[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 4th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 453 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
224/13:30:14
000 0
0 0
0 0
0
N/A 0
0 0
0 227
8
000/00:00:00
000 0
0 0
0 219
6
226/17:17:51
120 -2
6 3
7 3
7
N/A 1
8 0
2 228
0
000/00:07:42
239 -1
9 -0
3 221
5
227/10:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 221
2
Coasting Arc #1 (Orbit 1882)
---------------------------------------
Vector Time (GMT): 2014/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3752433
90 A = 6797827
56 meter
Y = -5239735
78 meter E =
0014397
Z = 2132772
37 I = 51
42561
XDOT = 5154
124012 Wp = 42
14423
YDOT = -1452
645626 meter/sec RA = 219
08801 deg
ZDOT = 5488
324073 TA = 341
55016
MA = 341
60232
Ha = 226
948 n
mi
Hp = 221
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12311134
86 X = -3703923
36
Y = -17190734
19 feet Y = -5281426
73 meter
Z = 6997284
66 Z = 2114661
37
XDOT = 16909
855684 XDOT = 5143
324388
YDOT = -4765
897722 feet/sec YDOT = -1395
069404 meter/sec
ZDOT = 18006
312576 ZDOT = 5513
335685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4454343
40 X = -1357683
87
Y = 20695482
40 feet Y = 6307983
04 meter
Z = 6921214
45 Z = 2109586
16
XDOT = -13294
260899 XDOT = -4052
090722
YDOT = -8931
138786 feet/sec YDOT = -2722
211102 meter/sec
ZDOT = 18112
729383 ZDOT = 5520
759916
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 14216
56027831
00016717 00000-0 10270-3 0 9003
2 25544 51
6436 219
8175 0006858 330
1710 29
9049 15
50566429 18838
Satellite: ISS
Catalog Number: 25544
Epoch time: 14216
56027831 = yrday
fracday
Element set: 900
Inclination: 51
6436 deg
RA of node: 219
8175 deg
Eccentricity:
0006858
Arg of perigee: 330
1710 deg
Mean anomaly: 29
9049 deg
Mean motion: 15
50566429 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1883
Checksum: 315
Coasting Arc #2 (Orbit 1897)
---------------------------------------
Vector Time (GMT): 2014/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3730700
71 A = 6796890
63 meter
Y = 5046147
75 meter E =
0003241
Z = -2616387
65 I = 51
44635
XDOT = -5448
723205 Wp = 19
50825
YDOT = 1325
544149 meter/sec RA = 214
11710 deg
ZDOT = -5211
667571 TA = 189
96891
MA = 189
97534
Ha = 227
118 n
mi
Hp = 220
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12239831
72 X = 3686705
74
Y = 16555602
84 feet Y = 5087620
96 meter
Z = -8583949
00 Z = -2598371
22
XDOT = -17876
388469 XDOT = -5437
824342
YDOT = 4348
898127 feet/sec YDOT = 1264
674154 meter/sec
ZDOT = -17098
646888 ZDOT = -5238
110007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3676021
20 X = 1120451
26
Y = -20289958
11 feet Y = -6184379
23 meter
Z = -8508238
03 Z = -2593310
95
XDOT = 13841
306329 XDOT = 4218
830169
YDOT = 9726
425773 feet/sec YDOT = 2964
614576 meter/sec
ZDOT = -17211
130186 ZDOT = -5245
952481
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 14217
52703214
00016717 00000-0 10270-3 0 9017
2 25544 51
6428 215
0234 0006872 334
5140 25
5672 15
50557569 18989
Satellite: ISS
Catalog Number: 25544
Epoch time: 14217
52703214 = yrday
fracday
Element set: 901
Inclination: 51
6428 deg
RA of node: 215
0234 deg
Eccentricity:
0006872
Arg of perigee: 334
5140 deg
Mean anomaly: 25
5672 deg
Mean motion: 15
50557569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1898
Checksum: 300
Coasting Arc #3 (Orbit 1913)
---------------------------------------
