[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 30th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22604 21 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 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
There are no maneuvers
Coasting Arc #1 (Orbit 3218)
---------------------------------------
Vector Time (GMT): 2014/302/15:41:51
769
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2132902
29 A = 6787173
79 meter
Y = 3625523
33 meter E =
0013752
Z = -5338088
00 I = 51
78678
XDOT = -6694
410059 Wp = 74
76525
YDOT = 3705
772944 meter/sec RA = 151
94516 deg
ZDOT = -154
763769 TA = 193
74122
MA = 193
77869
Ha = 226
184 n
mi
Hp = 220
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6997710
93 X = 2118133
46
Y = 11894761
60 feet Y = 3649292
12 meter
Z = -17513412
08 Z = -5327762
46
XDOT = -21963
287595 XDOT = -6734
599520
YDOT = 12158
047716 feet/sec YDOT = 3630
686998 meter/sec
ZDOT = -507
755147 ZDOT = -187
382504
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11568131
73 X = -3525966
55
Y = 7625673
09 feet Y = 2324305
16 meter
Z = -17469984
33 Z = -5324851
22
XDOT = -12558
677728 XDOT = -3827
884971
YDOT = -20558
453601 feet/sec YDOT = -6266
216658 meter/sec
ZDOT = -647
308804 ZDOT = -197
299723
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 14302
67053343
00016717 00000-0 10270-3 0 9008
2 25544 51
6419 152
9463 0003666 334
5540 25
5430 15
50767519 32193
Satellite: ISS
Catalog Number: 25544
Epoch time: 14302
67053343 = yrday
fracday
Element set: 900
Inclination: 51
6419 deg
RA of node: 152
9463 deg
Eccentricity:
0003666
Arg of perigee: 334
5540 deg
Mean anomaly: 25
5430 deg
Mean motion: 15
50767519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3219
Checksum: 295
Coasting Arc #2 (Orbit 3234)
---------------------------------------
Vector Time (GMT): 2014/303/15:41:51
769
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1775330
16 A = 6787267
36 meter
Y = -3830489
34 meter E =
0004608
Z = 5313641
76 I = 51
81394
XDOT = 6628
440108 Wp = 15
56733
YDOT = -3810
839017 meter/sec RA = 146
99025 deg
ZDOT = -528
102319 TA = 79
48800
MA = 79
43609
Ha = 226
338 n
mi
Hp = 220
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5824574
03 X = -1758177
10
Y = -12567222
25 feet Y = -3850246
14 meter
Z = 17433207
87 Z = 5305059
14
XDOT = 21746
850749 XDOT = 6673
126537
YDOT = -12502
752679 feet/sec YDOT = -3736
465667 meter/sec
ZDOT = -1732
619157 ZDOT = -495
793188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12178377
89 X = 3711969
58
Y = -6693337
31 feet Y = -2040129
21 meter
Z = 17397236
05 Z = 5302677
55
XDOT = 13324
722812 XDOT = 4061
375513
YDOT = 20062
133885 feet/sec YDOT = 6114
938408 meter/sec
ZDOT = -1594
348701 ZDOT = -485
957484
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 14303
70159437
00016717 00000-0 10270-3 0 9015
2 25544 51
6417 147
8308 0003734 338
8028 21
2967 15
50754655 32359
Satellite: ISS
Catalog Number: 25544
Epoch time: 14303
70159437 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 147
8308 deg
Eccentricity:
0003734
Arg of perigee: 338
8028 deg
Mean anomaly: 21
2967 deg
Mean motion: 15
50754655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3235
Checksum: 308
Coasting Arc #3 (Orbit 3249)
---------------------------------------
Vector Time (GMT): 2014/304/15:41:51
769
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1457297
27 A = 6787392
04 meter
Y = 4080408
54 meter E =
0012842
Z = -5235299
98 I = 51
84211
XDOT = -6495
532237 Wp = 84
42006
YDOT = 3864
283351 meter/sec RA = 142
03957 deg
ZDOT = 1207
501723 TA = 197
13239
MA = 197
17578
Ha = 226
234 n
mi
Hp = 220
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4781159
02 X = 1436992
60
Y = 13387167
13 feet Y = 4096591
18 meter
Z = -17176181
