[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 6th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 123 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 362 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 1875)
---------------------------------------
Vector Time (GMT): 2013/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4368995
97 A = 6782393
61 meter
Y = -570380
85 meter E =
0013804
Z = -5163498
86 I = 51
28019
XDOT = -582
641741 Wp = 48
70578
YDOT = -7520
202075 meter/sec RA = 257
41224 deg
ZDOT = 1334
977266 TA = 234
13737
MA = 234
26564
Ha = 225
706 n
mi
Hp = 216
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14333976
27 X = -4337210
65
Y = -1871328
24 feet Y = -619060
30 meter
Z = -16940613
04 Z = -5184645
47
XDOT = -1911
554269 XDOT = -504
990793
YDOT = -24672
578986 feet/sec YDOT = -7526
283289 meter/sec
ZDOT = 4379
846674 ZDOT = 1332
335955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13118782
44 X = -3998604
89
Y = -5820294
07 feet Y = -1774025
63 meter
Z = -17028530
17 Z = -5190296
00
XDOT = 4693
827326 XDOT = 1430
678569
YDOT = -23256
632211 feet/sec YDOT = -7088
621498 meter/sec
ZDOT = 4369
711237 ZDOT = 1331
887985
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 13065
51380085
00016717 00000-0 10270-3 0 9002
2 25544 51
6439 258
2221 0012065 343
7768 16
2996 15
52597193 18766
Satellite: ISS
Catalog Number: 25544
Epoch time: 13065
51380085 = yrday
fracday
Element set: 900
Inclination: 51
6439 deg
RA of node: 258
2221 deg
Eccentricity:
0012065
Arg of perigee: 343
7768 deg
Mean anomaly: 16
2996 deg
Mean motion: 15
52597193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1876
Checksum: 322
Coasting Arc #2 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2013/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4535286
63 A = 6784178
78 meter
Y = 1706810
03 meter E =
0015837
Z = 4751083
56 I = 51
29358
XDOT = 68
205594 Wp = 14
35789
YDOT = 7195
710689 meter/sec RA = 252
40583 deg
ZDOT = -2633
171611 TA = 101
85754
MA = 101
67989
Ha = 225
895 n
mi
Hp = 216
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14879549
32 X = 4492784
61
Y = 5599770
44 feet Y = 1757289
18 meter
Z = 15587544
48 Z = 4773011
78
XDOT = 223
771634 XDOT =
527546
YDOT = 23607
974700 feet/sec YDOT = 7196
094794 meter/sec
ZDOT = -8639
014471 ZDOT = -2633
005219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12758107
72 X = 3888671
23
Y = 9335004
93 feet Y = 2845309
50 meter
Z = 15678594
66 Z = 4778835
65
XDOT = -5338
225631 XDOT = -1627
091172
YDOT = 21898
525717 feet/sec YDOT = 6674
670639 meter/sec
ZDOT = -8639
125710 ZDOT = -2633
205516
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 13066
54365476
00016717 00000-0 10270-3 0 9014
2 25544 51
6439 253
1001 0012092 347
1536 12
9306 15
52579490 18923
Satellite: ISS
Catalog Number: 25544
Epoch time: 13066
54365476 = yrday
fracday
Element set: 901
Inclination: 51
6439 deg
RA of node: 253
1001 deg
Eccentricity:
0012092
Arg of perigee: 347
1536 deg
Mean anomaly: 12
9306 deg
Mean motion: 15
52579490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1892
Checksum: 301
Coasting Arc #3 (Orbit 1906)
---------------------------------------
Vector Time (GMT): 2013/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4684135
87 A = 6786519
66 meter
Y = -2673925
44 meter E =
0010778
Z = -4117107
04 I = 51
31111
XDOT = 498
888228 Wp = 30
19303
YDOT = -6655
959537 meter/sec RA = 247
40335 deg
ZDOT = 3768
682851 TA = 278
78858
MA = 278
91062
Ha = 225
965 n
mi
Hp = 215
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15367899
85 X = -4633887
95
Y = -8772721
26 feet Y = -2726025
85 meter
Z = -13507569
02 Z = -4139739
37
XDOT = 1636
772403 XDOT = 554
972641
YDOT = -21837
