[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 12th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 26909 78 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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
322/05:01:03
600 -0
7 6
4 6
4
N/A 6
3 0
0 219
0
000/00:02:03
199 -1
2 -0
0 201
0
Coasting Arc #1 (Orbit 2359)
---------------------------------------
Vector Time (GMT): 2011/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2170842
30 A = 6760699
69 meter
Y = 3587582
53 meter E =
0033018
Z = -5327386
68 I = 51
79425
XDOT = -6535
119144 Wp = 58
73403
YDOT = 3989
806338 meter/sec RA = 148
35529 deg
ZDOT = 40
732247 TA = 211
55458
MA = 211
75300
Ha = 219
448 n
mi
Hp = 199
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7122186
04 X = 2156444
05
Y = 11770283
89 feet Y = 3611777
68 meter
Z = -17478302
76 Z = -5316875
46
XDOT = -21440
679607 XDOT = -6579
446110
YDOT = 13089
915806 feet/sec YDOT = 3916
478783 meter/sec
ZDOT = 133
635981 ZDOT = 8
876119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13561151
44 X = -4133438
96
Y = -2617521
18 feet Y = -797820
46 meter
Z = -17435594
01 Z = -5314369
06
XDOT = 4634
535194 XDOT = 1412
606327
YDOT = -23664
338750 feet/sec YDOT = -7212
890451 meter/sec
ZDOT = 3
469242 ZDOT = 1
057425
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 11313
51604435
00016717 00000-0 10270-3 0 9004
2 25544 51
6360 149
3013 0021763 37
3650 322
9015 15
59870852 23600
Satellite: ISS
Catalog Number: 25544
Epoch time: 11313
51604435 = yrday
fracday
Element set: 900
Inclination: 51
6360 deg
RA of node: 149
3013 deg
Eccentricity:
0021763
Arg of perigee: 37
3650 deg
Mean anomaly: 322
9015 deg
Mean motion: 15
59870852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2360
Checksum: 278
Coasting Arc #2 (Orbit 2375)
---------------------------------------
Vector Time (GMT): 2011/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1590477
46 A = 6765400
04 meter
Y = -5165411
22 meter E =
0030848
Z = 4061665
84 I = 51
83644
XDOT = 6541
082264 Wp = 52
77539
YDOT = -1068
695978 meter/sec RA = 143
31371 deg
ZDOT = -3882
020849 TA = 77
39822
MA = 77
05342
Ha = 219
328 n
mi
Hp = 198
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5218101
91 X = 1628388
55
Y = -16946887
22 feet Y = -5147413
61 meter
Z = 13325675
32 Z = 4069484
61
XDOT = 21460
243648 XDOT = 6571
405128
YDOT = -3506
220399 feet/sec YDOT = -995
379995 meter/sec
ZDOT = -12736
288874 ZDOT = -3850
169795
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9289478
47 X = 2831433
04
Y = 15075571
87 feet Y = 4595034
30 meter
Z = 13357841
12 Z = 4071469
97
XDOT = -10542
693037 XDOT = -3213
412838
YDOT = 17777
787639 feet/sec YDOT = 5418
669672 meter/sec
ZDOT = -12606
272521 ZDOT = -3842
391864
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 11314
54106794
00016717 00000-0 10270-3 0 9014
2 25544 51
6363 144
1456 0021653 40
7019 319
5750 15
59943037 23763
Satellite: ISS
Catalog Number: 25544
Epoch time: 11314
54106794 = yrday
fracday
Element set: 901
Inclination: 51
6363 deg
RA of node: 144
1456 deg
Eccentricity:
0021653
Arg of perigee: 40
7019 deg
Mean anomaly: 319
5750 deg
Mean motion: 15
59943037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2376
Checksum: 301
Coasting Arc #3 (Orbit 2390)
---------------------------------------
Vector Time (GMT): 2011/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4433472
46 A = 6771934
28 meter
Y = 5002623
70 meter E =
0031324
Z = -1003650
76 I = 51
