Date:
June 3rd 2008
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) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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 2626)
---------------------------------------
Vector Time (GMT): 2008/154/20:09:40
924
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3260371
81 A = 6716823
29 meter
Y = 4102160
54 meter E =
0004388
Z = 4199201
46 I = 51
95529
XDOT = -2923
542501 Wp = 104
02406
YDOT = -6102
091879 meter/sec RA = 89
64036 deg
ZDOT = 3686
932456 TA = 308
54270
MA = 308
58201
Ha = 184
427 n
mi
Hp = 181
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10696757
90 X = -3326399
84
Y = 13458531
94 feet Y = 4065331
19 meter
Z = 13776907
66 Z = 4183202
68
XDOT = -9591
674873 XDOT = -2873
001453
YDOT = -20019
986481 feet/sec YDOT = -6134
502734 meter/sec
ZDOT = 12096
235093 ZDOT = 3672
851189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7380816
67 X = 2249672
92
Y = -15580717
37 feet Y = -4749002
66 meter
Z = 13715709
53 Z = 4180548
26
XDOT = 12880
769954 XDOT = 3926
058682
YDOT = 16714
219991 feet/sec YDOT = 5094
494253 meter/sec
ZDOT = 12041
509503 ZDOT = 3670
252096
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 08154
89418808
00020000 00000-0 20000-3 0 9003
2 25544 51
6342 90
0830 0005842 287
4672 72
5854 15
76719797 26275
Satellite: ISS
Catalog Number: 25544
Epoch time: 08154
89418808 = yrday
fracday
Element set: 900
Inclination: 51
6342 deg
RA of node: 90
0830 deg
Eccentricity:
0005842
Arg of perigee: 287
4672 deg
Mean anomaly: 72
5854 deg
Mean motion: 15
76719797 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2627
Checksum: 320
Coasting Arc #2 (Orbit 2641)
---------------------------------------
Vector Time (GMT): 2008/155/20:09:40
924
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2476275
06 A = 6721870
91 meter
Y = 5747797
53 meter E =
0005852
Z = -2442015
02 I = 51
97187
XDOT = -3848
533305 Wp = 347
81813
YDOT = 3944
439326 meter/sec RA = 84
46029 deg
ZDOT = 5384
815376 TA = 344
70025
MA = 344
71794
Ha = 184
543 n
mi
Hp = 181
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8124262
01 X = 2423681
26
Y = 18857603
44 feet Y = 5775195
12 meter
Z = -8011860
30 Z = -2430111
60
XDOT = -12626
421603 XDOT = -3918
513407
YDOT = 12941
073903 feet/sec YDOT = 3901
010359 meter/sec
ZDOT = 17666
717113 ZDOT = 5365
949840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12579813
45 X = -3834327
14
Y = -16251185
07 feet Y = -4953361
21 meter
Z = -7965552
31 Z = -2427900
34
XDOT = 7945
791431 XDOT = 2421
877228
YDOT = -14769
394768 feet/sec YDOT = -4501
711525 meter/sec
ZDOT = 17594
458684 ZDOT = 5362
791007
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 08155
84489178
00020000 00000-0 20000-3 0 9018
2 25544 51
6352 85
1804 0005638 290
9027 69
1533 15
76720173 26421
Satellite: ISS
Catalog Number: 25544
Epoch time: 08155
84489178 = yrday
fracday
Element set: 901
Inclination: 51
6352 deg
RA of node: 85
1804 deg
Eccentricity:
0005638
Arg of perigee: 290
9027 deg
Mean anomaly: 69
1533 deg
Mean motion: 15
76720173 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2642
Checksum: 301
Coasting Arc #3 (Orbit 2657)
---------------------------------------
Vector Time (GMT): 2008/156/20:09:40
924
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3513274
15 A = 6713316
42 meter
Y = -2706736
86 meter E =
0009735
Z = -5048068
00 I = 51
93994
XDOT = 2751
067778 Wp = 55
45946
YDOT = 6957
638195 meter/sec RA = 79
36349 deg
ZDOT = -1813
050564 TA = 197
11968
MA = 197
15254
Ha = 184
625 n
mi
Hp = 181
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11526490
00 X = 3567802
92
Y = -8880370
28 feet Y = -2667143
38 meter
Z = -16561902
