[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 21st 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 27986 17 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 3574)
---------------------------------------
Vector Time (GMT): 2014/325/14:07:07
165
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 555117
61 A = 6787081
54 meter
Y = -4579382
83 meter E =
0018984
Z = -4996036
51 I = 51
86089
XDOT = 6632
920350 Wp = 66
02129
YDOT = 3147
038352 meter/sec RA = 38
65447 deg
ZDOT = -2146
530787 TA = 183
06898
MA = 183
08064
Ha = 227
717 n
mi
Hp = 217
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1821251
99 X = 630553
84
Y = -15024221
88 feet Y = -4572753
22 meter
Z = -16391195
89 Z = -4993156
65
XDOT = 21761
549705 XDOT = 6607
663883
YDOT = 10324
928975 feet/sec YDOT = 3221
070809 meter/sec
ZDOT = -7042
423842 ZDOT = -2114
369416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15069494
18 X = 4593181
82
Y = 1544769
16 feet Y = 470845
64 meter
Z = -16378019
97 Z = -4992020
49
XDOT = -9657
960227 XDOT = -2943
746277
YDOT = 20960
329995 feet/sec YDOT = 6388
708582 meter/sec
ZDOT = -6905
883312 ZDOT = -2104
913234
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
60809216
00016717 00000-0 10270-3 0 9004
2 25544 51
6465 39
1502 0006798 51
3816 308
7943 15
51298731 35759
Satellite: ISS
Catalog Number: 25544
Epoch time: 14325
60809216 = yrday
fracday
Element set: 900
Inclination: 51
6465 deg
RA of node: 39
1502 deg
Eccentricity:
0006798
Arg of perigee: 51
3816 deg
Mean anomaly: 308
7943 deg
Mean motion: 15
51298731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3575
Checksum: 317
Coasting Arc #2 (Orbit 3590)
---------------------------------------
Vector Time (GMT): 2014/326/14:07:07
165
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1057966
17 A = 6785892
32 meter
Y = 4212571
27 meter E =
0009274
Z = 5205568
43 I = 51
83189
XDOT = -6798
336791 Wp = 79
12922
YDOT = -3309
287015 meter/sec RA = 33
69933 deg
ZDOT = 1296
093182 TA = 358
45975
MA = 358
46261
Ha = 227
768 n
mi
Hp = 216
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3471017
63 X = -1130281
09
Y = 13820771
88 feet Y = 4200335
82 meter
Z = 17078636
59 Z = 5200253
40
XDOT = -22304
254563 XDOT = -6767
122457
YDOT = -10857
240864 feet/sec YDOT = -3385
135955 meter/sec
ZDOT = 4252
274218 ZDOT = 1263
142676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13961724
77 X = -4255533
71
Y = -2988976
48 feet Y = -911040
03 meter
Z = 17055139
62 Z = 5198406
56
XDOT = 9681
555323 XDOT = 2950
938063
YDOT = -21753
126702 feet/sec YDOT = -6630
353019 meter/sec
ZDOT = 4112
407520 ZDOT = 1253
461812
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
63877582
00016717 00000-0 10270-3 0 9010
2 25544 51
6457 34
0341 0006981 54
9885 305
1921 15
51373411 35918
Satellite: ISS
Catalog Number: 25544
Epoch time: 14326
63877582 = yrday
fracday
Element set: 901
Inclination: 51
6457 deg
RA of node: 34
0341 deg
Eccentricity:
0006981
Arg of perigee: 54
9885 deg
Mean anomaly: 305
1921 deg
Mean motion: 15
51373411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3591
Checksum: 312
Coasting Arc #3 (Orbit 3605)
---------------------------------------
Vector Time (GMT): 2014/327/14:07:07
165
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1624648
81 A = 6785367
71 meter
Y = -3893838
29 meter E =
0021162
Z = -5332220
43 I = 51
80465
XDOT = 6840
840109 Wp = 77
52679
YDOT = 3398
027686 meter/sec RA = 28
74059 deg
ZDOT = -393
969307 TA = 188
69688
MA = 188
73361
Ha = 227
704 n
mi
Hp = 216
734
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5330212
64 X = 1693972
63
Y = -12775060
02 feet Y = -3875282
48 meter
Z = -17494161
51 Z = -5324159
80
XDOT = 22443
701145 XDOT = 6804
247958
YDOT = 11148
