[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 28th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 33368 12 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
087/22:41:48
919 -1
5 3
4 3
4
N/A 2
9 -0
2 226
3
000/00:07:37
837 -1
0 -0
1 221
3
087/22:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
3
000/00:00:00
000 0
0 0
0 221
2
Coasting Arc #1 (Orbit 3880)
---------------------------------------
Vector Time (GMT): 2014/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901633
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2330076
28 A = 6786239
30 meter
Y = 3521718
24 meter E =
0014961
Z = -5324817
39 I = 51
86226
XDOT = -5978
719473 Wp = 78
77968
YDOT = 4748
062220 meter/sec RA = 138
43127 deg
ZDOT = 528
139174 TA = 196
22999
MA = 196
27796
Ha = 226
258 n
mi
Hp = 219
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7644607
22 X = 2316388
59
Y = 11554193
69 feet Y = 3547697
34 meter
Z = -17469873
32 Z = -5313532
02
XDOT = -19615
221367 XDOT = -6033
934542
YDOT = 15577
631956 feet/sec YDOT = 4680
895694 meter/sec
ZDOT = 1732
740071 ZDOT = 498
960734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8731874
21 X = 2661475
26
Y = 10832451
75 feet Y = 3301731
29 meter
Z = -17422636
05 Z = -5310419
47
XDOT = -17402
245154 XDOT = -5304
204323
YDOT = 16593
447038 feet/sec YDOT = 5057
682657 meter/sec
ZDOT = 1608
708022 ZDOT = 490
334205
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 14087
51528353
00016717 00000-0 10270-3 0 9009
2 25544 51
6481 139
3969 0003973 359
4649
6497 15
51109261 38816
Satellite: ISS
Catalog Number: 25544
Epoch time: 14087
51528353 = yrday
fracday
Element set: 900
Inclination: 51
6481 deg
RA of node: 139
3969 deg
Eccentricity:
0003973
Arg of perigee: 359
4649 deg
Mean anomaly:
6497 deg
Mean motion: 15
51109261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3881
Checksum: 329
Coasting Arc #2 (Orbit 3887)
---------------------------------------
Vector Time (GMT): 2014/087/22:45:37
837
Vector Time (MET): N/A
Weight (LBS) : 900578
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3685656
80 A = 6788230
63 meter
Y = 2197589
95 meter E =
0012792
Z = -5270804
22 I = 51
87467
XDOT = -4900
354970 Wp = 66
98475
YDOT = 5791
531660 meter/sec RA = 136
22678 deg
ZDOT = -1008
997992 TA = 193
35050
MA = 193
38438
Ha = 226
278 n
mi
Hp = 221
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12092049
87 X = 3686412
74
Y = 7209940
78 feet Y = 2238808
77 meter
Z = -17292664
78 Z = -5252898
37
XDOT = -16077
280084 XDOT = -4959
851601
YDOT = 19001
088123 feet/sec YDOT = 5736
399931 meter/sec
ZDOT = -3310
360865 ZDOT = -1032
948532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10240727
56 X = -3121373
76
Y = -9794435
64 feet Y = -2985343
98 meter
Z = -17217250
10 Z = -5247817
83
XDOT = 19242
834041 XDOT = 5865
215816
YDOT = -14104
160147 feet/sec YDOT = -4298
948013 meter/sec
ZDOT = -3412
434627 ZDOT = -1040
110074
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 14087
96626867
00016717 00000-0 10270-3 0 9018
2 25544 51
6493 137
1593 0003906 322
1069 37
9807 15
50523539 38889
Satellite: ISS
Catalog Number: 25544
Epoch time: 14087
96626867 = yrday
fracday
Element set: 901
Inclination: 51
6493 deg
RA of node: 137
1593 deg
Eccentricity:
0003906
Arg of perigee: 322
1069 deg
Mean anomaly: 37
9807 deg
Mean motion: 15
50523539 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3888
Checksum: 341
Coasting Arc #3 (Orbit 3903)
