[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 31st 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 105 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 ET - UTC (sec) : 66 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 1235)
---------------------------------------
Vector Time (GMT): 2011/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4552296
80 A = 6768519
01 meter
Y = -4499125
61 meter E =
0025832
Z = 2158307
85 I = 51
81921
XDOT = 4858
893675 Wp = 119
00066
YDOT = 2250
861521 meter/sec RA = 150
71406 deg
ZDOT = -5518
956673 TA = 37
01424
MA = 36
83631
Ha = 215
045 n
mi
Hp = 200
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14935356
96 X = 4591784
07
Y = -14760910
78 feet Y = -4447998
09 meter
Z = 7081062
50 Z = 2180518
80
XDOT = 15941
252214 XDOT = 4860
172624
YDOT = 7384
716277 feet/sec YDOT = 2305
203360 meter/sec
ZDOT = -18106
813231 ZDOT = -5495
349636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19535437
56 X = -5954401
37
Y = 7617442
47 feet Y = 2321796
46 meter
Z = 7171615
60 Z = 2185908
44
XDOT = -11232
188553 XDOT = -3423
571071
YDOT = -11735
118045 feet/sec YDOT = -3576
863980 meter/sec
ZDOT = -18010
788744 ZDOT = -5489
688409
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 11241
53642096
00016717 00000-0 10270-3 0 9001
2 25544 51
6401 151
5788 0012305 129
5863 230
6382 15
60609357 12367
Satellite: ISS
Catalog Number: 25544
Epoch time: 11241
53642096 = yrday
fracday
Element set: 900
Inclination: 51
6401 deg
RA of node: 151
5788 deg
Eccentricity:
0012305
Arg of perigee: 129
5863 deg
Mean anomaly: 230
6382 deg
Mean motion: 15
60609357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1236
Checksum: 292
Coasting Arc #2 (Orbit 1251)
---------------------------------------
Vector Time (GMT): 2011/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6041777
26 A = 6769424
58 meter
Y = 2584712
20 meter E =
0021426
Z = 1612267
66 I = 51
84830
XDOT = -608
537437 Wp = 95
43752
YDOT = -5050
817625 meter/sec RA = 145
72615 deg
ZDOT = 5749
372961 TA = 282
20078
MA = 282
44068
Ha = 214
959 n
mi
Hp = 200
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19822103
86 X = -6078062
99
Y = 8480026
92 feet Y = 2516946
61 meter
Z = 5289592
05 Z = 1582828
68
XDOT = -1996
513900 XDOT = -579
942080
YDOT = -16570
923965 feet/sec YDOT = -5057
462289 meter/sec
ZDOT = 18862
772182 ZDOT = 5746
486606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21587423
92 X = 6579846
81
Y = -253168
86 feet Y = -77165
87 meter
Z = 5169668
86 Z = 1575715
07
XDOT = -4398
040196 XDOT = -1340
522652
YDOT = 14545
310344 feet/sec YDOT = 4433
410593 meter/sec
ZDOT = 18851
182712 ZDOT = 5745
840491
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 11242
56095975
00016717 00000-0 10270-3 0 9014
2 25544 51
6401 146
4210 0012175 133
1339 227
0837 15
60635198 12529
Satellite: ISS
Catalog Number: 25544
Epoch time: 11242
56095975 = yrday
fracday
Element set: 901
Inclination: 51
6401 deg
RA of node: 146
4210 deg
Eccentricity:
0012175
Arg of perigee: 133
1339 deg
Mean anomaly: 227
0837 deg
Mean motion: 15
60635198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1252
Checksum: 287
Coasting Arc #3 (Orbit 1266)
---------------------------------------
Vector Time (GMT): 2011/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4906108
89 A = 6761367
54 meter
Y = 671956
19 meter E =
0018615
Z = -4616384
51 I = 51
84662
XDOT = -3645
136568 Wp = 106
96272
YDOT = 6037
687413 meter/sec RA = 140
71298 deg
ZDOT = -3010
353933 TA = 133
16639
MA = 133
01066
Ha = 214
821 n
mi
Hp = 200
927
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16096157
78 X = 4920655
74
Y = 2204580
69 feet Y = 726900
28 meter
Z = -15145618
46 Z = -4592515
50
XDOT = -11959
