Date:
August 30th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 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 2235)
---------------------------------------
Vector Time (GMT): 2007/241/13:32:14
583
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2265806
78 A = 6723400
97 meter
Y = -5953236
99 meter E =
0005645
Z = 2147112
03 I = 51
96554
XDOT = 4013
715149 Wp = 88
04880
YDOT = -3531
477566 meter/sec RA = 84
45156 deg
ZDOT = -5543
411170 TA = 68
02647
MA = 67
96649
Ha = 186
138 n
mi
Hp = 182
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7433749
26 X = -2209498
57
Y = -19531617
44 feet Y = -5978259
58 meter
Z = 7044330
81 Z = 2136241
94
XDOT = 13168
356788 XDOT = 4079
834966
YDOT = -11586
212486 feet/sec YDOT = -3486
224534 meter/sec
ZDOT = -18187
044520 ZDOT = -5523
751953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7371301
95 X = 2246772
83
Y = 19570348
44 feet Y = 5965042
20 meter
Z = 7002333
47 Z = 2134311
24
XDOT = -11903
413608 XDOT = -3628
160468
YDOT = 10979
246377 feet/sec YDOT = 3346
474296 meter/sec
ZDOT = -18112
872324 ZDOT = -5520
803484
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 07241
59997297
00020000 00000-0 20000-3 0 9000
2 25544 51
6315 84
9995 0009077 303
1176 56
9117 15
76389928 22361
Satellite: ISS
Catalog Number: 25544
Epoch time: 07241
59997297 = yrday
fracday
Element set: 900
Inclination: 51
6315 deg
RA of node: 84
9995 deg
Eccentricity:
0009077
Arg of perigee: 303
1176 deg
Mean anomaly: 56
9117 deg
Mean motion: 15
76389928 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2236
Checksum: 333
Coasting Arc #2 (Orbit 2251)
---------------------------------------
Vector Time (GMT): 2007/242/13:32:14
583
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3601662
63 A = 6714258
50 meter
Y = 2470125
66 meter E =
0003902
Z = 5101796
89 I = 51
92934
XDOT = -2599
762791 Wp = 309
01737
YDOT = -7074
108353 meter/sec RA = 79
35066 deg
ZDOT = 1592
938709 TA = 125
77206
MA = 125
73577
Ha = 186
440 n
mi
Hp = 182
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11816478
44 X = -3653799
78
Y = 8104086
83 feet Y = 2429558
61 meter
Z = 16738178
78 Z = 5084173
30
XDOT = -8529
405481 XDOT = -2528
204019
YDOT = -23209
016905 feet/sec YDOT = -7102
780174 meter/sec
ZDOT = 5226
176867 ZDOT = 1580
483320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11812283
96 X = 3600384
15
Y = -8246195
96 feet Y = -2513440
53 meter
Z = 16671599
06 Z = 5081503
39
XDOT = 8234
966296 XDOT = 2510
017727
YDOT = 22243
400011 feet/sec YDOT = 6779
788323 meter/sec
ZDOT = 5178
027927 ZDOT = 1578
262912
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 07242
61428397
00020000 00000-0 20000-3 0 9015
2 25544 51
6307 79
7700 0008789 307
3845 52
6519 15
76341622 22522
Satellite: ISS
Catalog Number: 25544
Epoch time: 07242
61428397 = yrday
fracday
Element set: 901
Inclination: 51
6307 deg
RA of node: 79
7700 deg
Eccentricity:
0008789
Arg of perigee: 307
3845 deg
Mean anomaly: 52
6519 deg
Mean motion: 15
76341622 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2252
Checksum: 299
Coasting Arc #3 (Orbit 2266)
---------------------------------------
Vector Time (GMT): 2007/243/13:32:14
583
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2265427
05 A = 6725186
17 meter
Y = 6294162
99 meter E =
0013964
Z = -595463
79 I = 51
96077
XDOT = -4306
113969 Wp = 1
83792
YDOT = 2119
009372 meter/sec RA = 74
19850 deg
ZDOT = 6033
326955 TA = 351
69815
MA = 351
72123
Ha = 186
403 n
mi
Hp = 182
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7432503
44 X = 2197769
07
Y = 20650141
04 feet Y = 6319117
