[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 17th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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
080/00:40:24
033 -0
6 4
4 4
4
N/A 2
9 -0
3 227
6
000/00:10:48
066 -3
3 -0
2 215
0
Coasting Arc #1 (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 = 2540282
55 A = 6787472
63 meter
Y = 5109533
75 meter E =
0015533
Z = -3694762
64 I = 51
45239
XDOT = -6327
451252 Wp = 36
08901
YDOT = 32
726224 meter/sec RA = 212
50564 deg
ZDOT = -4302
070258 TA = 187
93425
MA = 187
95885
Ha = 226
609 n
mi
Hp = 214
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8334260
34 X = 2500906
02
Y = 16763562
19 feet Y = 5137720
18 meter
Z = -12121924
66 Z = -3682518
43
XDOT = -20759
354501 XDOT = -6306
448630
YDOT = 107
369500 feet/sec YDOT = -37
914405 meter/sec
ZDOT = -14114
403732 ZDOT = -4332
757439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6131110
89 X = 1868762
60
Y = 17723062
40 feet Y = 5401989
42 meter
Z = -12071474
99 Z = -3679385
58
XDOT = -19213
956824 XDOT = -5856
414040
YDOT = -3060
479750 feet/sec YDOT = -932
834228 meter/sec
ZDOT = -14242
148756 ZDOT = -4341
006941
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
52440342
00016717 00000-0 10270-3 0 9006
2 25544 51
6454 213
4031 0012174 17
1108 343
0452 15
52803070 20165
Satellite: ISS
Catalog Number: 25544
Epoch time: 13074
52440342 = yrday
fracday
Element set: 900
Inclination: 51
6454 deg
RA of node: 213
4031 deg
Eccentricity:
0012174
Arg of perigee: 17
1108 deg
Mean anomaly: 343
0452 deg
Mean motion: 15
52803070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2016
Checksum: 245
Coasting Arc #2 (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 = -1541479
46 A = 6784517
56 meter
Y = -4833566
35 meter E =
0014965
Z = 4489153
10 I = 51
47002
XDOT = 6941
155491 Wp = 57
80308
YDOT = 750
346387 meter/sec RA = 207
51558 deg
ZDOT = 3191
387091 TA =
09407
MA =
09378
Ha = 226
615 n
mi
Hp = 214
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5057347
31 X = -1509122
02
Y = -15858157
33 feet Y = -4850622
76 meter
Z = 14728192
57 Z = 4481743
82
XDOT = 22772
819854 XDOT = 6916
746172
YDOT = 2461
766362 feet/sec YDOT = 827
830608 meter/sec
ZDOT = 10470
430089 ZDOT = 3225
047239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3299360
45 X = -1005645
06
Y = -16342134
28 feet Y = -4981082
53 meter
Z = 14697837
93 Z = 4479901
00
XDOT = 21085
077926 XDOT = 6426
731752
YDOT = 5285
877664 feet/sec YDOT = 1611
135512 meter/sec
ZDOT = 10610
483572 ZDOT = 3234
075393
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
55410911
00016717 00000-0 10270-3 0 9010
2 25544 51
6460 208
2800 0012136 20
5537 339
6101 15
52850716 20329
Satellite: ISS
Catalog Number: 25544
Epoch time: 13075
55410911 = yrday
fracday
Element set: 901
Inclination: 51
6460 deg
RA of node: 208
2800 deg
Eccentricity:
0012136
Arg of perigee: 20
5537 deg
Mean anomaly: 339
6101 deg
Mean motion: 15
52850716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2032
Checksum: 263
Coasting Arc #3 (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 = 430313
30 A = 6782341
77 meter
Y = 4528580
77 meter E =
0022702
Z = -5049988
84 I = 51
49039
XDOT = -7282
484237 Wp = 50
95252
YDOT = -1406
265164 meter/sec RA = 202
52322 deg
ZDOT = -1873
310709 TA = 200
76457
MA = 200
85694
Ha = 226
764 n
mi
Hp = 213
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1411789
04 X = 404173
22
Y = 14857548
