Date:
July 20th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 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 1082)
---------------------------------------
Vector Time (GMT): 2009/199/02:32:24
833
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -346383
63 A = 6721483
44 meter
Y = -4469692
44 meter E =
0001395
Z = 5009227
37 I = 51
80262
XDOT = 6952
245859 Wp = 303
93637
YDOT = -2693
814426 meter/sec RA = 147
11375 deg
ZDOT = -1922
543808 TA = 164
59061
MA = 164
58636
Ha = 188
923 n
mi
Hp = 186
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1136429
24 X = -320710
94
Y = -14664345
28 feet Y = -4473423
21 meter
Z = 16434473
01 Z = 5007606
25
XDOT = 22809
205574 XDOT = 6991
191210
YDOT = -8837
973839 feet/sec YDOT = -2615
852265 meter/sec
ZDOT = -6307
558426 ZDOT = -1888
675656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5469313
95 X = 1667046
89
Y = -13661577
98 feet Y = -4164048
97 meter
Z = 16427851
02 Z = 5007208
99
XDOT = 23387
672556 XDOT = 7128
562595
YDOT = 1936
633358 feet/sec YDOT = 590
285848 meter/sec
ZDOT = -6174
660508 ZDOT = -1882
036523
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 09199
15026519
00010596 00000-0 82463-4 0 9007
2 25544 51
6394 147
8855 0006278 247
3407 112
7093 15
73924188 10831
Satellite: ISS
Catalog Number: 25544
Epoch time: 09199
15026519 = yrday
fracday
Element set: 900
Inclination: 51
6394 deg
RA of node: 147
8855 deg
Eccentricity:
0006278
Arg of perigee: 247
3407 deg
Mean anomaly: 112
7093 deg
Mean motion: 15
73924188 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1083
Checksum: 328
Coasting Arc #2 (Orbit 1098)
---------------------------------------
Vector Time (GMT): 2009/200/02:32:24
833
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5837914
13 A = 6731275
32 meter
Y = 2898294
40 meter E =
0007966
Z = 1665312
05 I = 51
85973
XDOT = -863
641422 Wp = 58
16171
YDOT = -5050
967838 meter/sec RA = 142
02359 deg
ZDOT = 5747
225249 TA = 320
18397
MA = 320
24239
Ha = 188
713 n
mi
Hp = 186
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19153261
57 X = -5877979
21
Y = 9508839
90 feet Y = 2832787
10 meter
Z = 5463622
20 Z = 1636854
82
XDOT = -2833
469232 XDOT = -835
015292
YDOT = -16571
416790 feet/sec YDOT = -5060
466597 meter/sec
ZDOT = 18855
725883 ZDOT = 5743
098288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21410243
31 X = -6525842
16
Y = 272930
68 feet Y = 83189
27 meter
Z = 5351973
74 Z = 1631281
60
XDOT = 4535
786792 XDOT = 1382
507814
YDOT = -14651
975985 feet/sec YDOT = -4465
922280 meter/sec
ZDOT = 18839
229848 ZDOT = 5742
197258
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 09200
16616042
00010596 00000-0 82463-4 0 9018
2 25544 51
6394 142
6692 0006223 250
9823 109
0666 15
73910807 10990
Satellite: ISS
Catalog Number: 25544
Epoch time: 09200
16616042 = yrday
fracday
Element set: 901
Inclination: 51
6394 deg
RA of node: 142
6692 deg
Eccentricity:
0006223
Arg of perigee: 250
9823 deg
Mean anomaly: 109
0666 deg
Mean motion: 15
73910807 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1099
Checksum: 298
Coasting Arc #3 (Orbit 1113)
---------------------------------------
Vector Time (GMT): 2009/201/02:32:24
833
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1154566
80 A = 6721431
17 meter
Y = 4323810
02 meter E =
0008337
Z = -5022096
34 I = 51
84932
XDOT = -6352
107895 Wp = 125
01192
YDOT = 3905
264440 meter/sec RA = 136
87388 deg
ZDOT = 1899
461028 TA = 163
29669
MA = 163
26921
Ha = 188
432 n
mi
Hp = 186
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3787948
81 X = 1130527
56
Y = 14185728
41 feet Y = 4336587
61 meter
Z = -16476694
02 Z = -5016545
07
XDOT = -20840
248999 XDOT = -6404
532257
YDOT = 12812
547374 feet/sec YDOT = 3833
937968 meter/sec
ZDOT = 6231