03 Z = -5228270
08
XDOT = -21310
801301 XDOT = -6544
126512
YDOT = 12678
094985 feet/sec YDOT = 3791
374456 meter/sec
ZDOT = 3961
619826 ZDOT = 1175
828726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12960859
58 X = -3950470
00
Y = 5924364
06 feet Y = 1805746
17 meter
Z = -17146864
13 Z = -5226364
19
XDOT = -13881
019308 XDOT = -4230
934685
YDOT = -19329
922616 feet/sec YDOT = -5891
760413 meter/sec
ZDOT = 3826
034634 ZDOT = 1166
175356
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 14304
66818783
00016717 00000-0 10270-3 0 9028
2 25544 51
6428 143
0373 0003725 341
2397 18
8616 15
50841287 32506
Satellite: ISS
Catalog Number: 25544
Epoch time: 14304
66818783 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 143
0373 deg
Eccentricity:
0003725
Arg of perigee: 341
2397 deg
Mean anomaly: 18
8616 deg
Mean motion: 15
50841287 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3250
Checksum: 308
Coasting Arc #4 (Orbit 3265)
---------------------------------------
Vector Time (GMT): 2014/305/15:41:51
769
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1137489
87 A = 6788113
20 meter
Y = -4371766
94 meter E =
0007707
Z = 5065519
53 I = 51
86843
XDOT = 6342
463177 Wp = 28
72003
YDOT = -3860
250920 meter/sec RA = 137
08835 deg
ZDOT = -1899
547314 TA = 79
69008
MA = 79
60321
Ha = 226
365 n
mi
Hp = 220
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3731922
14 X = -1113126
21
Y = -14343067
37 feet Y = -4384350
52 meter
Z = 16619158
58 Z = 5060053
17
XDOT = 20808
606223 XDOT = 6394
385524
YDOT = -12664
865222 feet/sec YDOT = -3789
035199 meter/sec
ZDOT = -6232
110611 ZDOT = -1868
609735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13909229
94 X = 4239533
29
Y = -5189897
80 feet Y = -1581880
85 meter
Z = 16596552
04 Z = 5058629
06
XDOT = 14221
615387 XDOT = 4334
748370
YDOT = 18527
177010 feet/sec YDOT = 5647
083553 meter/sec
ZDOT = -6099
645322 ZDOT = -1859
171894
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 14305
69919839
00016717 00000-0 10270-3 0 9037
2 25544 51
6427 137
9217 0003765 345
8416 14
2629 15
50831799 32668
Satellite: ISS
Catalog Number: 25544
Epoch time: 14305
69919839 = yrday
fracday
Element set: 903
Inclination: 51
6427 deg
RA of node: 137
9217 deg
Eccentricity:
0003765
Arg of perigee: 345
8416 deg
Mean anomaly: 14
2629 deg
Mean motion: 15
50831799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3266
Checksum: 339
Coasting Arc #5 (Orbit 3280)
---------------------------------------
Vector Time (GMT): 2014/306/15:41:51
769
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 878255
22 A = 6788843
79 meter
Y = 4687274
91 meter E =
0010152
Z = -4840518
52 I = 51
89450
XDOT = -6138
562395 Wp = 89
09472
YDOT = 3790
168550 meter/sec RA = 132
14134 deg
ZDOT = 2561
201489 TA = 206
04114
MA = 206
09224
Ha = 226
292 n
mi
Hp = 219
949
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2881414
77 X = 849289
82
Y = 15378198
54 feet Y = 4696933
81 meter
Z = -15880966
27 Z = -4836322
73
XDOT = -20139
640402 XDOT = -6192
930402
YDOT = 12434
936187 feet/sec YDOT = 3721
219374 meter/sec
ZDOT = 8402
892023 ZDOT = 2531
248383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14942867
42 X = -4554585
99
Y = 4695347
58 feet Y = 1431141
94 meter
Z = -15863828
53 Z = -4835294
94
XDOT = -14289
540656 XDOT = -4355
451992
YDOT = -17572
572961 feet/sec YDOT = -5356
120239 meter/sec
ZDOT = 8274
620344 ZDOT = 2522
104281
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 14306
66574423
00016717 00000-0 10270-3 0 9042
2 25544 51
6433 133
1277 0003866 347
4344 12
6710 15
50909557 32817
Satellite: ISS
Catalog Number: 25544
Epoch time: 14306
66574423 = yrday
fracday
Element set: 904
Inclination: 51
6433 deg
RA of node: 133
1277 deg
Eccentricity:
0003866