95 meter
Z = -1953621
37 Z = -584622
95
XDOT = -14127
670502 XDOT = -4358
797877
YDOT = 6952
130484 feet/sec YDOT = 2070
561667 meter/sec
ZDOT = 19794
379772 ZDOT = 6012
279752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8042932
84 X = -2451485
93
Y = -20424095
76 feet Y = -6225264
39 meter
Z = -1911704
14 Z = -582687
42
XDOT = 12540
297246 XDOT = 3822
282601
YDOT = -6778
138540 feet/sec YDOT = -2065
976627 meter/sec
ZDOT = 19714
760991 ZDOT = 6009
059150
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 07243
56517827
00020000 00000-0 20000-3 0 9028
2 25544 51
6313 74
8677 0008716 310
1649 49
8751 15
76408047 22679
Satellite: ISS
Catalog Number: 25544
Epoch time: 07243
56517827 = yrday
fracday
Element set: 902
Inclination: 51
6313 deg
RA of node: 74
8677 deg
Eccentricity:
0008716
Arg of perigee: 310
1649 deg
Mean anomaly: 49
8751 deg
Mean motion: 15
76408047 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2267
Checksum: 309
Coasting Arc #4 (Orbit 2282)
---------------------------------------
Vector Time (GMT): 2007/244/13:32:14
583
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3969490
45 A = 6713156
31 meter
Y = -1213312
16 meter E =
0010445
Z = -5283487
77 I = 51
91199
XDOT = 2557
184933 Wp = 58
11121
YDOT = 7257
183235 meter/sec RA = 69
06919 deg
ZDOT = 260
430293 TA = 214
31826
MA = 214
38579
Ha = 186
543 n
mi
Hp = 181
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13023262
64 X = 4008429
23
Y = -3980682
95 feet Y = -1168705
47 meter
Z = -17334277
45 Z = -5264109
27
XDOT = 8389
714347 XDOT = 2474
578844
YDOT = 23809
656284 feet/sec YDOT = 7285
317252 meter/sec
ZDOT = 854
430096 ZDOT = 272
652362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12921694
66 X = -3938532
53
Y = 4584786
90 feet Y = 1397443
05 meter
Z = -17260878
23 Z = -5261115
69
XDOT = -9145
678122 XDOT = -2787
602692
YDOT = -22452
895265 feet/sec YDOT = -6843
642477 meter/sec
ZDOT = 901
697336 ZDOT = 274
837348
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 07244
57944756
00020000 00000-0 20000-3 0 9036
2 25544 51
6319 69
6398 0008619 314
6170 45
4290 15
76447957 22838
Satellite: ISS
Catalog Number: 25544
Epoch time: 07244
57944756 = yrday
fracday
Element set: 903
Inclination: 51
6319 deg
RA of node: 69
6398 deg
Eccentricity:
0008619
Arg of perigee: 314
6170 deg
Mean anomaly: 45
4290 deg
Mean motion: 15
76447957 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2283
Checksum: 326
Coasting Arc #5 (Orbit 2298)
---------------------------------------
Vector Time (GMT): 2007/245/13:32:14
583
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2146738
23 A = 6724541
73 meter
Y = -6283065
36 meter E =
0000905
Z = -1061281
62 I = 51
93959
XDOT = 4855
753231 Wp = 172
82751
YDOT = -656
068450 meter/sec RA = 63
94670 deg
ZDOT = -5939
436142 TA = 18
73644
MA = 18
73311
Ha = 186
651 n
mi
Hp = 181
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7043104
43 X = -2071164
96
Y = -20613731
49 feet Y = -6306648
84 meter
Z = -3481895
09 Z = -1071527
01
XDOT = 15930
948922 XDOT = 4891
581466
YDOT = -2152
455543 feet/sec YDOT = -601
568312 meter/sec
ZDOT = -19486
339048 ZDOT = -5915
759737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8319320
47 X = 2535728
88
Y = 20125668
97 feet Y = 6134303
90 meter
Z = -3521532
99 Z = -1073363
26
XDOT = -14403
354097 XDOT = -4390
142329
YDOT = 2560
744445 feet/sec YDOT = 780
514907 meter/sec
ZDOT = -19396
556973 ZDOT = -5912
070565
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 07245
59369488
00020000 00000-0 20000-3 0 9043
2 25544 51
6320 64
4104 0008874 319
2307 40
8192 15
76508943 22994