827520 ZDOT = 1868
476243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2386433
26 X = -727384
86
Y = 14512566
31 feet Y = 4423430
21 meter
Z = -16454642
13 Z = -5015374
92
XDOT = -23259
275990 XDOT = -7089
427322
YDOT = 3112
434792 feet/sec YDOT = 948
670125 meter/sec
ZDOT = 6110
283034 ZDOT = 1862
414269
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 09201
11855277
00010596 00000-0 82463-4 0 9020
2 25544 51
6390 137
7794 0006192 255
4814 104
5662 15
73935993 11146
Satellite: ISS
Catalog Number: 25544
Epoch time: 09201
11855277 = yrday
fracday
Element set: 902
Inclination: 51
6390 deg
RA of node: 137
7794 deg
Eccentricity:
0006192
Arg of perigee: 255
4814 deg
Mean anomaly: 104
5662 deg
Mean motion: 15
73935993 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1114
Checksum: 316
Coasting Arc #4 (Orbit 1129)
---------------------------------------
Vector Time (GMT): 2009/202/02:32:24
833
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5226227
50 A = 6731213
43 meter
Y = -3895325
04 meter E =
0007578
Z = -1659621
69 I = 51
90293
XDOT = 1755
964009 Wp = 189
68267
YDOT = 4806
387903 meter/sec RA = 131
78649 deg
ZDOT = -5755
067181 TA = 8
58968
MA = 8
57672
Ha = 188
351 n
mi
Hp = 186
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17146415
69 X = 5277459
26
Y = -12779937
80 feet Y = -3836595
56 meter
Z = -5444953
04 Z = -1634109
39
XDOT = 5761
036775 XDOT = 1730
044215
YDOT = 15768
989184 feet/sec YDOT = 4825
880228 meter/sec
ZDOT = -18881
454007 ZDOT = -5746
598957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20862939
01 X = 6359023
81
Y = -4810794
70 feet Y = -1466330
23 meter
Z = -5344897
09 Z = -1629124
63
XDOT = -1302
736709 XDOT = -397
074149
YDOT = 15277
758168 feet/sec YDOT = 4656
660689 meter/sec
ZDOT = -18847
909259 ZDOT = -5744
842742
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 09202
13442946
00010596 00000-0 82463-4 0 9039
2 25544 51
6389 132
5631 0006173 259
1103 100
9365 15
73932533 11303
Satellite: ISS
Catalog Number: 25544
Epoch time: 09202
13442946 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 132
5631 deg
Eccentricity:
0006173
Arg of perigee: 259
1103 deg
Mean anomaly: 100
9365 deg
Mean motion: 15
73932533 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1130
Checksum: 282
Coasting Arc #5 (Orbit 1145)
---------------------------------------
Vector Time (GMT): 2009/203/02:32:24
833
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1904527
09 A = 6721281
65 meter
Y = -4041782
71 meter E =
0003062
Z = 5023371
52 I = 51
89008
XDOT = 5557
499027 Wp = 326
03276
YDOT = -4979
021600 meter/sec RA = 126
63893 deg
ZDOT = -1897
133636 TA = 142
22836
MA = 142
20686
Ha = 188
016 n
mi
Hp = 186
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6248448
45 X = -1883591
70
Y = -13260441
97 feet Y = -4062963
96 meter
Z = 16480877
68 Z = 5014169
77
XDOT = 18233
264524 XDOT = 5621
977969
YDOT = -16335
372705 feet/sec YDOT = -4916
513583 meter/sec
ZDOT = -6224
191719 ZDOT = -1869
980071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -741189
23 X = -225914
48
Y = -14680982
70 feet Y = -4474763
53 meter
Z = 16444486
74 Z = 5012279
56
XDOT = 22084
354296 XDOT = 6731
311189
YDOT = -7974
680022 feet/sec YDOT = -2430
682471 meter/sec
ZDOT = -6117
731100 ZDOT = -1864
684439
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 09203
15029412
00010596 00000-0 82463-4 0 9042
2 25544 51
6399 127
3464 0006343 264
2108 95
8332 15
73988190 11464
Satellite: ISS
Catalog Number: 25544
Epoch time: 09203
15029412 = yrday
fracday
Element set: 904
Inclination: 51
6399 deg
RA of node: 127
3464 deg
Eccentricity:
0006343
Arg of perigee: 264
2108 deg
Mean anomaly: 95
8332 deg
Mean motion: 15
73988190 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1146
