Date:
March 4th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 2916)
---------------------------------------
Vector Time (GMT): 2009/061/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3220490
26 A = 6738696
51 meter
Y = 5635011
66 meter E =
0015484
Z = -1806968
77 I = 51
89921
XDOT = -5058
454575 Wp = 61
99094
YDOT = -1079
108030 meter/sec RA = 132
35812 deg
ZDOT = 5694
260166 TA = 278
08169
MA = 278
25733
Ha = 197
738 n
mi
Hp = 184
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10565912
94 X = -3274484
65
Y = 18487571
06 feet Y = 5598696
30 meter
Z = -5928375
22 Z = -1822745
21
XDOT = -16595
979578 XDOT = -5073
673439
YDOT = -3540
380675 feet/sec YDOT = -1135
759498 meter/sec
ZDOT = 18681
955926 ZDOT = 5669
649360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14373771
90 X = -4381125
67
Y = 15687427
81 feet Y = 4781528
00 meter
Z = -5989467
67 Z = -1825589
75
XDOT = -14356
537651 XDOT = -4375
872676
YDOT = -6112
757090 feet/sec YDOT = -1863
168361 meter/sec
ZDOT = 18585
820403 ZDOT = 5664
958059
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 09061
52440963
00010596 00000-0 82463-4 0 9009
2 25544 51
6398 133
2909 0009235 79
9705 280
2498 15
71202711 29176
Satellite: ISS
Catalog Number: 25544
Epoch time: 09061
52440963 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 133
2909 deg
Eccentricity:
0009235
Arg of perigee: 79
9705 deg
Mean anomaly: 280
2498 deg
Mean motion: 15
71202711 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2917
Checksum: 315
Coasting Arc #2 (Orbit 2932)
---------------------------------------
Vector Time (GMT): 2009/062/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4890588
00 A = 6730949
35 meter
Y = -437106
07 meter E =
0019567
Z = -4622442
51 I = 51
89217
XDOT = -2200
095294 Wp = 77
00081
YDOT = 6732
927818 meter/sec RA = 127
29955 deg
ZDOT = -2970
604484 TA = 163
59072
MA = 163
52729
Ha = 197
761 n
mi
Hp = 184
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16045236
23 X = 4917567
17
Y = -1434075
04 feet Y = -382265
88 meter
Z = -15165493
80 Z = -4598618
64
XDOT = -7218
160415 XDOT = -2260
789922
YDOT = 22089
658195 feet/sec YDOT = 6707
985671 meter/sec
ZDOT = -9746
077702 ZDOT = -2981
439998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16083474
15 X = 4902242
92
Y = 1907493
94 feet Y = 581404
15 meter
Z = -15072548
06 Z = -4594112
65
XDOT = -11404
008103 XDOT = -3475
941670
YDOT = 18976
526730 feet/sec YDOT = 5784
045347 meter/sec
ZDOT = -9787
809185 ZDOT = -2983
324240
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 09062
54202856
00010596 00000-0 82463-4 0 9010
2 25544 51
6398 128
0855 0009337 84
3669 275
8557 15
71233233 29337
Satellite: ISS
Catalog Number: 25544
Epoch time: 09062
54202856 = yrday
fracday
Element set: 901
Inclination: 51
6398 deg
RA of node: 128
0855 deg
Eccentricity:
0009337
Arg of perigee: 84
3669 deg
Mean anomaly: 275
8557 deg
Mean motion: 15
71233233 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2933
Checksum: 327
Coasting Arc #3 (Orbit 2948)
---------------------------------------
Vector Time (GMT): 2009/063/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 572837
15 A = 6735037
76 meter
Y = -5814733
56 meter E =
0021956
Z = 3331336
96 I = 51
92405
XDOT = 5707
006474 Wp = 89
31641
YDOT = -2149
681069 meter/sec RA = 122
15661 deg
ZDOT = -4706
777369 TA = 51
69238
MA = 51
49515
Ha = 197
653 n
mi
Hp = 184
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1879386
96 X = 621633
02
Y = -19077209
83 feet Y = -5808054
93 meter
Z = 10929583
21 Z = 3334238
29
XDOT = 18723