384798 feet/sec YDOT = 3474
321819 meter/sec
ZDOT = -1292
550221 ZDOT = -360
825439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13078248
93 X = 3986250
27
Y = 4669186
49 feet Y = 1423168
04 meter
Z = -17459012
42 Z = -5321506
99
XDOT = -9449
566449 XDOT = -2880
227854
YDOT = 22122
388915 feet/sec YDOT = 6742
904141 meter/sec
ZDOT = -1151
881871 ZDOT = -351
093594
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 14327
60501175
00016717 00000-0 10270-3 0 9021
2 25544 51
6466 29
2372 0006994 57
9366 302
2463 15
51396886 36066
Satellite: ISS
Catalog Number: 25544
Epoch time: 14327
60501175 = yrday
fracday
Element set: 902
Inclination: 51
6466 deg
RA of node: 29
2372 deg
Eccentricity:
0006994
Arg of perigee: 57
9366 deg
Mean anomaly: 302
2463 deg
Mean motion: 15
51396886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3606
Checksum: 321
Coasting Arc #4 (Orbit 3621)
---------------------------------------
Vector Time (GMT): 2014/328/14:07:07
165
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2244049
64 A = 6785194
71 meter
Y = 3576438
01 meter E =
0010058
Z = 5304171
16 I = 51
77548
XDOT = -6819
992776 Wp = 62
51845
YDOT = -3470
017605 meter/sec RA = 23
77895 deg
ZDOT = -540
310150 TA = 32
65656
MA = 32
59441
Ha = 227
781 n
mi
Hp = 216
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7362367
59 X = -2309641
81
Y = 11733720
51 feet Y = 3550976
49 meter
Z = 17402136
37 Z = 5293110
62
XDOT = -22375
304383 XDOT = -6778
058653
YDOT = -11384
572194 feet/sec YDOT = -3546
048680 meter/sec
ZDOT = -1772
671096 ZDOT = -573
339654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12274329
37 X = -3741215
59
Y = -6549027
39 feet Y = -1996143
55 meter
Z = 17354252
58 Z = 5289576
19
XDOT = 9156
602858 XDOT = 2790
932551
YDOT = -22276
670559 feet/sec YDOT = -6789
929187 meter/sec
ZDOT = -1912
833899 ZDOT = -583
031772
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 14328
63562950
00016717 00000-0 10270-3 0 9034
2 25544 51
6452 24
1200 0007192 61
7924 298
3953 15
51473546 36225
Satellite: ISS
Catalog Number: 25544
Epoch time: 14328
63562950 = yrday
fracday
Element set: 903
Inclination: 51
6452 deg
RA of node: 24
1200 deg
Eccentricity:
0007192
Arg of perigee: 61
7924 deg
Mean anomaly: 298
3953 deg
Mean motion: 15
51473546 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3622
Checksum: 303
Coasting Arc #5 (Orbit 3636)
---------------------------------------
Vector Time (GMT): 2014/329/14:07:07
165
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2882669
53 A = 6785793
73 meter
Y = -3330882
59 meter E =
0019856
Z = -5178675
21 I = 51
74946
XDOT = 6649
768672 Wp = 88
44910
YDOT = 3485
830408 meter/sec RA = 18
81572 deg
ZDOT = 1464
868283 TA = 195
63392
MA = 195
69533
Ha = 227
672 n
mi
Hp = 216
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9457577
20 X = 2944858
64
Y = -10928092
48 feet Y = -3298298
65 meter
Z = -16990404
22 Z = -5164520
59
XDOT = 21816
826352 XDOT = 6603
179128
YDOT = 11436
451471 feet/sec YDOT = 3559
931838 meter/sec
ZDOT = 4805
998305 ZDOT = 1497
059392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11779583
71 X = 3590417
12
Y = 8495915
56 feet Y = 2589555
06 meter
Z = -16929371
93 Z = -5160072
56
XDOT = -8720
794272 XDOT = -2658
098094
YDOT = 21904
875621 feet/sec YDOT = 6676
606089 meter/sec
ZDOT = 4942
580365 ZDOT = 1506
498495
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 14329
60180363
00016717 00000-0 10270-3 0 9047
2 25544 51
6461 19
3228 0007151 64
3865 295
8025 15
51492561 36375
Satellite: ISS
Catalog Number: 25544
Epoch time: 14329
60180363 = yrday
fracday
Element set: 904
Inclination: 51
6461 deg
RA of node: 19
3228 deg
Eccentricity:
0007151
Arg of perigee: 64
3865 deg
Mean anomaly: 295
8025 deg
Mean motion: 15