Vector Time (GMT): 2014/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3654268
65 A = 6795683
99 meter
Y = -4830519
11 meter E =
0012903
Z = 3062733
91 I = 51
46864
XDOT = 5765
234023 Wp = 53
06661
YDOT = -1251
263615 meter/sec RA = 209
14782 deg
ZDOT = 4898
537075 TA = 342
16192
MA = 342
20717
Ha = 227
179 n
mi
Hp = 220
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11989070
36 X = -3614858
72
Y = -15848159
83 feet Y = -4871163
30 meter
Z = 10048339
61 Z = 3045077
64
XDOT = 18914
809787 XDOT = 5755
002160
YDOT = -4105
195586 feet/sec YDOT = -1186
850505 meter/sec
ZDOT = 16071
315862 ZDOT = 4926
518595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2986650
35 X = -910331
03
Y = 19684210
20 feet Y = 5999747
27 meter
Z = 9974111
26 Z = 3040109
11
XDOT = -14607
618599 XDOT = -4452
402149
YDOT = -10431
367067 feet/sec YDOT = -3179
480682 meter/sec
ZDOT = 16190
337045 ZDOT = 4934
814731
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 14218
55822358
00016717 00000-0 10270-3 0 9023
2 25544 51
6423 209
9104 0006945 337
1356 22
9484 15
50605839 19146
Satellite: ISS
Catalog Number: 25544
Epoch time: 14218
55822358 = yrday
fracday
Element set: 902
Inclination: 51
6423 deg
RA of node: 209
9104 deg
Eccentricity:
0006945
Arg of perigee: 337
1356 deg
Mean anomaly: 22
9484 deg
Mean motion: 15
50605839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1914
Checksum: 313
Coasting Arc #4 (Orbit 1928)
---------------------------------------
Vector Time (GMT): 2014/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3535197
93 A = 6794538
98 meter
Y = 4637225
31 meter E =
0007431
Z = -3497063
51 I = 51
49184
XDOT = -6061
290850 Wp = 22
84055
YDOT = 1214
856229 meter/sec RA = 204
17813 deg
ZDOT = -4512
980976 TA = 198
25124
MA = 198
27792
Ha = 227
359 n
mi
Hp = 220
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11598418
40 X = 3500068
05
Y = 15213993
80 feet Y = 4676561
94 meter
Z = -11473305
48 Z = -3479975
33
XDOT = -19886
124835 XDOT = -6052
502848
YDOT = 3985
748783 feet/sec YDOT = 1147
124342 meter/sec
ZDOT = -14806
368031 ZDOT = -4542
404069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2470300
61 X = 752947
62
Y = -19013950
49 feet Y = -5795452
11 meter
Z = -11401445
41 Z = -3475160
56
XDOT = 15446
766670 XDOT = 4708
174481
YDOT = 10967
186691 feet/sec YDOT = 3342
798504 meter/sec
ZDOT = -14931
521941 ZDOT = -4551
127888
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 14219
52495795
00016717 00000-0 10270-3 0 9033
2 25544 51
6418 205
1158 0006997 342
1903 17
9002 15
50592066 19291
Satellite: ISS
Catalog Number: 25544
Epoch time: 14219
52495795 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 205
1158 deg
Eccentricity:
0006997
Arg of perigee: 342
1903 deg
Mean anomaly: 17
9002 deg
Mean motion: 15
50592066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1929
Checksum: 318
Coasting Arc #5 (Orbit 1944)
---------------------------------------
Vector Time (GMT): 2014/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3355429
52 A = 6793171
38 meter
Y = -4439144
54 meter E =
0010560
Z = 3884312
89 I = 51
51647
XDOT = 6366
657897 Wp = 61
34444
YDOT = -1227
573173 meter/sec RA = 199
21033 deg
ZDOT = 4093
358618 TA = 345
64356
MA = 345
67354
Ha = 227
401 n
mi
Hp = 220
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11008627
03 X = -3324409
01
Y = -14564122
52 feet Y = -4476493
85 meter
Z = 12743808
70 Z = 3868088
13
XDOT = 20887
985225 XDOT = 6360
027859
