Date:
September 22nd 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) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 63 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 2064)
---------------------------------------
Vector Time (GMT): 2009/261/11:40:19
931
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 95424
56 A = 6719719
28 meter
Y = 4210774
16 meter E =
0023671
Z = -5256172
42 I = 51
57765
XDOT = -7649
315255 Wp = 91
86428
YDOT = -491
310323 meter/sec RA = 186
85055 deg
ZDOT = -535
291980 TA = 173
05062
MA = 173
01774
Ha = 193
079 n
mi
Hp = 180
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 313072
71 X = 73865
46
Y = 13814875
86 feet Y = 4211720
17 meter
Z = -17244660
17 Z = -5255761
65
XDOT = -25096
178659 XDOT = -7640
652465
YDOT = -1611
910509 feet/sec YDOT = -576
801089 meter/sec
ZDOT = -1756
207284 ZDOT = -572
431328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1550921
45 X = 472720
86
Y = -13733506
54 feet Y = -4185972
79 meter
Z = -17242753
69 Z = -5255591
32
XDOT = 23601
446398 XDOT = 7193
720862
YDOT = 5042
294774 feet/sec YDOT = 1536
891447 meter/sec
ZDOT = -1902
499153 ZDOT = -579
881742
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 09261
50322865
00020000 00000-0 20000-3 0 9008
2 25544 51
6392 187
7867 0009008 101
3550 258
8626 15
74176458 20652
Satellite: ISS
Catalog Number: 25544
Epoch time: 09261
50322865 = yrday
fracday
Element set: 900
Inclination: 51
6392 deg
RA of node: 187
7867 deg
Eccentricity:
0009008
Arg of perigee: 101
3550 deg
Mean anomaly: 258
8626 deg
Mean motion: 15
74176458 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2065
Checksum: 302
Coasting Arc #2 (Orbit 2080)
---------------------------------------
Vector Time (GMT): 2009/262/11:40:19
931
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6712561
18 A = 6731569
05 meter
Y = -91952
63 meter E =
0021500
Z = 368345
05 I = 51
64823
XDOT = 409
819530 Wp = 120
79130
YDOT = 4782
573411 meter/sec RA = 181
70336 deg
ZDOT = -6026
485194 TA = 55
20268
MA = 55
00054
Ha = 193
056 n
mi
Hp = 180
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22022838
51 X = 6711301
14
Y = -301681
86 feet Y = -16895
83 meter
Z = 1208481
15 Z = 400951
88
XDOT = 1344
552264 XDOT = 385
585322
YDOT = 15690
857646 feet/sec YDOT = 4787
020149 meter/sec
ZDOT = -19771
933050 ZDOT = -6024
553620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21880805
54 X = -6669269
53
Y = -2449475
29 feet Y = -746600
07 meter
Z = 1336889
78 Z = 407484
01
XDOT = 332
050215 XDOT = 101
208905
YDOT = -14154
466378 feet/sec YDOT = -4314
281352 meter/sec
ZDOT = -19763
998359 ZDOT = -6024
066700
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 09262
51893740
00020000 00000-0 20000-3 0 9016
2 25544 51
6398 182
5691 0009032 105
4960 254
7201 15
74190739 20813
Satellite: ISS
Catalog Number: 25544
Epoch time: 09262
51893740 = yrday
fracday
Element set: 901
Inclination: 51
6398 deg
RA of node: 182
5691 deg
Eccentricity:
0009032
Arg of perigee: 105
4960 deg
Mean anomaly: 254
7201 deg
Mean motion: 15
74190739 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2081
Checksum: 291
Coasting Arc #3 (Orbit 2096)
---------------------------------------
Vector Time (GMT): 2009/263/11:40:19
931
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -627674
16 A = 6719366
22 meter
Y = -4129078
75 meter E =
0011415
Z = 5254663
78 I = 51
63744
XDOT = 7668
171387 Wp = 109
36549
YDOT = -728
200320 meter/sec RA = 176
57415 deg
ZDOT = 339
437255 TA = 337
39072
MA = 337
44097
Ha = 192
866 n
mi
Hp = 180
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2059298
43 X = -606981
97
Y = -13546846
29 feet Y = -4135981
62 meter
Z = 17239710
57 Z = 5251665
12
XDOT = 25158
042607 XDOT = 7674
095383
YDOT = -2389
108661 feet/sec YDOT = -642