Arg of perigee: 347
4344 deg
Mean anomaly: 12
6710 deg
Mean motion: 15
50909557 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3281
Checksum: 303
Coasting Arc #6 (Orbit 3296)
---------------------------------------
Vector Time (GMT): 2014/307/15:41:51
769
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -625794
44 A = 6790079
07 meter
Y = -5029128
45 meter E =
0010553
Z = 4516189
70 I = 51
91896
XDOT = 5927
522281 Wp = 47
41234
YDOT = -3638
626328 meter/sec RA = 127
19465 deg
ZDOT = -3218
801994 TA = 74
89299
MA = 74
77627
Ha = 226
385 n
mi
Hp = 219
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2053131
38 X = -591449
70
Y = -16499765
25 feet Y = -5035934
11 meter
Z = 14816895
33 Z = 4513233
42
XDOT = 19447
251579 XDOT = 5983
405920
YDOT = -11937
750419 feet/sec YDOT = -3572
028716 meter/sec
ZDOT = -10560
373995 ZDOT = -3189
870322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16080416
56 X = 4901310
97
Y = -4269326
90 feet Y = -1301290
84 meter
Z = 14805101
83 Z = 4512595
04
XDOT = 14058
582810 XDOT = 4285
056041
YDOT = 16626
636233 feet/sec YDOT = 5067
798724 meter/sec
ZDOT = -10436
467330 ZDOT = -3181
035242
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 14307
69670341
00016717 00000-0 10270-3 0 9053
2 25544 51
6432 128
0121 0003868 352
4677 7
6415 15
50916231 32974
Satellite: ISS
Catalog Number: 25544
Epoch time: 14307
69670341 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 128
0121 deg
Eccentricity:
0003868
Arg of perigee: 352
4677 deg
Mean anomaly: 7
6415 deg
Mean motion: 15
50916231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3297
Checksum: 301
Coasting Arc #7 (Orbit 3311)
---------------------------------------
Vector Time (GMT): 2014/308/15:41:51
769
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 447460
60 A = 6791280
95 meter
Y = 5367206
29 meter E =
0006869
Z = -4141647
46 I = 51
94202
XDOT = -5691
053306 Wp = 77
13252
YDOT = 3416
195211 meter/sec RA = 122
25154 deg
ZDOT = 3819
042499 TA = 232
13542
MA = 232
19758
Ha = 226
370 n
mi
Hp = 219
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1468046
59 X = 407529
28
Y = 17608944
52 feet Y = 5371986
53 meter
Z = -13588082
22 Z = -4139571
07
XDOT = -18671
434730 XDOT = -5747
383150
YDOT = 11207
989536 feet/sec YDOT = 3352
239465 meter/sec
ZDOT = 12529
666993 ZDOT = 3791
258439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17188893
69 X = -5239174
80
Y = 4121746
80 feet Y = 1256308
43 meter
Z = -13580103
22 Z = -4139215
46
XDOT = -13539
641673 XDOT = -4126
882782
YDOT = -15647
984881 feet/sec YDOT = -4769
505792 meter/sec
ZDOT = 12410
674825 ZDOT = 3782
773687
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 14308
66320113
00016717 00000-0 10270-3 0 9061
2 25544 51
6435 123
2172 0004073 353
6316 6
4783 15
50974421 33120
Satellite: ISS
Catalog Number: 25544
Epoch time: 14308
66320113 = yrday
fracday
Element set: 906
Inclination: 51
6435 deg
RA of node: 123
2172 deg
Eccentricity:
0004073
Arg of perigee: 353
6316 deg
Mean anomaly: 6
4783 deg
Mean motion: 15
50974421 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3312
Checksum: 275
Coasting Arc #8 (Orbit 3327)
---------------------------------------
Vector Time (GMT): 2014/309/15:41:51
769
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -278092
89 A = 6792762
73 meter
Y = -5709337
16 meter E =
0012733
Z = 3664194
86 I = 51
96327
XDOT = 5464
929045 Wp = 67
33358
YDOT = -3095
481866 meter/sec RA = 117
31002 deg
ZDOT = -4391
522235 TA = 69
41566
MA = 69
27911
Ha = 226
421 n
mi
Hp = 219
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -912378
26 X = -232029
05
Y = -18731421
12 feet Y = -5712189
22 meter
Z = 12021636
67 Z = 3662956
07
XDOT = 17929
557234 XDOT = 5520
470454
YDOT = -10155
780399 feet/sec YDOT = -3034
