Date:
September 8th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6189 25 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 ET - UTC (sec) : 65 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 2375)
---------------------------------------
Vector Time (GMT): 2007/250/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2369407
41 A = 6712640
28 meter
Y = -3421008
91 meter E =
0014721
Z = -5277448
94 I = 51
81442
XDOT = 6121
766512 Wp = 52
95384
YDOT = 4657
456080 meter/sec RA = 38
80170 deg
ZDOT = -262
445689 TA = 214
51190
MA = 214
60756
Ha = 187
293 n
mi
Hp = 180
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7773646
36 X = 2433122
09
Y = -11223782
51 feet Y = -3394156
56 meter
Z = -17314465
04 Z = -5265783
79
XDOT = 20084
535800 XDOT = 6070
506059
YDOT = 15280
367715 feet/sec YDOT = 4725
626519 meter/sec
ZDOT = -861
042287 ZDOT = -232
831023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12386769
09 X = -3775487
22
Y = 5872699
31 feet Y = 1789998
75 meter
Z = -17270579
76 Z = -5264072
71
XDOT = -9494
280567 XDOT = -2893
856717
YDOT = -22304
575341 feet/sec YDOT = -6798
434564 meter/sec
ZDOT = -748
072421 ZDOT = -228
012474
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 07250
47456636
00020000 00000-0 20000-3 0 9004
2 25544 51
6337 39
2564 0008936 338
8077 21
2711 15
76628196 23761
Satellite: ISS
Catalog Number: 25544
Epoch time: 07250
47456636 = yrday
fracday
Element set: 900
Inclination: 51
6337 deg
RA of node: 39
2564 deg
Eccentricity:
0008936
Arg of perigee: 338
8077 deg
Mean anomaly: 21
2711 deg
Mean motion: 15
76628196 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2376
Checksum: 307
Coasting Arc #2 (Orbit 2391)
---------------------------------------
Vector Time (GMT): 2007/251/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5258077
91 A = 6724299
51 meter
Y = -4138238
14 meter E =
0004094
Z = -673992
08 I = 51
83091
XDOT = 3429
954284 Wp = 80
89176
YDOT = -3385
292980 meter/sec RA = 33
66236 deg
ZDOT = -6003
260792 TA = 106
43202
MA = 106
38702
Ha = 187
404 n
mi
Hp = 179
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17250911
78 X = -5208138
64
Y = -13576896
80 feet Y = -4196757
73 meter
Z = -2211260
12 Z = -699414
08
XDOT = 11253
130853 XDOT = 3496
716545
YDOT = -11106
604266 feet/sec YDOT = -3346
564107 meter/sec
ZDOT = -19695
737508 ZDOT = -5986
436100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8633088
98 X = 2631365
52
Y = 20173187
22 feet Y = 6148787
46 meter
Z = -2308256
27 Z = -703556
51
XDOT = -13823
166702 XDOT = -4213
301211
YDOT = 3680
092222 feet/sec YDOT = 1121
692109 meter/sec
ZDOT = -19632
261112 ZDOT = -5983
913187
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 07251
48869810
00020000 00000-0 20000-3 0 9019
2 25544 51
6336 34
0260 0009243 342
6505 17
4343 15
76694443 23921
Satellite: ISS
Catalog Number: 25544
Epoch time: 07251
48869810 = yrday
fracday
Element set: 901
Inclination: 51
6336 deg
RA of node: 34
0260 deg
Eccentricity:
0009243
Arg of perigee: 342
6505 deg
Mean anomaly: 17
4343 deg
Mean motion: 15
76694443 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2392
Checksum: 282
Coasting Arc #3 (Orbit 2407)
---------------------------------------
Vector Time (GMT): 2007/252/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3641256
40 A = 6713678
69 meter
Y = 2539026
79 meter E =
0012137
Z = 5037788
70 I = 51
76982
XDOT = -5798
475264 Wp = 11
26459
YDOT = -4748
269575 meter/sec RA = 28
49567 deg
ZDOT = -1785
564381 TA = 95
96438
MA = 95
82604
Ha = 187
628 n
mi
Hp = 179
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11946379