417160 meter/sec
ZDOT = 1113
639288 ZDOT = 376
704155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 687279
46 X = 209482
78
Y = 13700442
62 feet Y = 4175894
91 meter
Z = 17227620
09 Z = 5250978
60
XDOT = -24263
056392 XDOT = -7395
379588
YDOT = -385
521228 feet/sec YDOT = -117
506870 meter/sec
ZDOT = 1260
365673 ZDOT = 384
159457
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 09263
53462680
00020000 00000-0 20000-3 0 9025
2 25544 51
6394 177
3520 0008828 109
5083 250
7034 15
74271205 20970
Satellite: ISS
Catalog Number: 25544
Epoch time: 09263
53462680 = yrday
fracday
Element set: 902
Inclination: 51
6394 deg
RA of node: 177
3520 deg
Eccentricity:
0008828
Arg of perigee: 109
5083 deg
Mean anomaly: 250
7034 deg
Mean motion: 15
74271205 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2097
Checksum: 287
Coasting Arc #4 (Orbit 2111)
---------------------------------------
Vector Time (GMT): 2009/264/11:40:19
931
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6623280
31 A = 6731446
14 meter
Y = 1166113
07 meter E =
0017065
Z = -210924
08 I = 51
70765
XDOT = -1001
603393 Wp = 72
72901
YDOT = -4669
983780 meter/sec RA = 171
43362 deg
ZDOT = 6037
826076 TA = 284
98193
MA = 285
17077
Ha = 192
858 n
mi
Hp = 180
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21729922
28 X = -6634803
08
Y = 3825830
28 feet Y = 1091983
21 meter
Z = -692008
13 Z = -243128
53
XDOT = -3286
100372 XDOT = -978
639506
YDOT = -15321
469094 feet/sec YDOT = -4681
055487 meter/sec
ZDOT = 19809
140668 ZDOT = 6033
016313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21982888
08 X = 6700384
29
Y = -1840546
56 feet Y = -560998
59 meter
Z = -818776
31 Z = -249563
02
XDOT = 1864
408763 XDOT = 568
271791
YDOT = 13963
418843 feet/sec YDOT = 4256
050063 meter/sec
ZDOT = 19789
883477 ZDOT = 6031
956484
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 09264
48682320
00020000 00000-0 20000-3 0 9036
2 25544 51
6393 172
4600 0008888 112
3636 247
8470 15
74245116 21127
Satellite: ISS
Catalog Number: 25544
Epoch time: 09264
48682320 = yrday
fracday
Element set: 903
Inclination: 51
6393 deg
RA of node: 172
4600 deg
Eccentricity:
0008888
Arg of perigee: 112
3636 deg
Mean anomaly: 247
8470 deg
Mean motion: 15
74245116 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2112
Checksum: 285
Coasting Arc #5 (Orbit 2127)
---------------------------------------
Vector Time (GMT): 2009/265/11:40:19
931
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1086232
88 A = 6719281
91 meter
Y = 4031271
41 meter E =
0023303
Z = -5284405
25 I = 51
69692
XDOT = -7447
676596 Wp = 99
45846
YDOT = 1890
515426 meter/sec RA = 166
30343 deg
ZDOT = -92
796994 TA = 169
68378
MA = 169
63587
Ha = 192
768 n
mi
Hp = 180
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3563756
17 X = 1066744
87
Y = 13225956
08 feet Y = 4043309
09 meter
Z = -17337287
57 Z = -5279175
78
XDOT = -24434
634501 XDOT = -7467
812336
YDOT = 6202
478432 feet/sec YDOT = 1807
118533 meter/sec
ZDOT = -304
452079 ZDOT = -129
027372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2682658
60 X = -817674
34
Y = -13459296
35 feet Y = -4102393
53 meter
Z = -17316422
76 Z = -5278045
66
XDOT = 23840
820223 XDOT = 7266
682004
YDOT = -4194
022420 feet/sec YDOT = -1278
338034 meter/sec
ZDOT = -447
043354 ZDOT = -136
258814
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 09265
50248081
00020000 00000-0 20000-3 0 9043
2 25544 51
6398 167
2415 0008893 116
3669 243
8408 15
74292886 21284
Satellite: ISS
Catalog Number: 25544
Epoch time: 09265
50248081 = yrday
fracday
Element set: 904
Inclination: 51
6398 deg
RA of node: 167
2415 deg
Eccentricity:
0008893
Arg of perigee: 116
3669 deg
Mean anomaly: 243
8408 deg
Mean motion: 15