059167 meter/sec
ZDOT = -14407
881349 ZDOT = -4364
838591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18315532
97 X = 5582574
45
Y = -4042791
03 feet Y = -1232242
71 meter
Z = 12017296
38 Z = 3662871
94
XDOT = 12676
673357 XDOT = 3863
850039
YDOT = 14777
422314 feet/sec YDOT = 4504
158321 meter/sec
ZDOT = -14293
618682 ZDOT = -4356
694974
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 14309
69410805
00016717 00000-0 10270-3 0 9074
2 25544 51
6436 118
1016 0004029 359
2231
8913 15
51003631 33287
Satellite: ISS
Catalog Number: 25544
Epoch time: 14309
69410805 = yrday
fracday
Element set: 907
Inclination: 51
6436 deg
RA of node: 118
1016 deg
Eccentricity:
0004029
Arg of perigee: 359
2231 deg
Mean anomaly:
8913 deg
Mean motion: 15
51003631 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3328
Checksum: 275
Coasting Arc #9 (Orbit 3342)
---------------------------------------
Vector Time (GMT): 2014/310/15:41:51
769
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 185609
25 A = 6794129
05 meter
Y = 6016359
83 meter E =
0006944
Z = -3148578
36 I = 51
98234
XDOT = -5243
755867 Wp = 39
90779
YDOT = 2711
227680 meter/sec RA = 112
37122 deg
ZDOT = 4882
673915 TA = 284
05308
MA = 284
13026
Ha = 226
469 n
mi
Hp = 219
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 608954
25 X = 133614
34
Y = 19738713
36 feet Y = 6018144
61 meter
Z = -10329981
51 Z = -3147803
17
XDOT = -17203
923448 XDOT = -5297
402842
YDOT = 8895
103937 feet/sec YDOT = 2652
288806 meter/sec
ZDOT = 16019
271374 ZDOT = 4857
069373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19290896
44 X = -5879865
24
Y = 4230417
29 feet Y = 1289431
19 meter
Z = -10327682
81 Z = -3147877
72
XDOT = -11569
156454 XDOT = -3526
278887
YDOT = -14004
945594 feet/sec YDOT = -4268
707417 meter/sec
ZDOT = 15909
658593 ZDOT = 4849
263939
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 14310
66055696
00016717 00000-0 10270-3 0 9087
2 25544 51
6442 113
3060 0004312
3710 359
7444 15
51041374 33439
Satellite: ISS
Catalog Number: 25544
Epoch time: 14310
66055696 = yrday
fracday
Element set: 908
Inclination: 51
6442 deg
RA of node: 113
3060 deg
Eccentricity:
0004312
Arg of perigee:
3710 deg
Mean anomaly: 359
7444 deg
Mean motion: 15
51041374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3343
Checksum: 270
Coasting Arc #10 (Orbit 3358)
---------------------------------------
Vector Time (GMT): 2014/311/15:41:51
769
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -95752
07 A = 6795469
49 meter
Y = -6300736
23 meter E =
0013712
Z = 2533110
50 I = 51
99841
XDOT = 5051
826198 Wp = 86
58180
YDOT = -2224
144149 meter/sec RA = 107
43494 deg
ZDOT = -5315
715576 TA = 65
16761
MA = 65
02508
Ha = 226
475 n
mi
Hp = 219
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -314147
22 X = -37594
03
Y = -20671706
80 feet Y = -6301481
78 meter
Z = 8310729
99 Z = 2532786
68
XDOT = 16574
232933 XDOT = 5102
144373
YDOT = -7297
060856 feet/sec YDOT = -2167
370077 meter/sec
ZDOT = -17440
011732 ZDOT = -5291
051593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20190816
27 X = 6154160
80
Y = -4444575
95 feet Y = -1354706
75 meter
Z = 8310419
14 Z = 2533015
75
XDOT = 10127
815477 XDOT = 3086
958157
YDOT = 13440
059742 feet/sec YDOT = 4096
530209 meter/sec
ZDOT = -17334
477140 ZDOT = -5283
548632
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
69141098
00016717 00000-0 10270-3 0 9094
2 25544 51
6443 108
1906 0004224 6
2123 353
9080 15
51089866 33593
Satellite: ISS
Catalog Number: 25544
Epoch time: 14311
69141098 = yrday
fracday
Element set: 909
Inclination: 51
6443 deg
RA of node: 108
1906 deg
Eccentricity:
0004224
Arg of perigee: 6
2123 deg
Mean anomaly: 353
9080 deg
Mean motion: 15
51089866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3359