46 feet Y = 4533246
19 meter
Z = -16568204
86 Z = -5047962
32
XDOT = -23892
664819 XDOT = -7257
117797
YDOT = -4613
730854 feet/sec YDOT = -1487
560825 meter/sec
ZDOT = -6146
032509 ZDOT = -1908
626589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 60518
81 X = 18446
13
Y = 14933202
43 feet Y = 4551640
10 meter
Z = -16560226
73 Z = -5047557
11
XDOT = -22202
893813 XDOT = -6767
442034
YDOT = -6918
811787 feet/sec YDOT = -2108
853833 meter/sec
ZDOT = -6292
927328 ZDOT = -1918
084250
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
51944802
00016717 00000-0 10270-3 0 9029
2 25544 51
6461 203
4783 0012286 24
0419 336
1304 15
52840508 20472
Satellite: ISS
Catalog Number: 25544
Epoch time: 13076
51944802 = yrday
fracday
Element set: 902
Inclination: 51
6461 deg
RA of node: 203
4783 deg
Eccentricity:
0012286
Arg of perigee: 24
0419 deg
Mean anomaly: 336
1304 deg
Mean motion: 15
52840508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2047
Checksum: 285
Coasting Arc #4 (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 = 803576
58 A = 6781016
17 meter
Y = -4156156
21 meter E =
0012940
Z = 5289637
20 I = 51
51566
XDOT = 7402
634026 Wp = 39
78597
YDOT = 1974
455540 meter/sec RA = 197
52717 deg
ZDOT = 435
946156 TA = 46
10555
MA = 45
99877
Ha = 226
731 n
mi
Hp = 213
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2636406
10 X = 824296
32
Y = -13635683
10 feet Y = -4147053
82 meter
Z = 17354452
77 Z = 5293591
57
XDOT = 24286
857041 XDOT = 7377
887358
YDOT = 6477
872505 feet/sec YDOT = 2057
098122 meter/sec
ZDOT = 1430
269542 ZDOT = 471
847117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3614842
20 X = 1101803
90
Y = -13387643
74 feet Y = -4080553
81 meter
Z = 17371339
41 Z = 5294784
25
XDOT = 22703
487521 XDOT = 6920
022996
YDOT = 8140
883132 feet/sec YDOT = 2481
341179 meter/sec
ZDOT = 1579
559538 ZDOT = 481
449747
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
54912797
00016717 00000-0 10270-3 0 9032
2 25544 51
6464 198
3546 0012331 27
4821 332
6981 15
52891669 20633
Satellite: ISS
Catalog Number: 25544
Epoch time: 13077
54912797 = yrday
fracday
Element set: 903
Inclination: 51
6464 deg
RA of node: 198
3546 deg
Eccentricity:
0012331
Arg of perigee: 27
4821 deg
Mean anomaly: 332
6981 deg
Mean motion: 15
52891669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2063
Checksum: 329
Coasting Arc #5 (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 = -2020280
60 A = 6781240
07 meter
Y = 3817431
94 meter E =
0022519
Z = -5244644
66 I = 51
54606
XDOT = -7186
659177 Wp = 67
54963
YDOT = -2424
132755 meter/sec RA = 192
53436 deg
ZDOT = 1015
800101 TA = 212
14102
MA = 212
27850
Ha = 226
873 n
mi
Hp = 213
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6628217
18 X = -2037340
83
Y = 12524383
00 feet Y = 3794744
07 meter
Z = -17206839
44 Z = -5254500
71
XDOT = -23578
278139 XDOT = -7163
952337
YDOT = -7953
191453 feet/sec YDOT = -2504
371456 meter/sec
ZDOT = 3332
677497 ZDOT = 980
943475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7298645
13 X = -2224627
03
Y = 12087006
24 feet Y = 3684119
50 meter
Z = -17248269
93 Z = -5257272
67
XDOT = -22168
550384 XDOT = -6756
974157
YDOT = -8892
911721 feet/sec YDOT = -2710
559492 meter/sec
ZDOT = 3187
764173 ZDOT = 971
630520
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
51444246
00016717 00000-0 10270-3 0 9040
2 25544 51
6465 193
5530 0012447 31
4462 328
7432 15
52901837 20780