88129
XDOT = -4169
355908 Wp = 42
98340
YDOT = -2529
265283 meter/sec RA = 138
31401 deg
ZDOT = 5941
261404 TA = 306
13774
MA = 306
42723
Ha = 219
346 n
mi
Hp = 198
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14545513
32 X = -4484207
60
Y = 16412807
41 feet Y = 4952762
25 meter
Z = -3292817
44 Z = -1025312
19
XDOT = -13678
989201 XDOT = -4169
625584
YDOT = -8298
114445 feet/sec YDOT = -2575
891271 meter/sec
ZDOT = 19492
327440 ZDOT = 5921
005428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3043892
80 X = -927778
53
Y = -21704727
45 feet Y = -6615600
93 meter
Z = -3381475
17 Z = -1030673
63
XDOT = 13687
182223 XDOT = 4171
853141
YDOT = -4878
382753 feet/sec YDOT = -1486
931063 meter/sec
ZDOT = 19409
801812 ZDOT = 5916
107592
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 11315
50199346
00016717 00000-0 10270-3 0 9027
2 25544 51
6352 139
3119 0021671 44
5488 315
7405 15
59975459 23910
Satellite: ISS
Catalog Number: 25544
Epoch time: 11315
50199346 = yrday
fracday
Element set: 902
Inclination: 51
6352 deg
RA of node: 139
3119 deg
Eccentricity:
0021671
Arg of perigee: 44
5488 deg
Mean anomaly: 315
7405 deg
Mean motion: 15
59975459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2391
Checksum: 321
Coasting Arc #4 (Orbit 2406)
---------------------------------------
Vector Time (GMT): 2011/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5549296
99 A = 6769274
66 meter
Y = -2891766
45 meter E =
0023259
Z = -2616770
20 I = 51
89518
XDOT = 427
174421 Wp = 61
05283
YDOT = 5553
806224 meter/sec RA = 133
33136 deg
ZDOT = -5255
865909 TA = 148
30697
MA = 148
16674
Ha = 219
356 n
mi
Hp = 198
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18206354
95 X = 5593932
94
Y = -9487422
74 feet Y = -2829461
11 meter
Z = -8585204
07 Z = -2589702
81
XDOT = 1401
490881 XDOT = 390
571542
YDOT = 18221
149030 feet/sec YDOT = 5558
378746 meter/sec
ZDOT = -17243
654557 ZDOT = -5253
879291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4300099
20 X = -1310670
23
Y = 20121603
19 feet Y = 6133064
65 meter
Z = -8474580
34 Z = -2583052
09
XDOT = -13545
559128 XDOT = -4128
686422
YDOT = -10119
931572 feet/sec YDOT = -3084
555143 meter/sec
ZDOT = -17235
849292 ZDOT = -5253
486864
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 11316
52694086
00016717 00000-0 10270-3 0 9032
2 25544 51
6353 134
1557 0021818 48
3066 311
9952 15
60065268 24070
Satellite: ISS
Catalog Number: 25544
Epoch time: 11316
52694086 = yrday
fracday
Element set: 903
Inclination: 51
6353 deg
RA of node: 134
1557 deg
Eccentricity:
0021818
Arg of perigee: 48
3066 deg
Mean anomaly: 311
9952 deg
Mean motion: 15
60065268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2407
Checksum: 306
Coasting Arc #5 (Orbit 2422)
---------------------------------------
Vector Time (GMT): 2011/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4537352
52 A = 6761582
29 meter
Y = -535528
20 meter E =
0024502
Z = 4961972
50 I = 51
88940
XDOT = 3138
451334 Wp = 66
23951
YDOT = -6691
164080 meter/sec RA = 128
31319 deg
ZDOT = 2149
055734 TA = 2
98255
MA = 2
96797
Ha = 219
476 n
mi
Hp = 198
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14886327
17 X = -4555131
75
Y = -1756982
27 feet Y = -586367
35 meter
Z = 16279437
32 Z = 4939886
39
XDOT = 10296
756346 XDOT = 3202
600065
YDOT = -21952
638057 feet/sec YDOT = -6655
709445 meter/sec
ZDOT = 7050
707790 ZDOT = 2164
458056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10709106
46 X = 3264135