109476 XDOT = -3697
756586
YDOT = 19808
685737 feet/sec YDOT = 5996
630818 meter/sec
ZDOT = -9876
489282 ZDOT = -3028
190179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14256993
61 X = -4345531
65
Y = -7976086
22 feet Y = -2431111
08 meter
Z = -15048468
75 Z = -4586773
27
XDOT = 17742
566723 XDOT = 5407
934337
YDOT = -13038
176039 feet/sec YDOT = -3974
036057 meter/sec
ZDOT = -9949
299029 ZDOT = -3032
546344
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 11243
52145058
00016717 00000-0 10270-3 0 9020
2 25544 51
6405 141
5851 0012103 136
8946 223
3160 15
60682536 12677
Satellite: ISS
Catalog Number: 25544
Epoch time: 11243
52145058 = yrday
fracday
Element set: 902
Inclination: 51
6405 deg
RA of node: 141
5851 deg
Eccentricity:
0012103
Arg of perigee: 136
8946 deg
Mean anomaly: 223
3160 deg
Mean motion: 15
60682536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1267
Checksum: 281
Coasting Arc #4 (Orbit 1282)
---------------------------------------
Vector Time (GMT): 2011/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1841114
02 A = 6758676
65 meter
Y = -3901301
37 meter E =
0012936
Z = 5192265
50 I = 51
86042
XDOT = 6072
061050 Wp = 123
12776
YDOT = -4543
877672 meter/sec RA = 135
66160 deg
ZDOT = -1265
688972 TA = 338
92672
MA = 338
97997
Ha = 214
668 n
mi
Hp = 200
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6040400
33 X = -1822575
09
Y = -12799545
17 feet Y = -3921785
86 meter
Z = 17034991
81 Z = 5183366
66
XDOT = 19921
460137 XDOT = 6128
568759
YDOT = -14907
735143 feet/sec YDOT = -4475
660298 meter/sec
ZDOT = -4152
522875 ZDOT = -1236
053448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1275120
10 X = 388656
61
Y = 14139213
55 feet Y = 4309632
29 meter
Z = 16998895
49 Z = 5181263
34
XDOT = -22871
101285 XDOT = -6971
111672
YDOT = 6891
367117 feet/sec YDOT = 2100
488697 meter/sec
ZDOT = -4031
713028 ZDOT = -1228
866131
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 11244
54595963
00016717 00000-0 10270-3 0 9038
2 25544 51
6400 136
4269 0011967 141
2906 218
9109 15
60730826 12838
Satellite: ISS
Catalog Number: 25544
Epoch time: 11244
54595963 = yrday
fracday
Element set: 903
Inclination: 51
6400 deg
RA of node: 136
4269 deg
Eccentricity:
0011967
Arg of perigee: 141
2906 deg
Mean anomaly: 218
9109 deg
Mean motion: 15
60730826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1283
Checksum: 310
Coasting Arc #5 (Orbit 1297)
---------------------------------------
Vector Time (GMT): 2011/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1730668
69 A = 6766083
39 meter
Y = 5763952
77 meter E =
0014234
Z = -3112310
10 I = 51
90622
XDOT = -5826
578743 Wp = 127
67602
YDOT = 892
425863 meter/sec RA = 130
62950 deg
ZDOT = 4899
557456 TA = 196
61391
MA = 196
66059
Ha = 214
531 n
mi
Hp = 201
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5678046
87 X = -1779874
69
Y = 18910606
19 feet Y = 5744324
12 meter
Z = -10210991
13 Z = -3120837
42
XDOT = -19116
071990 XDOT = -5859
926107
YDOT = 2927
906376 feet/sec YDOT = 827
083235 meter/sec
ZDOT = 16074
663568 ZDOT = 4871
170945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11606740
99 X = 3537734
66
Y = -15950558
58 feet Y = -4861730
26 meter
Z = -10245917
58 Z = -3122955
68
XDOT = 17925
016652 XDOT = 5463
545075
YDOT = 2806
402451 feet/sec YDOT = 855
391467 meter/sec
ZDOT = 15959
053697 ZDOT = 4864
319567
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 11245
50642556
00016717 00000-0 10270-3 0 9047
2 25544 51
6401 131
5906 0011954 144
6320 215
5632 15
60716157 12987
Satellite: ISS
Catalog Number: 25544
Epoch time: 11245
50642556 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 131
5906 deg
Eccentricity:
0011954
Arg of perigee: 144
6320 deg
Mean anomaly: 215
5632 deg