Satellite: ISS
Catalog Number: 25544
Epoch time: 13078
51444246 = yrday
fracday
Element set: 904
Inclination: 51
6465 deg
RA of node: 193
5530 deg
Eccentricity:
0012447
Arg of perigee: 31
4462 deg
Mean anomaly: 328
7432 deg
Mean motion: 15
52901837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2078
Checksum: 304
Coasting Arc #6 (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 = 3253101
96 A = 6782861
92 meter
Y = -3446400
62 meter E =
0019083
Z = 4846297
68 I = 51
58196
XDOT = 6689
965149 Wp = 44
12098
YDOT = 2844
694826 meter/sec RA = 187
54300 deg
ZDOT = -2448
464840 TA = 70
02261
MA = 69
81720
Ha = 226
927 n
mi
Hp = 213
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10672906
70 X = 3267856
72
Y = -11307088
65 feet Y = -3409939
47 meter
Z = 15899926
76 Z = 4862136
98
XDOT = 21948
704558 XDOT = 6669
551853
YDOT = 9332
988275 feet/sec YDOT = 2919
391881 meter/sec
ZDOT = -8033
021128 ZDOT = -2416
015636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11082209
79 X = 3377857
54
Y = -10808911
39 feet Y = -3294556
19 meter
Z = 15966243
24 Z = 4866510
94
XDOT = 20758
309566 XDOT = 6327
132756
YDOT = 9523
707500 feet/sec YDOT = 2902
826046 meter/sec
ZDOT = -7898
159041 ZDOT = -2407
358876
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
54409791
00016717 00000-0 10270-3 0 9051
2 25544 51
6467 188
4291 0012551 35
2038 324
9941 15
52898827 20941
Satellite: ISS
Catalog Number: 25544
Epoch time: 13079
54409791 = yrday
fracday
Element set: 905
Inclination: 51
6467 deg
RA of node: 188
4291 deg
Eccentricity:
0012551
Arg of perigee: 35
2038 deg
Mean anomaly: 324
9941 deg
Mean motion: 15
52898827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2094
Checksum: 336
Coasting Arc #7 (Orbit 2101)
---------------------------------------
Vector Time (GMT): 2013/080/00:45:48
066
Vector Time (MET): N/A
Weight (LBS) : 921879
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5743588
93 A = 6792588
34 meter
Y = 2554559
84 meter E =
0011779
Z = -2589196
40 I = 51
62157
XDOT = -4056
994228 Wp = 72
21628
YDOT = 3820
181368 meter/sec RA = 184
93895 deg
ZDOT = -5246
715425 TA = 136
85035
MA = 136
75799
Ha = 227
598 n
mi
Hp = 214
991
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18843795
69 X = 5727173
94
Y = 8381101
85 feet Y = 2618696
26 meter
Z = -8494738
83 Z = -2561334
87
XDOT = -13310
348516 XDOT = -4073
923852
YDOT = 12533
403437 feet/sec YDOT = 3774
718378 meter/sec
ZDOT = -17213
633284 ZDOT = -5266
465247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20005857
56 X = -6097785
39
Y = -5201057
37 feet Y = -1585282
29 meter
Z = -8378947
27 Z = -2553903
13
XDOT = 10614
500747 XDOT = 3235
299828
YDOT = -13051
028073 feet/sec YDOT = -3977
953357 meter/sec
ZDOT = -17296
278566 ZDOT = -5271
905707
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 13080
05893687
00016717 00000-0 10270-3 0 9061
2 25544 51
6460 185
8707 0009987 45
8693 314
3279 15
52059871 21025
Satellite: ISS
Catalog Number: 25544
Epoch time: 13080
05893687 = yrday
fracday
Element set: 906
Inclination: 51
6460 deg
RA of node: 185
8707 deg
Eccentricity:
0009987
Arg of perigee: 45
8693 deg
Mean anomaly: 314
3279 deg
Mean motion: 15
52059871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2102
Checksum: 340
Coasting Arc #8 (Orbit 2117)
---------------------------------------
Vector Time (GMT): 2013/081/00:45:48
066
Vector Time (MET): N/A
Weight (LBS) : 921879