---------------------------------------
Vector Time (GMT): 2014/088/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3349126
73 A = 6787773
00 meter
Y = -2527297
73 meter E =
0002603
Z = 5335384
25 I = 51
89509
XDOT = 4887
065016 Wp = 6
12686
YDOT = -5896
419559 meter/sec RA = 131
27899 deg
ZDOT = 277
163584 TA = 81
25349
MA = 81
22401
Ha = 226
384 n
mi
Hp = 221
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10987948
59 X = -3346534
64
Y = -8291659
23 feet Y = -2564734
51 meter
Z = 17504541
51 Z = 5319121
32
XDOT = 16033
677875 XDOT = 4951
290516
YDOT = -19345
208528 feet/sec YDOT = -5841
410114 meter/sec
ZDOT = 909
329344 ZDOT = 301
061196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9118675
47 X = 2779372
28
Y = 10427229
46 feet Y = 3178219
54 meter
Z = 17436118
94 Z = 5314529
05
XDOT = -18957
746275 XDOT = -5778
321065
YDOT = 14901
568689 feet/sec YDOT = 4541
998137 meter/sec
ZDOT = 1011
205635 ZDOT = 308
215478
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 14088
99749425
00016717 00000-0 10270-3 0 9029
2 25544 51
6490 132
0465 0003891 325
6427 34
4471 15
50564427 39046
Satellite: ISS
Catalog Number: 25544
Epoch time: 14088
99749425 = yrday
fracday
Element set: 902
Inclination: 51
6490 deg
RA of node: 132
0465 deg
Eccentricity:
0003891
Arg of perigee: 325
6427 deg
Mean anomaly: 34
4471 deg
Mean motion: 15
50564427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3904
Checksum: 319
Coasting Arc #4 (Orbit 3918)
---------------------------------------
Vector Time (GMT): 2014/089/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3159072
07 A = 6787620
67 meter
Y = 2770357
29 meter E =
0013080
Z = -5341671
97 I = 51
91407
XDOT = -4730
982640 Wp = 77
67419
YDOT = 6007
607375 meter/sec RA = 126
33391 deg
ZDOT = 321
201095 TA = 195
36241
MA = 195
40215
Ha = 226
336 n
mi
Hp = 220
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10364409
68 X = 3153806
82
Y = 9089098
71 feet Y = 2805653
83 meter
Z = -17525170
49 Z = -5326338
74
XDOT = -15521
596589 XDOT = -4799
369744
YDOT = 19709
997949 feet/sec YDOT = 5954
320164 meter/sec
ZDOT = 1053
809368 ZDOT = 298
051513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8531628
18 X = -2600440
27
Y = -10931562
95 feet Y = -3331940
39 meter
Z = -17460714
66 Z = -5322025
83
XDOT = 18229
973980 XDOT = 5556
496069
YDOT = -15735
467365 feet/sec YDOT = -4796
170453 meter/sec
ZDOT = 955
066868 ZDOT = 291
104381
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 14089
96423776
00016717 00000-0 10270-3 0 9036
2 25544 51
6482 127
2525 0003990 329
4602 30
6316 15
50618579 39197
Satellite: ISS
Catalog Number: 25544
Epoch time: 14089
96423776 = yrday
fracday
Element set: 903
Inclination: 51
6482 deg
RA of node: 127
2525 deg
Eccentricity:
0003990
Arg of perigee: 329
4602 deg
Mean anomaly: 30
6316 deg
Mean motion: 15
50618579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3919
Checksum: 327
Coasting Arc #5 (Orbit 3934)
---------------------------------------
Vector Time (GMT): 2014/090/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2972854
87 A = 6787719
75 meter
Y = -3062991
13 meter E =
0005430
Z = 5277357
56 I = 51
93249
XDOT = 4573
823456 Wp = 12
27907
YDOT = -6075
806989 meter/sec RA = 121
39011 deg
ZDOT = -944
531751 TA = 86
75893
MA = 86
69681
Ha = 226
398 n
mi
Hp = 220
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9753460
84 X = -2964018
81
Y = -10049183
48 feet Y = -3096185