Mean motion: 15
60716157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1298
Checksum: 288
Coasting Arc #6 (Orbit 1313)
---------------------------------------
Vector Time (GMT): 2011/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4314459
62 A = 6770166
74 meter
Y = -5163537
13 meter E =
0022797
Z = -635024
41 I = 51
93844
XDOT = 3296
305627 Wp = 144
78827
YDOT = 3477
991465 meter/sec RA = 125
64305 deg
ZDOT = -6009
482946 TA = 42
06534
MA = 41
89055
Ha = 214
559 n
mi
Hp = 201
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14155051
26 X = 4374963
47
Y = -16940738
62 feet Y = -5114951
92 meter
Z = -2083413
41 Z = -613917
75
XDOT = 10814
651008 XDOT = 3286
361964
YDOT = 11410
733152 feet/sec YDOT = 3514
797052 meter/sec
ZDOT = -19716
151398 ZDOT = -5993
493758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18813645
16 X = -5734399
04
Y = 11565135
68 feet Y = 3525053
36 meter
Z = -1997274
43 Z = -608769
25
XDOT = -5900
823444 XDOT = -1798
570986
YDOT = -12919
191498 feet/sec YDOT = -3937
769569 meter/sec
ZDOT = -19651
175384 ZDOT = -5989
678257
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 11246
53090799
00016717 00000-0 10270-3 0 9058
2 25544 51
6401 126
4319 0012070 149
3081 210
8783 15
60691149 13141
Satellite: ISS
Catalog Number: 25544
Epoch time: 11246
53090799 = yrday
fracday
Element set: 905
Inclination: 51
6401 deg
RA of node: 126
4319 deg
Eccentricity:
0012070
Arg of perigee: 149
3081 deg
Mean anomaly: 210
8783 deg
Mean motion: 15
60691149 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1314
Checksum: 293
Coasting Arc #7 (Orbit 1329)
---------------------------------------
Vector Time (GMT): 2011/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4968149
75 A = 6763422
66 meter
Y = 2226515
12 meter E =
0020553
Z = 4008409
74 I = 51
93292
XDOT = 279
244580 Wp = 127
73054
YDOT = -6569
044056 meter/sec RA = 120
64676 deg
ZDOT = 3968
839831 TA = 281
12797
MA = 281
35899
Ha = 214
376 n
mi
Hp = 201
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16299703
91 X = -5012149
86
Y = 7304839
65 feet Y = 2170712
25 meter
Z = 13150950
59 Z = 3984167
71
XDOT = 916
156758 XDOT = 333
400358
YDOT = -21551
981811 feet/sec YDOT = -6565
618542 meter/sec
ZDOT = 13021
128055 ZDOT = 3970
327986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17818436
97 X = 5431059
59
Y = -2033081
92 feet Y = -619683
37 meter
Z = 13052142
08 Z = 3978292
91
XDOT = -7438
156609 XDOT = -2267
150135
YDOT = 18998
935455 feet/sec YDOT = 5790
875527 meter/sec
ZDOT = 13027
445803 ZDOT = 3970
765481
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 11247
55537473
00016717 00000-0 10270-3 0 9067
2 25544 51
6400 121
2731 0011823 152
1884 207
9907 15
60737166 13302
Satellite: ISS
Catalog Number: 25544
Epoch time: 11247
55537473 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 121
2731 deg
Eccentricity:
0011823
Arg of perigee: 152
1884 deg
Mean anomaly: 207
9907 deg
Mean motion: 15
60737166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1330
Checksum: 293
Coasting Arc #8 (Orbit 1344)
---------------------------------------
Vector Time (GMT): 2011/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3679169
52 A = 6758029
90 meter
Y = 1980408
04 meter E =
0022496
Z = -5328619
11 I = 51
92967
XDOT = -3429
917125 Wp = 119
65400
YDOT = 6852
402950 meter/sec RA = 115
60466 deg
ZDOT = 168
221990 TA = 152
00416
MA = 151
88297
Ha = 214
096 n
mi
Hp = 201
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12070766
14 X = 3682635
99
Y = 6497401
70 feet Y = 2021570
12 meter
Z = -17482346
15 Z = -5310737
46
XDOT = -11253
008939 XDOT = -3507
104298
YDOT = 22481
636974 feet/sec YDOT = 6813
615944 meter/sec
ZDOT = 551
909415 ZDOT = 151
372092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9821980
