Date:
March 26th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 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 3240)
---------------------------------------
Vector Time (GMT): 2009/082/02:55:38
824
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5760661
71 A = 6734022
18 meter
Y = -120564
32 meter E =
0013203
Z = -3502213
40 I = 51
79632
XDOT = 2868
329528 Wp = 129
20120
YDOT = 5502
139835 meter/sec RA = 27
38007 deg
ZDOT = 4531
800009 TA = 189
42496
MA = 189
44976
Ha = 196
855 n
mi
Hp = 185
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18899808
76 X = 5778594
64
Y = -395552
24 feet Y = -56045
25 meter
Z = -11490201
45 Z = -3474184
91
XDOT = 9410
529946 XDOT = 2784
576122
YDOT = 18051
639878 feet/sec YDOT = 5533
747236 meter/sec
ZDOT = 14868
110265 ZDOT = 4545
530300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13394638
75 X = -4082685
89
Y = 13433026
21 feet Y = 4094386
39 meter
Z = -11380747
85 Z = -3468851
94
XDOT = -18254
805113 XDOT = -5564
064599
YDOT = -5569
299364 feet/sec YDOT = -1697
522446 meter/sec
ZDOT = 14922
104433 ZDOT = 4548
257431
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 09082
12924171
00010596 00000-0 82463-4 0 9006
2 25544 51
6413 27
8951 0009595 147
7249 212
4502 15
71525176 32412
Satellite: ISS
Catalog Number: 25544
Epoch time: 09082
12924171 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 27
8951 deg
Eccentricity:
0009595
Arg of perigee: 147
7249 deg
Mean anomaly: 212
4502 deg
Mean motion: 15
71525176 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3241
Checksum: 298
Coasting Arc #2 (Orbit 3256)
---------------------------------------
Vector Time (GMT): 2009/083/02:55:38
824
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3742383
73 A = 6734123
66 meter
Y = -4440379
03 meter E =
0012639
Z = -3409617
21 I = 51
76959
XDOT = 5964
589693 Wp = 130
32540
YDOT = -1489
954327 meter/sec RA = 22
32421 deg
ZDOT = -4625
534023 TA = 89
80749
MA = 89
66266
Ha = 196
746 n
mi
Hp = 185
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12278161
85 X = -3675889
40
Y = -14568172
67 feet Y = -4481857
09 meter
Z = -11186408
15 Z = -3427635
58
XDOT = 19568
863821 XDOT = 6003
277088
YDOT = -4888
301598 feet/sec YDOT = -1423
038939 meter/sec
ZDOT = -15175
636559 ZDOT = -4596
464237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18933669
19 X = 5770982
37
Y = 1707358
07 feet Y = 520402
74 meter
Z = -11257075
13 Z = -3431156
50
XDOT = -10356
526832 XDOT = -3156
669378
YDOT = 15951
779609 feet/sec YDOT = 4862
102425 meter/sec
ZDOT = -15062
212913 ZDOT = -4590
962496
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 09083
14667333
00010596 00000-0 82463-4 0 9014
2 25544 51
6408 22
6890 0009595 151
4265 208
7425 15
71523800 32572
Satellite: ISS
Catalog Number: 25544
Epoch time: 09083
14667333 = yrday
fracday
Element set: 901
Inclination: 51
6408 deg
RA of node: 22
6890 deg
Eccentricity:
0009595
Arg of perigee: 151
4265 deg
Mean anomaly: 208
7425 deg
Mean motion: 15
71523800 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3257
Checksum: 306
Coasting Arc #3 (Orbit 3272)
---------------------------------------
Vector Time (GMT): 2009/084/02:55:38
824
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4389992
26 A = 6730293
36 meter
Y = 2365171
89 meter E =
0013192
Z = 4506974
87 I = 51
73025
XDOT = -5556
333034 Wp = 112
32180
YDOT = -4313
936008 meter/sec RA = 17
16687 deg
ZDOT = -3145
870387 TA = 9
02171
MA = 8
99803
Ha = 196
625 n
mi
Hp = 185
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14402861
76 X = -4438007
68
Y = 7759750
28 feet Y = 2315812