89 Z = -5030868
59
XDOT = 9025
812921 XDOT = 2681
869423
YDOT = 22826
896965 feet/sec YDOT = 6988
015715 meter/sec
ZDOT = -5948
328623 ZDOT = -1799
852295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8864523
68 X = -2701906
82
Y = 11632791
59 feet Y = 3545674
88 meter
Z = -16495937
54 Z = -5027961
76
XDOT = -13915
150234 XDOT = -4241
337791
YDOT = -18979
655883 feet/sec YDOT = -5784
999113 meter/sec
ZDOT = -5896
936040 ZDOT = -1797
386105
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 08156
85896198
00020000 00000-0 20000-3 0 9025
2 25544 51
6359 79
9522 0005522 295
6154 64
4439 15
76760492 26589
Satellite: ISS
Catalog Number: 25544
Epoch time: 08156
85896198 = yrday
fracday
Element set: 902
Inclination: 51
6359 deg
RA of node: 79
9522 deg
Eccentricity:
0005522
Arg of perigee: 295
6154 deg
Mean anomaly: 64
4439 deg
Mean motion: 15
76760492 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2658
Checksum: 336
Coasting Arc #4 (Orbit 2673)
---------------------------------------
Vector Time (GMT): 2008/157/20:09:40
924
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2315794
56 A = 6724057
79 meter
Y = -6273069
40 meter E =
0007706
Z = 666202
69 I = 51
96921
XDOT = 4265
673055 Wp = 134
64781
YDOT = -2217
950505 meter/sec RA = 74
20692 deg
ZDOT = -6019
671925 TA = 38
12175
MA = 38
06726
Ha = 184
730 n
mi
Hp = 181
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7597751
17 X = -2248712
28
Y = -20580936
37 feet Y = -6298591
01 meter
Z = 2185704
37 Z = 655114
15
XDOT = 13994
990338 XDOT = 4319
399913
YDOT = -7276
740502 feet/sec YDOT = -2169
947588 meter/sec
ZDOT = -19749
579805 ZDOT = -5998
819300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13077566
93 X = 3986042
40
Y = 17620018
31 feet Y = 5370581
58 meter
Z = 2142490
61 Z = 653031
14
XDOT = -10214
857914 XDOT = -3113
488692
YDOT = 9988
193193 feet/sec YDOT = 3044
401285 meter/sec
ZDOT = -19669
501743 ZDOT = -5995
264131
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 08157
87301752
00020000 00000-0 20000-3 0 9036
2 25544 51
6353 74
7219 0005770 299
5053 60
5536 15
76792522 26747
Satellite: ISS
Catalog Number: 25544
Epoch time: 08157
87301752 = yrday
fracday
Element set: 903
Inclination: 51
6353 deg
RA of node: 74
7219 deg
Eccentricity:
0005770
Arg of perigee: 299
5053 deg
Mean anomaly: 60
5536 deg
Mean motion: 15
76792522 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2674
Checksum: 305
Coasting Arc #5 (Orbit 2689)
---------------------------------------
Vector Time (GMT): 2008/158/20:09:40
924
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3986053
85 A = 6712309
22 meter
Y = 1154083
43 meter E =
0004297
Z = 5277881
99 I = 51
92045
XDOT = -2521
009555 Wp = 329
24401
YDOT = -7273
489103 meter/sec RA = 69
07539 deg
ZDOT = -310
005687 TA = 123
70664
MA = 123
66567
Ha = 185
051 n
mi
Hp = 181
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13077604
48 X = -4024301
57
Y = 3786362
96 feet Y = 1109294
20 meter
Z = 17315885
81 Z = 5258425
19
XDOT = -8271
028723 XDOT = -2437
982945
YDOT = -23863
153225 feet/sec YDOT = -7301
216188 meter/sec
ZDOT = -1017
079027 ZDOT = -322
052438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11457149
93 X = 3492139
30
Y = -7528541
68 feet Y = -2294699
51 meter
Z = 17241083
51 Z = 5255082
25
XDOT = 14429
932495 XDOT = 4398
243424
YDOT = 19496
626536 feet/sec YDOT = 5942
571768 meter/sec
ZDOT = -1064
067463 ZDOT = -324
327763
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 08158
88706346
00020000 00000-0 20000-3 0 9047
2 25544 51
6358 69
4923 0005535 303
4595 56
6040 15
76749732 26909
Satellite: ISS
Catalog Number: 25544
Epoch time: 08158
88706346 = yrday
fracday
Element set: 904