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5193755
06 A = 6790468
72 meter
Y = -2701123
16 meter E =
0021178
Z = 3416708
76 I = 51
64497
XDOT = 4938
484997 Wp = 72
10394
YDOT = -3647
491552 meter/sec RA = 179
97172 deg
ZDOT = 4606
335693 TA = 327
89660
MA = 328
02540
Ha = 227
740 n
mi
Hp = 214
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17039878
79 X = -5179761
81
Y = -8861952
63 feet Y = -2759124
42 meter
Z = 11209674
41 Z = 3391512
45
XDOT = 16202
378600 XDOT = 4956
528851
YDOT = -11966
835802 feet/sec YDOT = -3592
164958 meter/sec
ZDOT = 15112
649912 ZDOT = 4630
370382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18420391
50 X = 5614535
33
Y = 5649507
85 feet Y = 1721969
99 meter
Z = 11104985
91 Z = 3384799
71
XDOT = -13289
996811 XDOT = -4050
791028
YDOT = 13317
292337 feet/sec YDOT = 4059
110704 meter/sec
ZDOT = 15213
134667 ZDOT = 4636
963447
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 13081
08913730
00016717 00000-0 10270-3 0 9078
2 25544 51
6459 180
7511 0010083 49
5338 310
6691 15
52069084 21187
Satellite: ISS
Catalog Number: 25544
Epoch time: 13081
08913730 = yrday
fracday
Element set: 907
Inclination: 51
6459 deg
RA of node: 180
7511 deg
Eccentricity:
0010083
Arg of perigee: 49
5338 deg
Mean anomaly: 310
6691 deg
Mean motion: 15
52069084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2118
Checksum: 299
Coasting Arc #9 (Orbit 2132)
---------------------------------------
Vector Time (GMT): 2013/082/00:45:48
066
Vector Time (MET): N/A
Weight (LBS) : 921879
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4515120
13 A = 6787985
06 meter
Y = 2912545
95 meter E =
0017393
Z = -4167229
14 I = 51
66865
XDOT = -5694
513151 Wp = 60
70526
YDOT = 3471
747906 meter/sec RA = 175
00268 deg
ZDOT = -3746
968150 TA = 170
67215
MA = 170
63980
Ha = 227
632 n
mi
Hp = 214
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14813386
27 X = 4502458
94
Y = 9555596
93 feet Y = 2962965
59 meter
Z = -13672011
61 Z = -4145326
38
XDOT = -18682
785930 XDOT = -5714
710157
YDOT = 11390
249035 feet/sec YDOT = 3407
954919 meter/sec
ZDOT = -12293
202593 ZDOT = -3774
680777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16482646
36 X = -5023910
61
Y = -6445704
01 feet Y = -1964650
58 meter
Z = -13581053
56 Z = -4139505
12
XDOT = 15540
019457 XDOT = 4736
597930
YDOT = -13617
046145 feet/sec YDOT = -4150
475665 meter/sec
ZDOT = -12409
001139 ZDOT = -3782
263547
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 13082
05493738
00016717 00000-0 10270-3 0 9088
2 25544 51
6468 175
9513 0010065 52
4586 307
7478 15
52108834 21337
Satellite: ISS
Catalog Number: 25544
Epoch time: 13082
05493738 = yrday
fracday
Element set: 908
Inclination: 51
6468 deg
RA of node: 175
9513 deg
Eccentricity:
0010065
Arg of perigee: 52
4586 deg
Mean anomaly: 307
7478 deg
Mean motion: 15
52108834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2133
Checksum: 319
Coasting Arc #10 (Orbit 2148)
---------------------------------------
Vector Time (GMT): 2013/083/00:45:48
066
Vector Time (MET): N/A
Weight (LBS) : 921879
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3720796
45 A = 6785828
85 meter
Y = -3130851
97 meter E =
0015631
Z = 4718679
66 I = 51
69198
XDOT = 6331
684892 Wp = 82
81474
YDOT = -3336
811241 meter/sec RA = 170
03185 deg
ZDOT = 2772
755328 TA = 339
74317
MA = 339
80511
Ha = 227
779 n
mi
Hp = 214
533
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12207337
43 X = -3708431