38 meter
Z = 17314165
22 Z = 5262937
59
XDOT = 15005
982468 XDOT = 4646
012838
YDOT = -19933
749965 feet/sec YDOT = -6024
256053 meter/sec
ZDOT = -3098
857450 ZDOT = -922
136389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7947306
78 X = 2422339
11
Y = 11621078
55 feet Y = 3542104
74 meter
Z = 17253615
64 Z = 5258902
05
XDOT = -17439
742989 XDOT = -5315
633663
YDOT = 16411
550718 feet/sec YDOT = 5002
240659 meter/sec
ZDOT = -3003
278553 ZDOT = -915
399303
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 14090
99539785
00016717 00000-0 10270-3 0 9040
2 25544 51
6482 122
1393 0003981 332
9048 27
1894 15
50667925 39356
Satellite: ISS
Catalog Number: 25544
Epoch time: 14090
99539785 = yrday
fracday
Element set: 904
Inclination: 51
6482 deg
RA of node: 122
1393 deg
Eccentricity:
0003981
Arg of perigee: 332
9048 deg
Mean anomaly: 27
1894 deg
Mean motion: 15
50667925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3935
Checksum: 340
Coasting Arc #6 (Orbit 3949)
---------------------------------------
Vector Time (GMT): 2014/091/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2838634
35 A = 6788097
15 meter
Y = 3377436
49 meter E =
0011787
Z = -5168738
51 I = 51
94850
XDOT = -4387
823559 Wp = 85
63824
YDOT = 6074
014861 meter/sec RA = 116
44628 deg
ZDOT = 1563
153202 TA = 199
36999
MA = 199
41483
Ha = 226
382 n
mi
Hp = 220
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9313104
82 X = 2825764
47
Y = 11080828
36 feet Y = 3409107
36 meter
Z = -16957803
53 Z = -5154980
33
XDOT = -14395
746585 XDOT = -4463
011830
YDOT = 19927
870279 feet/sec YDOT = 6024
527182 meter/sec
ZDOT = 5128
455386 ZDOT = 1541
654205
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7545665
34 X = -2299918
80
Y = -12431221
84 feet Y = -3789036
42 meter
Z = -16900101
69 Z = -5151151
00
XDOT = 16494
802737 XDOT = 5027
615874
YDOT = -16841
870170 feet/sec YDOT = -5133
402028 meter/sec
ZDOT = 5036
649491 ZDOT = 1535
170765
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 14091
96208022
00016717 00000-0 10270-3 0 9056
2 25544 51
6471 117
3444 0004019 336
5676 23
5291 15
50711942 39504
Satellite: ISS
Catalog Number: 25544
Epoch time: 14091
96208022 = yrday
fracday
Element set: 905
Inclination: 51
6471 deg
RA of node: 117
3444 deg
Eccentricity:
0004019
Arg of perigee: 336
5676 deg
Mean anomaly: 23
5291 deg
Mean motion: 15
50711942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3950
Checksum: 294
Coasting Arc #7 (Orbit 3965)
---------------------------------------
Vector Time (GMT): 2014/092/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2715038
86 A = 6788707
22 meter
Y = -3731872
24 meter E =
0008176
Z = 4977787
43 I = 51
96444
XDOT = 4216
019010 Wp = 28
88137
YDOT = -6010
194782 meter/sec RA = 111
50452 deg
ZDOT = -2197
855958 TA = 82
51909
MA = 82
42620
Ha = 226
394 n
mi
Hp = 220
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8907607
81 X = -2697287
19
Y = -12243675
34 feet Y = -3762133
81 meter
Z = 16331323
57 Z = 4964641
49
XDOT = 13832
083366 XDOT = 4293
589612
YDOT = -19718
486819 feet/sec YDOT = -5962
615042 meter/sec
ZDOT = -7210
813511 ZDOT = -2177
185920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7188711
83 X = 2191119
36
Y = 13392936
05 feet Y = 4082166
91 meter
Z = 16276267
34 Z = 4961006
28
XDOT = -15548
266783 XDOT = -4739
111716
YDOT = 17035
371213 feet/sec YDOT = 5192
381146 meter/sec
ZDOT = -7122
504034 ZDOT = -2170
939230