65
Y = -10626887
99 feet Y = -3239075
46 meter
Z = 16189320
35 Z = 4934504
84
XDOT = 10008
043246 XDOT = 3050
451581
YDOT = 20916
390722 feet/sec YDOT = 6375
315892 meter/sec
ZDOT = 7113
949551 ZDOT = 2168
331823
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 11317
55184918
00016717 00000-0 10270-3 0 9045
2 25544 51
6350 128
9989 0021704 52
0789 308
2325 15
60088692 24232
Satellite: ISS
Catalog Number: 25544
Epoch time: 11317
55184918 = yrday
fracday
Element set: 904
Inclination: 51
6350 deg
RA of node: 128
9989 deg
Eccentricity:
0021704
Arg of perigee: 52
0789 deg
Mean anomaly: 308
2325 deg
Mean motion: 15
60088692 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2423
Checksum: 321
Coasting Arc #6 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2011/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2081398
61 A = 6761114
17 meter
Y = 4028217
63 meter E =
0031784
Z = -5038983
89 I = 51
90744
XDOT = -5269
736629 Wp = 73
97209
YDOT = 5188
444823 meter/sec RA = 123
26860 deg
ZDOT = 1989
910021 TA = 215
20080
MA = 215
41117
Ha = 219
282 n
mi
Hp = 197
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6828735
60 X = 2060678
45
Y = 13215937
12 feet Y = 4051377
57 meter
Z = -16532099
38 Z = -5028922
38
XDOT = -17289
162167 XDOT = -5337
029958
YDOT = 17022
456770 feet/sec YDOT = 5129
139018 meter/sec
ZDOT = 6528
576185 ZDOT = 1964
146093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14699725
82 X = -4480476
43
Y = -2561124
56 feet Y = -780630
77 meter
Z = -16491259
37 Z = -5026535
86
XDOT = -3121
682050 XDOT = -951
488689
YDOT = -23040
967667 feet/sec YDOT = -7022
886945 meter/sec
ZDOT = 6423
107248 ZDOT = 1957
763089
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 11318
51266300
00016717 00000-0 10270-3 0 9059
2 25544 51
6358 124
1651 0021708 55
9889 304
3325 15
60160075 24380
Satellite: ISS
Catalog Number: 25544
Epoch time: 11318
51266300 = yrday
fracday
Element set: 905
Inclination: 51
6358 deg
RA of node: 124
1651 deg
Eccentricity:
0021708
Arg of perigee: 55
9889 deg
Mean anomaly: 304
3325 deg
Mean motion: 15
60160075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 293
Coasting Arc #7 (Orbit 2453)
---------------------------------------
Vector Time (GMT): 2011/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 949880
73 A = 6768663
98 meter
Y = -6149045
68 meter E =
0032902
Z = 2649413
93 I = 51
94889
XDOT = 5429
660234 Wp = 75
84798
YDOT = -1444
477965 meter/sec RA = 118
25034 deg
ZDOT = -5237
119784 TA = 74
31611
MA = 73
95336
Ha = 219
174 n
mi
Hp = 197
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3116406
58 X = 1005699
44
Y = -20174034
38 feet Y = -6138111
58 meter
Z = 8692302
92 Z = 2654163
75
XDOT = 17813
845913 XDOT = 5470
850421
YDOT = -4739
100936 feet/sec YDOT = -1383
529574 meter/sec
ZDOT = -17182
151521 ZDOT = -5210
642194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14377748
86 X = 4382337
85
Y = 14478957
42 feet Y = 4413186
22 meter
Z = 8712055
62 Z = 2655434
55
XDOT = -5811
103765 XDOT = -1771
224428
YDOT = 16166
183730 feet/sec YDOT = 4927
452801 meter/sec
ZDOT = -17073
971501 ZDOT = -5204
146513
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 11319
53749103
00016717 00000-0 10270-3 0 9060
2 25544 51
6356 119
0077 0021607 59
3972 300
9311 15
60224271 24546
Satellite: ISS
Catalog Number: 25544
Epoch time: 11319
53749103 = yrday
fracday
Element set: 906
Inclination: 51
6356 deg
RA of node: 119
0077 deg
Eccentricity:
0021607
Arg of perigee: 59