YDOT = -4027
471040 feet/sec YDOT = -1156
414351 meter/sec
ZDOT = 13429
654260 ZDOT = 4124
270230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2111226
90 X = -643501
96
Y = 18181881
96 feet Y = 5541837
62 meter
Z = 12675570
35 Z = 3863513
84
XDOT = -16453
714149 XDOT = -5015
092073
YDOT = -11372
824190 feet/sec YDOT = -3466
436813 meter/sec
ZDOT = 13561
149986 ZDOT = 4133
438516
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 14220
55612768
00016717 00000-0 10270-3 0 9040
2 25544 51
6417 200
0025 0007040 344
2547 15
8384 15
50641833 19459
Satellite: ISS
Catalog Number: 25544
Epoch time: 14220
55612768 = yrday
fracday
Element set: 904
Inclination: 51
6417 deg
RA of node: 200
0025 deg
Eccentricity:
0007040
Arg of perigee: 344
2547 deg
Mean anomaly: 15
8384 deg
Mean motion: 15
50641833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1945
Checksum: 283
Coasting Arc #6 (Orbit 1959)
---------------------------------------
Vector Time (GMT): 2014/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3142662
12 A = 6791996
63 meter
Y = 4278724
16 meter E =
0011522
Z = -4248222
58 I = 51
54239
XDOT = -6625
311906 Wp = 33
01099
YDOT = 1276
762588 meter/sec RA = 194
24210 deg
ZDOT = -3610
393947 TA = 199
91755
MA = 199
96256
Ha = 227
568 n
mi
Hp = 220
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10310571
27 X = 3115218
93
Y = 14037808
94 feet Y = 4313714
10 meter
Z = -13937738
12 Z = -4233022
85
XDOT = -21736
587617 XDOT = -6621
558804
YDOT = 4188
853634 feet/sec YDOT = 1202
695150 meter/sec
ZDOT = -11845
124498 ZDOT = -3642
568926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1945298
96 X = 592927
12
Y = -17359768
95 feet Y = -5291257
58 meter
Z = -13873814
82 Z = -4228738
76
XDOT = 17447
988812 XDOT = 5318
146990
YDOT = 11543
807735 feet/sec YDOT = 3518
552597 meter/sec
ZDOT = -11982
011960 ZDOT = -3652
117245
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 14221
52284167
00016717 00000-0 10270-3 0 9057
2 25544 51
6419 195
2077 0007110 349
3768 10
7237 15
50627113 19605
Satellite: ISS
Catalog Number: 25544
Epoch time: 14221
52284167 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 195
2077 deg
Eccentricity:
0007110
Arg of perigee: 349
3768 deg
Mean anomaly: 10
7237 deg
Mean motion: 15
50627113 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1960
Checksum: 296
Coasting Arc #7 (Orbit 1975)
---------------------------------------
Vector Time (GMT): 2014/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2868554
86 A = 6790670
68 meter
Y = -4130710
21 meter E =
0007901
Z = 4555125
24 I = 51
56948
XDOT = 6881
020839 Wp = 62
86984
YDOT = -1364
590018 meter/sec RA = 189
27617 deg
ZDOT = 3095
210726 TA = 356
10860
MA = 356
11474
Ha = 227
598 n
mi
Hp = 219
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9411269
24 X = -2844277
93
Y = -13552198
86 feet Y = -4162652
49 meter
Z = 14944636
62 Z = 4541249
51
XDOT = 22575
527686 XDOT = 6880
733404
YDOT = -4477
001372 feet/sec YDOT = -1287
643605 meter/sec
ZDOT = 10154
890833 ZDOT = 3128
636268
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1986022
31 X = -605339
60
Y = 16432588
15 feet Y = 5008652
87 meter
Z = 14886302
70 Z = 4537345
06
XDOT = -18538
470047 XDOT = -5650
525670
YDOT = -11570
537426 feet/sec YDOT = -3526
699807 meter/sec
ZDOT = 10297
120861 ZDOT = 3138
562438
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 14222
55398920
00016717 00000-0 10270-3 0 9065
2 25544 51