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 14092
99317414
00016717 00000-0 10270-3 0 9067
2 25544 51
6474 112
2308 0004027 339
6346 20
4644 15
50771003 39666
Satellite: ISS
Catalog Number: 25544
Epoch time: 14092
99317414 = yrday
fracday
Element set: 906
Inclination: 51
6474 deg
RA of node: 112
2308 deg
Eccentricity:
0004027
Arg of perigee: 339
6346 deg
Mean anomaly: 20
4644 deg
Mean motion: 15
50771003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3966
Checksum: 297
Coasting Arc #8 (Orbit 3980)
---------------------------------------
Vector Time (GMT): 2014/093/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2652211
22 A = 6789594
12 meter
Y = 4083229
10 meter E =
0009147
Z = -4739756
66 I = 51
97712
XDOT = -4034
421923 Wp = 88
58352
YDOT = 5870
991272 meter/sec RA = 106
56274 deg
ZDOT = 2805
129027 TA = 209
10833
MA = 209
15935
Ha = 226
409 n
mi
Hp = 220
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8701480
37 X = 2629378
94
Y = 13396420
94 feet Y = 4112759
79 meter
Z = -15550382
73 Z = -4726928
26
XDOT = -13236
292398 XDOT = -4113
399363
YDOT = 19261
782390 feet/sec YDOT = 5825
434413 meter/sec
ZDOT = 9203
179221 ZDOT = 2785
337899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7065360
24 X = -2153521
80
Y = -14384936
97 feet Y = -4384528
79 meter
Z = -15496726
46 Z = -4723402
22
XDOT = 14535
901635 XDOT = 4430
542818
YDOT = -16945
525396 feet/sec YDOT = -5164
996141 meter/sec
ZDOT = 9118
589434 ZDOT = 2779
346059
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 14093
95979459
00016717 00000-0 10270-3 0 9078
2 25544 51
6463 107
4353 0003967 343
8029 16
2995 15
50806618 39817
Satellite: ISS
Catalog Number: 25544
Epoch time: 14093
95979459 = yrday
fracday
Element set: 907
Inclination: 51
6463 deg
RA of node: 107
4353 deg
Eccentricity:
0003967
Arg of perigee: 343
8029 deg
Mean anomaly: 16
2995 deg
Mean motion: 15
50806618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3981
Checksum: 349
Coasting Arc #9 (Orbit 3996)
---------------------------------------
Vector Time (GMT): 2014/094/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2601210
58 A = 6790652
73 meter
Y = -4458745
83 meter E =
0010590
Z = 4409337
53 I = 51
98982
XDOT = 3886
549413 Wp = 48
64482
YDOT = -5654
617356 meter/sec RA = 101
62350 deg
ZDOT = -3413
066274 TA = 75
83419
MA = 75
71655
Ha = 226
371 n
mi
Hp = 220
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8534155
45 X = -2572577
84
Y = -14628431
21 feet Y = -4487673
84 meter
Z = 14466330
49 Z = 4396770
99
XDOT = 12751
146369 XDOT = 3966
071453
YDOT = -18551
894211 feet/sec YDOT = -5610
711071 meter/sec
ZDOT = -11197
723996 ZDOT = -3393
992292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7006558
92 X = 2135599
16
Y = 15467604
22 feet Y = 4714525
77 meter
Z = 14413843
30 Z = 4393339
44
XDOT = -13608
278361 XDOT = -4147
803244
YDOT = 16560
353520 feet/sec YDOT = 5047
595753 meter/sec
ZDOT = -11116
183213 ZDOT = -3388
212643
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
99082109
00016717 00000-0 10270-3 0 9081
2 25544 51
6469 102
3214 0004001 346
2223 13
8819 15
50874088 39977
Satellite: ISS
Catalog Number: 25544
Epoch time: 14094
99082109 = yrday
fracday
Element set: 908
Inclination: 51
6469 deg
RA of node: 102
3214 deg
Eccentricity:
0004001
Arg of perigee: 346
2223 deg
Mean anomaly: 13
8819 deg
Mean motion: 15
50874088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3997
Checksum: 312
Coasting Arc #10 (Orbit 4011)