3972 deg
Mean anomaly: 300
9311 deg
Mean motion: 15
60224271 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2454
Checksum: 290
Coasting Arc #8 (Orbit 2469)
---------------------------------------
Vector Time (GMT): 2011/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3301450
07 A = 6771113
97 meter
Y = 5819003
78 meter E =
0035124
Z = 938334
33 I = 51
97235
XDOT = -3737
886416 Wp = 60
23026
YDOT = -3105
721864 meter/sec RA = 113
27146 deg
ZDOT = 5959
644898 TA = 309
92548
MA = 310
23363
Ha = 219
141 n
mi
Hp = 197
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10831529
10 X = -3370832
25
Y = 19091219
75 feet Y = 5781696
96 meter
Z = 3078524
69 Z = 922127
45
XDOT = -12263
406878 XDOT = -3731
830969
YDOT = -10189
376195 feet/sec YDOT = -3147
487609 meter/sec
ZDOT = 19552
640742 ZDOT = 5941
500639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9214323
99 X = -2808525
95
Y = -19932337
18 feet Y = -6075376
37 meter
Z = 3012005
38 Z = 918059
24
XDOT = 14036
616884 XDOT = 4278
360826
YDOT = -3469
987725 feet/sec YDOT = -1057
652259 meter/sec
ZDOT = 19478
745432 ZDOT = 5937
121608
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 11320
56227913
00016717 00000-0 10270-3 0 9076
2 25544 51
6368 113
8517 0021678 63
5041 296
8335 15
60296631 24708
Satellite: ISS
Catalog Number: 25544
Epoch time: 11320
56227913 = yrday
fracday
Element set: 907
Inclination: 51
6368 deg
RA of node: 113
8517 deg
Eccentricity:
0021678
Arg of perigee: 63
5041 deg
Mean anomaly: 296
8335 deg
Mean motion: 15
60296631 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2470
Checksum: 308
Coasting Arc #9 (Orbit 2484)
---------------------------------------
Vector Time (GMT): 2011/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4429396
74 A = 6763968
38 meter
Y = -2990546
66 meter E =
0029420
Z = -4176958
85 I = 51
96055
XDOT = 919
465956 Wp = 67
76240
YDOT = 6602
716393 meter/sec RA = 108
27752 deg
ZDOT = -3762
575992 TA = 163
66997
MA = 163
57498
Ha = 219
097 n
mi
Hp = 197
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14532141
52 X = 4482799
50
Y = -9811504
80 feet Y = -2940715
72 meter
Z = -13703933
22 Z = -4155311
02
XDOT = 3016
620591 XDOT = 863
842810
YDOT = 21662
455357 feet/sec YDOT = 6612
687527 meter/sec
ZDOT = -12344
409423 ZDOT = -3758
244109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -220190
71 X = -67114
13
Y = 17601706
65 feet Y = 5365000
19 meter
Z = -13615358
55 Z = -4149961
29
XDOT = -18303
385434 XDOT = -5578
871880
YDOT = -9737
964853 feet/sec YDOT = -2968
131687 meter/sec
ZDOT = -12327
123056 ZDOT = -3757
307108
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 11321
52297995
00016717 00000-0 10270-3 0 9081
2 25544 51
6373 109
0172 0021758 66
6875 293
6567 15
60356016 24858
Satellite: ISS
Catalog Number: 25544
Epoch time: 11321
52297995 = yrday
fracday
Element set: 908
Inclination: 51
6373 deg
RA of node: 109
0172 deg
Eccentricity:
0021758
Arg of perigee: 66
6875 deg
Mean anomaly: 293
6567 deg
Mean motion: 15
60356016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2485
Checksum: 333
Coasting Arc #10 (Orbit 2495)
---------------------------------------
Vector Time (GMT): 2011/322/05:02:05
199
Vector Time (MET): N/A
Weight (LBS) : 870407
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4263344
28 A = 6762956
09 meter
Y = 21253
58 meter E =
0030760
Z = -5276385
79 I = 51
95521
XDOT = -1207
245707 Wp = 73
25566
YDOT = 7499
160031 meter/sec RA = 104
70957 deg
ZDOT = -941