94
Y = -10271824
05 feet Y = -3172390
51 meter
Z = 15481232
48 Z = 4700634
96
XDOT = 20773
244395 XDOT = 6355
058055
YDOT = -10947
543443 feet/sec YDOT = -3265
875303 meter/sec
ZDOT = 9096
966298 ZDOT = 2803
571036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14208395
52 X = 4330718
96
Y = 7413740
03 feet Y = 2259707
96 meter
Z = 15406361
37 Z = 4695858
95
XDOT = -17368
110511 XDOT = -5293
800084
YDOT = 14073
350233 feet/sec YDOT = 4289
557151 meter/sec
ZDOT = 9225
689733 ZDOT = 2811
990231
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 13083
08511310
00016717 00000-0 10270-3 0 9090
2 25544 51
6468 170
8314 0010106 56
3282 303
8832 15
52114056 21493
Satellite: ISS
Catalog Number: 25544
Epoch time: 13083
08511310 = yrday
fracday
Element set: 909
Inclination: 51
6468 deg
RA of node: 170
8314 deg
Eccentricity:
0010106
Arg of perigee: 56
3282 deg
Mean anomaly: 303
8832 deg
Mean motion: 15
52114056 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2149
Checksum: 277
Coasting Arc #11 (Orbit 2163)
---------------------------------------
Vector Time (GMT): 2013/084/00:45:48
066
Vector Time (MET): N/A
Weight (LBS) : 921879
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2861682
92 A = 6784081
12 meter
Y = 3426309
44 meter E =
0023149
Z = -5129102
08 I = 51
71694
XDOT = -6763
001505 Wp = 69
76936
YDOT = 3160
744448 meter/sec RA = 165
05975 deg
ZDOT = -1660
156400 TA = 184
16630
MA = 184
18561
Ha = 227
644 n
mi
Hp = 214
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9388723
50 X = 2848072
17
Y = 11241172
71 feet Y = 3458233
73 meter
Z = -16827762
74 Z = -5115233
92
XDOT = -22188
325147 XDOT = -6789
778435
YDOT = 10369
896482 feet/sec YDOT = 3084
966344 meter/sec
ZDOT = -5446
707348 ZDOT = -1693
075766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11821564
66 X = -3603212
91
Y = -8757439
67 feet Y = -2669267
61 meter
Z = -16770317
56 Z = -5111592
79
XDOT = 18539
362955 XDOT = 5650
797829
YDOT = -14321
686744 feet/sec YDOT = -4365
250120 meter/sec
ZDOT = -5584
188639 ZDOT = -1702
060697
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 13084
05089047
00016717 00000-0 10270-3 0 9107
2 25544 51
6473 166
0317 0010090 59
0266 301
1876 15
52153559 21640
Satellite: ISS
Catalog Number: 25544
Epoch time: 13084
05089047 = yrday
fracday
Element set: 910
Inclination: 51
6473 deg
RA of node: 166
0317 deg
Eccentricity:
0010090
Arg of perigee: 59
0266 deg
Mean anomaly: 301
1876 deg
Mean motion: 15
52153559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2164
Checksum: 291
Coasting Arc #12 (Orbit 2179)
---------------------------------------
Vector Time (GMT): 2013/085/00:45:48
066
Vector Time (MET): N/A
Weight (LBS) : 921879
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1937371
38 A = 6783139
56 meter
Y = -3745519
93 meter E =
0012051
Z = 5302860
00 I = 51
74339
XDOT = 7061
498687 Wp = 73
18085
YDOT = -2966
484247 meter/sec RA = 160
08740 deg
ZDOT = 487
084972 TA = 12
19785
MA = 12
16870
Ha = 227
703 n
mi
Hp = 214
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6356205
32 X = -1921104
01
Y = -12288451
23 feet Y = -3767093
07 meter
Z = 17397834
65 Z = 5293488
53
XDOT = 23167
646612 XDOT = 7091
779596
YDOT = -9732
559867 feet/sec YDOT = -2887
348735 meter/sec
ZDOT = 1598
047807 ZDOT = 521
463046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9293194
76 X = 2832565
76
Y = 10314468
29 feet Y = 3143849
94 meter
Z = 17359156
23 Z = 5291070
82
