Date:
April 27th 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 3750)
---------------------------------------
Vector Time (GMT): 2009/114/12:22:31
864
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5629482
42 A = 6735883
68 meter
Y = 3404204
77 meter E =
0006467
Z = 1427029
39 I = 51
43950
XDOT = -1463
913825 Wp = 147
02518
YDOT = 4852
262562 meter/sec RA = 221
11923 deg
ZDOT = -5793
216211 TA = 17
24516
MA = 17
22320
Ha = 191
008 n
mi
Hp = 189
974
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18469430
51 X = 5584065
22
Y = 11168650
81 feet Y = 3466903
00 meter
Z = 4681854
95 Z = 1454267
67
XDOT = -4802
866881 XDOT = -1489
920810
YDOT = 15919
496596 feet/sec YDOT = 4835
746754 meter/sec
ZDOT = -19006
614867 ZDOT = -5800
391284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21428650
91 X = 6531452
80
Y = -2379339
94 feet Y = -725222
81 meter
Z = 4788533
34 Z = 1459544
96
XDOT = 5804
088239 XDOT = 1769
086095
YDOT = 13920
100105 feet/sec YDOT = 4242
846512 meter/sec
ZDOT = -19034
275348 ZDOT = -5801
647126
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 09114
55026191
00010596 00000-0 82463-4 0 9004
2 25544 51
6414 221
9132 0008853 278
7812 81
2347 15
72373648 37519
Satellite: ISS
Catalog Number: 25544
Epoch time: 09114
55026191 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 221
9132 deg
Eccentricity:
0008853
Arg of perigee: 278
7812 deg
Mean anomaly: 81
2347 deg
Mean motion: 15
72373648 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3751
Checksum: 303
Coasting Arc #2 (Orbit 3766)
---------------------------------------
Vector Time (GMT): 2009/115/12:22:31
864
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 326171
18 A = 6726184
82 meter
Y = -4596388
91 meter E =
0003540
Z = 4903100
29 I = 51
43100
XDOT = 6823
888313 Wp = 246
31618
YDOT = 2810
481533 meter/sec RA = 216
01229 deg
ZDOT = 2180
565575 TA = 182
43416
MA = 182
43588
Ha = 191
134 n
mi
Hp = 189
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1070115
40 X = 353725
57
Y = -15080016
12 feet Y = -4592587
51 meter
Z = 16086287
03 Z = 4904751
71
XDOT = 22388
085016 XDOT = 6781
360814
YDOT = 9220
739937 feet/sec YDOT = 2886
552407 meter/sec
ZDOT = 7154
086532 ZDOT = 2213
613580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8627374
42 X = -2629623
72
Y = -12406613
11 feet Y = -3781535
68 meter
Z = 16092390
29 Z = 4904960
56
XDOT = 22321
329067 XDOT = 6803
541100
YDOT = -6074
047718 feet/sec YDOT = -1851
369745 meter/sec
ZDOT = 7283
425170 ZDOT = 2219
987992
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 09115
56712812
00010596 00000-0 82463-4 0 9019
2 25544 51
6419 216
7031 0008925 283
4604 76
5564 15
72437930 37676
Satellite: ISS
Catalog Number: 25544
Epoch time: 09115
56712812 = yrday
fracday
Element set: 901
Inclination: 51
6419 deg
RA of node: 216
7031 deg
Eccentricity:
0008925
Arg of perigee: 283
4604 deg
Mean anomaly: 76
5564 deg
Mean motion: 15
72437930 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3767
Checksum: 315
Coasting Arc #3 (Orbit 3781)
---------------------------------------
Vector Time (GMT): 2009/116/12:22:31
864
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6126466
38 A = 6734212
38 meter
Y = -1463830
85 meter E =
0008069
Z = -2366567
98 I = 51
48220
XDOT = -776
803386 Wp = 326
10885
YDOT = -5452
096429 meter/sec RA = 210
83824 deg
ZDOT = 5381
120283 TA = 7
17866
MA = 7
16711
Ha = 191
419 n
mi
Hp = 189
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20099955
33 X = -6098145
62
Y = -4802594
65 feet Y = -1532182
10 meter
Z = -7764330
65 Z = -2396262
32
XDOT = -2548
567539 XDOT = -741
920507