Satellite: ISS
Catalog Number: 25544
Epoch time: 07245
59369488 = yrday
fracday
Element set: 904
Inclination: 51
6320 deg
RA of node: 64
4104 deg
Eccentricity:
0008874
Arg of perigee: 319
2307 deg
Mean anomaly: 40
8192 deg
Mean motion: 15
76508943 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2299
Checksum: 309
Coasting Arc #6 (Orbit 2314)
---------------------------------------
Vector Time (GMT): 2007/246/13:32:14
583
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4550849
46 A = 6714639
72 meter
Y = -32907
18 meter E =
0010312
Z = 4940435
31 I = 51
89202
XDOT = -2291
855227 Wp =
08812
YDOT = -7032
339506 meter/sec RA = 58
78366 deg
ZDOT = -2147
864970 TA = 110
72495
MA = 110
61440
Ha = 186
865 n
mi
Hp = 181
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14930608
48 X = -4574143
08
Y = -107963
19 feet Y = -83927
73 meter
Z = 16208777
28 Z = 4918270
63
XDOT = -7519
210062 XDOT = -2202
614250
YDOT = -23071
980008 feet/sec YDOT = -7057
469290 meter/sec
ZDOT = -7046
801084 ZDOT = -2158
782280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14981142
30 X = 4566252
17
Y = -1104688
29 feet Y = -336708
99 meter
Z = 16124646
53 Z = 4914792
26
XDOT = 9236
711913 XDOT = 2815
349791
YDOT = 21300
543346 feet/sec YDOT = 6492
405612 meter/sec
ZDOT = -7089
070626 ZDOT = -2160
748727
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 07246
60792467
00020000 00000-0 20000-3 0 9054
2 25544 51
6323 59
1816 0008642 322
6696 37
3867 15
76465637 23151
Satellite: ISS
Catalog Number: 25544
Epoch time: 07246
60792467 = yrday
fracday
Element set: 905
Inclination: 51
6323 deg
RA of node: 59
1816 deg
Eccentricity:
0008642
Arg of perigee: 322
6696 deg
Mean anomaly: 37
3867 deg
Mean motion: 15
76465637 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2315
Checksum: 317
Coasting Arc #7 (Orbit 2330)
---------------------------------------
Vector Time (GMT): 2007/247/13:32:14
583
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1774361
72 A = 6721836
82 meter
Y = 5911147
74 meter E =
0013161
Z = 2641206
67 I = 51
90250
XDOT = -5603
358185 Wp = 39
88199
YDOT = -667
807653 meter/sec RA = 53
68704 deg
ZDOT = 5254
497534 TA = 350
11452
MA = 350
14038
Ha = 186
814 n
mi
Hp = 180
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5821396
71 X = 1695300
02
Y = 19393529
34 feet Y = 5930547
49 meter
Z = 8665376
20 Z = 2649634
71
XDOT = -18383
721079 XDOT = -5620
999577
YDOT = -2190
969989 feet/sec YDOT = -730
566425 meter/sec
ZDOT = 17239
165137 ZDOT = 5227
233570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7642468
08 X = -2329424
27
Y = -18735602
81 feet Y = -5710611
74 meter
Z = 8698060
33 Z = 2651168
79
XDOT = 17239
770290 XDOT = 5254
681984
YDOT = 929
663540 feet/sec YDOT = 283
361447 meter/sec
ZDOT = 17135
599474 ZDOT = 5222
930720
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 07247
62212909
00020000 00000-0 20000-3 0 9066
2 25544 51
6335 53
9529 0008728 325
7947 34
2654 15
76561290 23315
Satellite: ISS
Catalog Number: 25544
Epoch time: 07247
62212909 = yrday
fracday
Element set: 906
Inclination: 51
6335 deg
RA of node: 53
9529 deg
Eccentricity:
0008728
Arg of perigee: 325
7947 deg
Mean anomaly: 34
2654 deg
Mean motion: 15
76561290 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2331
Checksum: 303
Coasting Arc #8 (Orbit 2345)
---------------------------------------
Vector Time (GMT): 2007/248/13:32:14
583
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5223139
15 A = 6717709
46 meter
Y = 1062080
81 meter E =
0005853
Z = -4087376
76 I = 51
87080
XDOT = 1687
922831 Wp = 26
47572
YDOT = 6460
252429 meter/sec RA = 48