28 X = -3693849
90
Y = 8330140
40 feet Y = 2498014
35 meter
Z = 16528178
14 Z = 5019971
86
XDOT = -19023
868975 XDOT = -5736
274616
YDOT = -15578
312254 feet/sec YDOT = -4812
763693 meter/sec
ZDOT = -5858
150856 ZDOT = -1813
581722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14529027
83 X = 4428447
68
Y = -1798906
30 feet Y = -548306
64 meter
Z = 16460837
64 Z = 5017263
31
XDOT = 9472
430410 XDOT = 2887
196789
YDOT = 21548
001745 feet/sec YDOT = 6567
830932 meter/sec
ZDOT = -5965
073353 ZDOT = -1818
154358
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 07252
50281208
00020000 00000-0 20000-3 0 9023
2 25544 51
6338 28
7963 0008978 346
9885 13
1046 15
76644247 24083
Satellite: ISS
Catalog Number: 25544
Epoch time: 07252
50281208 = yrday
fracday
Element set: 902
Inclination: 51
6338 deg
RA of node: 28
7963 deg
Eccentricity:
0008978
Arg of perigee: 346
9885 deg
Mean anomaly: 13
1046 deg
Mean motion: 15
76644247 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2408
Checksum: 308
Coasting Arc #4 (Orbit 2423)
---------------------------------------
Vector Time (GMT): 2007/253/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4738232
39 A = 6721833
60 meter
Y = 4104332
80 meter E =
0017266
Z = 2395128
69 I = 51
77374
XDOT = -4906
733576 Wp = 42
84757
YDOT = 2509
356500 meter/sec RA = 23
38498 deg
ZDOT = 5396
652425 TA = 344
17460
MA = 344
22849
Ha = 187
470 n
mi
Hp = 179
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15545381
86 X = 4680349
99
Y = 13465658
79 feet Y = 4156994
90 meter
Z = 7858033
76 Z = 2418005
95
XDOT = -16098
207270 XDOT = -4960
644602
YDOT = 8232
796917 feet/sec YDOT = 2454
185528 meter/sec
ZDOT = 17705
552574 ZDOT = 5372
684650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7818911
32 X = -2383204
17
Y = -18985977
28 feet Y = -5786925
87 meter
Z = 7945366
66 Z = 2421747
76
XDOT = 16784
864323 XDOT = 5116
026646
YDOT = 472
931942 feet/sec YDOT = 144
149656 meter/sec
ZDOT = 17614
860535 ZDOT = 5369
009491
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 07253
51689982
00020000 00000-0 20000-3 0 9037
2 25544 51
6352 23
5669 0009000 350
0226 10
0758 15
76741964 24245
Satellite: ISS
Catalog Number: 25544
Epoch time: 07253
51689982 = yrday
fracday
Element set: 903
Inclination: 51
6352 deg
RA of node: 23
5669 deg
Eccentricity:
0009000
Arg of perigee: 350
0226 deg
Mean anomaly: 10
0758 deg
Mean motion: 15
76741964 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2424
Checksum: 284
Coasting Arc #5 (Orbit 2438)
---------------------------------------
Vector Time (GMT): 2007/254/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4878960
89 A = 6716738
60 meter
Y = -1893958
07 meter E =
0009164
Z = -4211463
02 I = 51
73008
XDOT = 4941
553098 Wp = 46
23424
YDOT = 4650
282585 meter/sec RA = 18
19076 deg
ZDOT = 3644
580150 TA = 260
77686
MA = 260
88052
Ha = 187
760 n
mi
Hp = 179
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16007089
54 X = 4920235
22
Y = -6213773
20 feet Y = -1839168
30 meter
Z = -13817135
90 Z = -4187660
77
XDOT = 16212
444547 XDOT = 4871
481059
YDOT = 15256
832627 feet/sec YDOT = 4705
150296 meter/sec
ZDOT = 11957
283958 ZDOT = 3668
415543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17189158
91 X = -5239255
63
Y = -1361370
60 feet Y = -414945
76 meter
Z = -13727003
43 Z = -4183990
65
XDOT = -8048
803877 XDOT = -2453
275422
YDOT = -19488
628820 feet/sec YDOT = -5940
134064 meter/sec
ZDOT = 12048
316266 ZDOT = 3672
326798
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 07254
46758993
00020000 00000-0 20000-3 0 9042
2 25544 51
6359 18
6651 0009145 353
9775 6