YDOT = -17887
455475 feet/sec YDOT = -5460
588328 meter/sec
ZDOT = 17654
594103 ZDOT = 5377
430943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18528510
70 X = -5647490
06
Y = 9052644
35 feet Y = 2759246
00 meter
Z = -7880474
06 Z = -2401968
49
XDOT = -12764
323425 XDOT = -3890
565780
YDOT = -10763
483316 feet/sec YDOT = -3280
709715 meter/sec
ZDOT = 17639
767616 ZDOT = 5376
601169
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 09116
52042837
00010596 00000-0 82463-4 0 9020
2 25544 51
6415 211
8200 0009053 288
4615 71
5563 15
72405079 37826
Satellite: ISS
Catalog Number: 25544
Epoch time: 09116
52042837 = yrday
fracday
Element set: 902
Inclination: 51
6415 deg
RA of node: 211
8200 deg
Eccentricity:
0009053
Arg of perigee: 288
4615 deg
Mean anomaly: 71
5563 deg
Mean motion: 15
72405079 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3782
Checksum: 296
Coasting Arc #4 (Orbit 3797)
---------------------------------------
Vector Time (GMT): 2009/117/12:22:31
864
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1679954
46 A = 6728014
14 meter
Y = 4751858
45 meter E =
0006743
Z = -4461089
74 I = 51
48647
XDOT = -6977
291045 Wp = 5
87660
YDOT = -540
483305 meter/sec RA = 205
74857 deg
ZDOT = -3197
043185 TA = 232
01611
MA = 232
07703
Ha = 191
639 n
mi
Hp = 189
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5511661
63 X = 1648365
11
Y = 15590086
78 feet Y = 4770468
40 meter
Z = -14636121
20 Z = -4453004
74
XDOT = -22891
374819 XDOT = -6955
197743
YDOT = -1773
239189 feet/sec YDOT = -618
383668 meter/sec
ZDOT = -10488
986826 ZDOT = -3230
885892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14379180
33 X = 4382774
16
Y = 8222083
18 feet Y = 2506090
95 meter
Z = -14604170
11 Z = -4451351
05
XDOT = -17914
234365 XDOT = -5460
258635
YDOT = 12427
573420 feet/sec YDOT = 3787
924378 meter/sec
ZDOT = -10621
286946 ZDOT = -3237
368261
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 09117
53726647
00010596 00000-0 82463-4 0 9031
2 25544 51
6404 206
6108 0008965 291
9574 68
0635 15
72443961 37987
Satellite: ISS
Catalog Number: 25544
Epoch time: 09117
53726647 = yrday
fracday
Element set: 903
Inclination: 51
6404 deg
RA of node: 206
6108 deg
Eccentricity:
0008965
Arg of perigee: 291
9574 deg
Mean anomaly: 68
0635 deg
Mean motion: 15
72443961 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3798
Checksum: 338
Coasting Arc #5 (Orbit 3813)
---------------------------------------
Vector Time (GMT): 2009/118/12:22:31
864
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5905194
72 A = 6731937
60 meter
Y = -495016
02 meter E =
0005976
Z = 3193825
47 I = 51
52755
XDOT = 3032
136903 Wp = 54
88430
YDOT = 5203
298099 meter/sec RA = 200
56703 deg
ZDOT = -4790
090107 TA = 87
81505
MA = 87
74663
Ha = 191
798 n
mi
Hp = 188
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19373998
43 X = 5894775
95
Y = -1624068
30 feet Y = -429039
23 meter
Z = 10478430
02 Z = 3222487
94
XDOT = 9947
955718 XDOT = 2996
997096
YDOT = 17071
187990 feet/sec YDOT = 5237
009182 meter/sec
ZDOT = -15715
518723 ZDOT = -4775
444668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13393938
32 X = 4082472
40
Y = -14008291
87 feet Y = -4269727
36 meter
Z = 10590424
15 Z = 3227961
28
XDOT = 17806
302396 XDOT = 5427
360970
YDOT = 5164
076509 feet/sec YDOT = 1574
010520 meter/sec
ZDOT = -15657
888923 ZDOT = -4772
524544
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 09118
55408886
00010596 00000-0 82463-4 0 9047
2 25544 51
6403 201
4008 0008971 297
2810 62
7439 15
72496953 38148
Satellite: ISS
Catalog Number: 25544
Epoch time: 09118
55408886 = yrday
