[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 3rd 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 1798)
---------------------------------------
Vector Time (GMT): 2013/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3726602
80 A = 6789459
19 meter
Y = -4601054
59 meter E =
0011741
Z = 3306488
01 I = 51
30685
XDOT = 2625
787286 Wp = 28
89727
YDOT = 5484
906895 meter/sec RA = 282
43586 deg
ZDOT = 4676
089502 TA = 9
76156
MA = 9
73877
Ha = 225
087 n
mi
Hp = 217
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12226387
15 X = 3761713
86
Y = -15095323
45 feet Y = -4559184
67 meter
Z = 10848057
77 Z = 3324677
23
XDOT = 8614
787685 XDOT = 2541
543665
YDOT = 17995
101362 feet/sec YDOT = 5513
799607 meter/sec
ZDOT = 15341
500991 ZDOT = 4688
640021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16821277
54 X = 5127125
39
Y = -9630096
69 feet Y = -2935253
47 meter
Z = 10924264
26 Z = 3329715
75
XDOT = 679
213944 XDOT = 207
024410
YDOT = 18636
540042 feet/sec YDOT = 5680
417405 meter/sec
ZDOT = 15393
053034 ZDOT = 4691
802565
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 13060
55745470
00016717 00000-0 10270-3 0 9004
2 25544 51
6467 282
8709 0012101 325
6032 34
4335 15
52468767 17992
Satellite: ISS
Catalog Number: 25544
Epoch time: 13060
55745470 = yrday
fracday
Element set: 900
Inclination: 51
6467 deg
RA of node: 282
8709 deg
Eccentricity:
0012101
Arg of perigee: 325
6032 deg
Mean anomaly: 34
4335 deg
Mean motion: 15
52468767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1799
Checksum: 310
Coasting Arc #2 (Orbit 1813)
---------------------------------------
Vector Time (GMT): 2013/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3834998
19 A = 6786793
87 meter
Y = 3788280
01 meter E =
0012879
Z = -4133117
33 I = 51
29158
XDOT = -2195
652598 Wp = 3
90494
YDOT = -6312
426946 meter/sec RA = 277
43901 deg
ZDOT = -3736
554565 TA = 227
33212
MA = 227
44071
Ha = 225
283 n
mi
Hp = 217
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12582015
06 X = -3856997
02
Y = 12428740
19 feet Y = 3745271
25 meter
Z = -13560096
23 Z = -4151801
14
XDOT = -7203
584638 XDOT = -2106
751399
YDOT = -20710
062159 feet/sec YDOT = -6336
483400 meter/sec
ZDOT = -12259
037286 ZDOT = -3747
004265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16042566
41 X = -4889774
24
Y = 7300054
40 feet Y = 2225056
58 meter
Z = -13638261
03 Z = -4156941
96
XDOT = 1059
500002 XDOT = 322
935601
YDOT = -20726
987095 feet/sec YDOT = -6317
585666 meter/sec
ZDOT = -12301
757962 ZDOT = -3749
575827
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 13061
52300425
00016717 00000-0 10270-3 0 9010
2 25544 51
6457 278
0695 0012096 328
5084 31
5342 15
52492575 18142
Satellite: ISS
Catalog Number: 25544
Epoch time: 13061
52300425 = yrday
fracday
Element set: 901
Inclination: 51
6457 deg
RA of node: 278
0695 deg
Eccentricity:
0012096
Arg of perigee: 328
5084 deg
Mean anomaly: 31
5342 deg
Mean motion: 15
52492575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1814
Checksum: 296
Coasting Arc #3 (Orbit 1829)
---------------------------------------
Vector Time (GMT): 2013/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3940500
68 A = 6784411
76 meter
Y = -2789041
49 meter E =
0007278
Z = 4762849
98 I = 51
28065
XDOT = 1796
714385 Wp = 7
88118
YDOT = 6983
080037 meter/sec RA = 272
43584 deg
ZDOT = 2609
282287 TA = 56
29628
MA = 56
22691
Ha = 225
414 n
mi
Hp = 217
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12928151
83 X = 3948258
93
Y = -9150398
57 feet Y = -2744932
59 meter
Z = 15626148
22 Z = 4782011
55
XDOT = 5894
732233 XDOT = 1705
819426
YDOT = 22910
367575 feet/sec YDOT = 7002
664003 meter/sec
ZDOT = 8560