45 meter
Z = 14786662
97 Z = 4485531
54
XDOT = -18229
439087 XDOT = -5492
398940
YDOT = -14153
333358 feet/sec YDOT = -4375
713028 meter/sec
ZDOT = -10321
097069 ZDOT = -3172
707129
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4521435
68 X = 1378133
59
Y = -15801184
89 feet Y = -4816201
15 meter
Z = 14703085
68 Z = 4481500
51
XDOT = 21658
401465 XDOT = 6601
480766
YDOT = -3511
460889 feet/sec YDOT = -1070
293279 meter/sec
ZDOT = -10426
188108 ZDOT = -3177
902135
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 09084
16408888
00010596 00000-0 82463-4 0 9026
2 25544 51
6417 17
4831 0009385 155
4218 204
7393 15
71594326 32737
Satellite: ISS
Catalog Number: 25544
Epoch time: 09084
16408888 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 17
4831 deg
Eccentricity:
0009385
Arg of perigee: 155
4218 deg
Mean anomaly: 204
7393 deg
Mean motion: 15
71594326 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3273
Checksum: 323
Coasting Arc #4 (Orbit 3288)
---------------------------------------
Vector Time (GMT): 2009/085/02:55:38
824
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5742793
71 A = 6737250
38 meter
Y = 2871910
07 meter E =
0017143
Z = 2033491
65 I = 51
72460
XDOT = -3826
512011 Wp = 102
38288
YDOT = 3676
084984 meter/sec RA = 12
09789 deg
ZDOT = 5571
740688 TA = 280
23553
MA = 280
42880
Ha = 196
507 n
mi
Hp = 185
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18841186
70 X = 5700374
38
Y = 9422277
14 feet Y = 2935892
39 meter
Z = 6671560
54 Z = 2061286
77
XDOT = -12554
173266 XDOT = -3894
400711
YDOT = 12060
646272 feet/sec YDOT = 3632
915724 meter/sec
ZDOT = 18279
989135 ZDOT = 5552
986199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19734104
88 X = -6014955
17
Y = 7271321
78 feet Y = 2216298
88 meter
Z = 6780289
60 Z = 2066632
27
XDOT = 391
060659 XDOT = 119
195289
YDOT = -16045
534099 feet/sec YDOT = -4890
678794 meter/sec
ZDOT = 18207
003577 ZDOT = 5549
494690
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 09085
18149322
00010596 00000-0 82463-4 0 9035
2 25544 51
6413 12
2774 0009458 158
1826 201
9740 15
71571241 32891
Satellite: ISS
Catalog Number: 25544
Epoch time: 09085
18149322 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 12
2774 deg
Eccentricity:
0009458
Arg of perigee: 158
1826 deg
Mean anomaly: 201
9740 deg
Mean motion: 15
71571241 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3289
Checksum: 306
Coasting Arc #5 (Orbit 3303)
---------------------------------------
Vector Time (GMT): 2009/086/02:55:38
824
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2154124
48 A = 6727791
07 meter
Y = -3816930
38 meter E =
0020124
Z = -5120992
10 I = 51
66332
XDOT = 7244
925600 Wp = 125
03687
YDOT = 2074
122135 meter/sec RA = 6
95347 deg
ZDOT = 1494
416022 TA = 159
36231
MA = 159
28092
Ha = 196
375 n
mi
Hp = 185
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7067337
54 X = 2221522
92
Y = -12522737
47 feet Y = -3792465
39 meter
Z = -16801155
18 Z = -5110363
21
XDOT = 23769
440944 XDOT = 7213
934318
YDOT = 6804
862648 feet/sec YDOT = 2154
965990 meter/sec
ZDOT = 4902
939706 ZDOT = 1529
536550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4471596
28 X = 1362942
55
Y = 13716972
28 feet Y = 4180933
15 meter
Z = -16759908
33 Z = -5108420
06
XDOT = -19981
296029 XDOT = -6090
299030
YDOT = 12700
897606 feet/sec YDOT = 3871
233590 meter/sec
ZDOT = 5040
210653 ZDOT = 1536
256207
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 09086
13529531
00010596 00000-0 82463-4 0 9046
2 25544 51
6411 7
3966 0009339 162
0245 198
1249 15
71583628 33045
Satellite: ISS