fracday
Element set: 904
Inclination: 51
6403 deg
RA of node: 201
4008 deg
Eccentricity:
0008971
Arg of perigee: 297
2810 deg
Mean anomaly: 62
7439 deg
Mean motion: 15
72496953 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3814
Checksum: 325
Coasting Arc #6 (Orbit 3829)
---------------------------------------
Vector Time (GMT): 2009/119/12:22:31
864
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3558765
98 A = 6729919
08 meter
Y = -4184985
52 meter E =
0004440
Z = 3882366
57 I = 51
54838
XDOT = 6332
373847 Wp = 51
18492
YDOT = -1603
638743 meter/sec RA = 195
48634 deg
ZDOT = 4075
540899 TA = 356
28809
MA = 356
29138
Ha = 192
002 n
mi
Hp = 188
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11675741
40 X = -3530564
25
Y = -13730267
46 feet Y = -4224624
39 meter
Z = 12737423
13 Z = 3865146
07
XDOT = 20775
504749 XDOT = 6330
036978
YDOT = -5261
281965 feet/sec YDOT = -1532
839884 meter/sec
ZDOT = 13371
197176 ZDOT = 4106
297983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17937011
67 X = -5467201
16
Y = -2196602
35 feet Y = -669524
40 meter
Z = 12669794
00 Z = 3861753
21
XDOT = 11556
808029 XDOT = 3522
515087
YDOT = -16546
655611 feet/sec YDOT = -5043
420630 meter/sec
ZDOT = 13491
313408 ZDOT = 4112
152327
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 09119
57089600
00010596 00000-0 82463-4 0 9050
2 25544 51
6398 196
1902 0008995 300
8522 59
1755 15
72518064 38308
Satellite: ISS
Catalog Number: 25544
Epoch time: 09119
57089600 = yrday
fracday
Element set: 905
Inclination: 51
6398 deg
RA of node: 196
1902 deg
Eccentricity:
0008995
Arg of perigee: 300
8522 deg
Mean anomaly: 59
1755 deg
Mean motion: 15
72518064 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3830
Checksum: 328
Coasting Arc #7 (Orbit 3844)
---------------------------------------
Vector Time (GMT): 2009/120/12:22:31
864
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5007046
61 A = 6729600
13 meter
Y = 2233473
70 meter E =
0003270
Z = -3899270
98 I = 51
57593
XDOT = -5026
255014 Wp = 347
22266
YDOT = -4186
418957 meter/sec RA = 190
30557 deg
ZDOT = 4058
741671 TA = 325
06372
MA = 325
08518
Ha = 192
033 n
mi
Hp = 188
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16427318
26 X = -5012707
54
Y = 7327669
61 feet Y = 2177450
63 meter
Z = -12792883
81 Z = -3923608
86
XDOT = -16490
337972 XDOT = -4998
784897
YDOT = -13734
970332 feet/sec YDOT = -4242
472194 meter/sec
ZDOT = 13316
081599 ZDOT = 4034
390455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6832808
79 X = -2082640
12
Y = 16565774
73 feet Y = 5049248
14 meter
Z = -12887871
62 Z = -3928223
27
XDOT = -20265
078306 XDOT = -6176
795868
YDOT = 1920
412661 feet/sec YDOT = 585
341779 meter/sec
ZDOT = 13220
562160 ZDOT = 4029
627346
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 09120
52414070
00010596 00000-0 82463-4 0 9061
2 25544 51
6389 191
3060 0008903 305
6327 54
4006 15
72550325 38454
Satellite: ISS
Catalog Number: 25544
Epoch time: 09120
52414070 = yrday
fracday
Element set: 906
Inclination: 51
6389 deg
RA of node: 191
3060 deg
Eccentricity:
0008903
Arg of perigee: 305
6327 deg
Mean anomaly: 54
4006 deg
Mean motion: 15
72550325 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3845
Checksum: 285
Coasting Arc #8 (Orbit 3860)
---------------------------------------
Vector Time (GMT): 2009/121/12:22:31
864
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5107218
74 A = 6731974
31 meter
Y = 3008779
47 meter E =
0005431
Z = -3194642
27 I = 51
61313
XDOT = -4986
199892 Wp = 334
72804
YDOT = 3360
839909 meter/sec RA = 185
22850 deg
ZDOT = -4798
227483 TA = 242
