332/11:11:28
187
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6721740
14 A = 6796371
84 meter
Y = 210463
78 meter E =
0018746
Z = 940357
29 I = 51
69808
XDOT = -990
204862 Wp = 107
38413
YDOT = -4768
323581 meter/sec RA = 4
54718 deg
ZDOT = -5918
929447 TA = 62
45194
MA = 62
26160
Ha = 227
582 n
mi
Hp = 216
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22052953
21 X = -6728162
00
Y = 690497
96 feet Y = 135260
99 meter
Z = 3085161
72 Z = 907688
24
XDOT = -3248
703617 XDOT = -908
058342
YDOT = -15644
106236 feet/sec YDOT = -4778
937222 meter/sec
ZDOT = -19419
059865 ZDOT = -5923
540353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12314782
86 X = 3753545
82
Y = -18330196
48 feet Y = -5587043
89 meter
Z = 2945806
49 Z = 897881
82
XDOT = 13194
766361 XDOT = 4021
764787
YDOT = 5690
088784 feet/sec YDOT = 1734
339061 meter/sec
ZDOT = -19437
764172 ZDOT = -5924
630520
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 14332
50030582
00016717 00000-0 10270-3 0 9003
2 25544 51
6462 4
9335 0007174 73
7931 286
4009 15
51592790 36821
Satellite: ISS
Catalog Number: 25544
Epoch time: 14332
50030582 = yrday
fracday
Element set: 900
Inclination: 51
6462 deg
RA of node: 4
9335 deg
Eccentricity:
0007174
Arg of perigee: 73
7931 deg
Mean anomaly: 286
4009 deg
Mean motion: 15
51592790 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3682
Checksum: 298
Coasting Arc #2 (Orbit 3696)
---------------------------------------
Vector Time (GMT): 2014/333/11:11:28
187
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6787935
11 A = 6796773
95 meter
Y = -130192
31 meter E =
0018587
Z = -103340
17 I = 51
66764
XDOT = 170
676624 Wp = 56
39038
YDOT = 4752
588474 meter/sec RA = 359
59078 deg
ZDOT = 6012
226630 TA = 302
49789
MA = 302
67740
Ha = 227
684 n
mi
Hp = 216
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22270128
32 X = 6789388
45
Y = -427140
11 feet Y = -54277
09 meter
Z = -339042
54 Z = -70361
57
XDOT = 559
962676 XDOT = 88
313713
YDOT = 15592
481869 feet/sec YDOT = 4754
036492 meter/sec
ZDOT = 19725
152985 ZDOT = 6012
855767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12328141
37 X = -3757617
49
Y = 18553532
97 feet Y = 5655116
85 meter
Z = -198389
93 Z = -60469
25
XDOT = -11715
464252 XDOT = -3570
873504
YDOT = -7620
849621 feet/sec YDOT = -2322
834964 meter/sec
ZDOT = 19726
881505 ZDOT = 6012
753483
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 14333
46641773
00016717 00000-0 10270-3 0 9010
2 25544 51
6459
1362 0007284 76
4424 283
7539 15
51570320 36973
Satellite: ISS
Catalog Number: 25544
Epoch time: 14333
46641773 = yrday
fracday
Element set: 901
Inclination: 51
6459 deg
RA of node:
1362 deg
Eccentricity:
0007284
Arg of perigee: 76
4424 deg
Mean anomaly: 283
7539 deg
Mean motion: 15
51570320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3697
Checksum: 307
Coasting Arc #3 (Orbit 3712)
---------------------------------------
Vector Time (GMT): 2014/334/11:11:28
187
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6744244
82 A = 6796230
42 meter
Y = -13501
94 meter E =
0015209
Z = -814073
49 I = 51
63597
XDOT = 715
138641 Wp = 115
68341
YDOT = -4788
396411 meter/sec RA = 354
63189 deg
ZDOT = -5938
198521 TA = 73
10792
MA = 72
94120
Ha = 227
541 n
mi
Hp = 215
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22126787
48 X = -6739638
04
Y = -44297
71 feet Y = -88894
70 meter
Z = -2670844
78 Z = -846825
22
XDOT = 2346
255383 XDOT = 797
476605
YDOT = -15709
961979 feet/sec YDOT = -4779
938847 meter/sec
ZDOT = -19482
278611 ZDOT = -5934
524481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12309430
05 X = 3751914
28
Y = -18365978
25 feet Y = -5597950
17 meter
Z = -2810493
37 Z = -856638
38
XDOT = 10359