165494 TA = 187
73745
MA = 187
78501
Ha = 219
045 n
mi
Hp = 201
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13987349
98 X = 4288421
71
Y = 69729
60 feet Y = 69069
22 meter
Z = -17310976
99 Z = -5255613
36
XDOT = -3960
779880 XDOT = -1286
441019
YDOT = 24603
543408 feet/sec YDOT = 7485
217079 meter/sec
ZDOT = -3087
813302 ZDOT = -947
222588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9309419
32 X = -2837511
01
Y = -10578988
47 feet Y = -3224475
69 meter
Z = -17226156
31 Z = -5250532
44
XDOT = 20237
787287 XDOT = 6168
477565
YDOT = -12718
108758 feet/sec YDOT = -3876
479549 meter/sec
ZDOT = -3113
008314 ZDOT = -948
844934
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 11322
22747399
00016717 00000-0 10270-3 0 9098
2 25544 51
6403 105
4769 0016689 64
9806 295
3080 15
59195509 24963
Satellite: ISS
Catalog Number: 25544
Epoch time: 11322
22747399 = yrday
fracday
Element set: 909
Inclination: 51
6403 deg
RA of node: 105
4769 deg
Eccentricity:
0016689
Arg of perigee: 64
9806 deg
Mean anomaly: 295
3080 deg
Mean motion: 15
59195509 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2496
Checksum: 345
Coasting Arc #11 (Orbit 2511)
---------------------------------------
Vector Time (GMT): 2011/323/05:02:05
199
Vector Time (MET): N/A
Weight (LBS) : 870407
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3084460
43 A = 6765031
06 meter
Y = -3751979
59 meter E =
0024611
Z = 4694044
13 I = 51
96959
XDOT = 3331
647345 Wp = 66
54690
YDOT = -6319
284783 meter/sec RA = 99
67966 deg
ZDOT = -2840
530460 TA = 51
53795
MA = 51
31737
Ha = 219
006 n
mi
Hp = 200
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10119620
83 X = -3065078
87
Y = -12309644
31 feet Y = -3786363
56 meter
Z = 15400407
26 Z = 4679106
73
XDOT = 10930
601524 XDOT = 3415
862155
YDOT = -20732
561623 feet/sec YDOT = -6281
557381 meter/sec
ZDOT = -9319
325655 ZDOT = -2824
140593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2144342
80 X = -653595
69
Y = 15849407
49 feet Y = 4830899
40 meter
Z = 15339644
34 Z = 4675523
60
XDOT = -21541
090344 XDOT = -6565
724337
YDOT = 6107
888789 feet/sec YDOT = 1861
684503 meter/sec
ZDOT = -9252
000328 ZDOT = -2820
009700
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 11323
25295158
00016717 00000-0 10270-3 0 9105
2 25544 51
6401 100
3248 0016633 68
0645 292
2276 15
59280276 25120
Satellite: ISS
Catalog Number: 25544
Epoch time: 11323
25295158 = yrday
fracday
Element set: 910
Inclination: 51
6401 deg
RA of node: 100
3248 deg
Eccentricity:
0016633
Arg of perigee: 68
0645 deg
Mean anomaly: 292
2276 deg
Mean motion: 15
59280276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2512
Checksum: 289
Coasting Arc #12 (Orbit 2526)
---------------------------------------
Vector Time (GMT): 2011/324/05:02:05
199
Vector Time (MET): N/A
Weight (LBS) : 870407
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1278135
09 A = 6772129
23 meter
Y = 6246284
45 meter E =
0022063
Z = -2282642
16 I = 51
99759
XDOT = -4526
414367 Wp = 64
35335
YDOT = 2906
874432 meter/sec RA = 94
68036 deg
ZDOT = 5470
161367 TA = 270
32103
MA = 270
57385
Ha = 218
934 n
mi
Hp = 200
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4193356
59 X = 1219281
73
Y = 20493059
21 feet Y = 6260248
26 meter
Z = -7488983
48 Z = -2276575
88
XDOT = -14850
440838 XDOT = -4585
156641
YDOT = 9536
989606 feet/sec YDOT = 2855
928871 meter/sec
ZDOT = 17946
723646 ZDOT = 5448
029023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11917690