---------------------------------------
Vector Time (GMT): 2014/095/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2610664
44 A = 6791899
67 meter
Y = 4803328
55 meter E =
0006300
Z = -4034165
85 I = 51
99838
XDOT = -3751
950562 Wp = 74
68282
YDOT = 5367
585951 meter/sec RA = 96
68430 deg
ZDOT = 3969
721391 TA = 236
42188
MA = 236
48204
Ha = 226
410 n
mi
Hp = 219
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8565172
05 X = 2576355
27
Y = 15758951
95 feet Y = 4832330
57 meter
Z = -13235452
27 Z = -4021567
22
XDOT = -12309
549087 XDOT = -3830
976976
YDOT = 17610
190129 feet/sec YDOT = 5325
187643 meter/sec
ZDOT = 13024
020311 ZDOT = 3951
302552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7192943
29 X = -2192409
11
Y = -16472917
08 feet Y = -5020945
13 meter
Z = -13182886
83 Z = -4018143
91
XDOT = 12725
903965 XDOT = 3878
855529
YDOT = -15898
750467 feet/sec YDOT = -4845
939142 meter/sec
ZDOT = 12945
279719 ZDOT = 3945
721258
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
95737815
00016717 00000-0 10270-3 0 9090
2 25544 51
6456 97
5256 0003840 351
4447 8
6637 15
50905114 40124
Satellite: ISS
Catalog Number: 25544
Epoch time: 14095
95737815 = yrday
fracday
Element set: 909
Inclination: 51
6456 deg
RA of node: 97
5256 deg
Eccentricity:
0003840
Arg of perigee: 351
4447 deg
Mean anomaly: 8
6637 deg
Mean motion: 15
50905114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4012
Checksum: 318
Coasting Arc #11 (Orbit 4027)
---------------------------------------
Vector Time (GMT): 2014/096/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2625043
56 A = 6793191
98 meter
Y = -5151643
71 meter E =
0012422
Z = 3560284
17 I = 52
00660
XDOT = 3672
239719 Wp = 69
47791
YDOT = -4995
685828 meter/sec RA = 91
74769 deg
ZDOT = -4504
123512 TA = 68
81467
MA = 68
68199
Ha = 226
327 n
mi
Hp = 219
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8612347
64 X = -2584536
37
Y = -16901718
20 feet Y = -5180771
88 meter
Z = 11680722
33 Z = 3547630
82
XDOT = 12048
030575 XDOT = 3749
709307
YDOT = -16390
045368 feet/sec YDOT = -4954
187663 meter/sec
ZDOT = -14777
308110 ZDOT = -4486
095716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7429207
67 X = 2264422
50
Y = 17489332
21 feet Y = 5330748
46 meter
Z = 11627984
18 Z = 3544209
58
XDOT = -12028
353220 XDOT = -3666
242062
YDOT = 14920
184762 feet/sec YDOT = 4547
672315 meter/sec
ZDOT = -14700
266505 ZDOT = -4480
641231
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
98833532
00016717 00000-0 10270-3 0 9109
2 25544 51
6461 92
4112 0003902 353
1569 6
9529 15
50980496 40282
Satellite: ISS
Catalog Number: 25544
Epoch time: 14096
98833532 = yrday
fracday
Element set: 910
Inclination: 51
6461 deg
RA of node: 92
4112 deg
Eccentricity:
0003902
Arg of perigee: 353
1569 deg
Mean anomaly: 6
9529 deg
Mean motion: 15
50980496 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4028
Checksum: 315
Coasting Arc #12 (Orbit 4042)
---------------------------------------
Vector Time (GMT): 2014/097/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2689033
03 A = 6794525
29 meter
Y = 5441947
57 meter E =
0006672
Z = -3050121
63 I = 52
01023
XDOT = -3628
470271 Wp = 39
63579
YDOT = 4569
144718 meter/sec RA = 86
81105 deg
ZDOT = 4964
196176 TA = 285
63514
MA = 285
70876
Ha = 226
388 n
mi
Hp = 219
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8822286
84 X = 2642796
61
Y = 17854158
70 feet Y = 5471759