179566 XDOT = 3157
477932
YDOT = 9877
432926 feet/sec YDOT = 3010
641556 meter/sec
ZDOT = -19465
651777 ZDOT = -5933
130662
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 14334
49691238
00016717 00000-0 10270-3 0 9026
2 25544 51
6466 355
0180 0007317 81
2945 278
9035 15
51649345 37130
Satellite: ISS
Catalog Number: 25544
Epoch time: 14334
49691238 = yrday
fracday
Element set: 902
Inclination: 51
6466 deg
RA of node: 355
0180 deg
Eccentricity:
0007317
Arg of perigee: 81
2945 deg
Mean anomaly: 278
9035 deg
Mean motion: 15
51649345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3713
Checksum: 320
Coasting Arc #4 (Orbit 3728)
---------------------------------------
Vector Time (GMT): 2014/335/11:11:28
187
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6580494
33 A = 6795329
39 meter
Y = 133353
38 meter E =
0021115
Z = 1654329
21 I = 51
60106
XDOT = -1547
318747 Wp = 70
57980
YDOT = 4881
109740 meter/sec RA = 349
67030 deg
ZDOT = 5708
771435 TA = 307
54225
MA = 307
73391
Ha = 227
596 n
mi
Hp = 215
799
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21589548
34 X = 6570477
76
Y = 437511
08 feet Y = 206884
71 meter
Z = 5427589
28 Z = 1686272
43
XDOT = -5076
505075 XDOT = -1629
517204
YDOT = 16014
139566 feet/sec YDOT = 4863
346959 meter/sec
ZDOT = 18729
565075 ZDOT = 5701
055072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12022800
11 X = -3664549
47
Y = 17895686
87 feet Y = 5454605
36 meter
Z = 5563758
45 Z = 1695833
58
XDOT = -9359
312348 XDOT = -2852
718404
YDOT = -12152
655563 feet/sec YDOT = -3704
129415 meter/sec
ZDOT = 18695
685009 ZDOT = 5698
444791
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 14335
52738374
00016717 00000-0 10270-3 0 9035
2 25544 51
6457 349
9006 0007471 83
9022 276
2981 15
51651747 37292
Satellite: ISS
Catalog Number: 25544
Epoch time: 14335
52738374 = yrday
fracday
Element set: 903
Inclination: 51
6457 deg
RA of node: 349
9006 deg
Eccentricity:
0007471
Arg of perigee: 83
9022 deg
Mean anomaly: 276
2981 deg
Mean motion: 15
51651747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3729
Checksum: 331
Coasting Arc #5 (Orbit 3743)
---------------------------------------
Vector Time (GMT): 2014/336/11:11:28
187
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6300835
26 A = 6793582
29 meter
Y = -350770
97 meter E =
0011802
Z = -2520933
02 I = 51
56560
XDOT = 2383
987948 Wp = 104
44553
YDOT = -5001
138151 meter/sec RA = 344
70409 deg
ZDOT = -5286
341986 TA = 103
82195
MA = 103
69060
Ha = 227
464 n
mi
Hp = 215
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20672031
71 X = -6284198
48
Y = -1150823
39 feet Y = -421137
92 meter
Z = -8270777
62 Z = -2551501
68
XDOT = 7821
482769 XDOT = 2465
414424
YDOT = -16407
933565 feet/sec YDOT = -4974
023449 meter/sec
ZDOT = -17343
641687 ZDOT = -5274
563051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11827843
16 X = 3605126
59
Y = -16928903
68 feet Y = -5159929
84 meter
Z = -8401035
55 Z = -2560635
63
XDOT = 8547
543477 XDOT = 2605
291252
YDOT = 14515
477517 feet/sec YDOT = 4424
317547 meter/sec
ZDOT = -17292
417541 ZDOT = -5270
728866
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 14336
49342530
00016717 00000-0 10270-3 0 9048
2 25544 51
6461 345
1020 0007376 88
3989 271
8007 15
51713526 37447
Satellite: ISS
Catalog Number: 25544
Epoch time: 14336
49342530 = yrday
fracday
Element set: 904
Inclination: 51
6461 deg
RA of node: 345
1020 deg
Eccentricity:
0007376
Arg of perigee: 88
3989 deg
Mean anomaly: 271
8007 deg
Mean motion: 15
51713526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3744
Checksum: 309
Coasting Arc #6 (Orbit 3759)
---------------------------------------
Vector Time (GMT): 2014/337/11:11:28
187