Inclination: 51
6358 deg
RA of node: 69
4923 deg
Eccentricity:
0005535
Arg of perigee: 303
4595 deg
Mean anomaly: 56
6040 deg
Mean motion: 15
76749732 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2690
Checksum: 318
Coasting Arc #6 (Orbit 2705)
---------------------------------------
Vector Time (GMT): 2008/159/20:09:40
924
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2026262
03 A = 6723510
87 meter
Y = 6288661
59 meter E =
0012821
Z = 1202002
74 I = 51
94849
XDOT = -4927
680483 Wp = 34
66802
YDOT = 454
087473 meter/sec RA = 63
95380 deg
ZDOT = 5910
835428 TA = 338
47019
MA = 338
52406
Ha = 184
930 n
mi
Hp = 181
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6647841
32 X = 1949951
57
Y = 20632091
84 feet Y = 6310893
54 meter
Z = 3943578
55 Z = 1211661
96
XDOT = -16166
930720 XDOT = -4961
105467
YDOT = 1489
788296 feet/sec YDOT = 398
795435 meter/sec
ZDOT = 19392
504684 ZDOT = 5886
815827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12756737
82 X = -3888253
69
Y = -17516956
20 feet Y = -5339168
25 meter
Z = 3981294
42 Z = 1213498
54
XDOT = 13713
167146 XDOT = 4179
773346
YDOT = -5585
110127 feet/sec YDOT = -1702
341567 meter/sec
ZDOT = 19300
073006 ZDOT = 5882
662252
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 08159
90109135
00020000 00000-0 20000-3 0 9055
2 25544 51
6370 64
2629 0005536 305
4877 54
5771 15
76827693 27064
Satellite: ISS
Catalog Number: 25544
Epoch time: 08159
90109135 = yrday
fracday
Element set: 905
Inclination: 51
6370 deg
RA of node: 64
2629 deg
Eccentricity:
0005536
Arg of perigee: 305
4877 deg
Mean anomaly: 54
5771 deg
Mean motion: 15
76827693 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2706
Checksum: 311
Coasting Arc #7 (Orbit 2720)
---------------------------------------
Vector Time (GMT): 2008/160/20:09:40
924
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4638711
18 A = 6713999
69 meter
Y = 318561
12 meter E =
0007123
Z = -4849490
83 I = 51
90242
XDOT = 2039
917032 Wp = 89
95065
YDOT = 7021
054065 meter/sec RA = 58
78698 deg
ZDOT = 2415
498628 TA = 203
52497
MA = 203
55756
Ha = 185
161 n
mi
Hp = 181
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15218868
72 X = 4658362
01
Y = 1045148
02 feet Y = 370544
42 meter
Z = -15910402
99 Z = -4826908
34
XDOT = 6692
641181 XDOT = 1949
520913
YDOT = 23034
954282 feet/sec YDOT = 7043
359801 meter/sec
ZDOT = 7924
864266 ZDOT = 2425
189936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14798079
44 X = -4510454
61
Y = 4059918
66 feet Y = 1237463
21 meter
Z = -15823436
04 Z = -4822983
30
XDOT = -13573
079274 XDOT = -4137
074563
YDOT = -18477
122018 feet/sec YDOT = -5631
826791 meter/sec
ZDOT = 7962
765641 ZDOT = 2427
050968
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 08160
85173337
00020000 00000-0 20000-3 0 9067
2 25544 51
6371 59
3609 0005612 309
6881 50
3789 15
76826581 27219
Satellite: ISS
Catalog Number: 25544
Epoch time: 08160
85173337 = yrday
fracday
Element set: 906
Inclination: 51
6371 deg
RA of node: 59
3609 deg
Eccentricity:
0005612
Arg of perigee: 309
6881 deg
Mean anomaly: 50
3789 deg
Mean motion: 15
76826581 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2721
Checksum: 308
Coasting Arc #8 (Orbit 2736)
---------------------------------------
Vector Time (GMT): 2008/161/20:09:40
924
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1435304
53 A = 6720267
76 meter
Y = -5864359
85 meter E =
0002242
Z = -2954408
14 I = 51
90776
XDOT = 5722
006359 Wp = 2
89013
YDOT = 1132
860097 meter/sec RA = 53
69096 deg
ZDOT = -5026
500455 TA = 211
06132
MA = 211
07457
Ha = 185
209 n
mi
Hp = 180
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4709004
38 X = -1355269
74
Y = -19240025
