[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 28th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 200 21 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
209/20:07:13
933 12
2 -2
2 15
4
N/A -4
9 5
2 220
1
000/00:00:07
867 8
0 -14
3 196
9
210/19:08:14
928 9
4 -3
1 15
4
N/A -8
8 4
1 220
9
000/00:00:07
855 8
5 -14
5 194
5
211/18:09:43
921 6
1 -2
9 15
4
N/A -9
9 1
4 222
2
000/00:00:07
842 10
2 -15
1 191
6
212/18:46:43
915 6
4 -2
6 15
4
N/A -8
2 0
7 223
7
000/00:00:07
830 11
3 -15
2 188
9
212/21:51:11
193 -163
6 -284
4 284
4
N/A -232
5 0
1 219
7
000/00:02:22
385 -8
5 -0
1 32
4
212/22:28:24
000 0
0 0
0 0
0
N/A 0
0 0
0 216
3
000/00:00:00
000 0
0 0
0 31
9
Coasting Arc #1 (Orbit 1696)
---------------------------------------
Vector Time (GMT): 2014/208/20:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 11589
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1184504
30 A = 6773477
27 meter
Y = -6651310
07 meter E =
0028853
Z = 467378
05 I = 51
31364
XDOT = 4801
379766 Wp = 278
93130
YDOT = -458
233517 meter/sec RA = 256
72667 deg
ZDOT = 5967
233619 TA = 86
14115
MA = 85
81131
Ha = 220
289 n
mi
Hp = 198
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3886168
97 X = -1112310
12
Y = -21821883
42 feet Y = -6664152
32 meter
Z = 1533392
54 Z = 461799
07
XDOT = 15752
558289 XDOT = 4777
160694
YDOT = -1503
390803 feet/sec YDOT = -404
677074 meter/sec
ZDOT = 19577
538121 ZDOT = 5990
498715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22073454
38 X = 6727988
90
Y = 2031791
46 feet Y = 619290
04 meter
Z = 1510838
51 Z = 460503
58
XDOT = -2549
424740 XDOT = -777
064661
YDOT = 13858
017389 feet/sec YDOT = 4223
923700 meter/sec
ZDOT = 19676
342384 ZDOT = 5997
349159
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 14208
92430530
00016717 00000-0 10270-3 0 9008
2 25544 51
6457 257
2934 0038598 264
4397 95
2356 15
59564862 16974
Satellite: ISS
Catalog Number: 25544
Epoch time: 14208
92430530 = yrday
fracday
Element set: 900
Inclination: 51
6457 deg
RA of node: 257
2934 deg
Eccentricity:
0038598
Arg of perigee: 264
4397 deg
Mean anomaly: 95
2356 deg
Mean motion: 15
59564862 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1697
Checksum: 346
Coasting Arc #2 (Orbit 1711)
---------------------------------------
Vector Time (GMT): 2014/209/20:07:17
867
Vector Time (MET): N/A
Weight (LBS) : 11571
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4213433
29 A = 6760372
17 meter
Y = -714409
22 meter E =
0037614
Z = 5270974
45 I = 51
28300
XDOT = 1955
325046 Wp = 278
54785
YDOT = 7374
384890 meter/sec RA = 251
76739 deg
ZDOT = -561
485108 TA = 176
86184
MA = 176
83817
Ha = 220
116 n
mi
Hp = 196
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13823600
03 X = 4195504
64
Y = -2343862
29 feet Y = -667392
29 meter
Z = 17293223
27 Z = 5291398
74
XDOT = 6415
108417 XDOT = 1875
445120
YDOT = 24194
176149 feet/sec YDOT = 7395
803977 meter/sec
ZDOT = -1842
142743 ZDOT = -552
180415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3106438
15 X = -946842
35
Y = 13561938
55 feet Y = 4133678
87 meter
Z = 17380018
53 Z = 5297429
65
XDOT = -23817
292961 XDOT = -7259
510895
YDOT = -3135
242175 feet/sec YDOT = -955
621815 meter/sec
ZDOT = -1803
881596 ZDOT = -549
823111
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 14209
88545032
00016717 00000-0 10270-3 0 9019
2 25544 51
6467 252
4483 0040061 276
4808 83
1787 15
60020810 17123
Satellite: ISS
Catalog Number: 25544
Epoch time: 14209
88545032 = yrday
fracday
Element set: 901
Inclination: 51
6467 deg
RA of node: 252
4483 deg
Eccentricity:
0040061
Arg of perigee: 276
4808 deg
Mean anomaly: 83
1787 deg
Mean motion: 15
60020810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1712
Checksum: 296
Coasting Arc #3 (Orbit 1726)
---------------------------------------