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5918428
07 A = 6791675
05 meter
Y = 578597
65 meter E =
0020113
Z = 3262975
08 I = 51
52822
XDOT = -3127
568958 Wp = 88
76969
YDOT = 5163
529163 meter/sec RA = 339
73330 deg
ZDOT = 4732
375171 TA = 309
14112
MA = 309
31971
Ha = 227
418 n
mi
Hp = 215
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19417414
94 X = 5895667
42
Y = 1898286
27 feet Y = 644653
96 meter
Z = 10705298
81 Z = 3291671
21
XDOT = -10261
053012 XDOT = -3208
065056
YDOT = 16940
712476 feet/sec YDOT = 5128
104390 meter/sec
ZDOT = 15526
165260 ZDOT = 4716
986297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11527905
98 X = -3513705
74
Y = 15656150
88 feet Y = 4771994
79 meter
Z = 10827522
33 Z = 3300228
81
XDOT = -8119
351106 XDOT = -2474
778217
YDOT = -16725
692494 feet/sec YDOT = -5097
991072 meter/sec
ZDOT = 15459
518843 ZDOT = 4712
061343
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 14337
52384769
00016717 00000-0 10270-3 0 9054
2 25544 51
6448 339
9838 0007495 91
3406 268
8605 15
51740144 37604
Satellite: ISS
Catalog Number: 25544
Epoch time: 14337
52384769 = yrday
fracday
Element set: 905
Inclination: 51
6448 deg
RA of node: 339
9838 deg
Eccentricity:
0007495
Arg of perigee: 91
3406 deg
Mean anomaly: 268
8605 deg
Mean motion: 15
51740144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3760
Checksum: 342
Coasting Arc #7 (Orbit 3774)
---------------------------------------
Vector Time (GMT): 2014/338/11:11:28
187
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5439245
60 A = 6789386
91 meter
Y = -927204
08 meter E =
0014045
Z = -3969389
68 I = 51
49205
XDOT = 3808
483198 Wp = 83
79270
YDOT = -5305
630735 meter/sec RA = 334
75673 deg
ZDOT = -3990
128288 TA = 144
47633
MA = 144
38274
Ha = 227
373 n
mi
Hp = 215
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17845293
95 X = -5409190
78
Y = -3042008
14 feet Y = -987860
98 meter
Z = -13022932
03 Z = -3995740
28
XDOT = 12495
023614 XDOT = 3886
912032
YDOT = -17406
924982 feet/sec YDOT = -5262
603053 meter/sec
ZDOT = -13090
972073 ZDOT = -3971
436701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11461906
18 X = 3493589
00
Y = -13906811
29 feet Y = -4238796
08 meter
Z = -13135082
61 Z = -4003573
18
XDOT = 7850
523933 XDOT = 2392
839695
YDOT = 18725
699725 feet/sec YDOT = 5707
593276 meter/sec
ZDOT = -13010
217472 ZDOT = -3965
514285
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 14338
48984465
00016717 00000-0 10270-3 0 9060
2 25544 51
6449 335
1849 0007419 95
2090 264
9908 15
51785005 37757
Satellite: ISS
Catalog Number: 25544
Epoch time: 14338
48984465 = yrday
fracday
Element set: 906
Inclination: 51
6449 deg
RA of node: 335
1849 deg
Eccentricity:
0007419
Arg of perigee: 95
2090 deg
Mean anomaly: 264
9908 deg
Mean motion: 15
51785005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3775
Checksum: 351
Coasting Arc #8 (Orbit 3790)
---------------------------------------
Vector Time (GMT): 2014/339/11:11:28
187
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4890674
16 A = 6787320
17 meter
Y = 1308637
43 meter E =
0016059
Z = 4509593
54 I = 51
45644
XDOT = -4377
678643 Wp = 105
74613
YDOT = 5455
571119 meter/sec RA = 329
77488 deg
ZDOT = 3150
822338 TA = 312
51044
MA = 312
64598
Ha = 227
233 n
mi
Hp = 215
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16045518
89 X = 4853770
69
Y = 4293429
89 feet Y = 1363121
44 meter
Z = 14795254
41 Z = 4533262
57
XDOT = -14362
462738 XDOT = -4453
664661
YDOT = 17898
855377 feet/sec YDOT = 5406
191980 meter/sec
ZDOT = 10337
343630 ZDOT = 3129
371710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11445814
11 X = -3488684
14
Y = 11912070
26 feet Y = 3630799
02 meter
Z = 14895895