29 meter
Z = -10006960
71 Z = -3037171
43
XDOT = -11904
430022 XDOT = -3703
408294
YDOT = 14990
632278 feet/sec YDOT = 4528
150245 meter/sec
ZDOT = 16286
732861 ZDOT = 4946
387167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7874960
25 X = -2400287
88
Y = -18321174
61 feet Y = -5584294
02 meter
Z = -9953017
27 Z = -3033679
66
XDOT = 11487
762635 XDOT = 3501
470051
YDOT = -13724
606833 feet/sec YDOT = -4183
260163 meter/sec
ZDOT = 16210
673021 ZDOT = 4941
013137
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
95482702
00016717 00000-0 10270-3 0 9117
2 25544 51
6450 87
6150 0003667 359
7727
3421 15
51007817 40438
Satellite: ISS
Catalog Number: 25544
Epoch time: 14097
95482702 = yrday
fracday
Element set: 911
Inclination: 51
6450 deg
RA of node: 87
6150 deg
Eccentricity:
0003667
Arg of perigee: 359
7727 deg
Mean anomaly:
3421 deg
Mean motion: 15
51007817 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4043
Checksum: 299
Coasting Arc #13 (Orbit 4058)
---------------------------------------
Vector Time (GMT): 2014/098/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2741415
88 A = 6795682
48 meter
Y = -5714052
09 meter E =
0013279
Z = 2441287
49 I = 52
01247
XDOT = 3657
893938 Wp = 89
79685
YDOT = -4060
760030 meter/sec RA = 81
87666 deg
ZDOT = -5371
758096 TA = 63
06866
MA = 62
93305
Ha = 226
269 n
mi
Hp = 219
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8994146
58 X = -2689175
31
Y = -18746890
07 feet Y = -5744416
04 meter
Z = 8009473
39 Z = 2428097
49
XDOT = 12000
964362 XDOT = 3729
124703
YDOT = -13322
703512 feet/sec YDOT = -4019
457340 meter/sec
ZDOT = -17623
878268 ZDOT = -5353
815160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8313713
26 X = 2534019
80
Y = 19081386
37 feet Y = 5816006
57 meter
Z = 7954564
11 Z = 2424551
14
XDOT = -11224
915434 XDOT = -3421
354224
YDOT = 12240
456528 feet/sec YDOT = 3730
891150 meter/sec
ZDOT = -17547
323593 ZDOT = -5348
424231
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
98571260
00016717 00000-0 10270-3 0 9120
2 25544 51
6452 82
4999 0003769 1
0531 359
0628 15
51094615 40599
Satellite: ISS
Catalog Number: 25544
Epoch time: 14098
98571260 = yrday
fracday
Element set: 912
Inclination: 51
6452 deg
RA of node: 82
4999 deg
Eccentricity:
0003769
Arg of perigee: 1
0531 deg
Mean anomaly: 359
0628 deg
Mean motion: 15
51094615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4059
Checksum: 323
Coasting Arc #14 (Orbit 4073)
---------------------------------------
Vector Time (GMT): 2014/099/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2822282
00 A = 6796737
50 meter
Y = 5906292
50 meter E =
0010549
Z = -1811603
11 I = 52
01046
XDOT = -3740
380965 Wp = 29
06929
YDOT = 3524
021599 meter/sec RA = 76
94196 deg
ZDOT = 5684
914003 TA = 311
14939
MA = 311
24036
Ha = 226
343 n
mi
Hp = 219
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9259455
39 X = 2764826
95
Y = 19377600
06 feet Y = 5937531
63 meter
Z = -5943579
76 Z = -1798033
01
XDOT = -12271
591092 XDOT = -3807
124902
YDOT = 11561
750653 feet/sec YDOT = 3481
821663 meter/sec
ZDOT = 18651
292661 ZDOT = 5666
581254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8879518
81 X = -2706477
33
Y = -19571694
91 feet Y = -5965452
61 meter
Z = -5887099
68 Z = -1794387
98
XDOT = 11205
609033 XDOT = 3415
469633
YDOT = -10647
917369 feet/sec YDOT = -3245
485214 meter/sec
ZDOT = 18573
167708 ZDOT = 5661
101517
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