XDOT = -19290
948449 XDOT = -5879
881087
YDOT = 14463
586142 feet/sec YDOT = 4408
501056 meter/sec
ZDOT = 1741
598494 ZDOT = 530
839221
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 13085
08104124
00016717 00000-0 10270-3 0 9116
2 25544 51
6472 160
9118 0010051 62
7874 297
4300 15
52169072 21808
Satellite: ISS
Catalog Number: 25544
Epoch time: 13085
08104124 = yrday
fracday
Element set: 911
Inclination: 51
6472 deg
RA of node: 160
9118 deg
Eccentricity:
0010051
Arg of perigee: 62
7874 deg
Mean anomaly: 297
4300 deg
Mean motion: 15
52169072 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2180
Checksum: 278
Coasting Arc #13 (Orbit 2194)
---------------------------------------
Vector Time (GMT): 2013/086/00:45:48
066
Vector Time (MET): N/A
Weight (LBS) : 921879
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1033736
02 A = 6783170
30 meter
Y = 4126142
30 meter E =
0023885
Z = -5303958
06 I = 51
77165
XDOT = -7124
369588 Wp = 83
56688
YDOT = 2689
142006 meter/sec RA = 155
11589 deg
ZDOT = 708
799718 TA = 193
17736
MA = 193
23986
Ha = 227
637 n
mi
Hp = 214
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3391522
36 X = 1013285
06
Y = 13537212
27 feet Y = 4137587
04 meter
Z = -17401437
21 Z = -5298986
55
XDOT = -23373
915972 XDOT = -7157
353817
YDOT = 8822
644377 feet/sec YDOT = 2609
288499 meter/sec
ZDOT = 2325
458394 ZDOT = 674
109542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6937787
73 X = -2114637
70
Y = -12138033
87 feet Y = -3699672
72 meter
Z = -17381133
22 Z = -5297769
41
XDOT = 19356
293269 XDOT = 5899
798188
YDOT = -14160
950864 feet/sec YDOT = -4316
257823 meter/sec
ZDOT = 2180
623896 ZDOT = 664
654164
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 13086
04679664
00016717 00000-0 10270-3 0 9120
2 25544 51
6468 156
1115 0010042 65
6094 294
6105 15
52185559 21959
Satellite: ISS
Catalog Number: 25544
Epoch time: 13086
04679664 = yrday
fracday
Element set: 912
Inclination: 51
6468 deg
RA of node: 156
1115 deg
Eccentricity:
0010042
Arg of perigee: 65
6094 deg
Mean anomaly: 294
6105 deg
Mean motion: 15
52185559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2195
Checksum: 313
Coasting Arc #14 (Orbit 2210)
---------------------------------------
Vector Time (GMT): 2013/087/00:45:48
066
Vector Time (MET): N/A
Weight (LBS) : 921879
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -118853
30 A = 6784033
95 meter
Y = -4515041
86 meter E =
0015444
Z = 5051834
86 I = 51
80221
XDOT = 7060
800627 Wp = 64
47486
YDOT = -2326
611957 meter/sec RA = 150
14710 deg
ZDOT = -1902
249865 TA = 43
97327
MA = 43
85050
Ha = 227
586 n
mi
Hp = 214
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -389938
64 X = -92896
94
Y = -14813129
47 feet Y = -4516225
12 meter
Z = 16574261
36 Z = 5051321
16
XDOT = 23165
356389 XDOT = 7095
533209
YDOT = -7633
241328 feet/sec YDOT = -2247
459700 meter/sec
ZDOT = -6240
977249 ZDOT = -1867
864187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4615881
01 X = 1406920
53
Y = 14082978
32 feet Y = 4292491
79 meter
Z = 16572578
58 Z = 5051321
95
XDOT = -19114
774889 XDOT = -5826
183386
YDOT = 13483
036187 feet/sec YDOT = 4109
629430 meter/sec
ZDOT = -6097
436371 ZDOT = -1858
498606
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 13087
07692255
00016717 00000-0 10270-3 0 9136
2 25544 51
6466 150
9913 0009982 68
9296 291
2922 15
52226158 22116
Satellite: ISS
Catalog Number: 25544
Epoch time: 13087