10 Z = 4540268
83
XDOT = -7871
165218 XDOT = -2399
131158
YDOT = -20429
645827 feet/sec YDOT = -6226
956048 meter/sec
ZDOT = 10244
797241 ZDOT = 3122
614199
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 14339
52021832
00016717 00000-0 10270-3 0 9077
2 25544 51
6439 330
0658 0007439 98
4509 261
7486 15
51817089 37912
Satellite: ISS
Catalog Number: 25544
Epoch time: 14339
52021832 = yrday
fracday
Element set: 907
Inclination: 51
6439 deg
RA of node: 330
0658 deg
Eccentricity:
0007439
Arg of perigee: 98
4509 deg
Mean anomaly: 261
7486 deg
Mean motion: 15
51817089 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3791
Checksum: 333
Coasting Arc #9 (Orbit 3805)
---------------------------------------
Vector Time (GMT): 2014/340/11:11:28
187
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4287324
49 A = 6785504
74 meter
Y = -1811521
29 meter E =
0019378
Z = -4955045
86 I = 51
42407
XDOT = 4830
208291 Wp = 84
20939
YDOT = -5522
980610 meter/sec RA = 324
78775 deg
ZDOT = -2165
570319 TA = 164
59140
MA = 164
53232
Ha = 227
271 n
mi
Hp = 215
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14066025
22 X = -4242678
69
Y = -5943311
31 feet Y = -1859214
86 meter
Z = -16256712
13 Z = -4975765
04
XDOT = 15847
140062 XDOT = 4902
128322
YDOT = -18120
015125 feet/sec YDOT = -5468
563771 meter/sec
ZDOT = -7104
889499 ZDOT = -2141
931361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11771201
72 X = 3587862
28
Y = -9578468
46 feet Y = -2919517
19 meter
Z = -16344676
69 Z = -4981857
46
XDOT = 7918
236386 XDOT = 2413
478450
YDOT = 21650
662848 feet/sec YDOT = 6599
122036 meter/sec
ZDOT = -7003
001522 ZDOT = -2134
514864
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 14340
48617025
00016717 00000-0 10270-3 0 9080
2 25544 51
6440 325
2667 0007431 102
1375 258
0609 15
51850972 38067
Satellite: ISS
Catalog Number: 25544
Epoch time: 14340
48617025 = yrday
fracday
Element set: 908
Inclination: 51
6440 deg
RA of node: 325
2667 deg
Eccentricity:
0007431
Arg of perigee: 102
1375 deg
Mean anomaly: 258
0609 deg
Mean motion: 15
51850972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3806
Checksum: 301
Coasting Arc #10 (Orbit 3821)
---------------------------------------
Vector Time (GMT): 2014/341/11:11:28
187
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3654992
08 A = 6784265
72 meter
Y = 2349254
34 meter E =
0011049
Z = 5202105
67 I = 51
39470
XDOT = -5176
226855 Wp = 110
99764
YDOT = 5550
349274 meter/sec RA = 319
79637 deg
ZDOT = 1124
468140 TA = 328
15924
MA = 328
22599
Ha = 227
073 n
mi
Hp = 215
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11991443
82 X = 3603180
16
Y = 7707527
37 feet Y = 2389836
64 meter
Z = 17067275
82 Z = 5219735
62
XDOT = -16982
371572 XDOT = -5243
369792
YDOT = 18209
807329 feet/sec YDOT = 5492
089825 meter/sec
ZDOT = 3689
199933 ZDOT = 1099
159995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12241043
00 X = -3731069
90
Y = 7127588
55 feet Y = 2172488
99 meter
Z = 17141964
73 Z = 5224870
85
XDOT = -8060
323598 XDOT = -2456
786633
YDOT = -22499
092953 feet/sec YDOT = -6857
723532 meter/sec
ZDOT = 3580
192658 ZDOT = 1091
242722
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 14341
51649508
00016717 00000-0 10270-3 0 9097
2 25544 51
6435 320
1473 0007374 105
4990 254
6976 15
51888717 38220
Satellite: ISS
Catalog Number: 25544
Epoch time: 14341
51649508 = yrday
fracday
Element set: 909
Inclination: 51
6435 deg
RA of node: 320
1473 deg
Eccentricity:
0007374
Arg of perigee: 105
4990 deg
Mean anomaly: 254
6976 deg
Mean motion: 15
51888717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3822
Checksum: 331
Coasting Arc #11 (Orbit 3836)
---------------------------------------