Checksum: 301
Coasting Arc #11 (Orbit 3373)
---------------------------------------
Vector Time (GMT): 2014/312/15:41:51
769
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 73031
72 A = 6796577
50 meter
Y = 6520331
26 meter E =
0011175
Z = -1898436
03 I = 52
01178
XDOT = -4894
320751 Wp = 27
05009
YDOT = 1693
044598 meter/sec RA = 102
50030 deg
ZDOT = 5649
303775 TA = 312
17641
MA = 312
27125
Ha = 226
567 n
mi
Hp = 219
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 239605
39 X = 9336
66
Y = 21392162
92 feet Y = 6520791
82 meter
Z = -6228464
66 Z = -1898235
92
XDOT = -16057
482779 XDOT = -4940
332197
YDOT = 5554
608261 feet/sec YDOT = 1638
055840 meter/sec
ZDOT = 18534
461203 ZDOT = 5625
415506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20834050
31 X = -6350218
53
Y = 4860147
26 feet Y = 1481372
88 meter
Z = -6228734
50 Z = -1898518
27
XDOT = -8541
328380 XDOT = -2603
396890
YDOT = -13086
866359 feet/sec YDOT = -3988
876866 meter/sec
ZDOT = 18432
312171 ZDOT = 5618
168750
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
65781032
00016717 00000-0 10270-3 0 9101
2 25544 51
6452 103
3948 0004542 7
6210 352
5009 15
51114786 33744
Satellite: ISS
Catalog Number: 25544
Epoch time: 14312
65781032 = yrday
fracday
Element set: 910
Inclination: 51
6452 deg
RA of node: 103
3948 deg
Eccentricity:
0004542
Arg of perigee: 7
6210 deg
Mean anomaly: 352
5009 deg
Mean motion: 15
51114786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3374
Checksum: 279
Coasting Arc #12 (Orbit 3389)
---------------------------------------
Vector Time (GMT): 2014/313/15:41:51
769
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -37249
11 A = 6797343
89 meter
Y = -6690832
69 meter E =
0012911
Z = 1176011
85 I = 52
02044
XDOT = 4781
459559 Wp = 103
22776
YDOT = -1070
985122 meter/sec RA = 97
56800 deg
ZDOT = -5890
471366 TA = 64
08573
MA = 63
95271
Ha = 226
533 n
mi
Hp = 218
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -122208
36 X = 31859
30
Y = -21951550
82 feet Y = -6690862
85 meter
Z = 3858306
59 Z = 1175998
65
XDOT = 15687
203276 XDOT = 4821
694829
YDOT = -3513
730714 feet/sec YDOT = -1017
290678 meter/sec
ZDOT = -19325
693457 ZDOT = -5867
145490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21322401
21 X = 6499067
89
Y = -5218443
12 feet Y = -1590581
46 meter
Z = 3859417
86 Z = 1176350
56
XDOT = 6695
171778 XDOT = 2040
688358
YDOT = 13012
604795 feet/sec YDOT = 3966
241942 meter/sec
ZDOT = -19226
039526 ZDOT = -5860
096848
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
68861083
00016717 00000-0 10270-3 0 9111
2 25544 51
6449 98
2795 0004442 13
0270 347
0995 15
51175044 33903
Satellite: ISS
Catalog Number: 25544
Epoch time: 14313
68861083 = yrday
fracday
Element set: 911
Inclination: 51
6449 deg
RA of node: 98
2795 deg
Eccentricity:
0004442
Arg of perigee: 13
0270 deg
Mean anomaly: 347
0995 deg
Mean motion: 15
51175044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3390
Checksum: 308
Coasting Arc #13 (Orbit 3404)
---------------------------------------
Vector Time (GMT): 2014/314/15:41:51
769
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 47020
58 A = 6797774
72 meter
Y = 6773855
38 meter E =
0015489
Z = -459284
21 I = 52
02614
XDOT = -4725
280959 Wp = 33
94914
YDOT = 433
633773 meter/sec RA = 92
63592 deg
ZDOT = 6021
820122 TA = 321
12810
MA = 321
23939
Ha = 226
642 n
mi
Hp = 218
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 154266
98 X = -26498
65
Y = 22223934
96 feet Y = 6773970
13 meter
Z = -1506837
97 Z = -459234
23
XDOT = -15502
890286 XDOT = -4759
031356
YDOT = 1422
682982 feet/sec YDOT = 380
603793 meter/sec
ZDOT = 19756
627696 ZDOT = 5998
782983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21489294