637424 ZDOT = 2617
789215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15140937
96 X = 4614957
89
Y = -4371640
17 feet Y = -1332475
92 meter
Z = 15706182
61 Z = 4787244
46
XDOT = -2412
578010 XDOT = -735
353777
YDOT = 22447
037275 feet/sec YDOT = 6841
856961 meter/sec
ZDOT = 8595
204512 ZDOT = 2619
818335
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 13062
55291559
00016717 00000-0 10270-3 0 9022
2 25544 51
6458 272
9468 0012121 333
0428 27
0092 15
52479872 18301
Satellite: ISS
Catalog Number: 25544
Epoch time: 13062
55291559 = yrday
fracday
Element set: 902
Inclination: 51
6458 deg
RA of node: 272
9468 deg
Eccentricity:
0012121
Arg of perigee: 333
0428 deg
Mean anomaly: 27
0092 deg
Mean motion: 15
52479872 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1830
Checksum: 307
Coasting Arc #4 (Orbit 1844)
---------------------------------------
Vector Time (GMT): 2013/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4062110
71 A = 6782628
92 meter
Y = 1735009
08 meter E =
0016144
Z = -5157494
95 I = 51
27354
XDOT = -1422
315721 Wp = 32
74339
YDOT = -7400
324726 meter/sec RA = 267
42918 deg
ZDOT = -1357
944693 TA = 224
05274
MA = 224
18149
Ha = 225
535 n
mi
Hp = 216
894
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13327134
86 X = -4056156
50
Y = 5692287
01 feet Y = 1689616
98 meter
Z = -16920915
20 Z = -5177213
82
XDOT = -4666
390161 XDOT = -1332
861523
YDOT = -24279
280598 feet/sec YDOT = -7415
729871 meter/sec
ZDOT = -4455
199125 ZDOT = -1364
636399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14342958
55 X = -4371733
77
Y = 1226606
95 feet Y = 373869
80 meter
Z = -17003146
82 Z = -5182559
15
XDOT = 3351
324172 XDOT = 1021
483608
YDOT = -23456
701289 feet/sec YDOT = -7149
602553 meter/sec
ZDOT = -4482
175062 ZDOT = -1366
166959
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 13063
51844488
00016717 00000-0 10270-3 0 9035
2 25544 51
6445 268
1448 0012110 336
0642 23
9945 15
52533388 18452
Satellite: ISS
Catalog Number: 25544
Epoch time: 13063
51844488 = yrday
fracday
Element set: 903
Inclination: 51
6445 deg
RA of node: 268
1448 deg
Eccentricity:
0012110
Arg of perigee: 336
0642 deg
Mean anomaly: 23
9945 deg
Mean motion: 15
52533388 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1845
Checksum: 311
Coasting Arc #5 (Orbit 1860)
---------------------------------------
Vector Time (GMT): 2013/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4205341
21 A = 6782039
45 meter
Y = -568225
95 meter E =
0011441
Z = 5291905
25 I = 51
27407
XDOT = 1022
437252 Wp = 351
13206
YDOT = 7596
511245 meter/sec RA = 262
42013 deg
ZDOT = 14
292271 TA = 98
79580
MA = 98
66622
Ha = 225
657 n
mi
Hp = 216
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13797051
20 X = 4185676
33
Y = -1864258
38 feet Y = -521308
85 meter
Z = 17361893
87 Z = 5312286
45
XDOT = 3354
452926 XDOT = 937
346028
YDOT = 24922
937154 feet/sec YDOT = 7607
469010 meter/sec
ZDOT = 46
890653 ZDOT = 19
052027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13619884
96 X = 4151340
94
Y = 2319285
23 feet Y = 706918
14 meter
Z = 17446750
11 Z = 5317769
43
XDOT = -4089
184205 XDOT = -1246
383346
YDOT = 23791
289634 feet/sec YDOT = 7251
585080 meter/sec
ZDOT = 65
817801 ZDOT = 20
061266
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 13064
54833455
00016717 00000-0 10270-3 0 9042
2 25544 51
6448 263
0227 0012082 339
9243 20
1432 15
52518415 18613
Satellite: ISS
Catalog Number: 25544
Epoch time: 13064
54833455 = yrday
fracday
Element set: 904
Inclination: 51
6448 deg
RA of node: 263
0227 deg
Eccentricity:
0012082
Arg of perigee: 339
9243 deg
Mean anomaly: 20
1432 deg
Mean motion: 15