50180 deg
ZDOT = 3842
828965 TA = 282
84627
MA = 282
91165
Ha = 187
122 n
mi
Hp = 180
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17136283
30 X = 5230730
22
Y = 3484517
09 feet Y = 1120531
51 meter
Z = -13410028
75 Z = -4061984
43
XDOT = 5537
804563 XDOT = 1596
890225
YDOT = 21195
053901 feet/sec YDOT = 6478
618586 meter/sec
ZDOT = 12607
706579 ZDOT = 3850
807995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17497820
35 X = -5333335
64
Y = -1483074
30 feet Y = -452041
05 meter
Z = -13313516
04 Z = -4057959
69
XDOT = -7975
127465 XDOT = -2430
818851
YDOT = -19150
113233 feet/sec YDOT = -5836
954513 meter/sec
ZDOT = 12638
748489 ZDOT = 3852
290540
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 07248
57292893
00020000 00000-0 20000-3 0 9072
2 25544 51
6341 49
0517 0008848 330
0564 30
0094 15
76560266 23462
Satellite: ISS
Catalog Number: 25544
Epoch time: 07248
57292893 = yrday
fracday
Element set: 907
Inclination: 51
6341 deg
RA of node: 49
0517 deg
Eccentricity:
0008848
Arg of perigee: 330
0564 deg
Mean anomaly: 30
0094 deg
Mean motion: 15
76560266 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2346
Checksum: 296
Coasting Arc #9 (Orbit 2361)
---------------------------------------
Vector Time (GMT): 2007/249/13:32:14
583
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1060352
73 A = 6717856
01 meter
Y = -5311321
23 meter E =
0010594
Z = -3984288
49 I = 51
85184
XDOT = 6361
187214 Wp = 15
07404
YDOT = 1718
684966 meter/sec RA = 43
41326 deg
ZDOT = -3976
380996 TA = 213
82082
MA = 213
88844
Ha = 187
121 n
mi
Hp = 180
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3478847
53 X = -981527
19
Y = -17425594
59 feet Y = -5322737
84 meter
Z = -13071812
64 Z = -3989248
32
XDOT = 20870
036790 XDOT = 6360
812175
YDOT = 5638
730204 feet/sec YDOT = 1789
817368 meter/sec
ZDOT = -13045
869410 ZDOT = -3945
479548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5676037
04 X = 1730056
09
Y = 16823422
11 feet Y = 5127779
06 meter
Z = -13091259
86 Z = -3990216
00
XDOT = -20277
347801 XDOT = -6180
535610
YDOT = -3238
479472 feet/sec YDOT = -987
088543 meter/sec
ZDOT = -12928
361702 ZDOT = -3940
564647
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 07249
58709322
00020000 00000-0 20000-3 0 9085
2 25544 51
6342 43
8225 0008915 333
8756 26
1958 15
76600402 23620
Satellite: ISS
Catalog Number: 25544
Epoch time: 07249
58709322 = yrday
fracday
Element set: 908
Inclination: 51
6342 deg
RA of node: 43
8225 deg
Eccentricity:
0008915
Arg of perigee: 333
8756 deg
Mean anomaly: 26
1958 deg
Mean motion: 15
76600402 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2362
Checksum: 297
Coasting Arc #10 (Orbit 2377)
---------------------------------------
Vector Time (GMT): 2007/250/13:32:14
583
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5846645
10 A = 6721506
81 meter
Y = -1859156
88 meter E =
0011492
Z = 2745107
17 I = 51
84249
XDOT = -634
568462 Wp = 60
47212
YDOT = -5671
454584 meter/sec RA = 38
22303 deg
ZDOT = -5170
933622 TA = 88
23507
MA = 88
10345
Ha = 187
251 n
mi
Hp = 180
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19181906
48 X = -5838756
24
Y = -6099596
08 feet Y = -1924493
28 meter
Z = 9006257
11 Z = 2716723
71
XDOT = -2081
917525 XDOT = -545
983137
YDOT = -18607
134461 feet/sec YDOT = -5678
055347 meter/sec
ZDOT = -16965
005321 ZDOT = -5173
801179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19926536
40 X = 6073608
29
Y = 3164949
12 feet Y = 964676
49 meter
Z = 8898287
47 Z = 2712198
02
XDOT = 4968
537649 XDOT = 1514
410275
YDOT = 16650
017595 feet/sec YDOT = 5074