74292886 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2128
Checksum: 319
Coasting Arc #6 (Orbit 2143)
---------------------------------------
Vector Time (GMT): 2009/266/11:40:19
931
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6375662
95 A = 6731379
32 meter
Y = -2130812
48 meter E =
0020978
Z = -51888
28 I = 51
76624
XDOT = 1479
193459 Wp = 129
38244
YDOT = 4533
636304 meter/sec RA = 161
17139 deg
ZDOT = -6052
246675 TA = 51
18058
MA = 50
99347
Ha = 192
763 n
mi
Hp = 180
410
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20917529
35 X = 6399268
27
Y = -6990854
59 feet Y = -2059384
08 meter
Z = -170237
13 Z = -20857
47
XDOT = 4852
996914 XDOT = 1457
788755
YDOT = 14874
134856 feet/sec YDOT = 4550
057653 meter/sec
ZDOT = -19856
452346 ZDOT = -6045
112782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21278834
68 X = -6485788
81
Y = 5801115
49 feet Y = 1768180
00 meter
Z = -48128
85 Z = -14669
67
XDOT = -3699
735111 XDOT = -1127
679262
YDOT = -13578
467195 feet/sec YDOT = -4138
716801 meter/sec
ZDOT = -19828
054783 ZDOT = -6043
591098
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 09266
51812172
00020000 00000-0 20000-3 0 9054
2 25544 51
6396 162
0231 0008891 121
0544 239
1493 15
74282619 21447
Satellite: ISS
Catalog Number: 25544
Epoch time: 09266
51812172 = yrday
fracday
Element set: 905
Inclination: 51
6396 deg
RA of node: 162
0231 deg
Eccentricity:
0008891
Arg of perigee: 121
0544 deg
Mean anomaly: 239
1493 deg
Mean motion: 15
74282619 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2144
Checksum: 283
Coasting Arc #7 (Orbit 2159)
---------------------------------------
Vector Time (GMT): 2009/267/11:40:19
931
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1504783
02 A = 6719031
22 meter
Y = -3876515
67 meter E =
0010602
Z = 5269405
37 I = 51
75335
XDOT = 7100
470257 Wp = 116
31992
YDOT = -2998
119021 meter/sec RA = 156
04041 deg
ZDOT = -182
264307 TA = 335
37980
MA = 335
43038
Ha = 192
560 n
mi
Hp = 180
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4936952
17 X = -1486921
43
Y = -12718227
25 feet Y = -3893243
07 meter
Z = 17288075
36 Z = 5262138
51
XDOT = 23295
506091 XDOT = 7134
353432
YDOT = -9836
348495 feet/sec YDOT = -2918
527937 meter/sec
ZDOT = -597
980009 ZDOT = -147
687472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4535764
90 X = 1382501
14
Y = 12905475
61 feet Y = 3933588
97 meter
Z = 17259197
16 Z = 5260603
29
XDOT = -22724
859595 XDOT = -6926
537205
YDOT = 8585
622099 feet/sec YDOT = 2616
897616 meter/sec
ZDOT = -461
940570 ZDOT = -140
799486
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 09267
53374258
00020000 00000-0 20000-3 0 9066
2 25544 51
6395 156
8049 0008681 124
6815 235
5165 15
74373691 21606
Satellite: ISS
Catalog Number: 25544
Epoch time: 09267
53374258 = yrday
fracday
Element set: 906
Inclination: 51
6395 deg
RA of node: 156
8049 deg
Eccentricity:
0008681
Arg of perigee: 124
6815 deg
Mean anomaly: 235
5165 deg
Mean motion: 15
74373691 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2160
Checksum: 314
Coasting Arc #8 (Orbit 2175)
---------------------------------------
Vector Time (GMT): 2009/268/11:40:19
931
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5978875
08 A = 6731099
80 meter
Y = 3073373
61 meter E =
0016549
Z = 280280
13 I = 51
82110
XDOT = -1942
307932 Wp = 79
01001
YDOT = -4356
633671 meter/sec RA = 150
91636 deg
ZDOT = 6042
580090 TA = 284
02764
MA = 284
21157
Ha = 192
442 n
mi
Hp = 180
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19615731
88 X = -6014159
27
Y = 10083246
75 feet Y = 3006317
03 meter
Z = 919554
24 Z = 251148
77
XDOT = -6372
401351 XDOT = -1922
800947
YDOT = -14293
417555 feet/sec YDOT = -4378
244548 meter/sec
ZDOT = 19824
737827 ZDOT = 6033