52518415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1861
Checksum: 289
Coasting Arc #6 (Orbit 1875)
---------------------------------------
Vector Time (GMT): 2013/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4366872
14 A = 6782454
97 meter
Y = -542021
39 meter E =
0013816
Z = -5168475
75 I = 51
27966
XDOT = -603
717467 Wp = 48
69675
YDOT = -7522
812183 meter/sec RA = 257
41076 deg
ZDOT = 1310
246478 TA = 233
90363
MA = 234
03164
Ha = 225
738 n
mi
Hp = 216
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14327008
33 X = -4335379
93
Y = -1778285
40 feet Y = -590678
73 meter
Z = -16956941
43 Z = -5189612
76
XDOT = -1980
700352 XDOT = -525
915632
YDOT = -24681
142332 feet/sec YDOT = -7529
128237 meter/sec
ZDOT = 4298
708917 ZDOT = 1307
503151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13138315
90 X = -4004558
69
Y = -5729051
74 feet Y = -1746214
97 meter
Z = -17044821
82 Z = -5195261
69
XDOT = 4637
062120 XDOT = 1413
376534
YDOT = -23282
840597 feet/sec YDOT = -7096
609814 meter/sec
ZDOT = 4288
149330 ZDOT = 1307
027916
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
51384451
00016717 00000-0 10270-3 0 9058
2 25544 51
6435 258
2200 0012047 343
5897 16
4863 15
52568825 18765
Satellite: ISS
Catalog Number: 25544
Epoch time: 13065
51384451 = yrday
fracday
Element set: 905
Inclination: 51
6435 deg
RA of node: 258
2200 deg
Eccentricity:
0012047
Arg of perigee: 343
5897 deg
Mean anomaly: 16
4863 deg
Mean motion: 15
52568825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1876
Checksum: 317
Coasting Arc #7 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2013/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4535015
02 A = 6784162
54 meter
Y = 1671505
26 meter E =
0015786
Z = 4763877
56 I = 51
29294
XDOT = 96
581532 Wp = 13
91452
YDOT = 7206
161121 meter/sec RA = 252
40442 deg
ZDOT = -2603
511128 TA = 101
98475
MA = 101
80775
Ha = 225
902 n
mi
Hp = 216
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14878658
20 X = 4492845
65
Y = 5483941
13 feet Y = 1721983
23 meter
Z = 15629519
55 Z = 4785805
27
XDOT = 316
868544 XDOT = 28
640436
YDOT = 23642
260895 feet/sec YDOT = 7206
861076 meter/sec
ZDOT = -8541
703177 ZDOT = -2603
207531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12787840
62 X = 3897733
82
Y = 9223053
93 feet Y = 2811186
84 meter
Z = 15720571
55 Z = 4791630
21
XDOT = -5266
364584 XDOT = -1605
187925
YDOT = 21954
041417 feet/sec YDOT = 6691
591824 meter/sec
ZDOT = -8541
244685 ZDOT = -2603
371380
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
54371144
00016717 00000-0 10270-3 0 9068
2 25544 51
6434 253
0980 0012084 346
9245 13
1591 15
52567292 18924
Satellite: ISS
Catalog Number: 25544
Epoch time: 13066
54371144 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 253
0980 deg
Eccentricity:
0012084
Arg of perigee: 346
9245 deg
Mean anomaly: 13
1591 deg
Mean motion: 15
52567292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1892
Checksum: 306
Coasting Arc #8 (Orbit 1906)
---------------------------------------
Vector Time (GMT): 2013/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4686674
57 A = 6786438
67 meter
Y = -2639989
88 meter E =
0010743
Z = -4136070
26 I = 51
31041
XDOT = 468
442217 Wp = 30
45936
YDOT = -6673
180207 meter/sec RA = 247
40180 deg
ZDOT = 3741
955061 TA = 278
19426
MA = 278
31610
Ha = 225
949 n
mi
Hp = 215
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15376228
92 X = -4636713
82
Y = -8661384
13 feet Y = -2692120
29 meter
Z = -13569784
33 Z = -4158715
63
XDOT = 1536
883915 XDOT = 524
851292
YDOT = -21893
635851 feet/sec YDOT = -6667
626024 meter/sec
ZDOT = 12276
755449 ZDOT = 3744
368331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12645478