Vector Time (GMT): 2014/342/11:11:28
187
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3022645
42 A = 6783819
04 meter
Y = -2979578
74 meter E =
0021982
Z = -5311053
36 I = 51
37013
XDOT = 5380
968045 Wp = 96
03678
YDOT = -5435
646581 meter/sec RA = 314
80182 deg
ZDOT = -15
276266 TA = 173
83030
MA = 173
80318
Ha = 227
134 n
mi
Hp = 215
414
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9916815
69 X = -2963302
93
Y = -9775520
81 feet Y = -3013047
62 meter
Z = -17424715
74 Z = -5325593
15
XDOT = 17654
094636 XDOT = 5441
424993
YDOT = -17833
486159 feet/sec YDOT = -5375
135072 meter/sec
ZDOT = -50
118982 ZDOT = 11
010163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13073109
19 X = 3984683
68
Y = -4566683
15 feet Y = -1391925
02 meter
Z = -17486108
21 Z = -5329765
78
XDOT = 8026
485299 XDOT = 2446
472719
YDOT = 22707
160855 feet/sec YDOT = 6921
142629 meter/sec
ZDOT = 63
032239 ZDOT = 19
212226
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 14342
48240145
00016717 00000-0 10270-3 0 9100
2 25544 51
6436 315
3481 0007390 108
9902 251
2050 15
51913753 38376
Satellite: ISS
Catalog Number: 25544
Epoch time: 14342
48240145 = yrday
fracday
Element set: 910
Inclination: 51
6436 deg
RA of node: 315
3481 deg
Eccentricity:
0007390
Arg of perigee: 108
9902 deg
Mean anomaly: 251
2050 deg
Mean motion: 15
51913753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3837
Checksum: 290
Coasting Arc #12 (Orbit 3852)
---------------------------------------
Vector Time (GMT): 2014/343/11:11:28
187
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2397702
76 A = 6784067
76 meter
Y = 3621773
22 meter E =
0010005
Z = 5202504
24 I = 51
34985
XDOT = -5505
312775 Wp = 93
33254
YDOT = 5229
625474 meter/sec RA = 309
80538 deg
ZDOT = -1102
129613 TA = 7
27318
MA = 7
25868
Ha = 226
910 n
mi
Hp = 215
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7866478
86 X = 2331752
92
Y = 11882458
09 feet Y = 3648216
69 meter
Z = 17068583
47 Z = 5213992
08
XDOT = -18062
049788 XDOT = -5558
028703
YDOT = 17157
563891 feet/sec YDOT = 5167
766840 meter/sec
ZDOT = -3615
910805 ZDOT = -1129
001267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14043995
76 X = -4280609
91
Y = 2047130
08 feet Y = 623965
25 meter
Z = 17116842
08 Z = 5217213
47
XDOT = -7840
623427 XDOT = -2389
822020
YDOT = -22554
100382 feet/sec YDOT = -6874
489796 meter/sec
ZDOT = -3731
510691 ZDOT = -1137
364458
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 14343
51267704
00016717 00000-0 10270-3 0 9116
2 25544 51
6434 310
2287 0007296 112
5910 247
6014 15
51967116 38536
Satellite: ISS
Catalog Number: 25544
Epoch time: 14343
51267704 = yrday
fracday
Element set: 911
Inclination: 51
6434 deg
RA of node: 310
2287 deg
Eccentricity:
0007296
Arg of perigee: 112
5910 deg
Mean anomaly: 247
6014 deg
Mean motion: 15
51967116 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3853
Checksum: 296
Coasting Arc #13 (Orbit 3867)
---------------------------------------
Vector Time (GMT): 2014/344/11:11:28
187
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1824829
25 A = 6785253
29 meter
Y = -4299653
29 meter E =
0019548
Z = -4939909
47 I = 51
33470
XDOT = 5500
139182 Wp = 109
50561
YDOT = -4845
891109 meter/sec RA = 304
80867 deg
ZDOT = 2186
747041 TA = 181
96669
MA = 181
97439
Ha = 226
957 n
mi
Hp = 215
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5986972
61 X = -1752617
43
Y = -14106474
04 feet Y = -4319655
59 meter
Z = -16207052
05 Z = -4948599
14
XDOT = 18045
076058 XDOT = 5543
295782
YDOT = -15898
592878 feet/sec YDOT = -4784
143844 meter/sec
ZDOT = 7174
366932 ZDOT = 2213
570384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15282540
00 X = 4658118
19
Y = 325048
60 feet Y = 99074