87 X = 3632512
18
Y = -17201244
68 feet Y = -5242939
38 meter
Z = -7464610
82 Z = -2275213
38
XDOT = 15968
413496 XDOT = 4867
172434
YDOT = 3386
451515 feet/sec YDOT = 1032
190422 meter/sec
ZDOT = 17856
155650 ZDOT = 5442
556242
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 11324
21430272
00016717 00000-0 10270-3 0 9111
2 25544 51
6401 95
4947 0016633 71
4237 288
8723 15
59296609 25276
Satellite: ISS
Catalog Number: 25544
Epoch time: 11324
21430272 = yrday
fracday
Element set: 911
Inclination: 51
6401 deg
RA of node: 95
4947 deg
Eccentricity:
0016633
Arg of perigee: 71
4237 deg
Mean anomaly: 288
8723 deg
Mean motion: 15
59296609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2527
Checksum: 311
Coasting Arc #13 (Orbit 2542)
---------------------------------------
Vector Time (GMT): 2011/325/05:02:05
199
Vector Time (MET): N/A
Weight (LBS) : 870407
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 867428
72 A = 6773708
30 meter
Y = -6619234
43 meter E =
0021985
Z = -1153391
71 I = 52
00437
XDOT = 4620
592042 Wp = 98
40454
YDOT = 1617
135950 meter/sec RA = 89
70943 deg
ZDOT = -5904
443973 TA = 94
07179
MA = 93
82046
Ha = 218
870 n
mi
Hp = 200
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2845894
75 X = 946984
91
Y = -21716648
39 feet Y = -6609089
49 meter
Z = -3784093
55 Z = -1148984
41
XDOT = 15159
422710 XDOT = 4630
848758
YDOT = 5305
564141 feet/sec YDOT = 1668
863586 meter/sec
ZDOT = -19371
535343 ZDOT = -5881
971798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17480901
63 X = -5328178
82
Y = 13201105
50 feet Y = 4023696
96 meter
Z = -3765659
27 Z = -1147772
94
XDOT = -5982
570578 XDOT = -1823
487512
YDOT = -13328
838169 feet/sec YDOT = -4062
629874 meter/sec
ZDOT = -19279
870652 ZDOT = -5876
504575
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 11325
23970515
00016717 00000-0 10270-3 0 9124
2 25544 51
6400 90
3418 0016518 75
5362 284
7625 15
59320112 25439
Satellite: ISS
Catalog Number: 25544
Epoch time: 11325
23970515 = yrday
fracday
Element set: 912
Inclination: 51
6400 deg
RA of node: 90
3418 deg
Eccentricity:
0016518
Arg of perigee: 75
5362 deg
Mean anomaly: 284
7625 deg
Mean motion: 15
59320112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2543
Checksum: 287
Coasting Arc #14 (Orbit 2558)
---------------------------------------
Vector Time (GMT): 2011/326/05:02:05
199
Vector Time (MET): N/A
Weight (LBS) : 870407
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2747570
16 A = 6767120
76 meter
Y = 4655161
63 meter E =
0026866
Z = 4047219
66 I = 51
98151
XDOT = -3594
510395 Wp = 87
40898
YDOT = -5552
266305 meter/sec RA = 84
72203 deg
ZDOT = 3924
926891 TA = 322
12315
MA = 322
31187
Ha = 218
909 n
mi
Hp = 200
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9014337
79 X = -2819082
00
Y = 15272839
98 feet Y = 4624036
70 meter
Z = 13278279
74 Z = 4033698
03
XDOT = -11793
013108 XDOT = -3551
223721
YDOT = -18216
096801 feet/sec YDOT = -5592
220358 meter/sec
ZDOT = 12877
056728 ZDOT = 3907
569418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17186454
60 X = 5238431
36
Y = -4540428
33 feet Y = -1383922
56 meter
Z = 13222742
85 Z = 4030292
02
XDOT = -4605
793240 XDOT = -1403
845780
YDOT = 20064
322687 feet/sec YDOT = 6115
605555 meter/sec
ZDOT = 12806
549391 ZDOT = 3903
436254
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 11326
26506761
00016717 00000-0 10270-3 0 9137
2 25544 51
6397 85
1886 0016686 78
2786 282
0240 15
59389528 25598