774520 XDOT = 5753
484847
YDOT = -7052
759413 feet/sec YDOT = -2085
602117 meter/sec
ZDOT = -15442
182969 ZDOT = -4678
940128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5377489
72 X = 1639058
87
Y = -18393405
01 feet Y = -5606309
85 meter
Z = 10940433
08 Z = 3334644
00
XDOT = 18463
211711 XDOT = 5627
586930
YDOT = -3774
785901 feet/sec YDOT = -1150
554742 meter/sec
ZDOT = -15333
701205 ZDOT = -4673
712127
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 09063
55963109
00010596 00000-0 82463-4 0 9028
2 25544 51
6402 122
8808 0009331 86
8357 273
3873 15
71303793 29498
Satellite: ISS
Catalog Number: 25544
Epoch time: 09063
55963109 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 122
8808 deg
Eccentricity:
0009331
Arg of perigee: 86
8357 deg
Mean anomaly: 273
3873 deg
Mean motion: 15
71303793 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2949
Checksum: 326
Coasting Arc #4 (Orbit 2964)
---------------------------------------
Vector Time (GMT): 2009/064/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4735317
59 A = 6734739
88 meter
Y = 3272141
25 meter E =
0021983
Z = 3478283
35 I = 51
93708
XDOT = -872
105623 Wp = 91
14786
YDOT = -6143
129284 meter/sec RA = 117
11293 deg
ZDOT = 4566
693611 TA = 309
91602
MA = 310
10902
Ha = 197
853 n
mi
Hp = 184
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15535818
88 X = -4788451
89
Y = 10735371
56 feet Y = 3218891
07 meter
Z = 11411690
79 Z = 3455150
50
XDOT = -2861
238920 XDOT = -825
531135
YDOT = -20154
623635 feet/sec YDOT = -6152
621287 meter/sec
ZDOT = 14982
590587 ZDOT = 4562
570087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17211156
60 X = -5245960
53
Y = 7901447
79 feet Y = 2408361
29 meter
Z = 11321650
44 Z = 3450839
06
XDOT = 1127
797562 XDOT = 343
752697
YDOT = -19106
382035 feet/sec YDOT = -5823
625244 meter/sec
ZDOT = 14965
997113 ZDOT = 4561
635920
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 09064
57722191
00010596 00000-0 82463-4 0 9036
2 25544 51
6399 117
6761 0009594 90
8255 269
4006 15
71288104 29656
Satellite: ISS
Catalog Number: 25544
Epoch time: 09064
57722191 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 117
6761 deg
Eccentricity:
0009594
Arg of perigee: 90
8255 deg
Mean anomaly: 269
4006 deg
Mean motion: 15
71288104 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2965
Checksum: 332
Coasting Arc #5 (Orbit 2979)
---------------------------------------
Vector Time (GMT): 2009/065/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1960526
42 A = 6731057
65 meter
Y = 4602856
36 meter E =
0019200
Z = -4521231
32 I = 51
93841
XDOT = -4751
009999 Wp = 102
34756
YDOT = 5134
052268 meter/sec RA = 111
97046 deg
ZDOT = 3173
848834 TA = 199
26964
MA = 199
34234
Ha = 197
714 n
mi
Hp = 184
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6432173
30 X = 1930873
67
Y = 15101234
77 feet Y = 4624614
27 meter
Z = -14833436
08 Z = -4511779
34
XDOT = -15587
303147 XDOT = -4823
484382
YDOT = 16844
003504 feet/sec YDOT = 5080
518508 meter/sec
ZDOT = 10412
889876 ZDOT = 3150
592839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4106563
05 X = 1251680
42
Y = 15926726
81 feet Y = 4854466
33 meter
Z = -14796164
50 Z = -4509870
94
XDOT = -16900
183416 XDOT = -5151
175905
YDOT = 13925
099921 feet/sec YDOT = 4244
370456 meter/sec
ZDOT = 10322
507127 ZDOT = 3146
300172
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 09065
53119879
00010596 00000-0 82463-4 0 9047
2 25544 51
6409 112
7966 0009537 93
6626 266
5627 15
71310163 29806
Satellite: ISS
Catalog Number: 25544