6424 190
0944 0007131 351
3684 8
7344 15
50677084 19765
Satellite: ISS
Catalog Number: 25544
Epoch time: 14222
55398920 = yrday
fracday
Element set: 906
Inclination: 51
6424 deg
RA of node: 190
0944 deg
Eccentricity:
0007131
Arg of perigee: 351
3684 deg
Mean anomaly: 8
7344 deg
Mean motion: 15
50677084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1976
Checksum: 314
Coasting Arc #8 (Orbit 1990)
---------------------------------------
Vector Time (GMT): 2014/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2578405
59 A = 6789676
16 meter
Y = 4032749
15 meter E =
0014899
Z = -4828768
71 I = 51
59760
XDOT = -7067
022392 Wp = 44
27684
YDOT = 1479
973581 meter/sec RA = 184
31013 deg
ZDOT = -2531
873740 TA = 200
71613
MA = 200
77658
Ha = 227
746 n
mi
Hp = 219
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8459335
92 X = 2556574
91
Y = 13230804
29 feet Y = 4061460
35 meter
Z = -15842417
03 Z = -4816296
60
XDOT = -23185
769003 XDOT = -7070
747810
YDOT = 4855
556367 feet/sec YDOT = 1400
924675 meter/sec
ZDOT = -8306
672375 ZDOT = -2566
212654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2207026
14 X = 672701
57
Y = -15601313
18 feet Y = -4755280
26 meter
Z = -15790021
75 Z = -4812798
63
XDOT = 19515
569120 XDOT = 5948
345468
YDOT = 11334
752800 feet/sec YDOT = 3454
832654 meter/sec
ZDOT = -8452
814979 ZDOT = -2576
418006
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 14223
52068200
00016717 00000-0 10270-3 0 9079
2 25544 51
6431 185
2998 0007203 356
0803 4
0291 15
50661916 19917
Satellite: ISS
Catalog Number: 25544
Epoch time: 14223
52068200 = yrday
fracday
Element set: 907
Inclination: 51
6431 deg
RA of node: 185
2998 deg
Eccentricity:
0007203
Arg of perigee: 356
0803 deg
Mean anomaly: 4
0291 deg
Mean motion: 15
50661916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1991
Checksum: 290
Coasting Arc #9 (Orbit 2006)
---------------------------------------
Vector Time (GMT): 2014/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2231377
55 A = 6788609
38 meter
Y = -3962066
66 meter E =
0006103
Z = 5035451
13 I = 51
62653
XDOT = 7239
617304 Wp = 50
00517
YDOT = -1617
188801 meter/sec RA = 179
34663 deg
ZDOT = 1937
936043 TA = 21
19874
MA = 21
17347
Ha = 227
768 n
mi
Hp = 219
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7320792
49 X = -2211367
11
Y = -12998906
37 feet Y = -3986907
25 meter
Z = 16520508
95 Z = 5024660
40
XDOT = 23752
025275 XDOT = 7247
749326
YDOT = -5305
737535 feet/sec YDOT = -1536
185169 meter/sec
ZDOT = 6358
057885 ZDOT = 1973
124238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2658644
09 X = -810354
72
Y = 14730609
19 feet Y = 4489889
68 meter
Z = 16475240
52 Z = 5021653
31
XDOT = -20506
403095 XDOT = -6250
351663
YDOT = -10971
305457 feet/sec YDOT = -3344
053903 meter/sec
ZDOT = 6507
842782 ZDOT = 1983
590480
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 14224
55180714
00016717 00000-0 10270-3 0 9089
2 25544 51
6439 180
1868 0007214 358
4360 1
6767 15
50711656 20078
Satellite: ISS
Catalog Number: 25544
Epoch time: 14224
55180714 = yrday
fracday
Element set: 908
Inclination: 51
6439 deg
RA of node: 180
1868 deg
Eccentricity:
0007214
Arg of perigee: 358
4360 deg
Mean anomaly: 1
6767 deg
Mean motion: 15
50711656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2007
Checksum: 301
Coasting Arc #10 (Orbit 2007)
---------------------------------------
Vector Time (GMT): 2014/224/13:30:14
000