137587 feet/sec YDOT = -6650
066699 meter/sec
ZDOT = 12364
445048 ZDOT = 3771
243231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12609990
77 X = -3843525
19
Y = -12311621
32 feet Y = -3752582
18 meter
Z = -13601452
80 Z = -4145722
81
XDOT = 6064
784165 XDOT = 1848
546213
YDOT = -19835
721989 feet/sec YDOT = -6045
928062 meter/sec
ZDOT = 12375
828952 ZDOT = 3772
152665
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 13067
50914311
00016717 00000-0 10270-3 0 9020
2 25544 51
6432 248
2971 0011996 351
3667 8
7277 15
52591297 19077
Satellite: ISS
Catalog Number: 25544
Epoch time: 13067
50914311 = yrday
fracday
Element set: 902
Inclination: 51
6432 deg
RA of node: 248
2971 deg
Eccentricity:
0011996
Arg of perigee: 351
3667 deg
Mean anomaly: 8
7277 deg
Mean motion: 15
52591297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1907
Checksum: 321
Coasting Arc #4 (Orbit 1922)
---------------------------------------
Vector Time (GMT): 2013/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4786915
80 A = 6789287
46 meter
Y = 3565827
66 meter E =
0016244
Z = 3237692
12 I = 51
33280
XDOT = -1183
748680 Wp = 45
40029
YDOT = 5908
102894 meter/sec RA = 242
40735 deg
ZDOT = -4730
801022 TA = 96
96306
MA = 96
77827
Ha = 226
184 n
mi
Hp = 215
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15705104
34 X = 4730958
66
Y = 11698909
65 feet Y = 3619045
48 meter
Z = 10622349
48 Z = 3260809
73
XDOT = -3883
689896 XDOT = -1226
745865
YDOT = 19383
539677 feet/sec YDOT = 5894
624499 meter/sec
ZDOT = -15521
000728 ZDOT = -4736
656590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12483487
49 X = 3804966
99
Y = 15021069
27 feet Y = 4578421
91 meter
Z = 10718167
56 Z = 3266897
47
XDOT = -7103
649011 XDOT = -2165
192218
YDOT = 17056
443443 feet/sec YDOT = 5198
803961 meter/sec
ZDOT = -15546
003888 ZDOT = -4738
421985
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 13068
53899605
00016717 00000-0 10270-3 0 9033
2 25544 51
6430 243
1746 0012072 354
6066 5
4954 15
52593406 19232
Satellite: ISS
Catalog Number: 25544
Epoch time: 13068
53899605 = yrday
fracday
Element set: 903
Inclination: 51
6430 deg
RA of node: 243
1746 deg
Eccentricity:
0012072
Arg of perigee: 354
6066 deg
Mean anomaly: 5
4954 deg
Mean motion: 15
52593406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1923
Checksum: 309
Coasting Arc #5 (Orbit 1937)
---------------------------------------
Vector Time (GMT): 2013/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4814908
66 A = 6791653
16 meter
Y = -4226004
67 meter E =
0016749
Z = -2227895
30 I = 51
35616
XDOT = 1930
535443 Wp = 13
85059
YDOT = -5053
736918 meter/sec RA = 237
41690 deg
ZDOT = 5438
407258 TA = 321
28039
MA = 321
40032
Ha = 226
247 n
mi
Hp = 215
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15796944
41 X = -4756472
38
Y = -13864844
72 feet Y = -4279521
58 meter
Z = -7309367
79 Z = -2251142
79
XDOT = 6333
777701 XDOT = 1960
486054
YDOT = -16580
501699 feet/sec YDOT = -5031
980255 meter/sec
ZDOT = 17842
543497 ZDOT = 5447
858898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12381416
98 X = -3773855
90
Y = -16942869
56 feet Y = -5164186
64 meter
Z = -7405667
67 Z = -2257247
50
XDOT = 8425
324543 XDOT = 2568
038921
YDOT = -13938
765818 feet/sec YDOT = -4248
535821 meter/sec
ZDOT = 17882
411987 ZDOT = 5450
559174
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 13069
50448477
00016717 00000-0 10270-3 0 9049
2 25544 51
6434 238
3719 0011969 359
1168
9961 15
52586923 19389
Satellite: ISS
Catalog Number: 25544
Epoch time: 13069
50448477 = yrday
fracday
Element set: 904
Inclination: 51
6434 deg
RA of node: 238
3719 deg
Eccentricity:
0011969
Arg of perigee: 359
1168 deg
Mean anomaly:
9961 deg
Mean motion: 15
