Date:
November 29th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8180 57 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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 3669)
---------------------------------------
Vector Time (GMT): 2007/332/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5914557
53 A = 6723936
07 meter
Y = -3132922
77 meter E =
0010089
Z = -592811
75 I = 51
52693
XDOT = 2716
683253 Wp = 40
13993
YDOT = 4006
648557 meter/sec RA = 336
12605 deg
ZDOT = 5994
125375 TA = 313
38963
MA = 313
47360
Ha = 185
522 n
mi
Hp = 179
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19404716
32 X = 5952030
56
Y = -10278618
00 feet Y = -3066573
24 meter
Z = -1944920
45 Z = -563988
05
XDOT = 8913
002800 XDOT = 2642
559854
YDOT = 13145
172430 feet/sec YDOT = 4036
612821 meter/sec
ZDOT = 19665
765666 ZDOT = 6007
143574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4449544
75 X = 1356221
24
Y = 21512982
32 feet Y = 6557157
01 meter
Z = -1835446
06 Z = -559443
96
XDOT = -13511
067071 XDOT = -4118
173243
YDOT = 4457
633762 feet/sec YDOT = 1358
686771 meter/sec
ZDOT = 19715
732615 ZDOT = 6009
355301
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 07332
52190962
00020000 00000-0 20000-3 0 9008
2 25544 51
6385 336
6337 0000947 223
2235 136
8855 15
76850596 36704
Satellite: ISS
Catalog Number: 25544
Epoch time: 07332
52190962 = yrday
fracday
Element set: 900
Inclination: 51
6385 deg
RA of node: 336
6337 deg
Eccentricity:
0000947
Arg of perigee: 223
2235 deg
Mean anomaly: 136
8855 deg
Mean motion: 15
76850596 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3670
Checksum: 304
Coasting Arc #2 (Orbit 3685)
---------------------------------------
Vector Time (GMT): 2007/333/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1615384
49 A = 6712159
32 meter
Y = -3881544
17 meter E =
0014244
Z = -5244582
93 I = 51
46008
XDOT = 6874
495055 Wp = 95
01024
YDOT = -3432
031191 meter/sec RA = 330
95984 deg
ZDOT = 422
409227 TA = 179
01547
MA = 179
01266
Ha = 185
508 n
mi
Hp = 179
649
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5299817
87 X = -1546383
07
Y = -12734724
96 feet Y = -3899221
95 meter
Z = -17206636
90 Z = -5252263
31
XDOT = 22554
117636 XDOT = 6910
309624
YDOT = -11259
944854 feet/sec YDOT = -3354
956488 meter/sec
ZDOT = 1385
857044 ZDOT = 455
892296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13654044
47 X = 4161752
75
Y = -1675650
89 feet Y = -510738
39 meter
Z = -17236267
19 Z = -5253614
24
XDOT = 4821
478979 XDOT = 1469
586793
YDOT = 23715
988414 feet/sec YDOT = 7228
633269 meter/sec
ZDOT = 1513
049486 ZDOT = 461
177483
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 07333
53592405
00020000 00000-0 20000-3 0 9019
2 25544 51
6378 331
4036 0000856 242
3677 117
7401 15
76815834 36864
Satellite: ISS
Catalog Number: 25544
Epoch time: 07333
53592405 = yrday
fracday
Element set: 901
Inclination: 51
6378 deg
RA of node: 331
4036 deg
Eccentricity:
0000856
Arg of perigee: 242
3677 deg
Mean anomaly: 117
7401 deg
Mean motion: 15
76815834 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3686
Checksum: 295
Coasting Arc #3 (Orbit 3701)
---------------------------------------
Vector Time (GMT): 2007/334/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5972010
88 A = 6723202
19 meter
Y = 2777892
65 meter E =
0008590
Z = -1329391
68 I = 51
47298
XDOT = -1001
946407 Wp = 147
22692
YDOT = -4933
314501 meter/sec RA = 325
80667 deg
ZDOT = -5832
223921 TA = 47
42224
MA = 47
34979
Ha = 185
404 n
mi
Hp = 179
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19593211
53 X = -5996171