77 feet Y = -5879962
37 meter
Z = -9692940
11 Z = -2961187
18
XDOT = 18772
986741 XDOT = 5733
330998
YDOT = 3716
732601 feet/sec YDOT = 1196
910818 meter/sec
ZDOT = -16491
143226 ZDOT = -4998
675400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11020401
29 X = 3359018
31
Y = 16443475
36 feet Y = 5011971
29 meter
Z = -9719530
61 Z = -2962512
93
XDOT = -17788
768151 XDOT = -5422
016533
YDOT = 2233
765746 feet/sec YDOT = 680
851799 meter/sec
ZDOT = -16383
923630 ZDOT = -4993
819923
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 08161
86573786
00020000 00000-0 20000-3 0 9072
2 25544 51
6373 54
1304 0005655 313
6255 46
4440 15
76844318 27378
Satellite: ISS
Catalog Number: 25544
Epoch time: 08161
86573786 = yrday
fracday
Element set: 907
Inclination: 51
6373 deg
RA of node: 54
1304 deg
Eccentricity:
0005655
Arg of perigee: 313
6255 deg
Mean anomaly: 46
4440 deg
Mean motion: 15
76844318 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2737
Checksum: 302
Coasting Arc #9 (Orbit 2752)
---------------------------------------
Vector Time (GMT): 2008/162/20:09:40
924
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5334747
92 A = 6718004
02 meter
Y = -1568621
69 meter E =
0009549
Z = 3767787
17 I = 51
88210
XDOT = -1147
963242 Wp = 54
65752
YDOT = -6325
223293 meter/sec RA = 48
50163 deg
ZDOT = -4245
818784 TA = 79
86328
MA = 79
75558
Ha = 185
389 n
mi
Hp = 180
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17502453
81 X = -5335114
08
Y = -5146396
64 feet Y = -1628280
41 meter
Z = 12361506
46 Z = 3741869
88
XDOT = -3766
283602 XDOT = -1056
522861
YDOT = -20752
044923 feet/sec YDOT = -6337
548691 meter/sec
ZDOT = -13929
851654 ZDOT = -4251
174248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18243906
73 X = 5560742
77
Y = -1562449
27 feet Y = -476234
54 meter
Z = 12261596
51 Z = 3737334
62
XDOT = 10833
619078 XDOT = 3302
087095
YDOT = 16680
568295 feet/sec YDOT = 5084
237216 meter/sec
ZDOT = -13950
996216 ZDOT = -4252
263647
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 08162
87973006
00020000 00000-0 20000-3 0 9084
2 25544 51
6379 48
9008 0005604 317
5526 42
5205 15
76844594 27534
Satellite: ISS
Catalog Number: 25544
Epoch time: 08162
87973006 = yrday
fracday
Element set: 908
Inclination: 51
6379 deg
RA of node: 48
9008 deg
Eccentricity:
0005604
Arg of perigee: 317
5526 deg
Mean anomaly: 42
5205 deg
Mean motion: 15
76844594 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2753
Checksum: 310
Coasting Arc #10 (Orbit 2768)
---------------------------------------
Vector Time (GMT): 2008/163/20:09:40
924
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 463001
45 A = 6715707
30 meter
Y = 5112782
98 meter E =
0005615
Z = 4324195
99 I = 51
85597
XDOT = -6463
606462 Wp = 76
43571
YDOT = -2356
702983 meter/sec RA = 43
41078 deg
ZDOT = 3476
104978 TA = 338
56413
MA = 338
58764
Ha = 185
407 n
mi
Hp = 180
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1519033
64 X = 384788
85
Y = 16774222
39 feet Y = 5117522
69 meter
Z = 14186994
72 Z = 4326255
91
XDOT = -21206
057947 XDOT = -6453
659403
YDOT = -7731
965167 feet/sec YDOT = -2428
927542 meter/sec
ZDOT = 11404
543892 ZDOT = 3444
728519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7670584
14 X = -2337994
04
Y = -14986897
73 feet Y = -4568006
43 meter
Z = 14195346
23 Z = 4326741
53
XDOT = 21522
427086 XDOT = 6560
035776
YDOT = -320
374099 feet/sec YDOT = -97
650025 meter/sec
ZDOT = 11283
554251 ZDOT = 3439
227336
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 08163
89370679
00020000 00000-0 20000-3 0 9095
2 25544 51
6390 43
6709 0005741 321
0419 39
0331 15
76918649 27691
Satellite: ISS
Catalog Number: 25544
Epoch time: 08163