191724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19837542
71 X = 6046483
02
Y = -9649783
53 feet Y = -2941254
02 meter
Z = 804959
25 Z = 245351
58
XDOT = 5468
684128 XDOT = 1666
854922
YDOT = 12985
594858 feet/sec YDOT = 3958
009313 meter/sec
ZDOT = 19787
469492 ZDOT = 6031
220701
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 09268
54934880
00020000 00000-0 20000-3 0 9072
2 25544 51
6398 151
5861 0008642 128
1438 232
0505 15
74371203 21764
Satellite: ISS
Catalog Number: 25544
Epoch time: 09268
54934880 = yrday
fracday
Element set: 907
Inclination: 51
6398 deg
RA of node: 151
5861 deg
Eccentricity:
0008642
Arg of perigee: 128
1438 deg
Mean anomaly: 232
0505 deg
Mean motion: 15
74371203 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2176
Checksum: 298
Coasting Arc #9 (Orbit 2190)
---------------------------------------
Vector Time (GMT): 2009/269/11:40:19
931
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1863560
54 A = 6719025
04 meter
Y = 3749820
83 meter E =
0022292
Z = -5273299
62 I = 51
80647
XDOT = -6556
833480 Wp = 107
70697
YDOT = 3977
266091 meter/sec RA = 145
78308 deg
ZDOT = 506
177332 TA = 167
12862
MA = 167
07162
Ha = 192
301 n
mi
Hp = 180
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6114043
77 X = 1847107
76
Y = 12302561
78 feet Y = 3770568
18 meter
Z = -17300851
78 Z = -5264286
43
XDOT = -21511
920866 XDOT = -6603
279567
YDOT = 13048
773263 feet/sec YDOT = 3903
684035 meter/sec
ZDOT = 1660
686784 ZDOT = 474
211183
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6156124
41 X = -1876386
72
Y = -12331769
70 feet Y = -3758723
40 meter
Z = -17265098
27 Z = -5262401
95
XDOT = 20683
970685 XDOT = 6304
474265
YDOT = -12497
119152 feet/sec YDOT = -3809
121918 meter/sec
ZDOT = 1534
962642 ZDOT = 467
856613
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 09269
50146259
00020000 00000-0 20000-3 0 9085
2 25544 51
6400 146
6933 0008547 131
8877 228
3017 15
74406448 21918
Satellite: ISS
Catalog Number: 25544
Epoch time: 09269
50146259 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 146
6933 deg
Eccentricity:
0008547
Arg of perigee: 131
8877 deg
Mean anomaly: 228
3017 deg
Mean motion: 15
74406448 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2191
Checksum: 305
Coasting Arc #10 (Orbit 2206)
---------------------------------------
Vector Time (GMT): 2009/270/11:40:19
931
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5467713
20 A = 6730967
23 meter
Y = -3862768
49 meter E =
0019591
Z = -608492
34 I = 51
87063
XDOT = 2318
641099 Wp = 138
56043
YDOT = 4211
137043 meter/sec RA = 140
66874 deg
ZDOT = -6022
020137 TA = 48
04756
MA = 47
88077
Ha = 192
341 n
mi
Hp = 180
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17938691
60 X = 5513456
93
Y = -12673124
97 feet Y = -3801369
55 meter
Z = -1996365
94 Z = -581818
89
XDOT = 7607
090220 XDOT = 2300
633082
YDOT = 13816
066415 feet/sec YDOT = 4236
964599 meter/sec
ZDOT = -19757
283913 ZDOT = -6010
800003
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17791072
01 X = -5422718
75
Y = 12895359
22 feet Y = 3930505
49 meter
Z = -1891480
13 Z = -576523
14
XDOT = -6953
048899 XDOT = -2119
289304
YDOT = -12421
312606 feet/sec YDOT = -3786
016082 meter/sec
ZDOT = -19712
801499 ZDOT = -6008
461897
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 09270
51703484
00020000 00000-0 20000-3 0 9098
2 25544 51
6401 141
4748 0008621 136
9371 223
2469 15
74376085 22070
Satellite: ISS
Catalog Number: 25544
Epoch time: 09270
51703484 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 141
4748 deg
Eccentricity:
0008621
Arg of perigee: 136
9371 deg
Mean anomaly: 223
2469 deg
Mean motion: 15
74376085 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2207
Checksum: 290
Coasting Arc #11 (Orbit 2222)
---------------------------------------