Checksum: 306
Coasting Arc #6 (Orbit 1161)
---------------------------------------
Vector Time (GMT): 2009/204/02:32:24
833
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4450083
79 A = 6731168
46 meter
Y = 4761991
72 meter E =
0008993
Z = 1660524
37 I = 51
93921
XDOT = -2575
939265 Wp = 46
96254
YDOT = -4419
422684 meter/sec RA = 121
55386 deg
ZDOT = 5757
075912 TA = 331
31160
MA = 331
36104
Ha = 188
007 n
mi
Hp = 186
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14600012
43 X = -4511068
78
Y = 15623332
42 feet Y = 4711887
10 meter
Z = 5447914
60 Z = 1638758
83
XDOT = -8451
244309 XDOT = -2554
295216
YDOT = -14499
418253 feet/sec YDOT = -4448
108008 meter/sec
ZDOT = 18888
044332 ZDOT = 5744
614357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19370100
03 X = -5904006
49
Y = 9108800
88 feet Y = 2776362
51 meter
Z = 5362613
49 Z = 1634524
59
XDOT = -1931
220689 XDOT = -588
636066
YDOT = -15224
146341 feet/sec YDOT = -4640
319805 meter/sec
ZDOT = 18838
813010 ZDOT = 5742
070205
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 09204
16615304
00010596 00000-0 82463-4 0 9056
2 25544 51
6394 122
1298 0006075 269
0924 90
9543 15
73946904 11623
Satellite: ISS
Catalog Number: 25544
Epoch time: 09204
16615304 = yrday
fracday
Element set: 905
Inclination: 51
6394 deg
RA of node: 122
1298 deg
Eccentricity:
0006075
Arg of perigee: 269
0924 deg
Mean anomaly: 90
9543 deg
Mean motion: 15
73946904 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1162
Checksum: 309
Coasting Arc #7 (Orbit 1176)
---------------------------------------
Vector Time (GMT): 2009/205/02:32:24
833
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2580466
44 A = 6721359
16 meter
Y = 3653327
21 meter E =
0007255
Z = -5023582
01 I = 51
92073
XDOT = -4589
789908 Wp = 113
54871
YDOT = 5873
071690 meter/sec RA = 116
40822 deg
ZDOT = 1912
796228 TA = 174
86272
MA = 174
85528
Ha = 187
959 n
mi
Hp = 186
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8466097
23 X = 2563825
62
Y = 11985981
66 feet Y = 3682090
89 meter
Z = -16481568
28 Z = -5011086
49
XDOT = -15058
365839 XDOT = -4664
414282
YDOT = 19268
607906 feet/sec YDOT = 5821
328555 meter/sec
ZDOT = 6275
578176 ZDOT = 1890
318792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3770742
24 X = 1149322
24
Y = 14238805
73 feet Y = 4339987
99 meter
Z = -16432241
66 Z = -5008547
26
XDOT = -19894
416631 XDOT = -6063
818189
YDOT = 12411
714633 feet/sec YDOT = 3783
090620 meter/sec
ZDOT = 6187
534049 ZDOT = 1885
960378
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 09205
11850918
00010596 00000-0 82463-4 0 9065
2 25544 51
6391 117
2392 0006145 273
1837 86
8623 15
73970681 11775
Satellite: ISS
Catalog Number: 25544
Epoch time: 09205
11850918 = yrday
fracday
Element set: 906
Inclination: 51
6391 deg
RA of node: 117
2392 deg
Eccentricity:
0006145
Arg of perigee: 273
1837 deg
Mean anomaly: 86
8623 deg
Mean motion: 15
73970681 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1177
Checksum: 320
Coasting Arc #8 (Orbit 1192)
---------------------------------------
Vector Time (GMT): 2009/206/02:32:24
833
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3550054
28 A = 6730934
88 meter
Y = -5458656
60 meter E =
0005545
Z = -1689877
36 I = 51
96593
XDOT = 3295
619546 Wp = 192
86468
YDOT = 3922
242506 meter/sec RA = 111
32512 deg
ZDOT = -5747
999666 TA = 5
73328
MA = 5
72693
Ha = 188
033 n
mi
Hp = 185
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11647159
70 X = 3619039
03
Y = -17908978
35 feet Y = -5418571
99 meter
Z = -5544217
05 Z = -1672464
32
XDOT = 10812
400086 XDOT = 3279
437651
YDOT = 12868
249693 feet/sec YDOT = 3959
005970 meter/sec
ZDOT = -18858
266622 ZDOT = -5732
028878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17037524