89 X = -2993739
78
Y = -9694667
94 feet Y = -2954934
79 meter
Z = -17409599
53 Z = -5306445
94
XDOT = 16484
780302 XDOT = 5024
561036
YDOT = -17629
615541 feet/sec YDOT = -5373
506817 meter/sec
ZDOT = 483
006848 ZDOT = 147
220487
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 11248
51579775
00016717 00000-0 10270-3 0 9076
2 25544 51
6397 116
4361 0011728 156
5997 203
5695 15
60793864 13458
Satellite: ISS
Catalog Number: 25544
Epoch time: 11248
51579775 = yrday
fracday
Element set: 907
Inclination: 51
6397 deg
RA of node: 116
4361 deg
Eccentricity:
0011728
Arg of perigee: 156
5997 deg
Mean anomaly: 203
5695 deg
Mean motion: 15
60793864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1345
Checksum: 348
Coasting Arc #9 (Orbit 1360)
---------------------------------------
Vector Time (GMT): 2011/249/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1146216
71 A = 6763655
15 meter
Y = -5449104
38 meter E =
0017846
Z = 3818518
35 I = 51
96170
XDOT = 5027
160042 Wp = 121
78623
YDOT = -4013
867208 meter/sec RA = 110
56729 deg
ZDOT = -4213
684533 TA = 12
31848
MA = 12
27491
Ha = 213
911 n
mi
Hp = 201
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3760553
53 X = -1103748
00
Y = -17877639
03 feet Y = -5461684
57 meter
Z = 12527947
33 Z = 3813053
31
XDOT = 16493
307226 XDOT = 5092
139309
YDOT = -13168
855668 feet/sec YDOT = -3957
287159 meter/sec
ZDOT = -13824
424320 ZDOT = -4189
105035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1099454
11 X = -335113
61
Y = 18250877
13 feet Y = 5562867
35 meter
Z = 12505914
16 Z = 3811802
64
XDOT = -18170
334764 XDOT = -5538
318036
YDOT = 8321
130355 feet/sec YDOT = 2536
280532 meter/sec
ZDOT = -13724
142916 ZDOT = -4183
118761
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 11249
54023537
00016717 00000-0 10270-3 0 9081
2 25544 51
6402 111
2779 0011561 160
6184 199
5414 15
60840472 13619
Satellite: ISS
Catalog Number: 25544
Epoch time: 11249
54023537 = yrday
fracday
Element set: 908
Inclination: 51
6402 deg
RA of node: 111
2779 deg
Eccentricity:
0011561
Arg of perigee: 160
6184 deg
Mean anomaly: 199
5414 deg
Mean motion: 15
60840472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1361
Checksum: 294
Coasting Arc #10 (Orbit 1375)
---------------------------------------
Vector Time (GMT): 2011/250/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1575928
97 A = 6769864
90 meter
Y = 6578608
01 meter E =
0011249
Z = -317835
43 I = 51
99104
XDOT = -4662
664919 Wp = 104
48103
YDOT = -833
917520 meter/sec RA = 105
57591 deg
ZDOT = 6033
427927 TA = 252
10411
MA = 252
22680
Ha = 213
792 n
mi
Hp = 201
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5170370
64 X = -1647831
16
Y = 21583359
61 feet Y = 6560582
97 meter
Z = -1042767
16 Z = -325665
98
XDOT = -15297
457083 XDOT = -4682
302180
YDOT = -2735
949869 feet/sec YDOT = -886
167932 meter/sec
ZDOT = 19794
711045 ZDOT = 6010
729391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10428315
57 X = 3178550
59
Y = -19589697
30 feet Y = -5970939
74 meter
Z = -1074942
69 Z = -327642
53
XDOT = 12803
894278 XDOT = 3902
626976
YDOT = 5765
426682 feet/sec YDOT = 1757
302053 meter/sec
ZDOT = 19702
285693 ZDOT = 6005
256679
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 11250
50063356
00016717 00000-0 10270-3 0 9093
2 25544 51
6393 106
4410 0011642 164
5131 195
6383 15
60829035 13761
Satellite: ISS
Catalog Number: 25544
Epoch time: 11250
50063356 = yrday
fracday
Element set: 909
Inclination: 51
6393 deg
RA of node: 106
4410 deg
Eccentricity:
0011642
Arg of perigee: 164
5131 deg
Mean anomaly: 195
6383 deg
Mean motion: 15
60829035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1376
Checksum: 288
Coasting Arc #11 (Orbit 1391)