86
Y = 9113821
04 feet Y = 2710975
26 meter
Z = -4361521
28 Z = -1358462
31
XDOT = -3287
225744 XDOT = -918
374841
YDOT = -16185
415028 feet/sec YDOT = -4944
051066 meter/sec
ZDOT = -19134
592917 ZDOT = -5836
888824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4020288
00 X = -1225383
78
Y = -21208896
71 feet Y = -6464471
72 meter
Z = -4471971
03 Z = -1363056
77
XDOT = 14923
547223 XDOT = 4548
697194
YDOT = 1192
977922 feet/sec YDOT = 363
619671 meter/sec
ZDOT = -19152
845644 ZDOT = -5837
787352
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 07334
54991525
00020000 00000-0 20000-3 0 9028
2 25544 51
6375 326
1736 0000741 249
7870 110
3215 15
76873086 37022
Satellite: ISS
Catalog Number: 25544
Epoch time: 07334
54991525 = yrday
fracday
Element set: 902
Inclination: 51
6375 deg
RA of node: 326
1736 deg
Eccentricity:
0000741
Arg of perigee: 249
7870 deg
Mean anomaly: 110
3215 deg
Mean motion: 15
76873086 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3702
Checksum: 292
Coasting Arc #4 (Orbit 3717)
---------------------------------------
Vector Time (GMT): 2007/335/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 186910
76 A = 6714064
72 meter
Y = 4743999
07 meter E =
0006646
Z = 4744017
38 I = 51
41853
XDOT = -6688
618729 Wp = 58
10838
YDOT = 2840
072800 meter/sec RA = 320
60206 deg
ZDOT = -2570
447379 TA = 57
17575
MA = 57
11177
Ha = 185
302 n
mi
Hp = 179
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 613224
28 X = 110803
00
Y = 15564301
42 feet Y = 4745663
34 meter
Z = 15564361
49 Z = 4744740
87
XDOT = -21944
287169 XDOT = -6707
392878
YDOT = 9317
824148 feet/sec YDOT = 2765
172083 meter/sec
ZDOT = -8433
226308 ZDOT = -2602
986338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15270142
43 X = -4654339
41
Y = -3057095
72 feet Y = -931802
78 meter
Z = 15567587
71 Z = 4745000
73
XDOT = -4272
245244 XDOT = -1302
180350
YDOT = -22335
913344 feet/sec YDOT = -6807
986387 meter/sec
ZDOT = -8556
877911 ZDOT = -2608
136387
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 07335
56388250
00020000 00000-0 20000-3 0 9037
2 25544 51
6370 320
9438 0000877 259
4517 100
6549 15
76912353 37184
Satellite: ISS
Catalog Number: 25544
Epoch time: 07335
56388250 = yrday
fracday
Element set: 903
Inclination: 51
6370 deg
RA of node: 320
9438 deg
Eccentricity:
0000877
Arg of perigee: 259
4517 deg
Mean anomaly: 100
6549 deg
Mean motion: 15
76912353 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3718
Checksum: 303
Coasting Arc #5 (Orbit 3733)
---------------------------------------
Vector Time (GMT): 2007/336/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5598855
30 A = 6719472
18 meter
Y = -2058225
60 meter E =
0012156
Z = 3081758
36 I = 51
41620
XDOT = -504
021867 Wp = 85
96603
YDOT = 5950
082469 meter/sec RA = 315
47417 deg
ZDOT = 4873
968947 TA = 309
99051
MA = 310
09717
Ha = 185
120 n
mi
Hp = 179
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18368947
83 X = 5606483
78
Y = -6752708
66 feet Y = -1995573
57 meter
Z = 10110755
77 Z = 3108976
30
XDOT = -1653
615048 XDOT = -594
196254
YDOT = 19521
267944 feet/sec YDOT = 5943
941712 meter/sec
ZDOT = 15990
711767 ZDOT = 4871
301721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2707304
03 X = 825186
27
Y = 19328346
66 feet Y = 5891280
06 meter
Z = 10214216
62 Z = 3113293
23
XDOT = -17295
414295 XDOT = -5271
642277
YDOT = -6049
631419 feet/sec YDOT = -1843
927657 meter/sec
ZDOT = 15981
146823 ZDOT = 4871
053552
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 07336
57782533
00020000 00000-0 20000-3 0 9042
2 25544 51
6371 315
7143 0000949 254