51492561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3637
Checksum: 306
Coasting Arc #6 (Orbit 3652)
---------------------------------------
Vector Time (GMT): 2014/330/14:07:07
165
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3545381
01 A = 6786752
92 meter
Y = 3093796
85 meter E =
0014245
Z = 4882039
15 I = 51
72207
XDOT = -6382
084037 Wp = 63
47230
YDOT = -3518
678863 meter/sec RA = 13
85014 deg
ZDOT = -2393
289077 TA = 50
00895
MA = 49
88398
Ha = 227
720 n
mi
Hp = 216
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11631827
48 X = -3603428
65
Y = 10150252
12 feet Y = 3053825
25 meter
Z = 16017188
81 Z = 4864675
22
XDOT = -20938
595922 XDOT = -6330
637089
YDOT = -11544
221992 feet/sec YDOT = -3589
759670 meter/sec
ZDOT = -7851
998284 ZDOT = -2424
167848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11391572
99 X = -3472151
45
Y = -10533070
87 feet Y = -3210480
00 meter
Z = 15942517
01 Z = 4859279
18
XDOT = 8386
310215 XDOT = 2556
147354
YDOT = -21210
568216 feet/sec YDOT = -6464
981192 meter/sec
ZDOT = -7982
975370 ZDOT = -2433
210893
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 14330
63235636
00016717 00000-0 10270-3 0 9057
2 25544 51
6447 14
2046 0007295 68
1752 292
0175 15
51576082 36531
Satellite: ISS
Catalog Number: 25544
Epoch time: 14330
63235636 = yrday
fracday
Element set: 905
Inclination: 51
6447 deg
RA of node: 14
2046 deg
Eccentricity:
0007295
Arg of perigee: 68
1752 deg
Mean anomaly: 292
0175 deg
Mean motion: 15
51576082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3653
Checksum: 302
Coasting Arc #7 (Orbit 3667)
---------------------------------------
Vector Time (GMT): 2014/331/14:07:07
165
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4171972
81 A = 6788322
00 meter
Y = -2937975
24 meter E =
0015627
Z = -4491001
61 I = 51
69739
XDOT = 5966
306814 Wp = 92
72190
YDOT = 3526
478276 meter/sec RA = 8
88536 deg
ZDOT = 3244
528906 TA = 209
93628
MA = 210
02573
Ha = 227
632 n
mi
Hp = 216
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13687574
84 X = 4226331
84
Y = -9639026
39 feet Y = -2891017
41 meter
Z = -14734257
26 Z = -4470602
72
XDOT = 19574
497420 XDOT = 5910
668506
YDOT = 11569
810618 feet/sec YDOT = 3592
886157 meter/sec
ZDOT = 10644
779876 ZDOT = 3273
377572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11326247
30 X = 3452240
18
Y = 12431809
60 feet Y = 3789215
57 meter
Z = -14646675
52 Z = -4464306
70
XDOT = -8069
989228 XDOT = -2459
732717
YDOT = 20002
527435 feet/sec YDOT = 6096
770362 meter/sec
ZDOT = 10767
095602 ZDOT = 3281
810740
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 14331
59847011
00016717 00000-0 10270-3 0 9060
2 25544 51
6453 9
4073 0007295 70
8689 289
3252 15
51587880 36682
Satellite: ISS
Catalog Number: 25544
Epoch time: 14331
59847011 = yrday
fracday
Element set: 906
Inclination: 51
6453 deg
RA of node: 9
4073 deg
Eccentricity:
0007295
Arg of perigee: 70
8689 deg
Mean anomaly: 289
3252 deg
Mean motion: 15
51587880 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3668
Checksum: 336
Coasting Arc #8 (Orbit 3683)
---------------------------------------
Vector Time (GMT): 2014/332/14:07:07
165
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4782721
04 A = 6790046
52 meter
Y = 2781454
53 meter E =
0018500
Z = 3923640
90 I = 51
67186
XDOT = -5431
252573 Wp = 77
84440
YDOT = -3587
229215 meter/sec RA = 3
91905 deg
ZDOT = -4057
466406 TA = 54
64489
MA = 54
47213
Ha = 227
593 n
mi
Hp = 215
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15691342
00 X = -4832528
35
Y = 9125507
00 feet Y = 2727692
46 meter
Z = 12872837
58 Z = 3900286
07
XDOT = -17819
070121 XDOT = -5371
025694
YDOT = -11769
124722 feet/sec YDOT = -3647
628151 meter/sec
ZDOT = -13311