---------------------------------------
Vector Time (GMT): 2011/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3566575
31 A = 6765039
92 meter
Y = -4634895
98 meter E =
0013497
Z = -3394554
62 I = 51
98101
XDOT = 2688
948203 Wp = 148
42850
YDOT = 5473
261176 meter/sec RA = 100
59107 deg
ZDOT = -4667
464068 TA = 71
15563
MA = 71
00930
Ha = 213
732 n
mi
Hp = 202
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11701362
57 X = 3634628
39
Y = -15206351
66 feet Y = -4594632
01 meter
Z = -11136990
24 Z = -3377063
00
XDOT = 8822
008539 XDOT = 2650
218577
YDOT = 17956
893621 feet/sec YDOT = 5503
113878 meter/sec
ZDOT = -15313
202323 ZDOT = -4654
495709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15011322
35 X = -4575451
05
Y = 12016724
95 feet Y = 3662697
76 meter
Z = -11065536
19 Z = -3372775
43
XDOT = -3570
166197 XDOT = -1088
186657
YDOT = -18453
119861 feet/sec YDOT = -5624
510934 meter/sec
ZDOT = -15260
608570 ZDOT = -4651
433492
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 11251
52504291
00016717 00000-0 10270-3 0 9106
2 25544 51
6383 101
2818 0011605 168
8321 191
3095 15
60832198 13927
Satellite: ISS
Catalog Number: 25544
Epoch time: 11251
52504291 = yrday
fracday
Element set: 910
Inclination: 51
6383 deg
RA of node: 101
2818 deg
Eccentricity:
0011605
Arg of perigee: 168
8321 deg
Mean anomaly: 191
3095 deg
Mean motion: 15
60832198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1392
Checksum: 287
Coasting Arc #12 (Orbit 1407)
---------------------------------------
Vector Time (GMT): 2011/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4194257
45 A = 6758112
10 meter
Y = 530309
19 meter E =
0013845
Z = 5270214
22 I = 51
96220
XDOT = 92
207303 Wp = 161
23614
YDOT = -7636
567592 meter/sec RA = 95
55993 deg
ZDOT = 828
414537 TA = 280
81625
MA = 280
97205
Ha = 213
659 n
mi
Hp = 202
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13760687
18 X = -4225477
06
Y = 1739859
54 feet Y = 483232
23 meter
Z = 17290729
07 Z = 5249763
00
XDOT = 302
517399 XDOT = 173
569823
YDOT = -25054
355618 feet/sec YDOT = -7635
081496 meter/sec
ZDOT = 2717
895463 ZDOT = 829
060605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13910438
00 X = 4239901
50
Y = 1326022
93 feet Y = 404171
79 meter
Z = 17207391
22 Z = 5244812
84
XDOT = -5648
476705 XDOT = -1721
655700
YDOT = 23373
933890 feet/sec YDOT = 7124
375050 meter/sec
ZDOT = 2720
859849 ZDOT = 829
318082
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 11252
54943793
00016717 00000-0 10270-3 0 9114
2 25544 51
6382 96
1223 0011584 172
1908 187
9431 15
60838024 14080
Satellite: ISS
Catalog Number: 25544
Epoch time: 11252
54943793 = yrday
fracday
Element set: 911
Inclination: 51
6382 deg
RA of node: 96
1223 deg
Eccentricity:
0011584
Arg of perigee: 172
1908 deg
Mean anomaly: 187
9431 deg
Mean motion: 15
60838024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1408
Checksum: 308
Coasting Arc #13 (Orbit 1422)
---------------------------------------
Vector Time (GMT): 2011/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3376866
25 A = 6761699
52 meter
Y = 3927270
40 meter E =
0017162
Z = -4363257
51 I = 51
97523
XDOT = -2770
683841 Wp = 148
50728
YDOT = 6248
034422 meter/sec RA = 90
51441 deg
ZDOT = 3471
278267 TA = 156
62022
MA = 156
54209
Ha = 213
343 n
mi
Hp = 202
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11078957
53 X = 3353895
37
Y = 12884745
42 feet Y = 3964903
78 meter
Z = -14315149
31 Z = -4346909
07
XDOT = -9090
170083 XDOT = -2857
207254
YDOT = 20498
800596 feet/sec YDOT = 6216
567457 meter/sec
ZDOT = 11388
708226 ZDOT = 3457
607794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8342243
77 X = -2542715
90
Y = -14868234
25 feet Y = -4531837
80 meter
Z = -14248720
77 Z = -4343010