7174 105
3886 15
76984824 37343
Satellite: ISS
Catalog Number: 25544
Epoch time: 07336
57782533 = yrday
fracday
Element set: 904
Inclination: 51
6371 deg
RA of node: 315
7143 deg
Eccentricity:
0000949
Arg of perigee: 254
7174 deg
Mean anomaly: 105
3886 deg
Mean motion: 15
76984824 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3734
Checksum: 317
Coasting Arc #6 (Orbit 3748)
---------------------------------------
Vector Time (GMT): 2007/337/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 985788
43 A = 6718172
61 meter
Y = -5597443
37 meter E =
0004650
Z = -3586613
01 I = 51
39140
XDOT = 6076
014522 Wp = 98
97949
YDOT = -1744
275970 meter/sec RA = 310
24743 deg
ZDOT = 4396
335405 TA = 217
94629
MA = 217
97907
Ha = 185
274 n
mi
Hp = 179
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3234214
02 X = 1065730
01
Y = -18364315
53 feet Y = -5585972
52 meter
Z = -11767103
06 Z = -3581630
16
XDOT = 19934
430847 XDOT = 6073
710771
YDOT = -5722
690189 feet/sec YDOT = -1676
343697 meter/sec
ZDOT = 14423
672588 ZDOT = 4425
847422
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17363580
62 X = 5292419
37
Y = 6829890
11 feet Y = 2081750
50 meter
Z = -11748685
41 Z = -3580999
31
XDOT = 2225
778467 XDOT = 678
417277
YDOT = 19322
551858 feet/sec YDOT = 5889
513806 meter/sec
ZDOT = 14535
900959 ZDOT = 4430
542612
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 07337
52837795
00020000 00000-0 20000-3 0 9050
2 25544 51
6369 310
8106 0000780 272
2324 87
8751 15
76959241 37496
Satellite: ISS
Catalog Number: 25544
Epoch time: 07337
52837795 = yrday
fracday
Element set: 905
Inclination: 51
6369 deg
RA of node: 310
8106 deg
Eccentricity:
0000780
Arg of perigee: 272
2324 deg
Mean anomaly: 87
8751 deg
Mean motion: 15
76959241 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3749
Checksum: 318
Coasting Arc #7 (Orbit 3764)
---------------------------------------
Vector Time (GMT): 2007/338/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4957508
32 A = 6714841
54 meter
Y = 856777
06 meter E =
0009120
Z = -4456390
29 I = 51
36360
XDOT = 1680
095530 Wp = 67
03752
YDOT = -6806
185649 meter/sec RA = 305
11945 deg
ZDOT = -3179
213827 TA = 171
05045
MA = 171
03418
Ha = 185
165 n
mi
Hp = 179
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16264791
07 X = -4945071
73
Y = 2810948
37 feet Y = 801409
27 meter
Z = -14620703
05 Z = -4480444
04
XDOT = 5512
124442 XDOT = 1771
522795
YDOT = -22330
005411 feet/sec YDOT = -6786
886435 meter/sec
ZDOT = -10430
491558 ZDOT = -3170
830198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 127033
90 X = 38719
93
Y = -16423882
98 feet Y = -5005999
53 meter
Z = -14712231
20 Z = -4484288
07
XDOT = 19776
814918 XDOT = 6027
973187
YDOT = 9463
615828 feet/sec YDOT = 2884
510104 meter/sec
ZDOT = -10399
243037 ZDOT = -3169
689278
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 07338
54227612
00020000 00000-0 20000-3 0 9065
2 25544 51
6374 305
5798 0000800 275
2757 84
8317 15
77017035 37656
Satellite: ISS
Catalog Number: 25544
Epoch time: 07338
54227612 = yrday
fracday
Element set: 906
Inclination: 51
6374 deg
RA of node: 305
5798 deg
Eccentricity:
0000800
Arg of perigee: 275
2757 deg
Mean anomaly: 84
8317 deg
Mean motion: 15
77017035 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3765
Checksum: 303
Coasting Arc #8 (Orbit 3780)
---------------------------------------
Vector Time (GMT): 2007/339/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1851030
48 A = 6722031
78 meter
Y = 6184750
19 meter E =
0013323
Z = 1850179
87 I = 51
37262
XDOT = -5260
142956 Wp = 114
29580
YDOT = 118