Catalog Number: 25544
Epoch time: 09086
13529531 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 7
3966 deg
Eccentricity:
0009339
Arg of perigee: 162
0245 deg
Mean anomaly: 198
1249 deg
Mean motion: 15
71583628 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3304
Checksum: 311
Coasting Arc #6 (Orbit 3319)
---------------------------------------
Vector Time (GMT): 2009/087/02:55:38
824
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6672226
04 A = 6738769
82 meter
Y = -658436
52 meter E =
0019746
Z = -559024
24 I = 51
67203
XDOT = 960
695550 Wp = 150
78632
YDOT = -4722
376328 meter/sec RA = 1
85651 deg
ZDOT = -6009
800495 TA = 35
29378
MA = 35
16321
Ha = 196
173 n
mi
Hp = 185
802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21890505
39 X = -6661651
73
Y = -2160224
79 feet Y = -732990
16 meter
Z = -1834069
03 Z = -591412
47
XDOT = 3151
888286 XDOT = 1042
625350
YDOT = -15493
360657 feet/sec YDOT = -4711
175684 meter/sec
ZDOT = -19717
193224 ZDOT = -6004
933985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16033291
80 X = 4886947
34
Y = -15043747
01 feet Y = -4585334
09 meter
Z = -1960570
43 Z = -597581
87
XDOT = 8412
703519 XDOT = 2564
192033
YDOT = 11491
035161 feet/sec YDOT = 3502
467517 meter/sec
ZDOT = -19698
503395 ZDOT = -6004
103835
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 09087
15267066
00010596 00000-0 82463-4 0 9052
2 25544 51
6417 2
1905 0009338 165
1147 195
0292 15
71633359 33200
Satellite: ISS
Catalog Number: 25544
Epoch time: 09087
15267066 = yrday
fracday
Element set: 905
Inclination: 51
6417 deg
RA of node: 2
1905 deg
Eccentricity:
0009338
Arg of perigee: 165
1147 deg
Mean anomaly: 195
0292 deg
Mean motion: 15
71633359 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3320
Checksum: 302
Coasting Arc #7 (Orbit 3335)
---------------------------------------
Vector Time (GMT): 2009/088/02:55:38
824
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 526489
20 A = 6726790
17 meter
Y = 4149458
07 meter E =
0010465
Z = 5264949
62 I = 51
60163
XDOT = -7669
982335 Wp = 156
01415
YDOT = 638
945446 meter/sec RA = 356
73585 deg
ZDOT = 253
847557 TA = 291
51943
MA = 291
63096
Ha = 196
042 n
mi
Hp = 185
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1727326
78 X = 454473
67
Y = 13613707
58 feet Y = 4154943
23 meter
Z = 17273456
76 Z = 5267332
16
XDOT = -25163
984040 XDOT = -7677
790237
YDOT = 2096
277710 feet/sec YDOT = 553
131591 meter/sec
ZDOT = 832
833192 ZDOT = 216
567350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11448733
97 X = -3489574
11
Y = -7544032
62 feet Y = -2299421
14 meter
Z = 17283028
16 Z = 5267866
98
XDOT = 14093
665393 XDOT = 4295
749212
YDOT = -19741
861041 feet/sec YDOT = -6017
319245 meter/sec
ZDOT = 687
320427 ZDOT = 209
495266
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 09088
17003110
00010596 00000-0 82463-4 0 9064
2 25544 51
6410 356
9847 0009328 169
1986 190
9378 15
71657986 33360
Satellite: ISS
Catalog Number: 25544
Epoch time: 09088
17003110 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 356
9847 deg
Eccentricity:
0009328
Arg of perigee: 169
1986 deg
Mean anomaly: 190
9378 deg
Mean motion: 15
71657986 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3336
Checksum: 344
Coasting Arc #8 (Orbit 3350)
---------------------------------------
Vector Time (GMT): 2009/089/02:55:38
824
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6439610
65 A = 6738453
47 meter
Y = -1733624
12 meter E =
0007553
Z = -977974
19 I = 51
61161
XDOT = 2088
011523 Wp = 99
59719
YDOT = 4435
616129 meter/sec RA = 351
60434 deg
ZDOT = 5923