Epoch time: 09065
53119879 = yrday
fracday
Element set: 904
Inclination: 51
6409 deg
RA of node: 112
7966 deg
Eccentricity:
0009537
Arg of perigee: 93
6626 deg
Mean anomaly: 266
5627 deg
Mean motion: 15
71310163 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2980
Checksum: 333
Coasting Arc #6 (Orbit 2995)
---------------------------------------
Vector Time (GMT): 2009/066/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3328740
65 A = 6737995
76 meter
Y = -5495848
10 meter E =
0015237
Z = -2027144
87 I = 51
97207
XDOT = 3340
570658 Wp = 115
02338
YDOT = 4075
683405 meter/sec RA = 106
91802 deg
ZDOT = -5603
114983 TA = 87
43177
MA = 87
25734
Ha = 197
697 n
mi
Hp = 184
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10921065
13 X = 3399796
00
Y = -18030997
70 feet Y = -5458226
96 meter
Z = -6650737
76 Z = -2010801
48
XDOT = 10959
877488 XDOT = 3321
965663
YDOT = 13371
664716 feet/sec YDOT = 4112
935409 meter/sec
ZDOT = -18382
923171 ZDOT = -5586
932209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13334012
60 X = 4064207
04
Y = -16353274
22 feet Y = -4984477
98 meter
Z = -6587365
53 Z = -2007829
01
XDOT = 7930
148571 XDOT = 2417
109284
YDOT = 13793
462515 feet/sec YDOT = 4204
247375 meter/sec
ZDOT = -18319
410807 ZDOT = -5583
756414
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 09066
54876013
00010596 00000-0 82463-4 0 9050
2 25544 51
6411 107
5912 0009582 97
6206 262
6045 15
71342492 29968
Satellite: ISS
Catalog Number: 25544
Epoch time: 09066
54876013 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 107
5912 deg
Eccentricity:
0009582
Arg of perigee: 97
6206 deg
Mean anomaly: 262
6045 deg
Mean motion: 15
71342492 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2996
Checksum: 318
Coasting Arc #7 (Orbit 3011)
---------------------------------------
Vector Time (GMT): 2009/067/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3644510
81 A = 6728169
96 meter
Y = -2297047
32 meter E =
0013006
Z = 5157148
84 I = 51
94542
XDOT = 2574
452186 Wp = 87
05751
YDOT = -7136
270518 meter/sec RA = 101
79596 deg
ZDOT = -1355
659080 TA = 15
87150
MA = 15
83078
Ha = 197
754 n
mi
Hp = 184
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11957056
47 X = -3643605
84
Y = -7536244
48 feet Y = -2337796
99 meter
Z = 16919779
66 Z = 5139446
60
XDOT = 8446
365441 XDOT = 2660
645194
YDOT = -23412
961018 feet/sec YDOT = -7106
999647 meter/sec
ZDOT = -4447
700393 ZDOT = -1342
942920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11059467
16 X = -3370925
59
Y = -8932797
80 feet Y = -2722716
77 meter
Z = 16850472
80 Z = 5136024
11
XDOT = 10578
119970 XDOT = 3224
210967
YDOT = -21416
044963 feet/sec YDOT = -6527
610505 meter/sec
ZDOT = -4398
619012 ZDOT = -1340
699075
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 09067
56630662
00010596 00000-0 82463-4 0 9062
2 25544 51
6398 102
3863 0009623 101
0409 259
1836 15
71376343 30122
Satellite: ISS
Catalog Number: 25544
Epoch time: 09067
56630662 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 102
3863 deg
Eccentricity:
0009623
Arg of perigee: 101
0409 deg
Mean anomaly: 259
1836 deg
Mean motion: 15
71376343 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3012
Checksum: 304
Coasting Arc #8 (Orbit 3027)
---------------------------------------
Vector Time (GMT): 2009/068/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1030764
31 A = 6739572
71 meter
Y = 6647881
12 meter E =
0019834
Z = 314761
61 I = 51
98907
XDOT = -4642
909018 Wp = 72
02136
YDOT = -1020
842216 meter/sec RA = 96
71787 deg
ZDOT = 6052
319879 TA = 291