Vector Time (MET): N/A
Weight (LBS) : 941131
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3327719
67 A = 6790167
27 meter
Y = -3635722
27 meter E =
0008191
Z = 4662484
06 I = 51
63470
XDOT = 6681
714421 Wp = 63
90721
YDOT = -2403
277989 meter/sec RA = 179
04213 deg
ZDOT = 2894
428054 TA = 357
31241
MA = 357
31681
Ha = 227
804 n
mi
Hp = 219
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10917715
46 X = -3309465
29
Y = -11928222
67 feet Y = -3672832
69 meter
Z = 15296863
70 Z = 4646363
27
XDOT = 21921
635240 XDOT = 6694
031892
YDOT = -7884
770306 feet/sec YDOT = -2328
489739 meter/sec
ZDOT = 9496
155033 ZDOT = 2926
916300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6956650
24 X = 2120386
99
Y = 14668293
77 feet Y = 4470895
94 meter
Z = 15228894
28 Z = 4641766
98
XDOT = -22148
149023 XDOT = -6750
755822
YDOT = 499
811614 feet/sec YDOT = 152
342580 meter/sec
ZDOT = 9634
583379 ZDOT = 2936
621014
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 14224
61625227
00016717 00000-0 10270-3 0 9090
2 25544 51
6450 179
8675 0007175 359
0160 1
0976 15
50709846 20088
Satellite: ISS
Catalog Number: 25544
Epoch time: 14224
61625227 = yrday
fracday
Element set: 909
Inclination: 51
6450 deg
RA of node: 179
8675 deg
Eccentricity:
0007175
Arg of perigee: 359
0160 deg
Mean anomaly: 1
0976 deg
Mean motion: 15
50709846 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2008
Checksum: 312
Coasting Arc #11 (Orbit 2022)
---------------------------------------
Vector Time (GMT): 2014/225/13:30:14
000
Vector Time (MET): N/A
Weight (LBS) : 941131
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3005790
68 A = 6789152
73 meter
Y = 3601558
56 meter E =
0016047
Z = -4922029
20 I = 51
66300
XDOT = -6836
404324 Wp = 48
14411
YDOT = 2543
751560 meter/sec RA = 174
08044 deg
ZDOT = -2307
955624 TA = 199
20720
MA = 199
26777
Ha = 227
902 n
mi
Hp = 219
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9861517
97 X = 2989203
12
Y = 11816137
01 feet Y = 3635078
24 meter
Z = -16148389
76 Z = -4907468
18
XDOT = -22429
148044 XDOT = -6853
129896
YDOT = 8345
641602 feet/sec YDOT = 2467
208833 meter/sec
ZDOT = -7572
032887 ZDOT = -2341
206194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6231267
45 X = -1899290
32
Y = -14142830
18 feet Y = -4310734
64 meter
Z = -16087037
73 Z = -4903329
10
XDOT = 22794
148072 XDOT = 6947
656332
YDOT = -1247
929223 feet/sec YDOT = -380
368827 meter/sec
ZDOT = -7713
733272 ZDOT = -2351
145901
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 14225
58292281
00016717 00000-0 10270-3 0 9109
2 25544 51
6454 175
0733 0007313 3
4006 356
7194 15
50715045 20235
Satellite: ISS
Catalog Number: 25544
Epoch time: 14225
58292281 = yrday
fracday
Element set: 910
Inclination: 51
6454 deg
RA of node: 175
0733 deg
Eccentricity:
0007313
Arg of perigee: 3
4006 deg
Mean anomaly: 356
7194 deg
Mean motion: 15
50715045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2023
Checksum: 278
Coasting Arc #12 (Orbit 2038)
---------------------------------------
Vector Time (GMT): 2014/226/13:30:14
000
Vector Time (MET): N/A
Weight (LBS) : 941131
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2633083
80 A = 6788196
63 meter
Y = -3603967
14 meter E =
0006553
Z = 5109039
28 I = 51
69105
XDOT = 6973
818058 Wp = 50
78637
YDOT = -2701
043330 meter/sec RA = 169
12041 deg
ZDOT = 1691
400685 TA = 22
90084
MA = 22
87163
Ha = 227
937 n
mi
Hp = 219