51992
MA = 242
57514
Ha = 192
366 n
mi
Hp = 188
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16755967
00 X = 5088713
48
Y = 9871323
72 feet Y = 3065788
07 meter
Z = -10481109
82 Z = -3169876
18
XDOT = -16358
923530 XDOT = -5000
101853
YDOT = 11026
377653 feet/sec YDOT = 3305
003844 meter/sec
ZDOT = -15742
216153 ZDOT = -4822
484037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18918484
32 X = 5766354
02
Y = -4724587
84 feet Y = -1440054
37 meter
Z = -10384042
86 Z = -3165056
26
XDOT = -4240
904752 XDOT = -1292
627769
YDOT = 17882
487010 feet/sec YDOT = 5450
582041 meter/sec
ZDOT = -15836
811301 ZDOT = -4827
060085
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 09121
54092074
00010596 00000-0 82463-4 0 9071
2 25544 51
6391 186
0953 0008936 310
2786 49
7594 15
72545370 38617
Satellite: ISS
Catalog Number: 25544
Epoch time: 09121
54092074 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 186
0953 deg
Eccentricity:
0008936
Arg of perigee: 310
2786 deg
Mean anomaly: 49
7594 deg
Mean motion: 15
72545370 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3861
Checksum: 328
Coasting Arc #9 (Orbit 3876)
---------------------------------------
Vector Time (GMT): 2009/122/12:22:31
864
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3609292
62 A = 6727473
50 meter
Y = -3523930
55 meter E =
0009920
Z = 4455015
57 I = 51
62873
XDOT = 6498
190137 Wp = 10
55266
YDOT = 2561
701180 meter/sec RA = 180
05455 deg
ZDOT = -3227
578527 TA = 111
84580
MA = 111
74026
Ha = 192
465 n
mi
Hp = 187
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11841511
21 X = 3626787
88
Y = -11561451
92 feet Y = -3483471
64 meter
Z = 14616192
81 Z = 4472591
92
XDOT = 21319
521446 XDOT = 6484
740805
YDOT = 8404
531430 feet/sec YDOT = 2634
292630 meter/sec
ZDOT = -10589
168397 ZDOT = -3196
042891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17197
60 X = 5241
83
Y = -16488848
44 feet Y = -5025801
00 meter
Z = 14684659
75 Z = 4475884
29
XDOT = 19790
813904 XDOT = 6032
240078
YDOT = -9331
009960 feet/sec YDOT = -2844
091836 meter/sec
ZDOT = -10465
651015 ZDOT = -3189
930429
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 09122
55768432
00010596 00000-0 82463-4 0 9082
2 25544 51
6395 180
8848 0009139 314
2089 45
8322 15
72600269 38774
Satellite: ISS
Catalog Number: 25544
Epoch time: 09122
55768432 = yrday
fracday
Element set: 908
Inclination: 51
6395 deg
RA of node: 180
8848 deg
Eccentricity:
0009139
Arg of perigee: 314
2089 deg
Mean anomaly: 45
8322 deg
Mean motion: 15
72600269 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3877
Checksum: 336
Coasting Arc #10 (Orbit 3892)
---------------------------------------
Vector Time (GMT): 2009/123/12:22:31
864
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6115054
11 A = 6733776
36 meter
Y = -1389647
79 meter E =
0013128
Z = 2429198
16 I = 51
67866
XDOT = 3163
212075 Wp = 35
73256
YDOT = -4534
544493 meter/sec RA = 174
97493 deg
ZDOT = 5364
719041 TA = 351
68141
MA = 351
70316
Ha = 192
851 n
mi
Hp = 187
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20062513
47 X = -6110860
99
Y = -4559211
92 feet Y = -1458006
48 meter
Z = 7969810
24 Z = 2399501
29
XDOT = 10377
992372 XDOT = 3187
622088
YDOT = -14877
114478 feet/sec YDOT = -4499
035181 meter/sec
ZDOT = 17600
784255 ZDOT = 5380
145225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17167479
11 X = -5232647
63
Y = 11419630
01 feet Y = 3480703
23 meter
Z = 7853562
70 Z = 2393765
91
XDOT = -2856
087142 XDOT = -870
535361
YDOT = -16448
655651 feet/sec YDOT = -5013
550242 meter/sec
ZDOT = 17660
769663 ZDOT = 5383
002593