52586923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1938
Checksum: 342
Coasting Arc #6 (Orbit 1953)
---------------------------------------
Vector Time (GMT): 2013/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4730802
75 A = 6793199
48 meter
Y = 4760484
16 meter E =
0012779
Z = 1060593
28 I = 51
37873
XDOT = -2772
904148 Wp = 68
63983
YDOT = 4075
221376 meter/sec RA = 232
43206 deg
ZDOT = -5861
277162 TA = 99
83563
MA = 99
69132
Ha = 226
453 n
mi
Hp = 215
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15521006
40 X = 4672066
39
Y = 15618386
34 feet Y = 4813058
71 meter
Z = 3479636
74 Z = 1083431
43
XDOT = -9097
454554 XDOT = -2789
795912
YDOT = 13370
148873 feet/sec YDOT = 4044
117709 meter/sec
ZDOT = -19229
911950 ZDOT = -5874
789135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12074222
42 X = 3680222
99
Y = 18395158
00 feet Y = 5606844
16 meter
Z = 3574187
78 Z = 1089412
44
XDOT = -10122
391385 XDOT = -3085
304894
YDOT = 10429
876271 feet/sec YDOT = 3179
026288 meter/sec
ZDOT = -19286
570546 ZDOT = -5878
546702
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 13070
53433693
00016717 00000-0 10270-3 0 9059
2 25544 51
6432 233
2492 0012164 2
3777 357
7431 15
52623940 19544
Satellite: ISS
Catalog Number: 25544
Epoch time: 13070
53433693 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 233
2492 deg
Eccentricity:
0012164
Arg of perigee: 2
3777 deg
Mean anomaly: 357
7431 deg
Mean motion: 15
52623940 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1954
Checksum: 297
Coasting Arc #7 (Orbit 1969)
---------------------------------------
Vector Time (GMT): 2013/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4513299
97 A = 6793790
97 meter
Y = -5057906
33 meter E =
0022789
Z = 119459
93 I = 51
40117
XDOT = 3648
815166 Wp = 27
25769
YDOT = -3104
048218 meter/sec RA = 227
45062 deg
ZDOT = 5996
947335 TA = 334
03417
MA = 334
14833
Ha = 226
517 n
mi
Hp = 215
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14807414
59 X = -4456986
24
Y = -16594180
87 feet Y = -5108062
00 meter
Z = 391928
90 Z = 97672
46
XDOT = 11971
178366 XDOT = 3654
122793
YDOT = -10183
885230 feet/sec YDOT = -3063
214286 meter/sec
ZDOT = 19675
024066 ZDOT = 6014
686164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11532714
46 X = -3515171
37
Y = -19018028
41 feet Y = -5796695
06 meter
Z = 301772
01 Z = 91980
11
XDOT = 12121
992880 XDOT = 3694
783430
YDOT = -7008
191121 feet/sec YDOT = -2136
096654 meter/sec
ZDOT = 19749
172171 ZDOT = 6019
547678
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 13071
56419175
00016717 00000-0 10270-3 0 9063
2 25544 51
6445 228
1269 0011939 7
1578 352
9742 15
52597400 19705
Satellite: ISS
Catalog Number: 25544
Epoch time: 13071
56419175 = yrday
fracday
Element set: 906
Inclination: 51
6445 deg
RA of node: 228
1269 deg
Eccentricity:
0011939
Arg of perigee: 7
1578 deg
Mean anomaly: 352
9742 deg
Mean motion: 15
52597400 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1970
Checksum: 322
Coasting Arc #8 (Orbit 1984)
---------------------------------------
Vector Time (GMT): 2013/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4133913
07 A = 6792980
63 meter
Y = 5228188
36 meter E =
0009097
Z = -1335272
59 I = 51
42008
XDOT = -4535
857138 Wp = 57
37823
YDOT = 2113
074428 meter/sec RA = 222
47061 deg
ZDOT = -5793
188159 TA = 137
17505
MA = 137
10416
Ha = 226
709 n
mi
Hp = 214
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13562706
92 X = 4081629
48
Y = 17152848
96 feet Y = 5274123
85 meter
Z = -4380815
60 Z = -1315318
27
XDOT = -14881
421055 XDOT = -4531
007243
YDOT = 6932
658885 feet/sec YDOT = 2062
377878 meter/sec
ZDOT = -19006
522831 ZDOT = -5815
211381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10562451