94 X = -3854341
98
Y = -12205797
38 feet Y = -3720327
04 meter
Z = -13663726
07 Z = -4164703
71
XDOT = 5990
407218 XDOT = 1825
876120
YDOT = -19912
651317 feet/sec YDOT = -6069
376122 meter/sec
ZDOT = 12287
529087 ZDOT = 3745
238866
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
50920165
00016717 00000-0 10270-3 0 9079
2 25544 51
6427 248
2950 0012002 351
0942 8
9995 15
52596199 19075
Satellite: ISS
Catalog Number: 25544
Epoch time: 13067
50920165 = yrday
fracday
Element set: 907
Inclination: 51
6427 deg
RA of node: 248
2950 deg
Eccentricity:
0012002
Arg of perigee: 351
0942 deg
Mean anomaly: 8
9995 deg
Mean motion: 15
52596199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1907
Checksum: 318
Coasting Arc #9 (Orbit 1922)
---------------------------------------
Vector Time (GMT): 2013/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4792122
12 A = 6789168
69 meter
Y = 3539966
46 meter E =
0016236
Z = 3258135
97 I = 51
33214
XDOT = -1157
162724 Wp = 44
91594
YDOT = 5927
750851 meter/sec RA = 242
40553 deg
ZDOT = -4712
804669 TA = 97
16695
MA = 96
98233
Ha = 226
145 n
mi
Hp = 215
738
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15722185
42 X = 4736354
46
Y = 11614063
18 feet Y = 3593243
55 meter
Z = 10689422
46 Z = 3281279
33
XDOT = -3796
465630 XDOT = -1200
469012
YDOT = 19448
001479 feet/sec YDOT = 5914
568031 meter/sec
ZDOT = -15461
957576 ZDOT = -4718
531841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12519460
72 X = 3815931
63
Y = 14942444
52 feet Y = 4554457
09 meter
Z = 10785350
50 Z = 3287374
83
XDOT = -7039
931513 XDOT = -2145
771125
YDOT = 17136
746948 feet/sec YDOT = 5223
280470 meter/sec
ZDOT = -15486
428539 ZDOT = -4720
263419
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
53904547
00016717 00000-0 10270-3 0 9080
2 25544 51
6425 243
1724 0012091 354
2916 5
8096 15
52614687 19239
Satellite: ISS
Catalog Number: 25544
Epoch time: 13068
53904547 = yrday
fracday
Element set: 908
Inclination: 51
6425 deg
RA of node: 243
1724 deg
Eccentricity:
0012091
Arg of perigee: 354
2916 deg
Mean anomaly: 5
8096 deg
Mean motion: 15
52614687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1923
Checksum: 313
Coasting Arc #10 (Orbit 1937)
---------------------------------------
Vector Time (GMT): 2013/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4820027
53 A = 6791512
50 meter
Y = -4212412
56 meter E =
0016715
Z = -2242110
40 I = 51
35559
XDOT = 1914
195159 Wp = 13
57689
YDOT = -5068
108391 meter/sec RA = 237
41475 deg
ZDOT = 5430
907784 TA = 321
38377
MA = 321
50319
Ha = 226
185 n
mi
Hp = 215
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15813738
60 X = -4761673
81
Y = -13820251
17 feet Y = -4265987
17 meter
Z = -7356005
26 Z = -2265382
96
XDOT = 6280
167846 XDOT = 1944
344119
YDOT = -16627
652202 feet/sec YDOT = -5046
533348 meter/sec
ZDOT = 17817
938925 ZDOT = 5440
280530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12407173
16 X = -3781706
38
Y = -16902902
42 feet Y = -5152004
66 meter
Z = -7452410
90 Z = -2271494
84
XDOT = 8386
240246 XDOT = 2556
126027
YDOT = -13994
481945 feet/sec YDOT = -4265
518097 meter/sec
ZDOT = 17857
480607 ZDOT = 5442
960089
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
50451503
00016717 00000-0 10270-3 0 9098
2 25544 51
6430 238
3695 0012005 358
7518 1
3602 15
52625795 19382
Satellite: ISS
Catalog Number: 25544
Epoch time: 13069
50451503 = yrday
fracday
Element set: 909
Inclination: 51
6430 deg
RA of node: 238
3695 deg
Eccentricity:
0012005
Arg of perigee: 358
7518 deg
Mean anomaly: 1
3602 deg
Mean motion: 15
52625795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1938
Checksum: 304
Coasting Arc #11 (Orbit 1953)