17 X = 5193037
37
Y = -12917498
22 feet Y = -3937253
46 meter
Z = -5476055
82 Z = -1669101
81
XDOT = 4997
107625 XDOT = 1523
118404
YDOT = 14556
330107 feet/sec YDOT = 4436
769416 meter/sec
ZDOT = -18795
260371 ZDOT = -5728
795361
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 09206
13434704
00010596 00000-0 82463-4 0 9070
2 25544 51
6396 112
0223 0006029 277
5346 82
5132 15
74009976 11937
Satellite: ISS
Catalog Number: 25544
Epoch time: 09206
13434704 = yrday
fracday
Element set: 907
Inclination: 51
6396 deg
RA of node: 112
0223 deg
Eccentricity:
0006029
Arg of perigee: 277
5346 deg
Mean anomaly: 82
5132 deg
Mean motion: 15
74009976 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1193
Checksum: 297
Coasting Arc #9 (Orbit 1208)
---------------------------------------
Vector Time (GMT): 2009/207/02:32:24
833
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3162818
84 A = 6721229
24 meter
Y = -3176548
96 meter E =
0004638
Z = 5010457
27 I = 51
94236
XDOT = 3500
044178 Wp = 344
45389
YDOT = -6573
100155 meter/sec RA = 106
18042 deg
ZDOT = -1953
903484 TA = 124
37109
MA = 124
32721
Ha = 188
189 n
mi
Hp = 185
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10376702
22 X = -3151402
62
Y = -10421748
57 feet Y = -3211853
94 meter
Z = 16438508
09 Z = 4995120
03
XDOT = 11483
084572 XDOT = 3582
777158
YDOT = -21565
289222 feet/sec YDOT = -6533
497905 meter/sec
ZDOT = -6410
444501 ZDOT = -1936
699946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6569826
21 X = -2002483
03
Y = -13232940
87 feet Y = -4033400
38 meter
Z = 16378034
06 Z = 4992024
78
XDOT = 16871
666095 XDOT = 5142
483826
YDOT = -16243
233905 feet/sec YDOT = -4950
937694 meter/sec
ZDOT = -6343
161218 ZDOT = -1933
395539
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 09207
15017395
00010596 00000-0 82463-4 0 9087
2 25544 51
6387 106
8054 0006121 281
5281 78
5195 15
74037777 12098
Satellite: ISS
Catalog Number: 25544
Epoch time: 09207
15017395 = yrday
fracday
Element set: 908
Inclination: 51
6387 deg
RA of node: 106
8054 deg
Eccentricity:
0006121
Arg of perigee: 281
5281 deg
Mean anomaly: 78
5195 deg
Mean motion: 15
74037777 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1209
Checksum: 315
Coasting Arc #10 (Orbit 1224)
---------------------------------------
Vector Time (GMT): 2009/208/02:32:24
833
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2548808
36 A = 6730919
72 meter
Y = 5978058
50 meter E =
0010578
Z = 1727280
83 I = 51
98149
XDOT = -3916
522574 Wp = 42
06649
YDOT = -3330
771931 meter/sec RA = 101
09839 deg
ZDOT = 5735
989333 TA = 336
96293
MA = 337
01033
Ha = 188
568 n
mi
Hp = 185
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8362232
15 X = -2623857
34
Y = 19613052
83 feet Y = 5949136
50 meter
Z = 5666931
84 Z = 1714716
93
XDOT = -12849
483510 XDOT = -3906
850373
YDOT = -10927
729431 feet/sec YDOT = -3374
515080 meter/sec
ZDOT = 18818
862640 ZDOT = 5716
986311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13974813
39 X = -4259523
12
Y = 16120088
08 feet Y = 4913402
85 meter
Z = 5617849
75 Z = 1712320
60
XDOT = -7834
955212 XDOT = -2388
094349
YDOT = -13338
847534 feet/sec YDOT = -4065
680728 meter/sec
ZDOT = 18743
969008 ZDOT = 5713
161754
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 09208
16599452
00010596 00000-0 82463-4 0 9099
2 25544 51
6385 101
5876 0005948 287
8201 72
2313 15
73994723 12250
Satellite: ISS
Catalog Number: 25544
Epoch time: 09208
16599452 = yrday
fracday
Element set: 909
Inclination: 51
6385 deg
RA of node: 101
5876 deg
Eccentricity:
0005948
Arg of perigee: 287
8201 deg
Mean anomaly: 72
2313 deg
Mean motion: 15
73994723 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1225
Checksum: 329
Coasting Arc #11 (Orbit 1239)