897657 ZDOT = -4083
704624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11319290
48 X = -3450119
74
Y = -14280588
41 feet Y = -4352723
35 meter
Z = 12772685
58 Z = 3893114
57
XDOT = 8030
241055 XDOT = 2447
617474
YDOT = -18429
858683 feet/sec YDOT = -5617
420927 meter/sec
ZDOT = -13423
065752 ZDOT = -4091
350441
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
62895866
00016717 00000-0 10270-3 0 9077
2 25544 51
6443 4
2885 0007336 74
2506 285
9454 15
51678374 36840
Satellite: ISS
Catalog Number: 25544
Epoch time: 14332
62895866 = yrday
fracday
Element set: 907
Inclination: 51
6443 deg
RA of node: 4
2885 deg
Eccentricity:
0007336
Arg of perigee: 74
2506 deg
Mean anomaly: 285
9454 deg
Mean motion: 15
51678374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3684
Checksum: 341
Coasting Arc #9 (Orbit 3698)
---------------------------------------
Vector Time (GMT): 2014/333/14:07:07
165
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5302532
40 A = 6791949
98 meter
Y = -2696581
13 meter E =
0012046
Z = -3285197
02 I = 51
64720
XDOT = 4780
959400 Wp = 78
92683
YDOT = 3657
379396 meter/sec RA = 358
95484 deg
ZDOT = 4731
726609 TA = 243
01553
MA = 243
13859
Ha = 227
570 n
mi
Hp = 215
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17396759
84 X = 5348250
65
Y = -8847050
94 feet Y = -2637029
10 meter
Z = -10778205
45 Z = -3259326
86
XDOT = 15685
562336 XDOT = 4716
721020
YDOT = 11999
276235 feet/sec YDOT = 3710
483950 meter/sec
ZDOT = 15524
037430 ZDOT = 4754
796022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11562672
42 X = 3524302
56
Y = 15798719
13 feet Y = 4815449
59 meter
Z = -10667350
00 Z = -3251408
28
XDOT = -8162
471879 XDOT = -2487
921429
YDOT = 16483
636677 feet/sec YDOT = 5024
212459 meter/sec
ZDOT = 15621
674519 ZDOT = 4761
486393
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
59501293
00016717 00000-0 10270-3 0 9083
2 25544 51
6444 359
4911 0007446 77
7451 282
4533 15
51692657 36991
Satellite: ISS
Catalog Number: 25544
Epoch time: 14333
59501293 = yrday
fracday
Element set: 908
Inclination: 51
6444 deg
RA of node: 359
4911 deg
Eccentricity:
0007446
Arg of perigee: 77
7451 deg
Mean anomaly: 282
4533 deg
Mean motion: 15
51692657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3699
Checksum: 338
Coasting Arc #10 (Orbit 3714)
---------------------------------------
Vector Time (GMT): 2014/334/14:07:07
165
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5762976
80 A = 6793658
22 meter
Y = 2583412
72 meter E =
0020654
Z = 2482106
61 I = 51
62177
XDOT = -4010
601591 Wp = 96
25699
YDOT = -3808
223313 meter/sec RA = 353
98943 deg
ZDOT = -5312
367632 TA = 55
92925
MA = 55
73336
Ha = 227
441 n
mi
Hp = 215
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18907404
19 X = -5803494
20
Y = 8475763
51 feet Y = 2518740
81 meter
Z = 8143394
40 Z = 2454012
19
XDOT = -13158
141703 XDOT = -3941
913026
YDOT = -12494
170975 feet/sec YDOT = -3852
688365 meter/sec
ZDOT = -17429
027664 ZDOT = -5331
683959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11734761
11 X = -3576755
19
Y = -17133851
77 feet Y = -5222398
02 meter
Z = 8023084
06 Z = 2445436
02
XDOT = 8707
540234 XDOT = 2654
058263
YDOT = -14219
064946 feet/sec YDOT = -4333
970995 meter/sec
ZDOT = -17510
626399 ZDOT = -5337
238926
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
62543798
00016717 00000-0 10270-3 0 9095
2 25544 51
6438 354
3718 0007387 80
4611 279
7375 15
51774004 37155
Satellite: ISS
Catalog Number: 25544
Epoch time: 14334
62543798 = yrday
fracday
Element set: 909
Inclination: 51
6438 deg
RA of node: 354
3718 deg
Eccentricity:
0007387
Arg of perigee: 80
4611 deg
Mean anomaly: 279
7375 deg
Mean motion: 15
51774004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3715