17 X = 3219435
12
Y = 19165543
40 feet Y = 5841657
63 meter
Z = -4298297
74 Z = -1310121
15
XDOT = -14310
104704 XDOT = -4361
719914
YDOT = 3621
380742 feet/sec YDOT = 1103
796850 meter/sec
ZDOT = -19098
402995 ZDOT = -5821
193233
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 13072
52967883
00016717 00000-0 10270-3 0 9075
2 25544 51
6444 223
3247 0012150 10
6014 349
5391 15
52620378 19856
Satellite: ISS
Catalog Number: 25544
Epoch time: 13072
52967883 = yrday
fracday
Element set: 907
Inclination: 51
6444 deg
RA of node: 223
3247 deg
Eccentricity:
0012150
Arg of perigee: 10
6014 deg
Mean anomaly: 349
5391 deg
Mean motion: 15
52620378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1985
Checksum: 305
Coasting Arc #9 (Orbit 2000)
---------------------------------------
Vector Time (GMT): 2013/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3585220
85 A = 6791251
70 meter
Y = -5205745
78 meter E =
0022245
Z = 2444219
40 I = 51
43866
XDOT = 5397
007466 Wp = 46
95132
YDOT = -1209
616974 meter/sec RA = 217
49005 deg
ZDOT = 5324
391730 TA = 340
51592
MA = 340
60081
Ha = 226
749 n
mi
Hp = 214
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11762535
60 X = -3538615
97
Y = -17079218
45 feet Y = -5245577
06 meter
Z = 8019092
53 Z = 2426916
66
XDOT = 17706
717407 XDOT = 5384
268115
YDOT = -3968
559627 feet/sec YDOT = -1149
334741 meter/sec
ZDOT = 17468
476805 ZDOT = 5350
579092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9143559
75 X = -2786957
01
Y = -18643865
73 feet Y = -5682650
27 meter
Z = 7947601
99 Z = 2422429
09
XDOT = 16633
232955 XDOT = 5069
809405
YDOT = -642
168724 feet/sec YDOT = -195
733027 meter/sec
ZDOT = 17577
602249 ZDOT = 5357
653166
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 13073
55953201
00016717 00000-0 10270-3 0 9089
2 25544 51
6457 218
2030 0011921 14
4628 345
6863 15
52614688 20019
Satellite: ISS
Catalog Number: 25544
Epoch time: 13073
55953201 = yrday
fracday
Element set: 908
Inclination: 51
6457 deg
RA of node: 218
2030 deg
Eccentricity:
0011921
Arg of perigee: 14
4628 deg
Mean anomaly: 345
6863 deg
Mean motion: 15
52614688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2001
Checksum: 292
Coasting Arc #10 (Orbit 2015)
---------------------------------------
Vector Time (GMT): 2013/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2870900
68 A = 6788789
46 meter
Y = 5099077
63 meter E =
0014435
Z = -3460909
52 I = 51
45532
XDOT = -6145
423923 Wp = 37
09384
YDOT = 375
679269 meter/sec RA = 212
50714 deg
ZDOT = -4542
931625 TA = 183
51380
MA = 183
52395
Ha = 226
923 n
mi
Hp = 214
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9418965
49 X = 2830480
50
Y = 16729257
31 feet Y = 5130955
43 meter
Z = -11354690
01 Z = -3447061
73
XDOT = -20162
151977 XDOT = -6127
099764
YDOT = 1232
543532 feet/sec YDOT = 307
059179 meter/sec
ZDOT = -14904
631317 ZDOT = -4572
741082
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7206187
81 X = 2196446
04
Y = 17831148
31 feet Y = 5434934
01 meter
Z = -11297564
05 Z = -3443497
52
XDOT = -18757
220800 XDOT = -5717
200900
YDOT = -1944
344874 feet/sec YDOT = -592
636318 meter/sec
ZDOT = -15028
757481 ZDOT = -4580
765280
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 13074
52502021
00016717 00000-0 10270-3 0 9098
2 25544 51
6458 213
4015 0012062 18
0177 342
1400 15
52593861 20160
Satellite: ISS
Catalog Number: 25544
Epoch time: 13074
52502021 = yrday
fracday
Element set: 909
Inclination: 51
6458 deg
RA of node: 213
4015 deg
Eccentricity:
0012062
Arg of perigee: 18
0177 deg
Mean anomaly: 342
1400 deg
Mean motion: 15
52593861 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2016
Checksum: 262
Coasting Arc #11 (Orbit 2031)
---------------------------------------