1278 15
76743003 24394
Satellite: ISS
Catalog Number: 25544
Epoch time: 07254
46758993 = yrday
fracday
Element set: 904
Inclination: 51
6359 deg
RA of node: 18
6651 deg
Eccentricity:
0009145
Arg of perigee: 353
9775 deg
Mean anomaly: 6
1278 deg
Mean motion: 15
76743003 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2439
Checksum: 318
Coasting Arc #6 (Orbit 2454)
---------------------------------------
Vector Time (GMT): 2007/255/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3747267
79 A = 6717640
78 meter
Y = -4016923
66 meter E =
0012647
Z = -3880308
22 I = 51
70619
XDOT = 6242
680877 Wp = 28
03090
YDOT = -1865
451779 meter/sec RA = 13
09072 deg
ZDOT = -4091
937871 TA = 199
28506
MA = 199
33296
Ha = 187
760 n
mi
Hp = 178
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12294185
65 X = -3683221
61
Y = -13178883
40 feet Y = -4058469
92 meter
Z = -12730670
03 Z = -3898356
57
XDOT = 20481
236473 XDOT = 6282
954558
YDOT = -6120
248620 feet/sec YDOT = -1795
417727 meter/sec
ZDOT = -13424
993014 ZDOT = -4061
512971
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5607639
21 X = 1709208
43
Y = 17076976
31 feet Y = 5205062
38 meter
Z = -12799655
86 Z = -3901335
11
XDOT = -19989
605592 XDOT = -6092
831784
YDOT = -3425
564726 feet/sec YDOT = -1044
112129 meter/sec
ZDOT = -13309
721869 ZDOT = -4056
803226
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 07255
48163696
00020000 00000-0 20000-3 0 9056
2 25544 51
6363 13
4354 0009206 357
7682 2
3440 15
76784703 24558
Satellite: ISS
Catalog Number: 25544
Epoch time: 07255
48163696 = yrday
fracday
Element set: 905
Inclination: 51
6363 deg
RA of node: 13
4354 deg
Eccentricity:
0009206
Arg of perigee: 357
7682 deg
Mean anomaly: 2
3440 deg
Mean motion: 15
76784703 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2455
Checksum: 296
Coasting Arc #7 (Orbit 2470)
---------------------------------------
Vector Time (GMT): 2007/256/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5938584
00 A = 6720840
82 meter
Y = 1416665
12 meter E =
0015245
Z = 2807697
48 I = 51
68873
XDOT = -3518
202545 Wp = 63
07930
YDOT = -4563
815922 meter/sec RA = 7
88828 deg
ZDOT = -5110
657216 TA = 84
74698
MA = 84
57304
Ha = 187
874 n
mi
Hp = 178
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19483543
30 X = -5967623
34
Y = 4647851
45 feet Y = 1350094
36 meter
Z = 9211605
90 Z = 2778777
07
XDOT = -11542
659269 XDOT = -3442
081030
YDOT = -14973
149349 feet/sec YDOT = -4602
733213 meter/sec
ZDOT = -16767
248085 ZDOT = -5127
563481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19756932
04 X = 6021912
89
Y = 3589142
98 feet Y = 1093970
78 meter
Z = 9101997
31 Z = 2774288
78
XDOT = 4732
663888 XDOT = 1442
515953
YDOT = 16869
535173 feet/sec YDOT = 5141
834321 meter/sec
ZDOT = -16831
959060 ZDOT = -5130
381122
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 07256
49566207
00020000 00000-0 20000-3 0 9064
2 25544 51
6366 8
2057 0009208 1
8228 358
2969 15
76810446 24719
Satellite: ISS
Catalog Number: 25544
Epoch time: 07256
49566207 = yrday
fracday
Element set: 906
Inclination: 51
6366 deg
RA of node: 8
2057 deg
Eccentricity:
0009208
Arg of perigee: 1
8228 deg
Mean anomaly: 358
2969 deg
Mean motion: 15
76810446 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2471
Checksum: 305
Coasting Arc #8 (Orbit 2486)
---------------------------------------
Vector Time (GMT): 2007/257/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2303101
83 A = 6713470
66 meter
Y = 3981294
06 meter E =
0008483
Z = 4883099
79 I = 51
63710
XDOT = -7236
001407 Wp = 46
51997
YDOT = 1431
573969 meter/sec RA = 2