Vector Time (GMT): 2009/271/11:40:19
931
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2197112
11 A = 6718975
54 meter
Y = -3595094
00 meter E =
0009506
Z = 5226217
41 I = 51
85357
XDOT = 5919
269969 Wp = 120
62485
YDOT = -4863
200478 meter/sec RA = 135
53263 deg
ZDOT = -860
500266 TA = 337
51417
MA = 337
55580
Ha = 192
125 n
mi
Hp = 180
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7208373
07 X = -2182135
92
Y = -11794927
82 feet Y = -3619579
44 meter
Z = 17146382
59 Z = 5215580
35
XDOT = 19420
177063 XDOT = 5977
391346
YDOT = -15955
382145 feet/sec YDOT = -4796
682779 meter/sec
ZDOT = -2823
163601 ZDOT = -831
603017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7654561
90 X = 2333110
47
Y = 11572911
02 feet Y = 3527423
28 meter
Z = 17104233
77 Z = 5213370
45
XDOT = -18111
084434 XDOT = -5520
258536
YDOT = 15966
172198 feet/sec YDOT = 4866
489286 meter/sec
ZDOT = -2709
564057 ZDOT = -825
875125
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 09271
53258658
00020000 00000-0 20000-3 0 9101
2 25544 51
6402 136
2559 0008389 140
1674 220
0106 15
74469786 22239
Satellite: ISS
Catalog Number: 25544
Epoch time: 09271
53258658 = yrday
fracday
Element set: 910
Inclination: 51
6402 deg
RA of node: 136
2559 deg
Eccentricity:
0008389
Arg of perigee: 140
1674 deg
Mean anomaly: 220
0106 deg
Mean motion: 15
74469786 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2223
Checksum: 292
Coasting Arc #12 (Orbit 2238)
---------------------------------------
Vector Time (GMT): 2009/272/11:40:19
931
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4839416
54 A = 6730429
54 meter
Y = 4584914
56 meter E =
0015980
Z = 906937
47 I = 51
91223
XDOT = -2698
121342 Wp = 86
05866
YDOT = -4045
976708 meter/sec RA = 130
42601 deg
ZDOT = 5968
193234 TA = 283
80320
MA = 283
98097
Ha = 191
904 n
mi
Hp = 180
923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15877350
85 X = -4894731
92
Y = 15042370
62 feet Y = 4530488
13 meter
Z = 2975516
63 Z = 883292
90
XDOT = -8852
104139 XDOT = -2681
670469
YDOT = -13274
201798 feet/sec YDOT = -4076
056352 meter/sec
ZDOT = 19580
686463 ZDOT = 5955
125934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15172705
05 X = 4624640
50
Y = -15770115
61 feet Y = -4806731
24 meter
Z = 2882595
72 Z = 878615
18
XDOT = 8427
872947 XDOT = 2568
815674
YDOT = 11733
108436 feet/sec YDOT = 3576
251451 meter/sec
ZDOT = 19528
928026 ZDOT = 5952
417262
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 09272
54812176
00020000 00000-0 20000-3 0 9115
2 25544 51
6395 131
0364 0008329 144
4405 215
7315 15
74498520 22398
Satellite: ISS
Catalog Number: 25544
Epoch time: 09272
54812176 = yrday
fracday
Element set: 911
Inclination: 51
6395 deg
RA of node: 131
0364 deg
Eccentricity:
0008329
Arg of perigee: 144
4405 deg
Mean anomaly: 215
7315 deg
Mean motion: 15
74498520 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2239
Checksum: 285
Coasting Arc #13 (Orbit 2253)
---------------------------------------
Vector Time (GMT): 2009/273/11:40:19
931
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2506780
00 A = 6719150
20 meter
Y = 3492639
39 meter E =
0020660
Z = -5181201
68 I = 51
89191
XDOT = -5148
178869 Wp = 117
02689
YDOT = 5567
985964 meter/sec RA = 125
28514 deg
ZDOT = 1257
215772 TA = 165
00085
MA = 164
93949
Ha = 191
774 n
mi
Hp = 181
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8224343
84 X = 2492707
84
Y = 11458790
64 feet Y = 3520592
59 meter
Z = -16998693
17 Z = -5169058
15
XDOT = -16890
350621 XDOT = -5216
165778
YDOT = 18267
670484 feet/sec YDOT = 5510
035958 meter/sec
ZDOT = 4124
723663 ZDOT = 1232
040248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9039617
81 X = -2755275
51
Y = -10902360
19 feet Y = -3323039
38 meter