---------------------------------------
Vector Time (GMT): 2009/209/02:32:24
833
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3658427
47 A = 6721339
61 meter
Y = 2622872
25 meter E =
0006913
Z = -4997452
29 I = 51
95515
XDOT = -2316
988090 Wp = 100
15502
YDOT = 7058
108028 meter/sec RA = 95
95344 deg
ZDOT = 2009
365483 TA = 189
20147
MA = 189
21415
Ha = 188
656 n
mi
Hp = 186
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12002714
79 X = 3653102
73
Y = 8605223
91 feet Y = 2663753
54 meter
Z = -16395840
85 Z = -4979692
49
XDOT = -7601
666961 XDOT = -2405
501930
YDOT = 23156
522403 feet/sec YDOT = 7031
703047 meter/sec
ZDOT = 6592
406440 ZDOT = 1997
895171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9101721
47 X = 2774204
70
Y = 11728730
76 feet Y = 3574917
14 meter
Z = -16325874
52 Z = -4976126
55
XDOT = -13139
196099 XDOT = -4004
826971
YDOT = 19305
081759 feet/sec YDOT = 5884
188920 meter/sec
ZDOT = 6547
669463 ZDOT = 1995
729652
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 09209
11831366
00010596 00000-0 82463-4 0 9100
2 25544 51
6396 96
6965 0006111 290
1992 69
8513 15
74026257 12402
Satellite: ISS
Catalog Number: 25544
Epoch time: 09209
11831366 = yrday
fracday
Element set: 910
Inclination: 51
6396 deg
RA of node: 96
6965 deg
Eccentricity:
0006111
Arg of perigee: 290
1992 deg
Mean anomaly: 69
8513 deg
Mean motion: 15
74026257 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1240
Checksum: 312
Coasting Arc #12 (Orbit 1255)
---------------------------------------
Vector Time (GMT): 2009/210/02:32:24
833
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1498213
17 A = 6730632
72 meter
Y = -6309360
21 meter E =
0003529
Z = -1793565
96 I = 51
98820
XDOT = 4421
027888 Wp = 195
23532
YDOT = 2672
115019 meter/sec RA = 90
87324 deg
ZDOT = -5707
702275 TA = 4
54039
MA = 4
53719
Ha = 188
705 n
mi
Hp = 185
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4915397
54 X = 1577366
94
Y = -20700000
69 feet Y = -6292163
57 meter
Z = -5884402
75 Z = -1786095
99
XDOT = 14504
684672 XDOT = 4418
546110
YDOT = 8766
781558 feet/sec YDOT = 2721
540196 meter/sec
ZDOT = -18726
057332 ZDOT = -5686
230804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10391947
69 X = 3167465
66
Y = -18574167
98 feet Y = -5661406
40 meter
Z = -5855344
92 Z = -1784709
13
XDOT = 10324
456102 XDOT = 3146
894220
YDOT = 11652
097725 feet/sec YDOT = 3551
559387 meter/sec
ZDOT = -18641
494998 ZDOT = -5681
927675
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 09210
13411296
00010596 00000-0 82463-4 0 9111
2 25544 51
6392 91
4791 0006033 294
0816 65
9716 15
74054900 12564
Satellite: ISS
Catalog Number: 25544
Epoch time: 09210
13411296 = yrday
fracday
Element set: 911
Inclination: 51
6392 deg
RA of node: 91
4791 deg
Eccentricity:
0006033
Arg of perigee: 294
0816 deg
Mean anomaly: 65
9716 deg
Mean motion: 15
74054900 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1256
Checksum: 295
Coasting Arc #13 (Orbit 1271)
---------------------------------------
Vector Time (GMT): 2009/211/02:32:24
833
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4049832
23 A = 6721297
47 meter
Y = -2029392
51 meter E =
0006312
Z = 4967650
28 I = 51
95547
XDOT = 1095
746092 Wp = 358
29095
YDOT = -7327
393397 meter/sec RA = 85
72717 deg
ZDOT = -2094
000084 TA = 111
94619
MA = 111
87909
Ha = 188
946 n
mi
Hp = 185
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13286851
15 X = -4050970
04
Y = -6658111
90 feet Y = -2074687
00 meter
Z = 16298065
22 Z = 4947973
31
XDOT = 3594
967494 XDOT = 1187
773038
YDOT = -24040
004583 feet/sec YDOT = -7314
625346 meter/sec
ZDOT = -6870
079016 ZDOT = -2088
454238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11237946
71 X = -3425326
16
Y = -9853871