585959 meter/sec RA = 299
90052 deg
ZDOT = -5632
611116 TA = 45
05450
MA = 44
94652
Ha = 185
113 n
mi
Hp = 179
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6072934
64 X = -1929039
75
Y = 20291175
15 feet Y = 6163614
57 meter
Z = 6070143
94 Z = 1840998
45
XDOT = -17257
686862 XDOT = -5233
715270
YDOT = 389
061545 feet/sec YDOT = 59
912335 meter/sec
ZDOT = -18479
695262 ZDOT = -5658
101228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19035585
29 X = -5802046
40
Y = -9309922
63 feet Y = -2837664
42 meter
Z = 6035793
63 Z = 1839709
90
XDOT = 1712
718987 XDOT = 522
036747
YDOT = -15601
962482 feet/sec YDOT = -4755
478164 meter/sec
ZDOT = -18576
769161 ZDOT = -5662
199240
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 07339
55615044
00020000 00000-0 20000-3 0 9078
2 25544 51
6376 300
3493 0000842 281
8882 78
2188 15
77052900 37812
Satellite: ISS
Catalog Number: 25544
Epoch time: 07339
55615044 = yrday
fracday
Element set: 907
Inclination: 51
6376 deg
RA of node: 300
3493 deg
Eccentricity:
0000842
Arg of perigee: 281
8882 deg
Mean anomaly: 78
2188 deg
Mean motion: 15
77052900 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3781
Checksum: 302
Coasting Arc #9 (Orbit 3796)
---------------------------------------
Vector Time (GMT): 2007/340/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4216598
99 A = 6711541
68 meter
Y = 734332
45 meter E =
0002644
Z = 5168188
45 I = 51
32519
XDOT = -2468
152209 Wp = 129
45561
YDOT = 7235
443783 meter/sec RA = 294
74690 deg
ZDOT = 983
649746 TA = 311
12501
MA = 311
14783
Ha = 184
843 n
mi
Hp = 179
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13833986
18 X = 4182967
50
Y = 2409227
19 feet Y = 781296
24 meter
Z = 16955998
85 Z = 5188591
53
XDOT = -8097
612234 XDOT = -2553
655098
YDOT = 23738
332622 feet/sec YDOT = 7207
365327 meter/sec
ZDOT = 3227
197328 ZDOT = 971
452300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4373262
48 X = -1332970
40
Y = 13244402
33 feet Y = 4036893
83 meter
Z = 17033784
91 Z = 5191897
64
XDOT = -21347
069686 XDOT = -6506
586840
YDOT = -11148
826900 feet/sec YDOT = -3398
162439 meter/sec
ZDOT = 3181
462332 ZDOT = 969
709719
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 07340
56999976
00020000 00000-0 20000-3 0 9081
2 25544 51
6383 295
1193 0000971 282
7236 77
3820 15
77115931 37978
Satellite: ISS
Catalog Number: 25544
Epoch time: 07340
56999976 = yrday
fracday
Element set: 908
Inclination: 51
6383 deg
RA of node: 295
1193 deg
Eccentricity:
0000971
Arg of perigee: 282
7236 deg
Mean anomaly: 77
3820 deg
Mean motion: 15
77115931 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3797
Checksum: 331
Coasting Arc #10 (Orbit 3812)
---------------------------------------
Vector Time (GMT): 2007/341/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2383949
03 A = 6723266
84 meter
Y = -6277204
10 meter E =
0012227
Z = 181242
65 I = 51
35374
XDOT = 4441
237717 Wp = 43
36079
YDOT = 1867
032095 meter/sec RA = 289
55899 deg
ZDOT = 6015
422919 TA = 318
61904
MA = 318
71160
Ha = 184
979 n
mi
Hp = 179
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7821355
07 X = 2453084
03
Y = -20594501
64 feet Y = -6250158
90 meter
Z = 594628
10 Z = 192991
24
XDOT = 14570
989886 XDOT = 4390
807727
YDOT = 6125
433381 feet/sec YDOT = 1916
413782 meter/sec
ZDOT = 19735
639499 ZDOT = 6036
876669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19426814
91 X = 5921293
19
Y = 10385159
26 feet Y = 3165396
54 meter
Z = 638752
47 Z = 194691
75
XDOT = -7165
409161 XDOT = -2184
016712
YDOT = 12141
612184 feet/sec YDOT = 3700
763394 meter/sec
ZDOT = 19817