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8638726
36 X = -2617405
52
Y = -11824039
17 feet Y = -3633324
07 meter
Z = 16761939
89 Z = 5096286
52
XDOT = 22879
980506 XDOT = 6995
287241
YDOT = -8861
690714 feet/sec YDOT = -2622
937470 meter/sec
ZDOT = 5549
214846 ZDOT = 1725
330433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5296263
15 X = 1614301
01
Y = 13717924
05 feet Y = 4181223
25 meter
Z = 16708269
83 Z = 5092680
64
XDOT = -23376
162328 XDOT = -7125
054278
YDOT = 2100
522992 feet/sec YDOT = 640
239408 meter/sec
ZDOT = 5693
838213 ZDOT = 1735
481887
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 14226
61402455
00016717 00000-0 10270-3 0 9111
2 25544 51
6454 169
9599 0007216 6
0476 354
0761 15
50748073 20394
Satellite: ISS
Catalog Number: 25544
Epoch time: 14226
61402455 = yrday
fracday
Element set: 911
Inclination: 51
6454 deg
RA of node: 169
9599 deg
Eccentricity:
0007216
Arg of perigee: 6
0476 deg
Mean anomaly: 354
0761 deg
Mean motion: 15
50748073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2039
Checksum: 309
Coasting Arc #13 (Orbit 2040)
---------------------------------------
Vector Time (GMT): 2014/226/17:21:42
239
Vector Time (MET): N/A
Weight (LBS) : 940792
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2915054
87 A = 6790556
50 meter
Y = 3480167
21 meter E =
0013905
Z = -5061894
79 I = 51
69729
XDOT = -6806
683088 Wp = 51
13796
YDOT = 2935
868837 meter/sec RA = 168
32567 deg
ZDOT = -1896
377448 TA = 200
42367
MA = 200
47932
Ha = 227
980 n
mi
Hp = 221
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9563828
30 X = 2900511
00
Y = 11417871
42 feet Y = 3512683
67 meter
Z = -16607266
39 Z = -5047769
50
XDOT = -22331
637428 XDOT = -6829
794860
YDOT = 9632
115608 feet/sec YDOT = 2859
622797 meter/sec
ZDOT = -6221
710788 ZDOT = -1929
499301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14845825
45 X = -4525007
60
Y = -1846498
69 feet Y = -562812
80 meter
Z = -16547743
22 Z = -5043752
13
XDOT = 9735
685600 XDOT = 2967
436971
YDOT = -21104
784187 feet/sec YDOT = -6432
738220 meter/sec
ZDOT = -6362
937315 ZDOT = -1939
423294
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 14226
74291611
00016717 00000-0 10270-3 0 9126
2 25544 51
6458 169
3211 0005853 343
0178 17
0776 15
50033445 20416
Satellite: ISS
Catalog Number: 25544
Epoch time: 14226
74291611 = yrday
fracday
Element set: 912
Inclination: 51
6458 deg
RA of node: 169
3211 deg
Eccentricity:
0005853
Arg of perigee: 343
0178 deg
Mean anomaly: 17
0776 deg
Mean motion: 15
50033445 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2041
Checksum: 286
Coasting Arc #14 (Orbit 2051)
---------------------------------------
Vector Time (GMT): 2014/227/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 930248
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4095339
75 A = 6795782
03 meter
Y = 4059112
30 meter E =
0006347
Z = -3595450
02 I = 51
73448
XDOT = -5899
867582 Wp = 40
62055
YDOT = -2022
861106 meter/sec RA = 164
71605 deg
ZDOT = 4445
543248 TA = 277
01067
MA = 277
08286
Ha = 228
051 n
mi
Hp = 221
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13436154
04 X = -4122959
90
Y = 13317297
56 feet Y = 4013160
99 meter
Z = -11796095
85 Z = -3615411
69
XDOT = -19356
520937 XDOT = -5898
403838
YDOT = -6636
683419 feet/sec YDOT = -2088
828872 meter/sec
ZDOT = 14585
115642 ZDOT = 4416
886393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18440735
58 X = 5620736
20
Y = 3974465