95 feet Y = -3003460
17 meter
Z = 16220590
58 Z = 4944036
01
XDOT = 8934
078618 XDOT = 2723
107163
YDOT = -21495
680895 feet/sec YDOT = -6551
883537 meter/sec
ZDOT = -6848
624924 ZDOT = -2087
460877
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 09211
14990240
00010596 00000-0 82463-4 0 9125
2 25544 51
6385 86
2617 0006055 298
9181 61
1374 15
74086597 12720
Satellite: ISS
Catalog Number: 25544
Epoch time: 09211
14990240 = yrday
fracday
Element set: 912
Inclination: 51
6385 deg
RA of node: 86
2617 deg
Eccentricity:
0006055
Arg of perigee: 298
9181 deg
Mean anomaly: 61
1374 deg
Mean motion: 15
74086597 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1272
Checksum: 315
Coasting Arc #14 (Orbit 1287)
---------------------------------------
Vector Time (GMT): 2009/212/02:32:24
833
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -417227
00 A = 6730409
30 meter
Y = 6445201
49 meter E =
0011871
Z = 1866256
98 I = 51
98305
XDOT = -4822
594837 Wp = 40
98418
YDOT = -1960
042972 meter/sec RA = 80
64849 deg
ZDOT = 5679
493252 TA = 339
64732
MA = 339
69459
Ha = 189
116 n
mi
Hp = 185
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1368854
98 X = -498333
20
Y = 21145674
18 feet Y = 6440082
10 meter
Z = 6122890
35 Z = 1864033
88
XDOT = -15822
161540 XDOT = -4827
908618
YDOT = -6430
587177 feet/sec YDOT = -2014
002451 meter/sec
ZDOT = 18633
508044 ZDOT = 5656
052114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6410614
06 X = -1953955
17
Y = 20199520
22 feet Y = 6156813
76 meter
Z = 6114449
84 Z = 1863684
31
XDOT = -12462
331078 XDOT = -3798
518512
YDOT = -9578
968013 feet/sec YDOT = -2919
669450 meter/sec
ZDOT = 18541
232049 ZDOT = 5651
367529
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 09212
16568294
00010596 00000-0 82463-4 0 9139
2 25544 51
6387 81
0448 0006146 303
0993 56
9580 15
74091376 12886
Satellite: ISS
Catalog Number: 25544
Epoch time: 09212
16568294 = yrday
fracday
Element set: 913
Inclination: 51
6387 deg
RA of node: 81
0448 deg
Eccentricity:
0006146
Arg of perigee: 303
0993 deg
Mean anomaly: 56
9580 deg
Mean motion: 15
74091376 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1288
Checksum: 325
Coasting Arc #15 (Orbit 1302)
---------------------------------------
Vector Time (GMT): 2009/213/02:32:24
833
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4350915
76 A = 6721447
60 meter
Y = 1381332
47 meter E =
0007057
Z = -4939415
37 I = 51
94671
XDOT = 138
609975 Wp = 87
70703
YDOT = 7376
946043 meter/sec RA = 75
50065 deg
ZDOT = 2188
039648 TA = 203
44235
MA = 203
47453
Ha = 189
355 n
mi
Hp = 185
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14274658
00 X = 4359140
62
Y = 4531930
68 feet Y = 1430033
58 meter
Z = -16205430
99 Z = -4918258
69
XDOT = 454
757135 XDOT = 45
480415
YDOT = 24202
578880 feet/sec YDOT = 7377
975066 meter/sec
ZDOT = 7178
607770 ZDOT = 2188
487742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13004742
80 X = 3963845
60
Y = 7607417
09 feet Y = 2318740
73 meter
Z = -16122162
39 Z = -4914035
10
XDOT = -4413
756578 XDOT = -1345
313005
YDOT = 22742
511071 feet/sec YDOT = 6931
917374 meter/sec
ZDOT = 7180
706656 ZDOT = 2188
679389
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 09213
11796830
00010596 00000-0 82463-4 0 9145
2 25544 51
6388 76
1537 0006254 306
7808 53
2781 15
74081506 13031
Satellite: ISS
Catalog Number: 25544
Epoch time: 09213
11796830 = yrday
fracday
Element set: 914
Inclination: 51
6388 deg
RA of node: 76
1537 deg
Eccentricity:
0006254
Arg of perigee: 306
7808 deg
Mean anomaly: 53
2781 deg
Mean motion: 15
74081506 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1303
Checksum: 306
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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