Z = -16950608
74 Z = -5166545
54
XDOT = 14915
368100 XDOT = 4546
204197
YDOT = -18653
556744 feet/sec YDOT = -5685
604096 meter/sec
ZDOT = 4025
821123 ZDOT = 1227
070278
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 09273
50017067
00020000 00000-0 20000-3 0 9129
2 25544 51
6386 126
1425 0008233 147
9480 212
2185 15
74512585 22548
Satellite: ISS
Catalog Number: 25544
Epoch time: 09273
50017067 = yrday
fracday
Element set: 912
Inclination: 51
6386 deg
RA of node: 126
1425 deg
Eccentricity:
0008233
Arg of perigee: 147
9480 deg
Mean anomaly: 212
2185 deg
Mean motion: 15
74512585 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2254
Checksum: 279
Coasting Arc #14 (Orbit 2269)
---------------------------------------
Vector Time (GMT): 2009/274/11:40:19
931
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4154091
50 A = 6730058
79 meter
Y = -5123575
03 meter E =
0017247
Z = -1295663
76 I = 51
94441
XDOT = 3038
062915 Wp = 147
58177
YDOT = 3938
595318 meter/sec RA = 120
18863 deg
ZDOT = -5884
327676 TA = 46
58742
MA = 46
44398
Ha = 191
766 n
mi
Hp = 181
190
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13628909
12 X = 4217369
61
Y = -16809629
35 feet Y = -5076767
84 meter
Z = -4250865
34 Z = -1275328
85
XDOT = 9967
398014 XDOT = 3022
380275
YDOT = 12921
900649 feet/sec YDOT = 3972
480490 meter/sec
ZDOT = -19305
536995 ZDOT = -5869
607123
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12244281
20 X = -3732056
91
Y = 17862275
81 feet Y = 5444421
67 meter
Z = -4171011
81 Z = -1271324
40
XDOT = -9792
701339 XDOT = -2984
815368
YDOT = -11168
091132 feet/sec YDOT = -3404
034177 meter/sec
ZDOT = -19247
266179 ZDOT = -5866
566731
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 09274
51567175
00020000 00000-0 20000-3 0 9132
2 25544 51
6382 120
9239 0008266 152
6656 207
4943 15
74498001 22705
Satellite: ISS
Catalog Number: 25544
Epoch time: 09274
51567175 = yrday
fracday
Element set: 913
Inclination: 51
6382 deg
RA of node: 120
9239 deg
Eccentricity:
0008266
Arg of perigee: 152
6656 deg
Mean anomaly: 207
4943 deg
Mean motion: 15
74498001 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2270
Checksum: 299
Coasting Arc #15 (Orbit 2285)
---------------------------------------
Vector Time (GMT): 2009/275/11:40:19
931
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2814878
57 A = 6719405
30 meter
Y = -3372449
73 meter E =
0008668
Z = 5077203
63 I = 51
92262
XDOT = 4331
162241 Wp = 121
46570
YDOT = -6149
700073 meter/sec RA = 115
04287 deg
ZDOT = -1685
912553 TA = 344
65252
MA = 344
67879
Ha = 191
615 n
mi
Hp = 181
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9235165
91 X = -2801622
47
Y = -11064467
62 feet Y = -3403852
72 meter
Z = 16657492
24 Z = 5063561
34
XDOT = 14209
849873 XDOT = 4407
797305
YDOT = -20176
181343 feet/sec YDOT = -6100
838151 meter/sec
ZDOT = -5531
209164 ZDOT = -1664
684735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10374458
95 X = 3162135
09
Y = 10093408
96 feet Y = 3076471
05 meter
Z = 16603508
00 Z = 5060749
24
XDOT = -11453
856938 XDOT = -3491
135595
YDOT = 20721
837089 feet/sec YDOT = 6316
015945 meter/sec
ZDOT = -5447
890722 ZDOT = -1660
517092
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 09275
53115283
00020000 00000-0 20000-3 0 9145
2 25544 51
6377 115
7036 0008140 156
4341 203
7197 15
74560176 22860
Satellite: ISS
Catalog Number: 25544
Epoch time: 09275
53115283 = yrday
fracday
Element set: 914
Inclination: 51
6377 deg
RA of node: 115
7036 deg
Eccentricity:
0008140
Arg of perigee: 156
4341 deg
Mean anomaly: 203
7197 deg
Mean motion: 15
74560176 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2286
Checksum: 287
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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