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 09123
57443761
00010596 00000-0 82463-4 0 9091
2 25544 51
6391 175
6738 0008993 320
1548 39
8953 15
72565152 38935
Satellite: ISS
Catalog Number: 25544
Epoch time: 09123
57443761 = yrday
fracday
Element set: 909
Inclination: 51
6391 deg
RA of node: 175
6738 deg
Eccentricity:
0008993
Arg of perigee: 320
1548 deg
Mean anomaly: 39
8953 deg
Mean motion: 15
72565152 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3893
Checksum: 346
Coasting Arc #11 (Orbit 3907)
---------------------------------------
Vector Time (GMT): 2009/124/12:22:31
864
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1854032
71 A = 6725801
76 meter
Y = 4248957
84 meter E =
0007423
Z = -4877097
08 I = 51
68255
XDOT = -7318
299756 Wp = 59
88961
YDOT = -543
583842 meter/sec RA = 169
81393 deg
ZDOT = 2314
749251 TA = 232
62152
MA = 232
68913
Ha = 192
880 n
mi
Hp = 187
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6082784
47 X = -1877715
22
Y = 13940150
40 feet Y = 4228092
56 meter
Z = -16000974
68 Z = -4886161
56
XDOT = -24010
169802 XDOT = -7322
922121
YDOT = -1783
411556 feet/sec YDOT = -625
447192 meter/sec
ZDOT = 7594
321688 ZDOT = 2279
185430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6204624
30 X = 1891169
49
Y = 13845765
93 feet Y = 4220189
46 meter
Z = -16036104
69 Z = -4887804
71
XDOT = -16586
859580 XDOT = -5055
674800
YDOT = 16043
782729 feet/sec YDOT = 4890
144976 meter/sec
ZDOT = 7455
184222 ZDOT = 2272
340151
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 09124
52762788
00010596 00000-0 82463-4 0 9102
2 25544 51
6399 170
7889 0009100 323
2757 36
7781 15
72596648 39089
Satellite: ISS
Catalog Number: 25544
Epoch time: 09124
52762788 = yrday
fracday
Element set: 910
Inclination: 51
6399 deg
RA of node: 170
7889 deg
Eccentricity:
0009100
Arg of perigee: 323
2757 deg
Mean anomaly: 36
7781 deg
Mean motion: 15
72596648 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3908
Checksum: 351
Coasting Arc #12 (Orbit 3923)
---------------------------------------
Vector Time (GMT): 2009/125/12:22:31
864
Vector Time (MET): N/A
Weight (LBS) : 670564
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6521706
96 A = 6734952
73 meter
Y = -455043
06 meter E =
0001220
Z = -1621902
27 I = 51
74256
XDOT = -1081
515219 Wp = 3
09710
YDOT = 4994
759090 meter/sec RA = 164
72718 deg
ZDOT = -5749
141056 TA = 194
76017
MA = 194
76373
Ha = 192
998 n
mi
Hp = 186
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21396676
37 X = 6534189
63
Y = -1492923
42 feet Y = -382043
72 meter
Z = -5321201
66 Z = -1590189
07
XDOT = -3548
278277 XDOT = -1109
358413
YDOT = 16387
004888 feet/sec YDOT = 4982
509311 meter/sec
ZDOT = -18862
011337 ZDOT = -5754
462728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13116339
67 X = 3997860
33
Y = -17009191
27 feet Y = -5184401
50 meter
Z = -5197192
81 Z = -1584104
37
XDOT = 8725
076188 XDOT = 2659
403222
YDOT = 12498
779800 feet/sec YDOT = 3809
628083 meter/sec
ZDOT = -18882
450124 ZDOT = -5755
370798
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 09125
54435123
00010596 00000-0 82463-4 0 9116
2 25544 51
6399 165
5780 0009043 327
7312 32
3296 15
72641036 39246
Satellite: ISS
Catalog Number: 25544
Epoch time: 09125
54435123 = yrday
fracday
Element set: 911
Inclination: 51
6399 deg
RA of node: 165
5780 deg
Eccentricity:
0009043
Arg of perigee: 327
7312 deg
Mean anomaly: 32
3296 deg
Mean motion: 15
72641036 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3924
Checksum: 302
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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