06 X = -6549936
83
Y = 5668717
83 feet Y = 1727825
20 meter
Z = -1507820
57 Z = -459583
71
XDOT = -4841
130451 XDOT = -1475
576562
YDOT = -13219
088195 feet/sec YDOT = -4029
178082 meter/sec
ZDOT = 19658
308349 ZDOT = 5991
852385
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
65495981
00016717 00000-0 10270-3 0 9120
2 25544 51
6457 93
4835 0004742 15
0124 345
1167 15
51197351 34059
Satellite: ISS
Catalog Number: 25544
Epoch time: 14314
65495981 = yrday
fracday
Element set: 912
Inclination: 51
6457 deg
RA of node: 93
4835 deg
Eccentricity:
0004742
Arg of perigee: 15
0124 deg
Mean anomaly: 345
1167 deg
Mean motion: 15
51197351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3405
Checksum: 303
Coasting Arc #14 (Orbit 3420)
---------------------------------------
Vector Time (GMT): 2014/315/15:41:51
769
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -20157
23 A = 6797627
36 meter
Y = -6787646
96 meter E =
0010139
Z = -322442
56 I = 52
02597
XDOT = 4719
440322 Wp = 112
85710
YDOT = 265
000783 meter/sec RA = 87
70486 deg
ZDOT = -6027
809377 TA = 70
59387
MA = 70
48432
Ha = 226
591 n
mi
Hp = 218
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -66132
66 X = 57311
66
Y = -22269182
95 feet Y = -6787439
21 meter
Z = -1057882
41 Z = -322352
41
XDOT = 15483
728090 XDOT = 4745
407867
YDOT = 869
425142 feet/sec YDOT = 317
921902 meter/sec
ZDOT = -19776
277483 ZDOT = -6004
819572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21460059
03 X = 6541025
99
Y = -5948959
62 feet Y = -1813242
89 meter
Z = -1056287
63 Z = -321956
47
XDOT = 2858
789315 XDOT = 871
358983
YDOT = 13716
700997 feet/sec YDOT = 4180
850464 meter/sec
ZDOT = -19678
277831 ZDOT = -5997
939083
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
68570614
00016717 00000-0 10270-3 0 9132
2 25544 51
6449 88
3679 0004694 19
5903 340
5428 15
51261590 34213
Satellite: ISS
Catalog Number: 25544
Epoch time: 14315
68570614 = yrday
fracday
Element set: 913
Inclination: 51
6449 deg
RA of node: 88
3679 deg
Eccentricity:
0004694
Arg of perigee: 19
5903 deg
Mean anomaly: 340
5428 deg
Mean motion: 15
51261590 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3421
Checksum: 319
Coasting Arc #15 (Orbit 3436)
---------------------------------------
Vector Time (GMT): 2014/316/15:41:51
769
Vector Time (MET): N/A
Weight (LBS) : 931508
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 8815
73 A = 6797116
40 meter
Y = 6702584
04 meter E =
0017865
Z = 1068994
28 I = 52
02287
XDOT = -4779
930137 Wp = 47
65876
YDOT = -946
365020 meter/sec RA = 82
77249 deg
ZDOT = 5921
897972 TA = 323
86691
MA = 323
98750
Ha = 226
687 n
mi
Hp = 218
277
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 28922
98 X = -71327
68
Y = 21990105
12 feet Y = 6702234
51 meter
Z = 3507199
07 Z = 1068842
46
XDOT = -15682
185489 XDOT = -4797
759467
YDOT = -3104
872114 feet/sec YDOT = -999
917009 meter/sec
ZDOT = 19428
799122 ZDOT = 5898
634125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21101744
05 X = -6431811
59
Y = 6188291
75 feet Y = 1886191
33 meter
Z = 3505345
66 Z = 1068429
36
XDOT = -1013
554350 XDOT = -308
931366
YDOT = -14500
704536 feet/sec YDOT = -4419
814743 meter/sec
ZDOT = 19329
749106 ZDOT = 5891
707527
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
71642403
00016717 00000-0 10270-3 0 9144
2 25544 51
6454 83
2516 0004916 22
5520 337
5847 15
51290245 34376
Satellite: ISS
Catalog Number: 25544
Epoch time: 14316
71642403 = yrday
fracday
Element set: 914
Inclination: 51
6454 deg
RA of node: 83
2516 deg
Eccentricity:
0004916
Arg of perigee: 22
5520 deg
Mean anomaly: 337
5847 deg
Mean motion: 15
51290245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3437
Checksum: 294
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