81 meter
Z = -16243254
03 Z = -4950943
83
XDOT = 7282
281729 XDOT = 2219
639471
YDOT = 21777
394432 feet/sec YDOT = 6637
749823 meter/sec
ZDOT = 7289
678525 ZDOT = 2221
894014
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 14344
47853753
00016717 00000-0 10270-3 0 9128
2 25544 51
6436 305
4295 0007323 115
7477 244
4431 15
51982191 38681
Satellite: ISS
Catalog Number: 25544
Epoch time: 14344
47853753 = yrday
fracday
Element set: 912
Inclination: 51
6436 deg
RA of node: 305
4295 deg
Eccentricity:
0007323
Arg of perigee: 115
7477 deg
Mean anomaly: 244
4431 deg
Mean motion: 15
51982191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3868
Checksum: 323
Coasting Arc #14 (Orbit 3883)
---------------------------------------
Vector Time (GMT): 2014/345/11:11:28
187
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1281106
18 A = 6786920
46 meter
Y = 4942497
86 meter E =
0014774
Z = 4458377
33 I = 51
32372
XDOT = -5454
158993 Wp = 90
78206
YDOT = 4329
265071 meter/sec RA = 299
81275 deg
ZDOT = -3223
049340 TA = 31
81249
MA = 31
72333
Ha = 226
735 n
mi
Hp = 215
530
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4203104
25 X = 1204085
47
Y = 16215544
16 feet Y = 4956393
11 meter
Z = 14627222
23 Z = 4464413
97
XDOT = -17894
222417 XDOT = -5486
507971
YDOT = 14203
625562 feet/sec YDOT = 4268
092444 meter/sec
ZDOT = -10574
308857 ZDOT = -3249
623146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16539442
86 X = -5041222
18
Y = -2516235
43 feet Y = -766948
56 meter
Z = 14651995
66 Z = 4465928
28
XDOT = -6339
782688 XDOT = -1932
365763
YDOT = -20739
750684 feet/sec YDOT = -6321
476008 meter/sec
ZDOT = -10688
448393 ZDOT = -3257
839070
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 14345
50876373
00016717 00000-0 10270-3 0 9137
2 25544 51
6435 300
3100 0007225 119
5428 240
6445 15
52049335 38844
Satellite: ISS
Catalog Number: 25544
Epoch time: 14345
50876373 = yrday
fracday
Element set: 913
Inclination: 51
6435 deg
RA of node: 300
3100 deg
Eccentricity:
0007225
Arg of perigee: 119
5428 deg
Mean anomaly: 240
6445 deg
Mean motion: 15
52049335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3884
Checksum: 295
Coasting Arc #15 (Orbit 3898)
---------------------------------------
Vector Time (GMT): 2014/346/11:11:28
187
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -823193
63 A = 6789107
17 meter
Y = -5547422
57 meter E =
0013306
Z = -3841367
78 I = 51
31643
XDOT = 5320
847895 Wp = 114
12083
YDOT = -3640
494993 meter/sec RA = 294
81897 deg
ZDOT = 4123
117122 TA = 199
49948
MA = 199
55042
Ha = 226
747 n
mi
Hp = 215
526
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2700766
51 X = -742439
77
Y = -18200205
30 feet Y = -5556176
36 meter
Z = -12602912
67 Z = -3845170
85
XDOT = 17456
850050 XDOT = 5341
132553
YDOT = -11943
881211 feet/sec YDOT = -3580
880595 meter/sec
ZDOT = 13527
287145 ZDOT = 4149
014116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17866401
63 X = 5445679
22
Y = 4353319
14 feet Y = 1326891
67 meter
Z = -12618055
54 Z = -3845983
33
XDOT = 4923
242819 XDOT = 1500
604411
YDOT = 19268
162731 feet/sec YDOT = 5872
936000 meter/sec
ZDOT = 13638
400872 ZDOT = 4156
984586
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 14346
47457804
00016717 00000-0 10270-3 0 9149
2 25544 51
6436 295
5105 0007258 122
7424 237
4428 15
52060026 38994
Satellite: ISS
Catalog Number: 25544
Epoch time: 14346
47457804 = yrday
fracday
Element set: 914
Inclination: 51
6436 deg
RA of node: 295
5105 deg
Eccentricity:
0007258
Arg of perigee: 122
7424 deg
Mean anomaly: 237
4428 deg
Mean motion: 15
52060026 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3899
Checksum: 317
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