77435 deg
ZDOT = 2248
964163 TA = 21
66250
MA = 21
62664
Ha = 187
816 n
mi
Hp = 178
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7556108
36 X = 2234689
81
Y = 13061988
37 feet Y = 4006666
45 meter
Z = 16020668
61 Z = 4894121
92
XDOT = -23740
162095 XDOT = -7262
396838
YDOT = 4696
764989 feet/sec YDOT = 1350
509474 meter/sec
ZDOT = 7378
491348 ZDOT = 2213
747167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1848589
22 X = -563449
99
Y = -14931033
87 feet Y = -4550979
12 meter
Z = 16062972
39 Z = 4895993
98
XDOT = 22663
340357 XDOT = 6907
786141
YDOT = 4976
656548 feet/sec YDOT = 1516
884916 meter/sec
ZDOT = 7244
988572 ZDOT = 2208
272517
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 07257
50966273
00020000 00000-0 20000-3 0 9075
2 25544 51
6376 2
9761 0009318 5
0531 355
0727 15
76892400 24872
Satellite: ISS
Catalog Number: 25544
Epoch time: 07257
50966273 = yrday
fracday
Element set: 907
Inclination: 51
6376 deg
RA of node: 2
9761 deg
Eccentricity:
0009318
Arg of perigee: 5
0531 deg
Mean anomaly: 355
0727 deg
Mean motion: 15
76892400 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2487
Checksum: 299
Coasting Arc #9 (Orbit 2501)
---------------------------------------
Vector Time (GMT): 2007/258/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6540026
86 A = 6723562
18 meter
Y = -1100278
48 meter E =
0018752
Z = -1041521
65 I = 51
64217
XDOT = 1713
597617 Wp = 23
53975
YDOT = 4623
950463 meter/sec RA = 357
58961 deg
ZDOT = 5928
698195 TA = 325
04894
MA = 325
17189
Ha = 188
094 n
mi
Hp = 177
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21456781
05 X = 6556903
85
Y = -3609837
52 feet Y = -1027049
89 meter
Z = -3417065
77 Z = -1009708
79
XDOT = 5622
039425 XDOT = 1632
963686
YDOT = 15170
441152 feet/sec YDOT = 4642
662337 meter/sec
ZDOT = 19451
109563 ZDOT = 5936
826845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21287785
50 X = -6488517
02
Y = -4589590
28 feet Y = -1398907
12 meter
Z = -3296447
78 Z = -1004757
28
XDOT = 154
827306 XDOT = 47
191363
YDOT = -14581
106159 feet/sec YDOT = -4444
321157 meter/sec
ZDOT = 19482
502478 ZDOT = 5938
266755
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 07258
46027038
00020000 00000-0 20000-3 0 9089
2 25544 51
6379 358
0739 0009524 9
2336 350
9002 15
76876942 25024
Satellite: ISS
Catalog Number: 25544
Epoch time: 07258
46027038 = yrday
fracday
Element set: 908
Inclination: 51
6379 deg
RA of node: 358
0739 deg
Eccentricity:
0009524
Arg of perigee: 9
2336 deg
Mean anomaly: 350
9002 deg
Mean motion: 15
76876942 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2502
Checksum: 305
Coasting Arc #10 (Orbit 2517)
---------------------------------------
Vector Time (GMT): 2007/259/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -627524
82 A = 6711747
95 meter
Y = -4131631
69 meter E =
0019600
Z = -5266774
18 I = 51
57407
XDOT = 7619
053448 Wp = 61
01942
YDOT = -1062
932955 meter/sec RA = 352
44087 deg
ZDOT = -64
809349 TA = 208
31109
MA = 208
41775
Ha = 188
065 n
mi
Hp = 177
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2058808
48 X = -555692
31
Y = -13555222
09 feet Y = -4138247
58 meter
Z = -17279442
84 Z = -5269648
11
XDOT = 24996
894516 XDOT = 7630
687892
YDOT = -3487
312844 feet/sec YDOT = -977
667345 meter/sec
ZDOT = -212
629098 ZDOT = -27
767233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2961630
48 X = -902704
97
Y = 13372276
89 feet Y = 4075870
00 meter
Z = -17290831
06 Z = -5270245
31
XDOT = -23639
303118 XDOT = -7205
259590
YDOT = -5367
597415 feet/sec YDOT = -1636
043692 meter/sec
ZDOT = -72
160340 ZDOT = -21
994472