09
XDOT = 12014
313050 XDOT = 3661
962618
YDOT = -17627
145732 feet/sec YDOT = -5372
754019 meter/sec
ZDOT = 11332
739711 ZDOT = 3454
219064
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 11253
50979229
00016717 00000-0 10270-3 0 9125
2 25544 51
6368 91
2838 0011591 176
1884 183
9362 15
60892881 14234
Satellite: ISS
Catalog Number: 25544
Epoch time: 11253
50979229 = yrday
fracday
Element set: 912
Inclination: 51
6368 deg
RA of node: 91
2838 deg
Eccentricity:
0011591
Arg of perigee: 176
1884 deg
Mean anomaly: 183
9362 deg
Mean motion: 15
60892881 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1423
Checksum: 333
Coasting Arc #14 (Orbit 1438)
---------------------------------------
Vector Time (GMT): 2011/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1371917
13 A = 6769082
96 meter
Y = -6522473
01 meter E =
0022029
Z = 1097858
81 I = 51
99999
XDOT = 4493
122800 Wp = 148
79695
YDOT = -1948
711695 meter/sec RA = 85
51561 deg
ZDOT = -5928
344591 TA = 19
30051
MA = 19
21721
Ha = 213
076 n
mi
Hp = 202
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4501040
44 X = -1304212
73
Y = -21399189
68 feet Y = -6537435
97 meter
Z = 3601898
98 Z = 1091359
21
XDOT = 14741
216535 XDOT = 4543
378233
YDOT = -6393
411074 feet/sec YDOT = -1898
186442 meter/sec
ZDOT = -19449
949446 ZDOT = -5906
394994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 497662
66 X = 151687
58
Y = 21866068
75 feet Y = 6664777
75 meter
Z = 3575713
83 Z = 1089877
58
XDOT = -14188
238557 XDOT = -4324
575112
YDOT = 3507
471051 feet/sec YDOT = 1069
077176 meter/sec
ZDOT = -19360
440548 ZDOT = -5901
062279
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 11254
53415531
00016717 00000-0 10270-3 0 9131
2 25544 51
6371 86
1247 0011359 180
4332 179
6816 15
60946982 14398
Satellite: ISS
Catalog Number: 25544
Epoch time: 11254
53415531 = yrday
fracday
Element set: 913
Inclination: 51
6371 deg
RA of node: 86
1247 deg
Eccentricity:
0011359
Arg of perigee: 180
4332 deg
Mean anomaly: 179
6816 deg
Mean motion: 15
60946982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1439
Checksum: 313
Coasting Arc #15 (Orbit 1454)
---------------------------------------
Vector Time (GMT): 2011/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886670
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1156502
88 A = 6766373
55 meter
Y = 6079378
43 meter E =
0015353
Z = 2738476
32 I = 51
98630
XDOT = -4646
160185 Wp = 125
80072
YDOT = -3231
631773 meter/sec RA = 80
53397 deg
ZDOT = 5183
015004 TA = 265
10487
MA = 265
28018
Ha = 212
999 n
mi
Hp = 202
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3794300
79 X = -1237700
65
Y = 19945467
30 feet Y = 6065992
00 meter
Z = 8984502
35 Z = 2732660
19
XDOT = -15243
307692 XDOT = -4634
856097
YDOT = -10602
466446 feet/sec YDOT = -3283
524217 meter/sec
ZDOT = 17004
642400 ZDOT = 5160
471934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7135582
64 X = 2174925
59
Y = -19019255
19 feet Y = -5797068
98 meter
Z = 8960527
84 Z = 2731168
89
XDOT = 11965
610878 XDOT = 3647
118196
YDOT = 12502
371744 feet/sec YDOT = 3810
722907 meter/sec
ZDOT = 16912
953385 ZDOT = 5155
068192
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 11255
55850333
00016717 00000-0 10270-3 0 9148
2 25544 51
6358 80
9639 0011629 184
3783 175
7273 15
60955525 14558
Satellite: ISS
Catalog Number: 25544
Epoch time: 11255
55850333 = yrday
fracday
Element set: 914
Inclination: 51
6358 deg
RA of node: 80
9639 deg
Eccentricity:
0011629
Arg of perigee: 184
3783 deg
Mean anomaly: 175
7273 deg
Mean motion: 15
60955525 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1455
Checksum: 330
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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