Vector Time (GMT): 2013/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1990023
79 A = 6786017
48 meter
Y = -4869752
47 meter E =
0016214
Z = 4269297
69 I = 51
47340
XDOT = 6793
308801 Wp = 59
45109
YDOT = 345
054409 meter/sec RA = 207
52058 deg
ZDOT = 3558
120824 TA = 354
20625
MA = 354
22498
Ha = 226
964 n
mi
Hp = 214
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6528949
44 X = -1956160
38
Y = -15976878
17 feet Y = -4891816
38 meter
Z = 14006882
17 Z = 4259713
09
XDOT = 22287
758532 XDOT = 6771
661037
YDOT = 1132
068272 feet/sec YDOT = 420
900794 meter/sec
ZDOT = 11673
624750 ZDOT = 3591
069496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4743252
23 X = -1445743
28
Y = -16628041
40 feet Y = -5068227
02 meter
Z = 13967475
16 Z = 4257286
43
XDOT = 20727
171019 XDOT = 6317
641727
YDOT = 4013
926727 feet/sec YDOT = 1223
444866 meter/sec
ZDOT = 11810
757435 ZDOT = 3599
918866
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 13075
55487225
00016717 00000-0 10270-3 0 9102
2 25544 51
6465 208
2796 0012002 21
5422 338
6232 15
52620586 20328
Satellite: ISS
Catalog Number: 25544
Epoch time: 13075
55487225 = yrday
fracday
Element set: 910
Inclination: 51
6465 deg
RA of node: 208
2796 deg
Eccentricity:
0012002
Arg of perigee: 21
5422 deg
Mean anomaly: 338
6232 deg
Mean motion: 15
52620586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2032
Checksum: 284
Coasting Arc #12 (Orbit 2046)
---------------------------------------
Vector Time (GMT): 2013/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 999390
75 A = 6783787
35 meter
Y = 4621611
09 meter E =
0021895
Z = -4884030
76 I = 51
49333
XDOT = -7210
968771 Wp = 48
87202
YDOT = -951
317584 meter/sec RA = 202
53190 deg
ZDOT = -2368
608132 TA = 197
78021
MA = 197
85695
Ha = 227
124 n
mi
Hp = 214
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3278841
06 X = 971361
92
Y = 15162766
04 feet Y = 4632629
74 meter
Z = -16023722
97 Z = -4879244
32
XDOT = -23658
034027 XDOT = -7188
288948
YDOT = -3121
120681 feet/sec YDOT = -1031
828580 meter/sec
ZDOT = -7771
024054 ZDOT = -2403
583164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1885610
58 X = 574734
10
Y = 15418430
48 feet Y = 4699537
61 meter
Z = -16004263
33 Z = -4878099
46
XDOT = -22069
315180 XDOT = -6726
727267
YDOT = -5542
676342 feet/sec YDOT = -1689
407749 meter/sec
ZDOT = -7916
545870 ZDOT = -2412
963181
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 13076
52036026
00016717 00000-0 10270-3 0 9110
2 25544 51
6466 203
4788 0012117 25
0013 335
1724 15
52588434 20478
Satellite: ISS
Catalog Number: 25544
Epoch time: 13076
52036026 = yrday
fracday
Element set: 911
Inclination: 51
6466 deg
RA of node: 203
4788 deg
Eccentricity:
0012117
Arg of perigee: 25
0013 deg
Mean anomaly: 335
1724 deg
Mean motion: 15
52588434 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2047
Checksum: 282
Coasting Arc #13 (Orbit 2062)
---------------------------------------
Vector Time (GMT): 2013/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 112609
42 A = 6782111
13 meter
Y = -4316802
07 meter E =
0012394
Z = 5220555
84 I = 51
51732
XDOT = 7456
655059 Wp = 46
62306
YDOT = 1471
095831 meter/sec RA = 197
53983 deg
ZDOT = 1062
342369 TA = 33
23011
MA = 33
15234
Ha = 227
116 n
mi
Hp = 214
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 369453
49 X = 135512
47
Y = -14162736
45 feet Y = -4315414
30 meter
Z = 17127807
89 Z = 5221158
88
XDOT = 24464
091402 XDOT = 7434
490196
YDOT = 4826
429892 feet/sec YDOT = 1554
356999 meter/sec
ZDOT = 3485
375227 ZDOT = 1098
512072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1398908
16 X = 426387
21
Y = -14094738
64 feet Y = -4296076
34 meter
Z = 17130756
00 Z = 5221454
43
XDOT = 22948