89370679 = yrday
fracday
Element set: 909
Inclination: 51
6390 deg
RA of node: 43
6709 deg
Eccentricity:
0005741
Arg of perigee: 321
0419 deg
Mean anomaly: 39
0331 deg
Mean motion: 15
76918649 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2769
Checksum: 318
Coasting Arc #11 (Orbit 2783)
---------------------------------------
Vector Time (GMT): 2008/164/20:09:40
924
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5865438
01 A = 6721966
08 meter
Y = 2435900
23 meter E =
0009635
Z = -2184468
14 I = 51
85466
XDOT = -180
962172 Wp = 4
82281
YDOT = 5375
704558 meter/sec RA = 38
22499 deg
ZDOT = 5519
699219 TA = 330
74811
MA = 330
80202
Ha = 185
734 n
mi
Hp = 180
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19243563
04 X = 5848375
29
Y = 7991798
66 feet Y = 2501395
81 meter
Z = -7166890
23 Z = -2156014
74
XDOT = -593
707915 XDOT = -267
874602
YDOT = 17636
825978 feet/sec YDOT = 5373
194249 meter/sec
ZDOT = 18109
249406 ZDOT = 5518
609701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20873026
92 X = -6362098
61
Y = 247473
60 feet Y = 75429
95 meter
Z = -7057151
24 Z = -2151019
70
XDOT = -6286
312411 XDOT = -1916
068023
YDOT = -14964
311439 feet/sec YDOT = -4561
122127 meter/sec
ZDOT = 18105
491577 ZDOT = 5518
553833
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 08164
84430126
00020000 00000-0 20000-3 0 9107
2 25544 51
6393 38
7687 0005920 325
9455 34
1329 15
76881290 27847
Satellite: ISS
Catalog Number: 25544
Epoch time: 08164
84430126 = yrday
fracday
Element set: 910
Inclination: 51
6393 deg
RA of node: 38
7687 deg
Eccentricity:
0005920
Arg of perigee: 325
9455 deg
Mean anomaly: 34
1329 deg
Mean motion: 15
76881290 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2784
Checksum: 306
Coasting Arc #12 (Orbit 2799)
---------------------------------------
Vector Time (GMT): 2008/165/20:09:40
924
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 873409
28 A = 6712444
32 meter
Y = -4251334
03 meter E =
0013210
Z = -5131337
29 I = 51
79945
XDOT = 6878
410980 Wp = 54
28666
YDOT = 3143
732361 meter/sec RA = 33
11256 deg
ZDOT = -1428
816221 TA = 202
02065
MA = 202
07746
Ha = 185
692 n
mi
Hp = 180
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2865516
02 X = 945810
81
Y = -13947946
29 feet Y = -4241161
48 meter
Z = -16835096
10 Z = -5126919
00
XDOT = 22566
965159 XDOT = 6849
687048
YDOT = 10314
082549 feet/sec YDOT = 3220
490302 meter/sec
ZDOT = -4687
717261 ZDOT = -1395
469860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3010405
37 X = 917571
56
Y = 13937533
60 feet Y = 4248160
24 meter
Z = -16818426
36 Z = -5126256
35
XDOT = -23819
379239 XDOT = -7260
146792
YDOT = -376
450751 feet/sec YDOT = -114
742189 meter/sec
ZDOT = -4559
087863 ZDOT = -1389
609980
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 08165
85825515
00020000 00000-0 20000-3 0 9110
2 25544 51
6396 33
5394 0005900 328
9501 31
1314 15
76916546 28004
Satellite: ISS
Catalog Number: 25544
Epoch time: 08165
85825515 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 33
5394 deg
Eccentricity:
0005900
Arg of perigee: 328
9501 deg
Mean anomaly: 31
1314 deg
Mean motion: 15
76916546 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2800
Checksum: 286
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
http://www aus-city com/cgi-bin/dada/mail cgi/u/[list]/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
http://www aus-city com/cgi-bin/dada/mail cgi/list/[list]
If you're still having trouble, please contact the list owner at:
<mailto:list
admin@aus-city
com>
The following physical address is associated with this mailing list:
http://www aus-city com
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list