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 07259
47422839
00020000 00000-0 20000-3 0 9090
2 25544 51
6379 352
8447 0009560 12
9628 347
1780 15
76936730 25187
Satellite: ISS
Catalog Number: 25544
Epoch time: 07259
47422839 = yrday
fracday
Element set: 909
Inclination: 51
6379 deg
RA of node: 352
8447 deg
Eccentricity:
0009560
Arg of perigee: 12
9628 deg
Mean anomaly: 347
1780 deg
Mean motion: 15
76936730 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2518
Checksum: 329
Coasting Arc #11 (Orbit 2533)
---------------------------------------
Vector Time (GMT): 2007/260/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6618756
11 A = 6723315
66 meter
Y = 720587
70 meter E =
0009008
Z = -950301
54 I = 51
58476
XDOT = 312
431991 Wp = 80
77416
YDOT = -4893
886197 meter/sec RA = 347
28735 deg
ZDOT = -5933
196634 TA = 109
61541
MA = 109
51815
Ha = 188
129 n
mi
Hp = 177
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21715079
09 X = -6621705
45
Y = 2364132
87 feet Y = 646556
52 meter
Z = -3117787
22 Z = -982463
03
XDOT = 1025
039340 XDOT = 395
955686
YDOT = -16056
057077 feet/sec YDOT = -4889
925504 meter/sec
ZDOT = -19465
868222 ZDOT = -5931
475855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21220946
04 X = 6468144
35
Y = 5101931
86 feet Y = 1555068
83 meter
Z = -3239771
87 Z = -987482
47
XDOT = -6117
872462 XDOT = -1864
727526
YDOT = 13182
137369 feet/sec YDOT = 4017
915470 meter/sec
ZDOT = -19459
903318 ZDOT = -5931
378531
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 07260
48816373
00020000 00000-0 20000-3 0 9105
2 25544 51
6377 347
6142 0009560 17
0090 343
1393 15
76966798 25349
Satellite: ISS
Catalog Number: 25544
Epoch time: 07260
48816373 = yrday
fracday
Element set: 910
Inclination: 51
6377 deg
RA of node: 347
6142 deg
Eccentricity:
0009560
Arg of perigee: 17
0090 deg
Mean anomaly: 343
1393 deg
Mean motion: 15
76966798 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2534
Checksum: 306
Coasting Arc #12 (Orbit 2549)
---------------------------------------
Vector Time (GMT): 2007/261/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 520639
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1136847
46 A = 6713181
42 meter
Y = 4452182
77 meter E =
0015478
Z = 4890780
88 I = 51
52329
XDOT = -7368
897609 Wp = 34
89564
YDOT = 547
285187 meter/sec RA = 342
09542 deg
ZDOT = -2195
169484 TA = 76
52217
MA = 76
34973
Ha = 188
245 n
mi
Hp = 177
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3729814
50 X = -1210306
72
Y = 14606898
84 feet Y = 4439059
18 meter
Z = 16045869
03 Z = 4885079
57
XDOT = -24176
173259 XDOT = -7363
805910
YDOT = 1795
555074 feet/sec YDOT = 464
910474 meter/sec
ZDOT = -7201
999621 ZDOT = -2230
955599
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8312716
88 X = 2533716
10
Y = -12603541
63 feet Y = -3841559
49 meter
Z = 16024743
36 Z = 4884341
77
XDOT = 22512
423871 XDOT = 6861
786796
YDOT = 5452
105380 feet/sec YDOT = 1661
801720 meter/sec
ZDOT = -7337
763596 ZDOT = -2236
550344
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 07261
50207567
00020000 00000-0 20000-3 0 9119
2 25544 51
6381 342
3838 0009751 20
7675 339
3884 15
77016723 25505
Satellite: ISS
Catalog Number: 25544
Epoch time: 07261
50207567 = yrday
fracday
Element set: 911
Inclination: 51
6381 deg
RA of node: 342
3838 deg
Eccentricity:
0009751
Arg of perigee: 20
7675 deg
Mean anomaly: 339
3884 deg
Mean motion: 15
77016723 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2550
Checksum: 296
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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