Vector Time (GMT): 2014/210/19:08:18
855
Vector Time (MET): N/A
Weight (LBS) : 11553
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3664973
34 A = 6758596
33 meter
Y = -2183845
66 meter E =
0041473
Z = 5275589
29 I = 51
29206
XDOT = 3365
729156 Wp = 286
06657
YDOT = 6850
643332 meter/sec RA = 246
91817 deg
ZDOT = 512
273415 TA = 159
09573
MA = 158
92567
Ha = 220
918 n
mi
Hp = 194
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12024190
75 X = 3663494
57
Y = -7164847
97 feet Y = -2142869
91 meter
Z = 17308363
81 Z = 5293389
27
XDOT = 11042
418492 XDOT = 3286
385131
YDOT = 22475
863951 feet/sec YDOT = 6887
837440 meter/sec
ZDOT = 1680
687056 ZDOT = 528
430734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1303516
02 X = -397311
68
Y = 13841380
98 feet Y = 4218852
92 meter
Z = 17384265
47 Z = 5298724
11
XDOT = -23628
309779 XDOT = -7201
908820
YDOT = -4360
833989 feet/sec YDOT = -1329
182200 meter/sec
ZDOT = 1748
134000 ZDOT = 532
831243
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 14210
84632248
00016717 00000-0 10270-3 0 9024
2 25544 51
6455 247
6033 0044255 286
4746 73
1549 15
60631481 17271
Satellite: ISS
Catalog Number: 25544
Epoch time: 14210
84632248 = yrday
fracday
Element set: 902
Inclination: 51
6455 deg
RA of node: 247
6033 deg
Eccentricity:
0044255
Arg of perigee: 286
4746 deg
Mean anomaly: 73
1549 deg
Mean motion: 15
60631481 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1727
Checksum: 309
Coasting Arc #4 (Orbit 1741)
---------------------------------------
Vector Time (GMT): 2014/211/18:09:47
842
Vector Time (MET): N/A
Weight (LBS) : 11534
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3058789
55 A = 6757323
01 meter
Y = -3110949
63 meter E =
0045549
Z = 5193097
37 I = 51
30506
XDOT = 4345
103892 Wp = 293
74372
YDOT = 6188
053951 meter/sec RA = 242
06768 deg
ZDOT = 1173
831720 TA = 145
07085
MA = 144
77116
Ha = 222
242 n
mi
Hp = 191
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10035398
80 X = 3068123
57
Y = -10206527
65 feet Y = -3076692
10 meter
Z = 17037721
02 Z = 5207978
96
XDOT = 14255
590196 XDOT = 4269
882710
YDOT = 20302
014276 feet/sec YDOT = 6236
223115 meter/sec
ZDOT = 3851
153937 ZDOT = 1194
756606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1064940
96 X = -324594
00
Y = 14197706
00 feet Y = 4327460
79 meter
Z = 17101386
44 Z = 5212502
59
XDOT = -22907
716686 XDOT = -6982
272046
YDOT = -6359
807733 feet/sec YDOT = -1938
469397 meter/sec
ZDOT = 3938
959209 ZDOT = 1200
594767
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 14211
80682157
00016717 00000-0 10270-3 0 9036
2 25544 51
6445 242
7634 0049504 294
5849 65
0154 15
61200415 17428
Satellite: ISS
Catalog Number: 25544
Epoch time: 14211
80682157 = yrday
fracday
Element set: 903
Inclination: 51
6445 deg
RA of node: 242
7634 deg
Eccentricity:
0049504
Arg of perigee: 294
5849 deg
Mean anomaly: 65
0154 deg
Mean motion: 15
61200415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1742
Checksum: 298
Coasting Arc #5 (Orbit 1756)
---------------------------------------
Vector Time (GMT): 2014/212/18:09:47
842
Vector Time (MET): N/A
Weight (LBS) : 11534
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4948863
62 A = 6760197
61 meter
Y = -1110363
64 meter E =
0039944
Z = -4428548
82 I = 51
33064
XDOT = -1364
266515 Wp = 300
30891
YDOT = -6859
973292 meter/sec RA = 236
97363 deg
ZDOT = 3242
678046 TA = 2
29659
MA = 2
27830
Ha = 222
255 n
mi
Hp = 191
738
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16236429
19 X = -4914567
27
Y = -3642925
31 feet Y = -1165513
27 meter
Z = -14529359
65 Z = -4452506
09
XDOT = -4475
940009 XDOT = -1303
207014
YDOT = -22506
474055 feet/sec YDOT = -6874
887985 meter/sec
ZDOT = 10638
707501 ZDOT = 3236
199046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14587994
86 X = 4446420