Checksum: 334
Coasting Arc #11 (Orbit 3729)
---------------------------------------
Vector Time (GMT): 2014/335/14:07:07
165
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6091036
79 A = 6794964
99 meter
Y = -2513994
47 meter E =
0014180
Z = -1650588
55 I = 51
59511
XDOT = 3183
887500 Wp = 60
46847
YDOT = 3993
669088 meter/sec RA = 349
02563 deg
ZDOT = 5710
337754 TA = 281
46816
MA = 281
62737
Ha = 227
438 n
mi
Hp = 215
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19983716
50 X = 6126714
30
Y = -8248013
36 feet Y = -2445681
04 meter
Z = -5415316
77 Z = -1620912
11
XDOT = 10445
825130 XDOT = 3111
253355
YDOT = 13102
588873 feet/sec YDOT = 4028
867196 meter/sec
ZDOT = 18734
703918 ZDOT = 5725
628467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12011739
86 X = 3661178
31
Y = 18012675
69 feet Y = 5490263
55 meter
Z = -5288281
88 Z = -1611868
32
XDOT = -9512
601249 XDOT = -2899
440861
YDOT = 11819
428727 feet/sec YDOT = 3602
561876 meter/sec
ZDOT = 18799
096472 ZDOT = 5729
964605
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
59143264
00016717 00000-0 10270-3 0 9108
2 25544 51
6434 349
5741 0007544 85
2745 274
9268 15
51812367 37309
Satellite: ISS
Catalog Number: 25544
Epoch time: 14335
59143264 = yrday
fracday
Element set: 910
Inclination: 51
6434 deg
RA of node: 349
5741 deg
Eccentricity:
0007544
Arg of perigee: 85
2745 deg
Mean anomaly: 274
9268 deg
Mean motion: 15
51812367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3730
Checksum: 321
Coasting Arc #12 (Orbit 3745)
---------------------------------------
Vector Time (GMT): 2014/336/14:07:07
165
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6323269
84 A = 6795759
32 meter
Y = 2373679
72 meter E =
0019391
Z = 687865
05 I = 51
56768
XDOT = -2263
047747 Wp = 113
05853
YDOT = -4266
700633 meter/sec RA = 344
05982 deg
ZDOT = -5953
491495 TA = 59
50986
MA = 59
31852
Ha = 227
288 n
mi
Hp = 215
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20745635
95 X = -6352684
40
Y = 7787663
11 feet Y = 2302804
33 meter
Z = 2256775
10 Z = 657075
60
XDOT = -7424
697333 XDOT = -2186
247684
YDOT = -13998
361656 feet/sec YDOT = -4291
577939 meter/sec
ZDOT = -19532
452410 ZDOT = -5964
298804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12027631
17 X = -3666021
98
Y = -18626392
06 feet Y = -5677324
30 meter
Z = 2125029
08 Z = 647708
86
XDOT = 10767
233131 XDOT = 3281
852658
YDOT = -9236
497316 feet/sec YDOT = -2815
284382 meter/sec
ZDOT = -19577
671075 ZDOT = -5967
274144
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
62179430
00016717 00000-0 10270-3 0 9118
2 25544 51
6435 344
4543 0007441 87
3292 272
8712 15
51859103 37467
Satellite: ISS
Catalog Number: 25544
Epoch time: 14336
62179430 = yrday
fracday
Element set: 911
Inclination: 51
6435 deg
RA of node: 344
4543 deg
Eccentricity:
0007441
Arg of perigee: 87
3292 deg
Mean anomaly: 272
8712 deg
Mean motion: 15
51859103 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3746
Checksum: 309
Coasting Arc #13 (Orbit 3761)
---------------------------------------
Vector Time (GMT): 2014/337/14:07:07
165
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6405507
18 A = 6795699
94 meter
Y = -2237854
54 meter E =
0018716
Z = 245761
61 I = 51
53778
XDOT = 1356
660732 Wp = 64
17744
YDOT = 4579
867479 meter/sec RA = 339
09367 deg
ZDOT = 5995
348078 TA = 298
47212
MA = 298
66052
Ha = 227
216 n
mi
Hp = 215
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21015443
50 X = 6428861
46
Y = -7342042
47 feet Y = -2166093
44 meter
Z = 806304
48 Z = 276935
84
XDOT = 4450
986655 XDOT = 1276
222769
YDOT = 15025
811939 feet/sec YDOT = 4594
588532 meter/sec
ZDOT = 19669
777160 ZDOT = 6001
743473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11969770