492829 TA = 249
73507
MA = 249
81628
Ha = 195
940 n
mi
Hp = 186
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21127331
54 X = 6463268
59
Y = -5687743
16 feet Y = -1661480
39 meter
Z = -3208576
73 Z = -946632
69
XDOT = 6850
431507 XDOT = 2009
480954
YDOT = 14552
546356 feet/sec YDOT = 4458
526587 meter/sec
ZDOT = 19434
031590 ZDOT = 5933
445611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8961704
14 X = -2731527
42
Y = 19979289
46 feet Y = 6089687
43 meter
Z = -3086320
82 Z = -940710
59
XDOT = -14078
275286 XDOT = -4291
058307
YDOT = -3326
457999 feet/sec YDOT = -1013
904398 meter/sec
ZDOT = 19473
173455 ZDOT = 5935
423269
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 09089
12379471
00010596 00000-0 82463-4 0 9077
2 25544 51
6412 352
1035 0009207 172
5019 187
6283 15
71658745 33519
Satellite: ISS
Catalog Number: 25544
Epoch time: 09089
12379471 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 352
1035 deg
Eccentricity:
0009207
Arg of perigee: 172
5019 deg
Mean anomaly: 187
6283 deg
Mean motion: 15
71658745 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3351
Checksum: 316
Coasting Arc #9 (Orbit 3366)
---------------------------------------
Vector Time (GMT): 2009/090/02:55:38
824
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3014304
30 A = 6727897
85 meter
Y = -3359153
08 meter E =
0014671
Z = -4999250
94 I = 51
54786
XDOT = 6727
318869 Wp = 113
93725
YDOT = -3186
564697 meter/sec RA = 346
50653 deg
ZDOT = -1925
376197 TA = 137
47128
MA = 137
35755
Ha = 195
784 n
mi
Hp = 186
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9889449
81 X = -2952232
00
Y = -11020843
43 feet Y = -3392513
75 meter
Z = -16401741
91 Z = -5013743
75
XDOT = 22071
256133 XDOT = 6771
804783
YDOT = -10454
608585 feet/sec YDOT = -3111
087176 meter/sec
ZDOT = -6316
851040 ZDOT = -1892
586538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14718336
23 X = 4486148
88
Y = -874310
11 feet Y = -266489
72 meter
Z = -16458538
99 Z = -5016562
68
XDOT = -5531
024182 XDOT = -1685
856171
YDOT = 22762
549676 feet/sec YDOT = 6938
025141 meter/sec
ZDOT = -6189
029660 ZDOT = -1886
416240
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 09090
14112815
00010596 00000-0 82463-4 0 9089
2 25544 51
6417 346
8965 0009275 176
5066 183
6162 15
71677607 33674
Satellite: ISS
Catalog Number: 25544
Epoch time: 09090
14112815 = yrday
fracday
Element set: 908
Inclination: 51
6417 deg
RA of node: 346
8965 deg
Eccentricity:
0009275
Arg of perigee: 176
5066 deg
Mean anomaly: 183
6162 deg
Mean motion: 15
71677607 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3367
Checksum: 333
Coasting Arc #10 (Orbit 3382)
---------------------------------------
Vector Time (GMT): 2009/091/02:55:38
824
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5089069
95 A = 6736301
27 meter
Y = 3702756
06 meter E =
0018810
Z = 2368040
07 I = 51
54668
XDOT = -4655
958208 Wp = 134
07616
YDOT = -2944
430724 meter/sec RA = 341
34588 deg
ZDOT = -5388
418561 TA = 19
19997
MA = 19
12918
Ha = 195
656 n
mi
Hp = 186
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16696423
72 X = -5141600
10
Y = 12148149
79 feet Y = 3645553
38 meter
Z = 7769160
33 Z = 2343189
72
XDOT = -15275
453439 XDOT = -4596
511001
YDOT = -9660
205787 feet/sec YDOT = -2996
163932 meter/sec
ZDOT = -17678
538585 ZDOT = -5410
892904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 460581
88 X = 140385
36
Y = -20679231
96 feet Y = -6303029
90 meter
Z = 7672365
38 Z = 2338536
97
XDOT = 15365
036269 XDOT = 4683
263055
YDOT = -6266
114558 feet/sec YDOT = -1909
911717 meter/sec
ZDOT = -17766