07692255 = yrday
fracday
Element set: 913
Inclination: 51
6466 deg
RA of node: 150
9913 deg
Eccentricity:
0009982
Arg of perigee: 68
9296 deg
Mean anomaly: 291
2922 deg
Mean motion: 15
52226158 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2211
Checksum: 326
Coasting Arc #15 (Orbit 2225)
---------------------------------------
Vector Time (GMT): 2013/088/00:45:48
066
Vector Time (MET): N/A
Weight (LBS) : 921879
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -692717
66 A = 6785812
29 meter
Y = 4921415
05 meter E =
0019263
Z = -4637214
89 I = 51
83300
XDOT = -6791
635917 Wp = 91
80692
YDOT = 1856
306313 meter/sec RA = 145
18190 deg
ZDOT = 2994
782864 TA = 207
99880
MA = 208
10256
Ha = 227
615 n
mi
Hp = 214
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2272695
74 X = -725171
91
Y = 16146374
83 feet Y = 4913486
63 meter
Z = -15213959
61 Z = -4640659
51
XDOT = -22282
270069 XDOT = -6826
436760
YDOT = 6090
243810 feet/sec YDOT = 1780
163739 meter/sec
ZDOT = 9825
403096 ZDOT = 2961
704607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2701271
41 X = -823347
53
Y = -16066150
94 feet Y = -4896962
81 meter
Z = -15228823
32 Z = -4641745
35
XDOT = 18364
106994 XDOT = 5597
379812
YDOT = -12238
538963 feet/sec YDOT = -3730
306676 meter/sec
ZDOT = 9687
346167 ZDOT = 2952
703112
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 13088
04265616
00016717 00000-0 10270-3 0 9142
2 25544 51
6454 146
1905 0009991 72
3905 287
8337 15
52215420 22264
Satellite: ISS
Catalog Number: 25544
Epoch time: 13088
04265616 = yrday
fracday
Element set: 914
Inclination: 51
6454 deg
RA of node: 146
1905 deg
Eccentricity:
0009991
Arg of perigee: 72
3905 deg
Mean anomaly: 287
8337 deg
Mean motion: 15
52215420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2226
Checksum: 310
Coasting Arc #16 (Orbit 2241)
---------------------------------------
Vector Time (GMT): 2013/089/00:45:48
066
Vector Time (MET): N/A
Weight (LBS) : 921879
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1471157
62 A = 6788003
07 meter
Y = -5288859
39 meter E =
0020856
Z = 3978430
68 I = 51
86538
XDOT = 6420
356367 Wp = 77
59216
YDOT = -1247
818228 meter/sec RA = 140
22197 deg
ZDOT = -4010
891671 TA = 54
15836
MA = 53
96479
Ha = 227
524 n
mi
Hp = 214
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4826632
61 X = 1510863
07
Y = -17351900
90 feet Y = -5272185
59 meter
Z = 13052594
11 Z = 3985674
47
XDOT = 21064
161309 XDOT = 6453
316614
YDOT = -4093
891823 feet/sec YDOT = -1175
837856 meter/sec
ZDOT = -13159
093408 ZDOT = -3979
621618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 915541
89 X = 279057
17
Y = 17965049
43 feet Y = 5475747
07 meter
Z = 13083342
16 Z = 3987802
69
XDOT = -17495
293231 XDOT = -5332
565377
YDOT = 10432
538389 feet/sec YDOT = 3179
837701 meter/sec
ZDOT = -13028
622504 ZDOT = -3971
124139
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 13089
07275802
00016717 00000-0 10270-3 0 9155
2 25544 51
6454 141
0698 0009965 75
3234 284
9021 15
52268734 22428
Satellite: ISS
Catalog Number: 25544
Epoch time: 13089
07275802 = yrday
fracday
Element set: 915
Inclination: 51
6454 deg
RA of node: 141
0698 deg
Eccentricity:
0009965
Arg of perigee: 75
3234 deg
Mean anomaly: 284
9021 deg
Mean motion: 15
52268734 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2242
Checksum: 317
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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