14 X = 3648385
94
Y = 18762894
86 feet Y = 5718930
35 meter
Z = 939659
15 Z = 286408
11
XDOT = -12264
496015 XDOT = -3738
218385
YDOT = 6788
648442 feet/sec YDOT = 2069
180045 meter/sec
ZDOT = 19696
120572 ZDOT = 6003
377550
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
65212199
00016717 00000-0 10270-3 0 9123
2 25544 51
6430 339
3359 0007505 93
0250 267
1760 15
51928291 37622
Satellite: ISS
Catalog Number: 25544
Epoch time: 14337
65212199 = yrday
fracday
Element set: 912
Inclination: 51
6430 deg
RA of node: 339
3359 deg
Eccentricity:
0007505
Arg of perigee: 93
0250 deg
Mean anomaly: 267
1760 deg
Mean motion: 15
51928291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3762
Checksum: 309
Coasting Arc #14 (Orbit 3776)
---------------------------------------
Vector Time (GMT): 2014/338/14:07:07
165
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6373812
28 A = 6794962
89 meter
Y = 1983708
86 meter E =
0014948
Z = -1253589
04 I = 51
50726
XDOT = -407
283836 Wp = 120
16867
YDOT = -4955
341268 meter/sec RA = 334
12380 deg
ZDOT = -5830
099721 TA = 73
47081
MA = 73
30666
Ha = 227
112 n
mi
Hp = 215
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20911457
60 X = -6389431
22
Y = 6508231
18 feet Y = 1912345
51 meter
Z = -4112824
95 Z = -1284590
47
XDOT = -1336
233057 XDOT = -323
520555
YDOT = -16257
681326 feet/sec YDOT = -4959
427081 meter/sec
ZDOT = -19127
623755 ZDOT = -5831
875121
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11451575
21 X = -3490440
12
Y = -18638657
62 feet Y = -5681062
84 meter
Z = -4245389
06 Z = -1293994
58
XDOT = 14099
964553 XDOT = 4297
669196
YDOT = -4347
797391 feet/sec YDOT = -1325
208645 meter/sec
ZDOT = -19134
194083 ZDOT = -5832
102356
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
61802625
00016717 00000-0 10270-3 0 9130
2 25544 51
6436 334
5356 0007436 94
5553 265
6448 15
51947638 37775
Satellite: ISS
Catalog Number: 25544
Epoch time: 14338
61802625 = yrday
fracday
Element set: 913
Inclination: 51
6436 deg
RA of node: 334
5356 deg
Eccentricity:
0007436
Arg of perigee: 94
5553 deg
Mean anomaly: 265
6448 deg
Mean motion: 15
51947638 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3777
Checksum: 339
Coasting Arc #15 (Orbit 3792)
---------------------------------------
Vector Time (GMT): 2014/339/14:07:07
165
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6202823
64 A = 6793410
55 meter
Y = -1695199
04 meter E =
0020698
Z = 2167034
35 I = 51
47494
XDOT = -463
721576 Wp = 80
58819
YDOT = 5352
027370 meter/sec RA = 329
15116 deg
ZDOT = 5472
653789 TA = 303
50418
MA = 303
70178
Ha = 226
976 n
mi
Hp = 215
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20350471
27 X = 6210791
83
Y = -5561676
64 feet Y = -1625790
66 meter
Z = 7109692
75 Z = 2197186
47
XDOT = -1521
396246 XDOT = -550
119512
YDOT = 17559
144916 feet/sec YDOT = 5346
358237 meter/sec
ZDOT = 17954
900883 ZDOT = 5470
191614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10704496
10 X = 3262730
41
Y = 18128387
29 feet Y = 5525532
45 meter
Z = 7238576
95 Z = 2206318
26
XDOT = -16050
742328 XDOT = -4892
266262
YDOT = 2259
736347 feet/sec YDOT = 688
767638 meter/sec
ZDOT = 17943
325844 ZDOT = 5469
125717
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
64828953
00016717 00000-0 10270-3 0 9147
2 25544 51
6436 329
4167 0007426 99
8374 260
3616 15
52020677 37939
Satellite: ISS
Catalog Number: 25544
Epoch time: 14339
64828953 = yrday
fracday
Element set: 914
Inclination: 51
6436 deg
RA of node: 329
4167 deg
Eccentricity:
0007426
Arg of perigee: 99
8374 deg
Mean anomaly: 260
3616 deg
Mean motion: 15
52020677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3793
Checksum: 340
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