Satellite: ISS
Catalog Number: 25544
Epoch time: 11326
26506761 = yrday
fracday
Element set: 913
Inclination: 51
6397 deg
RA of node: 85
1886 deg
Eccentricity:
0016686
Arg of perigee: 78
2786 deg
Mean anomaly: 282
0240 deg
Mean motion: 15
59389528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2559
Checksum: 349
Coasting Arc #15 (Orbit 2573)
---------------------------------------
Vector Time (GMT): 2011/327/05:02:05
199
Vector Time (MET): N/A
Weight (LBS) : 870407
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4052531
24 A = 6761845
98 meter
Y = -1052124
79 meter E =
0031360
Z = -5336612
99 I = 51
96036
XDOT = 1579
120192 Wp = 84
48845
YDOT = 7484
067062 meter/sec RA = 79
69625 deg
ZDOT = -274
800784 TA = 182
88959
MA = 182
90775
Ha = 218
633 n
mi
Hp = 200
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13295706
16 X = 4089920
06
Y = -3451853
00 feet Y = -1006597
62 meter
Z = -17508572
80 Z = -5316834
52
XDOT = 5180
840525 XDOT = 1496
649474
YDOT = 24554
025795 feet/sec YDOT = 7501
264645 meter/sec
ZDOT = -901
577375 ZDOT = -267
329230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12104165
30 X = -3689349
58
Y = -6708562
83 feet Y = -2044769
95 meter
Z = -17427724
46 Z = -5311970
42
XDOT = 12630
067644 XDOT = 3849
644618
YDOT = -20510
792753 feet/sec YDOT = -6251
689631 meter/sec
ZDOT = -871
591899 ZDOT = -265
661211
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 11327
22630704
00016717 00000-0 10270-3 0 9140
2 25544 51
6393 80
3569 0016528 81
6003 278
7025 15
59483501 25740
Satellite: ISS
Catalog Number: 25544
Epoch time: 11327
22630704 = yrday
fracday
Element set: 914
Inclination: 51
6393 deg
RA of node: 80
3569 deg
Eccentricity:
0016528
Arg of perigee: 81
6003 deg
Mean anomaly: 278
7025 deg
Mean motion: 15
59483501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2574
Checksum: 304
Coasting Arc #16 (Orbit 2589)
---------------------------------------
Vector Time (GMT): 2011/328/05:02:05
199
Vector Time (MET): N/A
Weight (LBS) : 870407
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4303828
18 A = 6765616
84 meter
Y = -2885487
89 meter E =
0026002
Z = 4331033
33 I = 51
96823
XDOT = 988
008111 Wp = 79
90155
YDOT = -6771
486727 meter/sec RA = 74
66721 deg
ZDOT = -3507
371220 TA = 45
58982
MA = 45
37726
Ha = 218
577 n
mi
Hp = 200
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14120171
19 X = -4292282
10
Y = -9466823
77 feet Y = -2933551
69 meter
Z = 14209426
95 Z = 4310152
66
XDOT = 3241
496426 XDOT = 1080
693374
YDOT = -22216
163804 feet/sec YDOT = -6759
919724 meter/sec
ZDOT = -11507
123425 ZDOT = -3502
346722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4090268
84 X = 1246713
94
Y = 16573472
36 feet Y = 5051594
38 meter
Z = 14124358
95 Z = 4305104
61
XDOT = -16231
890591 XDOT = -4947
480252
YDOT = 13857
270858 feet/sec YDOT = 4223
696158 meter/sec
ZDOT = -11486
107531 ZDOT = -3500
965575
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 11328
25159124
00016717 00000-0 10270-3 0 9157
2 25544 51
6401 75
2039 0016412 84
8909 275
4119 15
59569851 25906
Satellite: ISS
Catalog Number: 25544
Epoch time: 11328
25159124 = yrday
fracday
Element set: 915
Inclination: 51
6401 deg
RA of node: 75
2039 deg
Eccentricity:
0016412
Arg of perigee: 84
8909 deg
Mean anomaly: 275
4119 deg
Mean motion: 15
59569851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2590
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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