37940
MA = 291
59092
Ha = 197
583 n
mi
Hp = 184
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3381772
67 X = -1106554
43
Y = 21810633
60 feet Y = 6635930
78 meter
Z = 1032682
45 Z = 309569
60
XDOT = -15232
641136 XDOT = -4660
549121
YDOT = -3349
219868 feet/sec YDOT = -1072
860030 meter/sec
ZDOT = 19856
692517 ZDOT = 6029
722394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5623006
63 X = -1713892
42
Y = 21343905
57 feet Y = 6505622
42 meter
Z = 1012940
57 Z = 308744
29
XDOT = -13362
548550 XDOT = -4072
904798
YDOT = -4506
743298 feet/sec YDOT = -1373
655357 meter/sec
ZDOT = 19768
370196 ZDOT = 6025
399236
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 09068
58383894
00010596 00000-0 82463-4 0 9078
2 25544 51
6402 97
1813 0009594 104
5976 255
6250 15
71390761 30286
Satellite: ISS
Catalog Number: 25544
Epoch time: 09068
58383894 = yrday
fracday
Element set: 907
Inclination: 51
6402 deg
RA of node: 97
1813 deg
Eccentricity:
0009594
Arg of perigee: 104
5976 deg
Mean anomaly: 255
6250 deg
Mean motion: 15
71390761 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3028
Checksum: 334
Coasting Arc #9 (Orbit 3042)
---------------------------------------
Vector Time (GMT): 2009/069/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4153669
78 A = 6727681
55 meter
Y = -533897
86 meter E =
0023914
Z = -5285561
64 I = 51
95083
XDOT = 242
141900 Wp = 94
36167
YDOT = 7652
871667 meter/sec RA = 91
62640 deg
ZDOT = -586
773796 TA = 170
09365
MA = 170
04642
Ha = 197
536 n
mi
Hp = 184
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13627525
51 X = 4185007
04
Y = -1751633
39 feet Y = -487274
45 meter
Z = -17341081
50 Z = -5265307
31
XDOT = 794
428805 XDOT = 159
398606
YDOT = 25107
846676 feet/sec YDOT = 7655
116734 meter/sec
ZDOT = -1925
110878 ZDOT = -585
799288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13827405
59 X = 4214593
22
Y = -562022
49 feet Y = -171304
46 meter
Z = -17262032
44 Z = -5261467
49
XDOT = -1402
596492 XDOT = -427
511411
YDOT = 24075
510577 feet/sec YDOT = 7338
215624 meter/sec
ZDOT = -1920
695607 ZDOT = -585
428021
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 09069
53776179
00010596 00000-0 82463-4 0 9087
2 25544 51
6399 92
3006 0009522 108
3529 251
8669 15
71387135 30439
Satellite: ISS
Catalog Number: 25544
Epoch time: 09069
53776179 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 92
3006 deg
Eccentricity:
0009522
Arg of perigee: 108
3529 deg
Mean anomaly: 251
8669 deg
Mean motion: 15
71387135 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3043
Checksum: 336
Coasting Arc #10 (Orbit 3058)
---------------------------------------
Vector Time (GMT): 2009/070/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1433549
38 A = 6738742
88 meter
Y = -6437858
84 meter E =
0023521
Z = 1329985
34 I = 51
98681
XDOT = 4463
164325 Wp = 116
60416
YDOT = -2221
168439 meter/sec RA = 86
51529 deg
ZDOT = -5872
041608 TA = 48
86550
MA = 48
66273
Ha = 197
506 n
mi
Hp = 184
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4703246
01 X = -1367914
38
Y = -21121584
13 feet Y = -6453522
49 meter
Z = 4363468
97 Z = 1323181
41
XDOT = 14642
927575 XDOT = 4516
195052
YDOT = -7287
298029 feet/sec YDOT = -2170
962898 meter/sec
ZDOT = -19265
228374 ZDOT = -5850
230767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3258773
93 X = -993274
29
Y = -21397611
90 feet Y = -6521992
11 meter
Z = 4336392
33 Z = 1321732
38
XDOT = 13661
615270 XDOT = 4164
060334
YDOT = -6013
750441 feet/sec YDOT = -1832
991134 meter/sec
ZDOT = -19180
234267 ZDOT = -5846