90 feet Y = 1211417
21 meter
Z = -11881557
95 Z = -3621498
86
XDOT = 5294
286698 XDOT = 1613
698585
YDOT = 18585
300274 feet/sec YDOT = 5664
799524 meter/sec
ZDOT = 14463
599560 ZDOT = 4408
505146
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 14227
45211322
00016717 00000-0 10270-3 0 9137
2 25544 51
6435 165
8069 0005751 347
4140 12
6866 15
50013545 20529
Satellite: ISS
Catalog Number: 25544
Epoch time: 14227
45211322 = yrday
fracday
Element set: 913
Inclination: 51
6435 deg
RA of node: 165
8069 deg
Eccentricity:
0005751
Arg of perigee: 347
4140 deg
Mean anomaly: 12
6866 deg
Mean motion: 15
50013545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2052
Checksum: 280
Coasting Arc #15 (Orbit 2067)
---------------------------------------
Vector Time (GMT): 2014/228/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 930248
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4100235
74 A = 6796498
41 meter
Y = -4289653
10 meter E =
0012809
Z = 3309230
57 I = 51
76746
XDOT = 5748
803552 Wp = 65
46054
YDOT = 1841
431875 meter/sec RA = 159
76933 deg
ZDOT = -4716
387310 TA = 76
21978
MA = 76
07725
Ha = 228
106 n
mi
Hp = 221
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13452216
98 X = 4131823
82
Y = -14073665
04 feet Y = -4243624
91 meter
Z = 10857055
69 Z = 3329225
64
XDOT = 18860
904043 XDOT = 5750
695508
YDOT = 6041
443159 feet/sec YDOT = 1905
729157 meter/sec
ZDOT = -15473
711648 ZDOT = -4688
456083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19146343
77 X = -5835805
58
Y = -3252775
11 feet Y = -991445
85 meter
Z = 10942706
32 Z = 3335336
89
XDOT = -5804
299165 XDOT = -1769
150385
YDOT = -17705
982903 feet/sec YDOT = -5396
783589 meter/sec
ZDOT = -15355
242614 ZDOT = -4680
277949
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 14228
48366055
00016717 00000-0 10270-3 0 9146
2 25544 51
6439 160
6960 0005798 350
7988 9
3056 15
50058069 20685
Satellite: ISS
Catalog Number: 25544
Epoch time: 14228
48366055 = yrday
fracday
Element set: 914
Inclination: 51
6439 deg
RA of node: 160
6960 deg
Eccentricity:
0005798
Arg of perigee: 350
7988 deg
Mean anomaly: 9
3056 deg
Mean motion: 15
50058069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2068
Checksum: 335
Coasting Arc #16 (Orbit 2082)
---------------------------------------
Vector Time (GMT): 2014/229/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 930248
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4042392
38 A = 6797250
90 meter
Y = 4539892
11 meter E =
0008052
Z = -3035846
90 I = 51
79871
XDOT = -5596
404389 Wp = 27
58957
YDOT = -1677
991614 meter/sec RA = 154
82497 deg
ZDOT = 4954
807122 TA = 297
76077
MA = 297
84240
Ha = 228
202 n
mi
Hp = 220
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13262442
19 X = -4078111
00
Y = 14894659
17 feet Y = 4494487
71 meter
Z = -9960127
64 Z = -3055570
96
XDOT = -18360
906788 XDOT = -5601
293448
YDOT = -5505
221830 feet/sec YDOT = -1740
601479 meter/sec
ZDOT = 16255
928877 ZDOT = 4927
608929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19767451
96 X = 6025119
36
Y = 2302105
50 feet Y = 701681
76 meter
Z = -10044677
21 Z = -3061617
61
XDOT = 6219
251882 XDOT = 1895
627974
YDOT = 16849
224707 feet/sec YDOT = 5135
643691 meter/sec
ZDOT = 16140
540567 ZDOT = 4919
636765
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 14229
45072573
00016717 00000-0 10270-3 0 9154
2 25544 51
6438 155
9047 0005834 353
8498 6
2580 15
50050380 20831