83
Y = -7818119
08 feet Y = -2382962
70 meter
Z = -14630866
34 Z = -4459488
06
XDOT = 17600
765523 XDOT = 5364
713332
YDOT = 12970
321579 feet/sec YDOT = 3953
354017 meter/sec
ZDOT = 10612
309287 ZDOT = 3234
631871
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 14212
76698402
00016717 00000-0 10270-3 0 9043
2 25544 51
6443 237
9253 0049414 298
2509 61
3664 15
61220430 17573
Satellite: ISS
Catalog Number: 25544
Epoch time: 14212
76698402 = yrday
fracday
Element set: 904
Inclination: 51
6443 deg
RA of node: 237
9253 deg
Eccentricity:
0049414
Arg of perigee: 298
2509 deg
Mean anomaly: 61
3664 deg
Mean motion: 15
61220430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1757
Checksum: 310
Coasting Arc #6 (Orbit 1757)
---------------------------------------
Vector Time (GMT): 2014/212/18:46:47
830
Vector Time (MET): N/A
Weight (LBS) : 11516
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3378815
92 A = 6755396
94 meter
Y = -2572045
37 meter E =
0052125
Z = 5290280
74 I = 51
32010
XDOT = 4369
607330 Wp = 303
67611
YDOT = 6271
773881 meter/sec RA = 236
86805 deg
ZDOT = 288
809183 TA = 143
72912
MA = 143
37464
Ha = 223
659 n
mi
Hp = 188
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11085354
07 X = 3381627
84
Y = -8438469
08 feet Y = -2534245
54 meter
Z = 17356564
10 Z = 5306701
18
XDOT = 14335
982053 XDOT = 4297
747233
YDOT = 20576
685962 feet/sec YDOT = 6320
235856 meter/sec
ZDOT = 947
536688 ZDOT = 309
861290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -547947
38 X = -167014
36
Y = 13833075
97 feet Y = 4216321
56 meter
Z = 17426672
53 Z = 5311649
79
XDOT = -23972
039738 XDOT = -7306
677712
YDOT = -2129
514865 feet/sec YDOT = -649
076131 meter/sec
ZDOT = 1035
884201 ZDOT = 315
737505
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 14212
83098565
00016717 00000-0 10270-3 0 9056
2 25544 51
6449 237
6012 0054530 302
7242 56
8664 15
61718043 17581
Satellite: ISS
Catalog Number: 25544
Epoch time: 14212
83098565 = yrday
fracday
Element set: 905
Inclination: 51
6449 deg
RA of node: 237
6012 deg
Eccentricity:
0054530
Arg of perigee: 302
7242 deg
Mean anomaly: 56
8664 deg
Mean motion: 15
61718043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1758
Checksum: 311
Coasting Arc #7 (Orbit 1758)
---------------------------------------
Vector Time (GMT): 2014/212/21:52:22
385
Vector Time (MET): N/A
Weight (LBS) : 11183
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3675630
76 A = 6607747
66 meter
Y = -2124674
24 meter E =
0268222
Z = 5292403
22 I = 51
32389
XDOT = 4044
912348 Wp = 274
59382
YDOT = 6384
145030 meter/sec RA = 236
21098 deg
ZDOT = -235
818848 TA = 177
75745
MA = 177
63472
Ha = 219
672 n
mi
Hp = 32
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12059156
05 X = 3673407
70
Y = -6970716
01 feet Y = -2083583
37 meter
Z = 17363527
62 Z = 5310253
31
XDOT = 13270
709803 XDOT = 3974
368266
YDOT = 20945
357709 feet/sec YDOT = 6428
983412 meter/sec
ZDOT = -773
683886 ZDOT = -216
340842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8316568
64 X = 2534890
12
Y = 11054416
58 feet Y = 3369386
17 meter
Z = 17439632
38 Z = 5315599
95
XDOT = -18446
203216 XDOT = -5622
402740
YDOT = 15023
268403 feet/sec YDOT = 4579
092209 meter/sec
ZDOT = -692
033707 ZDOT = -210
931874
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 14212
95684777
00016717 00000-0 10270-3 0 9066
2 25544 51
6474 236
9451 0211875 274
3912 83
3101 16
29582797 17595
Satellite: ISS
Catalog Number: 25544
Epoch time: 14212
95684777 = yrday
fracday
Element set: 906
Inclination: 51
6474 deg
RA of node: 236
9451 deg
Eccentricity:
0211875
Arg of perigee: 274
3912 deg
Mean anomaly: 83
3101 deg
Mean motion: 16
29582797 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1759
Checksum: 345
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