---------------------------------------
Vector Time (GMT): 2013/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4730927
91 A = 6793035
45 meter
Y = 4760202
60 meter E =
0012720
Z = 1060555
47 I = 51
37825
XDOT = -2772
833140 Wp = 68
27147
YDOT = 4075
339764 meter/sec RA = 232
42960 deg
ZDOT = -5861
278469 TA = 100
20412
MA = 100
06064
Ha = 226
369 n
mi
Hp = 215
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15521417
03 X = 4672194
87
Y = 15617462
61 feet Y = 4812778
58 meter
Z = 3479512
70 Z = 1083394
24
XDOT = -9097
221588 XDOT = -2789
726226
YDOT = 13370
537284 feet/sec YDOT = 4044
236884 meter/sec
ZDOT = -19229
916237 ZDOT = -5874
790100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12074809
72 X = 3680402
00
Y = 18394334
82 feet Y = 5606593
25 meter
Z = 3574066
35 Z = 1089375
42
XDOT = -10122
300538 XDOT = -3085
277204
YDOT = 10430
260509 feet/sec YDOT = 3179
143403 meter/sec
ZDOT = -19286
573423 ZDOT = -5878
547579
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
53433533
00016717 00000-0 10270-3 0 9108
2 25544 51
6427 233
2466 0012215 1
9690 358
1508 15
52680261 19544
Satellite: ISS
Catalog Number: 25544
Epoch time: 13070
53433533 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 233
2466 deg
Eccentricity:
0012215
Arg of perigee: 1
9690 deg
Mean anomaly: 358
1508 deg
Mean motion: 15
52680261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1954
Checksum: 286
Coasting Arc #12 (Orbit 1969)
---------------------------------------
Vector Time (GMT): 2013/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4499987
85 A = 6793573
85 meter
Y = -5068796
41 meter E =
0022842
Z = 141383
30 I = 51
40067
XDOT = 3669
852091 Wp = 27
10964
YDOT = -3080
667565 meter/sec RA = 227
44782 deg
ZDOT = 5996
435783 TA = 334
41942
MA = 334
53227
Ha = 226
409 n
mi
Hp = 215
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14763739
68 X = -4443659
84
Y = -16629909
48 feet Y = -5118803
14 meter
Z = 463855
96 Z = 119660
53
XDOT = 12040
197149 XDOT = 3674
899192
YDOT = -10107
177051 feet/sec YDOT = -3039
599842 meter/sec
ZDOT = 19673
345745 ZDOT = 6014
276170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11483690
79 X = -3500228
95
Y = -19045263
28 feet Y = -5804996
25 meter
Z = 373969
49 Z = 113985
90
XDOT = 12173
877659 XDOT = 3710
597910
YDOT = -6923
749447 feet/sec YDOT = -2110
358831 meter/sec
ZDOT = 19747
914121 ZDOT = 6019
164224
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
56414636
00016717 00000-0 10270-3 0 9116
2 25544 51
6440 228
1239 0012005 6
6953 353
4357 15
52671355 19703
Satellite: ISS
Catalog Number: 25544
Epoch time: 13071
56414636 = yrday
fracday
Element set: 911
Inclination: 51
6440 deg
RA of node: 228
1239 deg
Eccentricity:
0012005
Arg of perigee: 6
6953 deg
Mean anomaly: 353
4357 deg
Mean motion: 15
52671355 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1970
Checksum: 293
Coasting Arc #13 (Orbit 1984)
---------------------------------------
Vector Time (GMT): 2013/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4096552
12 A = 6792660
61 meter
Y = 5244969
98 meter E =
0009058
Z = -1382849
86 I = 51
41941
XDOT = -4578
923032 Wp = 55
65445
YDOT = 2058
554220 meter/sec RA = 222
46735 deg
ZDOT = -5778
947872 TA = 139
43002
MA = 139
36247
Ha = 226
579 n
mi
Hp = 214
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13440131
63 X = 4044314
77
Y = 17207906
77 feet Y = 5290487
93 meter
Z = -4536908
98 Z = -1363076
92
XDOT = -15022
713358 XDOT = -4573
529454
YDOT = 6753
786811 feet/sec YDOT = 2007
379122 meter/sec
ZDOT = -18959
802729 ZDOT = -5801
178975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10433405
92 X = 3180102
12
Y = 19199698
85 feet Y = 5852068