925363 meter/sec
ZDOT = -16976
553470 ZDOT = -5174
453498
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
60123569
00020000 00000-0 20000-3 0 9094
2 25544 51
6345 38
5931 0008909 337
9370 22
1410 15
76627950 23781
Satellite: ISS
Catalog Number: 25544
Epoch time: 07250
60123569 = yrday
fracday
Element set: 909
Inclination: 51
6345 deg
RA of node: 38
5931 deg
Eccentricity:
0008909
Arg of perigee: 337
9370 deg
Mean anomaly: 22
1410 deg
Mean motion: 15
76627950 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2378
Checksum: 297
Coasting Arc #11 (Orbit 2393)
---------------------------------------
Vector Time (GMT): 2007/251/13:32:14
583
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -43525
38 A = 6713968
08 meter
Y = 4580666
09 meter E =
0005661
Z = 4904660
10 I = 51
79556
XDOT = -6961
447904 Wp = 25
35058
YDOT = -2447
660449 meter/sec RA = 33
12036 deg
ZDOT = 2228
271360 TA = 43
08737
MA = 43
04306
Ha = 187
316 n
mi
Hp = 179
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -142799
81 X = -118569
44
Y = 15028432
04 feet Y = 4579759
86 meter
Z = 16091404
52 Z = 4904266
29
XDOT = -22839
396009 XDOT = -6944
384794
YDOT = -8030
382050 feet/sec YDOT = -2525
411843 meter/sec
ZDOT = 7310
601574 ZDOT = 2194
494633
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2265277
72 X = -690456
65
Y = -14858449
37 feet Y = -4528855
37 meter
Z = 16090446
23 Z = 4904368
01
XDOT = 22812
386039 XDOT = 6953
215265
YDOT = 4285
192344 feet/sec YDOT = 1306
126627 meter/sec
ZDOT = 7182
085524 ZDOT = 2189
099668
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
61535372
00020000 00000-0 20000-3 0 9107
2 25544 51
6355 33
3636 0009059 341
4805 18
6028 15
76708741 23948
Satellite: ISS
Catalog Number: 25544
Epoch time: 07251
61535372 = yrday
fracday
Element set: 910
Inclination: 51
6355 deg
RA of node: 33
3636 deg
Eccentricity:
0009059
Arg of perigee: 341
4805 deg
Mean anomaly: 18
6028 deg
Mean motion: 15
76708741 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2394
Checksum: 287
Coasting Arc #12 (Orbit 2408)
---------------------------------------
Vector Time (GMT): 2007/252/13:32:14
583
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6203118
54 A = 6724048
98 meter
Y = 2330221
62 meter E =
0017043
Z = -1078742
24 I = 51
80480
XDOT = -799
754579 Wp = 12
37058
YDOT = 4860
201278 meter/sec RA = 27
94783 deg
ZDOT = 5933
243901 TA = 335
83201
MA = 335
91188
Ha = 187
574 n
mi
Hp = 179
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20351438
78 X = 6181840
89
Y = 7645084
07 feet Y = 2399469
38 meter
Z = -3539180
59 Z = -1048659
67
XDOT = -2623
866730 XDOT = -882
864892
YDOT = 15945
542250 feet/sec YDOT = 4850
793534 meter/sec
ZDOT = 19466
023297 ZDOT = 5929
156661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21425959
92 X = -6530632
58
Y = -3788644
40 feet Y = -1154778
81 meter
Z = -3424702
21 Z = -1043849
23
XDOT = -506
814594 XDOT = -154
477088
YDOT = -14613
918057 feet/sec YDOT = -4454
322224 meter/sec
ZDOT = 19451
078588 ZDOT = 5928
688754
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
56607122
00020000 00000-0 20000-3 0 9116
2 25544 51
6360 28
4615 0009234 345
9992 14
0915 15
76693298 24099
Satellite: ISS
Catalog Number: 25544
Epoch time: 07252
56607122 = yrday
fracday
Element set: 911
Inclination: 51
6360 deg
RA of node: 28
4615 deg
Eccentricity:
0009234
Arg of perigee: 345
9992 deg
Mean anomaly: 14
0915 deg
Mean motion: 15
76693298 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2409
Checksum: 297
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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