543914 ZDOT = 6040
387385
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 07341
58382673
00020000 00000-0 20000-3 0 9095
2 25544 51
6381 289
8879 0000895 287
0021 73
1046 15
77133878 38135
Satellite: ISS
Catalog Number: 25544
Epoch time: 07341
58382673 = yrday
fracday
Element set: 909
Inclination: 51
6381 deg
RA of node: 289
8879 deg
Eccentricity:
0000895
Arg of perigee: 287
0021 deg
Mean anomaly: 73
1046 deg
Mean motion: 15
77133878 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3813
Checksum: 322
Coasting Arc #11 (Orbit 3827)
---------------------------------------
Vector Time (GMT): 2007/342/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3561270
41 A = 6711792
94 meter
Y = -2549918
00 meter E =
0013079
Z = -5097166
20 I = 51
30751
XDOT = 2956
037394 Wp = 99
95055
YDOT = -6962
906568 meter/sec RA = 284
36306 deg
ZDOT = 1418
821939 TA = 183
70650
MA = 183
71619
Ha = 184
934 n
mi
Hp = 179
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11683958
05 X = -3507730
57
Y = -8365872
70 feet Y = -2589442
03 meter
Z = -16722986
22 Z = -5114337
52
XDOT = 9698
285412 XDOT = 3026
785457
YDOT = -22844
181655 feet/sec YDOT = -6929
455121 meter/sec
ZDOT = 4654
927622 ZDOT = 1433
353472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9597308
61 X = 2925259
66
Y = -10592159
38 feet Y = -3228490
18 meter
Z = -16788650
85 Z = -5117180
78
XDOT = 20860
821554 XDOT = 6358
378410
YDOT = 11441
222363 feet/sec YDOT = 3487
284576 meter/sec
ZDOT = 4709
587858 ZDOT = 1435
482379
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 07342
53426739
00020000 00000-0 20000-3 0 9105
2 25544 51
6388 284
9839 0000945 293
2836 66
8229 15
77159415 38286
Satellite: ISS
Catalog Number: 25544
Epoch time: 07342
53426739 = yrday
fracday
Element set: 910
Inclination: 51
6388 deg
RA of node: 284
9839 deg
Eccentricity:
0000945
Arg of perigee: 293
2836 deg
Mean anomaly: 66
8229 deg
Mean motion: 15
77159415 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3828
Checksum: 333
Coasting Arc #12 (Orbit 3843)
---------------------------------------
Vector Time (GMT): 2007/343/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2754288
05 A = 6720808
16 meter
Y = 5698097
86 meter E =
0005052
Z = -2257504
68 I = 51
33322
XDOT = -3759
061400 Wp = 139
39102
YDOT = -3964
198841 meter/sec RA = 279
21308 deg
ZDOT = -5430
224612 TA = 66
09489
MA = 66
04197
Ha = 184
872 n
mi
Hp = 179
109
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9036378
13 X = -2806833
62
Y = 18694546
80 feet Y = 5667004
42 meter
Z = -7406511
43 Z = -2271011
94
XDOT = -12332
878610 XDOT = -3688
074275
YDOT = -13005
901709 feet/sec YDOT = -4005
837005 meter/sec
ZDOT = -17815
697545 ZDOT = -5448
314641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17770820
81 X = -5416546
18
Y = -10704379
66 feet Y = -3262694
92 meter
Z = -7457399
36 Z = -2273015
32
XDOT = 13312
931778 XDOT = 4057
781606
YDOT = -9665
516289 feet/sec YDOT = -2946
049365 meter/sec
ZDOT = -17885
008781 ZDOT = -5451
350676
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 07343
54804764
00020000 00000-0 20000-3 0 9116
2 25544 51
6395 279
7532 0000917 297
9810 62
1262 15
77207443 38447
Satellite: ISS
Catalog Number: 25544
Epoch time: 07343
54804764 = yrday
fracday
Element set: 911
Inclination: 51
6395 deg
RA of node: 279
7532 deg
Eccentricity:
0000917
Arg of perigee: 297
9810 deg
Mean anomaly: 62
1262 deg
Mean motion: 15
77207443 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3844
Checksum: 305
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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