95213675
00016717 00000-0 10270-3 0 9132
2 25544 51
6447 77
7034 0003490 8
9774 351
1439 15
51115620 40746
Satellite: ISS
Catalog Number: 25544
Epoch time: 14099
95213675 = yrday
fracday
Element set: 913
Inclination: 51
6447 deg
RA of node: 77
7034 deg
Eccentricity:
0003490
Arg of perigee: 8
9774 deg
Mean anomaly: 351
1439 deg
Mean motion: 15
51115620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4074
Checksum: 312
Coasting Arc #15 (Orbit 4089)
---------------------------------------
Vector Time (GMT): 2014/100/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2865809
77 A = 6797329
12 meter
Y = -6061292
29 meter E =
0012623
Z = 1092644
84 I = 52
00536
XDOT = 3905
255140 Wp = 107
80646
YDOT = -2921
237520 meter/sec RA = 72
00860 deg
ZDOT = -5910
110253 TA = 60
41658
MA = 60
29084
Ha = 226
210 n
mi
Hp = 218
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9402263
02 X = -2803125
77
Y = -19886129
55 feet Y = -6092989
00 meter
Z = 3584792
78 Z = 1078876
04
XDOT = 12812
516863 XDOT = 3966
340339
YDOT = -9584
112600 feet/sec YDOT = -2877
225579 meter/sec
ZDOT = -19390
125503 ZDOT = -5890
990311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9340763
92 X = 2847064
84
Y = 19925317
45 feet Y = 6073236
76 meter
Z = 3527504
98 Z = 1075183
52
XDOT = -11520
873143 XDOT = -3511
562134
YDOT = 8850
056230 feet/sec YDOT = 2697
497139 meter/sec
ZDOT = -19308
762060 ZDOT = -5885
310676
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
98294881
00016717 00000-0 10270-3 0 9147
2 25544 51
6446 72
5875 0003631 10
4131 349
7095 15
51213094 40906
Satellite: ISS
Catalog Number: 25544
Epoch time: 14100
98294881 = yrday
fracday
Element set: 914
Inclination: 51
6446 deg
RA of node: 72
5875 deg
Eccentricity:
0003631
Arg of perigee: 10
4131 deg
Mean anomaly: 349
7095 deg
Mean motion: 15
51213094 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4090
Checksum: 297
Coasting Arc #16 (Orbit 4104)
---------------------------------------
Vector Time (GMT): 2014/101/22:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2908759
60 A = 6797705
65 meter
Y = 6124249
35 meter E =
0014435
Z = -375499
52 I = 51
99687
XDOT = -4129
919465 Wp = 37
11938
YDOT = 2322
950324 meter/sec RA = 67
07454 deg
ZDOT = 6026
020195 TA = 318
85636
MA = 318
96510
Ha = 226
257 n
mi
Hp = 218
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9543174
52 X = 2841884
74
Y = 20092681
60 feet Y = 6156403
00 meter
Z = -1231953
81 Z = -361532
28
XDOT = -13549
604544 XDOT = -4184
860921
YDOT = 7621
228098 feet/sec YDOT = 2276
460452 meter/sec
ZDOT = 19770
407463 ZDOT = 6005
823779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9810981
63 X = -2990387
20
Y = -19966784
12 feet Y = -6085875
80 meter
Z = -1173846
32 Z = -357788
36
XDOT = 12116
878673 XDOT = 3693
224620
YDOT = -7084
445301 feet/sec YDOT = -2159
338928 meter/sec
ZDOT = 19684
583509 ZDOT = 5999
861054
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
94930316
00016717 00000-0 10270-3 0 9155
2 25544 51
6452 67
7909 0003314 18
7126 341
4147 15
51232830 41053
Satellite: ISS
Catalog Number: 25544
Epoch time: 14101
94930316 = yrday
fracday
Element set: 915
Inclination: 51
6452 deg
RA of node: 67
7909 deg
Eccentricity:
0003314
Arg of perigee: 18
7126 deg
Mean anomaly: 341
4147 deg
Mean motion: 15
51232830 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4105
Checksum: 282
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