135405
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 09070
55526499
00010596 00000-0 82463-4 0 9090
2 25544 51
6386 87
0942 0009641 111
3038 248
9154 15
71432642 30593
Satellite: ISS
Catalog Number: 25544
Epoch time: 09070
55526499 = yrday
fracday
Element set: 909
Inclination: 51
6386 deg
RA of node: 87
0942 deg
Eccentricity:
0009641
Arg of perigee: 111
3038 deg
Mean anomaly: 248
9154 deg
Mean motion: 15
71432642 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3059
Checksum: 323
Coasting Arc #11 (Orbit 3074)
---------------------------------------
Vector Time (GMT): 2009/071/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3341325
09 A = 6729358
39 meter
Y = 3255696
38 meter E =
0016521
Z = 4840083
47 I = 51
95172
XDOT = -2943
909178 Wp = 117
31194
YDOT = -6684
682779 meter/sec RA = 81
45343 deg
ZDOT = 2450
395691 TA = 308
79308
MA = 308
94052
Ha = 197
498 n
mi
Hp = 184
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10962352
65 X = -3400994
58
Y = 10681418
57 feet Y = 3217998
64 meter
Z = 15879538
95 Z = 4823706
13
XDOT = -9658
494678 XDOT = -2880
844641
YDOT = -21931
373946 feet/sec YDOT = -6717
250402 meter/sec
ZDOT = 8039
355940 ZDOT = 2436
248209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11593138
63 X = -3533588
65
Y = 10093758
54 feet Y = 3076577
60 meter
Z = 15815840
50 Z = 4820668
19
XDOT = -7818
012082 XDOT = -2382
930083
YDOT = -21559
820246 feet/sec YDOT = -6571
433211 meter/sec
ZDOT = 7983
592629 ZDOT = 2433
399033
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 09071
57275277
00010596 00000-0 82463-4 0 9100
2 25544 51
6380 81
8881 0009521 115
0993 245
1149 15
71443499 30752
Satellite: ISS
Catalog Number: 25544
Epoch time: 09071
57275277 = yrday
fracday
Element set: 910
Inclination: 51
6380 deg
RA of node: 81
8881 deg
Eccentricity:
0009521
Arg of perigee: 115
0993 deg
Mean anomaly: 245
1149 deg
Mean motion: 15
71443499 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3075
Checksum: 322
Coasting Arc #12 (Orbit 3089)
---------------------------------------
Vector Time (GMT): 2009/072/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3528746
86 A = 6735838
96 meter
Y = 4970202
68 meter E =
0012786
Z = -2880398
24 I = 51
96849
XDOT = -2882
805307 Wp = 100
86714
YDOT = 4986
325610 meter/sec RA = 76
31768 deg
ZDOT = 5088
978690 TA = 226
28463
MA = 226
39060
Ha = 197
351 n
mi
Hp = 184
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11577253
49 X = 3486899
38
Y = 16306439
25 feet Y = 5009428
92 meter
Z = -9450125
45 Z = -2863357
77
XDOT = -9458
022662 XDOT = -2963
070246
YDOT = 16359
335991 feet/sec YDOT = 4953
640114 meter/sec
ZDOT = 16696
124310 ZDOT = 5074
778613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11059032
15 X = 3370793
00
Y = 16700026
03 feet Y = 5090167
93 meter
Z = -9383206
75 Z = -2860001
42
XDOT = -8898
285062 XDOT = -2712
197287
YDOT = 15211
772749 feet/sec YDOT = 4636
548334 meter/sec
ZDOT = 16641
054732 ZDOT = 5072
193482
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 09072
52663349
00010596 00000-0 82463-4 0 9118
2 25544 51
6383 77
0082 0009553 118
2504 241
9623 15
71469838 30906
Satellite: ISS
Catalog Number: 25544
Epoch time: 09072
52663349 = yrday
fracday
Element set: 911
Inclination: 51
6383 deg
RA of node: 77
0082 deg
Eccentricity:
0009553
Arg of perigee: 118
2504 deg
Mean anomaly: 241
9623 deg
Mean motion: 15
71469838 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3090
Checksum: 314
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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