407840 XDOT = 6994
674710
YDOT = 6669
694001 feet/sec YDOT = 2032
922731 meter/sec
ZDOT = 3635
835191 ZDOT = 1108
202566
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 13077
55021170
00016717 00000-0 10270-3 0 9129
2 25544 51
6470 198
3564 0012130 28
5136 331
6677 15
52628255 20638
Satellite: ISS
Catalog Number: 25544
Epoch time: 13077
55021170 = yrday
fracday
Element set: 912
Inclination: 51
6470 deg
RA of node: 198
3564 deg
Eccentricity:
0012130
Arg of perigee: 28
5136 deg
Mean anomaly: 331
6677 deg
Mean motion: 15
52628255 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2063
Checksum: 291
Coasting Arc #14 (Orbit 2077)
---------------------------------------
Vector Time (GMT): 2013/078/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1229399
55 A = 6781810
21 meter
Y = 4051370
64 meter E =
0023555
Z = -5316102
84 I = 51
54565
XDOT = -7409
245626 Wp = 65
62485
YDOT = -1883
891926 meter/sec RA = 192
54996 deg
ZDOT = 288
262014 TA = 207
07147
MA = 207
19450
Ha = 227
298 n
mi
Hp = 213
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4033463
09 X = -1248787
40
Y = 13291898
43 feet Y = 4037513
88 meter
Z = -17441282
29 Z = -5322122
55
XDOT = -24308
548642 XDOT = -7389
029164
YDOT = -6180
747790 feet/sec YDOT = -1966
633714 meter/sec
ZDOT = 945
741516 ZDOT = 252
317995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4756055
46 X = -1449645
71
Y = 13016679
30 feet Y = 3967483
85 meter
Z = -17466760
22 Z = -5323868
52
XDOT = -22926
620675 XDOT = -6988
033982
YDOT = -7354
689701 feet/sec YDOT = -2241
709421 meter/sec
ZDOT = 796
245276 ZDOT = 242
695560
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 13078
51569936
00016717 00000-0 10270-3 0 9134
2 25544 51
6470 193
5559 0012262 32
3560 327
8342 15
52607799 20781
Satellite: ISS
Catalog Number: 25544
Epoch time: 13078
51569936 = yrday
fracday
Element set: 913
Inclination: 51
6470 deg
RA of node: 193
5559 deg
Eccentricity:
0012262
Arg of perigee: 32
3560 deg
Mean anomaly: 327
8342 deg
Mean motion: 15
52607799 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2078
Checksum: 329
Coasting Arc #15 (Orbit 2093)
---------------------------------------
Vector Time (GMT): 2013/079/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922334
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2388535
26 A = 6782638
12 meter
Y = -3766431
70 meter E =
0017105
Z = 5103391
32 I = 51
57898
XDOT = 7140
001082 Wp = 41
74589
YDOT = 2269
029231 meter/sec RA = 187
56029 deg
ZDOT = -1651
436165 TA = 64
28988
MA = 64
11338
Ha = 227
333 n
mi
Hp = 213
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7836401
76 X = 2405684
04
Y = -12357059
39 feet Y = -3739625
28 meter
Z = 16743409
85 Z = 5115036
51
XDOT = 23425
200400 XDOT = 7122
119829
YDOT = 7444
321624 feet/sec YDOT = 2348
773096 meter/sec
ZDOT = -5418
097654 ZDOT = -1616
794542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8291717
40 X = 2527315
46
Y = -11988089
48 feet Y = -3653969
67 meter
Z = 16792290
37 Z = 5118290
10
XDOT = 22217
766274 XDOT = 6771
975160
YDOT = 7907
698175 feet/sec YDOT = 2410
266404 meter/sec
ZDOT = -5274
046391 ZDOT = -1607
529340
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 13079
54555150
00016717 00000-0 10270-3 0 9142
2 25544 51
6474 188
4333 0012340 36
0166 324
1815 15
52607875 20946
Satellite: ISS
Catalog Number: 25544
Epoch time: 13079
54555150 = yrday
fracday
Element set: 914
Inclination: 51
6474 deg
RA of node: 188
4333 deg
Eccentricity:
0012340
Arg of perigee: 36
0166 deg
Mean anomaly: 324
1815 deg
Mean motion: 15
52607875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2094
Checksum: 302
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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