473745 ZDOT = -5415
221197
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 09091
15844714
00010596 00000-0 82463-4 0 9092
2 25544 51
6405 341
6898 0009151 179
6931 180
4238 15
71720414 33839
Satellite: ISS
Catalog Number: 25544
Epoch time: 09091
15844714 = yrday
fracday
Element set: 909
Inclination: 51
6405 deg
RA of node: 341
6898 deg
Eccentricity:
0009151
Arg of perigee: 179
6931 deg
Mean anomaly: 180
4238 deg
Mean motion: 15
71720414 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3383
Checksum: 321
Coasting Arc #11 (Orbit 3398)
---------------------------------------
Vector Time (GMT): 2009/092/02:55:38
824
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4908597
50 A = 6730471
02 meter
Y = 1595205
38 meter E =
0014911
Z = 4319645
99 I = 51
49927
XDOT = -4682
300843 Wp = 144
80322
YDOT = 5047
202253 meter/sec RA = 336
26398 deg
ZDOT = 3438
933118 TA = 270
29162
MA = 270
46249
Ha = 195
422 n
mi
Hp = 186
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16104322
51 X = 4869410
82
Y = 5233613
45 feet Y = 1649877
04 meter
Z = 14172066
89 Z = 4343396
73
XDOT = -15361
879407 XDOT = -4755
097180
YDOT = 16559
062511 feet/sec YDOT = 4994
434983 meter/sec
ZDOT = 11282
588969 ZDOT = 3416
009772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13695954
02 X = -4174526
79
Y = 9824496
53 feet Y = 2994506
54 meter
Z = 14264904
65 Z = 4347942
94
XDOT = -3512
879784 XDOT = -1070
725758
YDOT = -21234
304190 feet/sec YDOT = -6472
215917 meter/sec
ZDOT = 11193
400117 ZDOT = 3411
748356
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 09092
17575277
00010596 00000-0 82463-4 0 9102
2 25544 51
6400 336
4826 0009090 183
4285 176
6816 15
71722742 33996
Satellite: ISS
Catalog Number: 25544
Epoch time: 09092
17575277 = yrday
fracday
Element set: 910
Inclination: 51
6400 deg
RA of node: 336
4826 deg
Eccentricity:
0009090
Arg of perigee: 183
4285 deg
Mean anomaly: 176
6816 deg
Mean motion: 15
71722742 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3399
Checksum: 328
Coasting Arc #12 (Orbit 3413)
---------------------------------------
Vector Time (GMT): 2009/093/02:55:38
824
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2965540
67 A = 6733109
08 meter
Y = -4885830
37 meter E =
0010395
Z = -3571832
51 I = 51
48266
XDOT = 6261
288151 Wp = 156
63601
YDOT = 563
273008 meter/sec RA = 331
08557 deg
ZDOT = 4423
011668 TA = 160
72749
MA = 160
68815
Ha = 195
273 n
mi
Hp = 186
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9729464
12 X = 3037305
63
Y = -16029627
21 feet Y = -4852266
73 meter
Z = -11718610
60 Z = -3557251
67
XDOT = 20542
283959 XDOT = 6233
038142
YDOT = 1848
008558 feet/sec YDOT = 633
132456 meter/sec
ZDOT = 14511
193138 ZDOT = 4453
360171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7429787
10 X = 2264599
11
Y = 17254957
75 feet Y = 5259311
12 meter
Z = -11661987
46 Z = -3554573
78
XDOT = -12064
108122 XDOT = -3677
140156
YDOT = 15093
459485 feet/sec YDOT = 4600
486451 meter/sec
ZDOT = 14629
731563 ZDOT = 4459
142181
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 09093
12946297
00010596 00000-0 82463-4 0 9113
2 25544 51
6410 331
6017 0009015 187
7143 172
3881 15
71753192 34149
Satellite: ISS
Catalog Number: 25544
Epoch time: 09093
12946297 = yrday
fracday
Element set: 911
Inclination: 51
6410 deg
RA of node: 331
6017 deg
Eccentricity:
0009015
Arg of perigee: 187
7143 deg
Mean anomaly: 172
3881 deg
Mean motion: 15
71753192 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3414
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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