21 meter
Z = -4455147
79 Z = -1357929
05
XDOT = -14417
627573 XDOT = -4394
492884
YDOT = 3430
952571 feet/sec YDOT = 1045
754344 meter/sec
ZDOT = -19052
542548 ZDOT = -5807
214969
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
52958139
00016717 00000-0 10270-3 0 9125
2 25544 51
6440 223
3213 0012232 10
1029 350
0366 15
52711781 19855
Satellite: ISS
Catalog Number: 25544
Epoch time: 13072
52958139 = yrday
fracday
Element set: 912
Inclination: 51
6440 deg
RA of node: 223
3213 deg
Eccentricity:
0012232
Arg of perigee: 10
1029 deg
Mean anomaly: 350
0366 deg
Mean motion: 15
52711781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1985
Checksum: 274
Coasting Arc #14 (Orbit 2000)
---------------------------------------
Vector Time (GMT): 2013/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3509991
05 A = 6790777
93 meter
Y = -5221404
38 meter E =
0022096
Z = 2517676
95 I = 51
43763
XDOT = 5460
177229 Wp = 47
07534
YDOT = -1117
381143 meter/sec RA = 217
48599 deg
ZDOT = 5280
296801 TA = 341
29320
MA = 341
37428
Ha = 226
597 n
mi
Hp = 214
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11515718
66 X = -3463573
50
Y = -17130591
79 feet Y = -5260395
43 meter
Z = 8260094
98 Z = 2500739
21
XDOT = 17913
967288 XDOT = 5446
615984
YDOT = -3665
948631 feet/sec YDOT = -1056
397107 meter/sec
ZDOT = 17323
808402 ZDOT = 5306
789027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8893326
37 X = -2710685
88
Y = -18658207
67 feet Y = -5687021
70 meter
Z = 8190125
33 Z = 2496350
20
XDOT = 16793
062457 XDOT = 5118
525437
YDOT = -330
252571 feet/sec YDOT = -100
660984 meter/sec
ZDOT = 17434
193420 ZDOT = 5313
942154
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
55936724
00016717 00000-0 10270-3 0 9136
2 25544 51
6452 218
1990 0012022 13
8884 346
2597 15
52724125 20017
Satellite: ISS
Catalog Number: 25544
Epoch time: 13073
55936724 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 218
1990 deg
Eccentricity:
0012022
Arg of perigee: 13
8884 deg
Mean anomaly: 346
2597 deg
Mean motion: 15
52724125 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2001
Checksum: 297
Coasting Arc #15 (Orbit 2015)
---------------------------------------
Vector Time (GMT): 2013/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2744775
82 A = 6788146
56 meter
Y = 5104975
79 meter E =
0014909
Z = -3552632
68 I = 51
45392
XDOT = -6218
375599 Wp = 36
31679
YDOT = 243
855175 meter/sec RA = 212
50188 deg
ZDOT = -4451
791695 TA = 185
60942
MA = 185
62614
Ha = 226
747 n
mi
Hp = 214
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9005170
02 X = 2704744
63
Y = 16748608
24 feet Y = 5135445
35 meter
Z = -11655619
02 Z = -3539396
65
XDOT = -20401
494747 XDOT = -6199
014666
YDOT = 800
049788 feet/sec YDOT = 174
425102 meter/sec
ZDOT = -14605
615798 ZDOT = -4481
953010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6795291
90 X = 2071204
97
Y = 17796131
42 feet Y = 5424260
86 meter
Z = -11601040
23 Z = -3535997
06
XDOT = -18941
980828 XDOT = -5773
515756
YDOT = -2374
819038 feet/sec YDOT = -723
844843 meter/sec
ZDOT = -14731
193257 ZDOT = -4490
067705
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
52478110
00016717 00000-0 10270-3 0 9145
2 25544 51
6453 213
3971 0012179 17
3957 342
7610 15
52721199 20168
Satellite: ISS
Catalog Number: 25544
Epoch time: 13074
52478110 = yrday
fracday
Element set: 914
Inclination: 51
6453 deg
RA of node: 213
3971 deg
Eccentricity:
0012179
Arg of perigee: 17
3957 deg
Mean anomaly: 342
7610 deg
Mean motion: 15
52721199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2016
Checksum: 297
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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