Satellite: ISS
Catalog Number: 25544
Epoch time: 14229
45072573 = yrday
fracday
Element set: 915
Inclination: 51
6438 deg
RA of node: 155
9047 deg
Eccentricity:
0005834
Arg of perigee: 353
8498 deg
Mean anomaly: 6
2580 deg
Mean motion: 15
50050380 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2083
Checksum: 309
Coasting Arc #17 (Orbit 2098)
---------------------------------------
Vector Time (GMT): 2014/230/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 930248
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3997511
14 A = 6797942
21 meter
Y = -4780839
24 meter E =
0013355
Z = 2709153
94 I = 51
83000
XDOT = 5413
311980 Wp = 76
40805
YDOT = 1573
297358 meter/sec RA = 149
88281 deg
ZDOT = -5186
709806 TA = 73
12036
MA = 72
97396
Ha = 228
268 n
mi
Hp = 220
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13115194
03 X = 4037514
40
Y = -15685168
11 feet Y = -4735912
80 meter
Z = 8888300
31 Z = 2728670
31
XDOT = 17760
209909 XDOT = 5420
511820
YDOT = 5161
736738 feet/sec YDOT = 1633
872722 meter/sec
ZDOT = -17016
764457 ZDOT = -5160
395462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20362243
94 X = -6206411
95
Y = -1384420
22 feet Y = -421971
28 meter
Z = 8972017
49 Z = 2734670
93
XDOT = -6395
039046 XDOT = -1949
207901
YDOT = -16014
896222 feet/sec YDOT = -4881
340369 meter/sec
ZDOT = -16905
106762 ZDOT = -5152
676541
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 14230
48225092
00016717 00000-0 10270-3 0 9166
2 25544 51
6446 150
7936 0005843 357
7483 2
3640 15
50090245 20992
Satellite: ISS
Catalog Number: 25544
Epoch time: 14230
48225092 = yrday
fracday
Element set: 916
Inclination: 51
6446 deg
RA of node: 150
7936 deg
Eccentricity:
0005843
Arg of perigee: 357
7483 deg
Mean anomaly: 2
3640 deg
Mean motion: 15
50090245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2099
Checksum: 302
Coasting Arc #18 (Orbit 2113)
---------------------------------------
Vector Time (GMT): 2014/231/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 930248
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3885423
67 A = 6798616
33 meter
Y = 5029696
87 meter E =
0010453
Z = -2401021
74 I = 51
85858
XDOT = -5243
034356 Wp = 23
48361
YDOT = -1487
550508 meter/sec RA = 144
94285 deg
ZDOT = 5385
727978 TA = 309
81511
MA = 309
90707
Ha = 228
344 n
mi
Hp = 220
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12747452
99 X = -3929714
87
Y = 16501630
15 feet Y = 4985999
90 meter
Z = -7877367
91 Z = -2420003
97
XDOT = -17201
556286 XDOT = -5252
172384
YDOT = -4880
415054 feet/sec YDOT = -1546
232568 meter/sec
ZDOT = 17669
711214 ZDOT = 5360
236163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20819360
66 X = 6345741
13
Y = 254872
65 feet Y = 77685
18 meter
Z = -7958865
63 Z = -2425862
24
XDOT = 6505
066431 XDOT = 1982
744248
YDOT = 15258
271111 feet/sec YDOT = 4650
721035 meter/sec
ZDOT = 17561
526572 ZDOT = 5352
753299
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 14231
44929525
00016717 00000-0 10270-3 0 9176
2 25544 51
6445 146
0021 0005884
4725 359
6430 15
50086740 21148
Satellite: ISS
Catalog Number: 25544
Epoch time: 14231
44929525 = yrday
fracday
Element set: 917
Inclination: 51
6445 deg
RA of node: 146
0021 deg
Eccentricity:
0005884
Arg of perigee:
4725 deg
Mean anomaly: 359
6430 deg
Mean motion: 15
50086740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2114
Checksum: 288
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