Date:
August 10th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 2421 88 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 12 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 1871)
---------------------------------------
Vector Time (GMT): 2007/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1987290
88 A = 6717829
55 meter
Y = 4661357
50 meter E =
0005874
Z = -4411818
87 I = 51
49437
XDOT = -6966
643416 Wp = 133
38697
YDOT = -129
273137 meter/sec RA = 203
06712 deg
ZDOT = -3281
384541 TA = 103
65914
MA = 103
59373
Ha = 187
644 n
mi
Hp = 181
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6519983
20 X = 1956450
95
Y = 15293167
64 feet Y = 4683408
53 meter
Z = -14474471
37 Z = -4402239
06
XDOT = -22856
441653 XDOT = -6948
739760
YDOT = -424
124466 feet/sec YDOT = -207
077620 meter/sec
ZDOT = -10765
697314 ZDOT = -3315
184933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6440099
70 X = 1962942
39
Y = -15361720
92 feet Y = -4682252
54 meter
Z = -14437594
16 Z = -4400578
70
XDOT = 14383
259957 XDOT = 4384
017635
YDOT = 16247
616067 feet/sec YDOT = 4952
273377 meter/sec
ZDOT = -10893
758967 ZDOT = -3320
417733
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 07218
52174873
00020000 00000-0 20000-3 0 9004
2 25544 51
6288 203
9038 0008555 211
3510 148
7145 15
76076168 18728
Satellite: ISS
Catalog Number: 25544
Epoch time: 07218
52174873 = yrday
fracday
Element set: 900
Inclination: 51
6288 deg
RA of node: 203
9038 deg
Eccentricity:
0008555
Arg of perigee: 211
3510 deg
Mean anomaly: 148
7145 deg
Mean motion: 15
76076168 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1872
Checksum: 294
Coasting Arc #2 (Orbit 1887)
---------------------------------------
Vector Time (GMT): 2007/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6327278
52 A = 6723907
85 meter
Y = 168457
36 meter E =
0013835
Z = 2241768
78 I = 51
54232
XDOT = 1800
119678 Wp = 143
41030
YDOT = 5136
645633 meter/sec RA = 197
86277 deg
ZDOT = -5460
457147 TA = 11
35399
MA = 11
32281
Ha = 187
252 n
mi
Hp = 181
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20758787
80 X = 6314034
51
Y = 552681
63 feet Y = 239138
22 meter
Z = 7354884
43 Z = 2272474
37
XDOT = 5905
904457 XDOT = 1769
072910
YDOT = 16852
511920 feet/sec YDOT = 5156
602681 meter/sec
ZDOT = -17914
885653 ZDOT = -5451
786982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14230643
20 X = -4337500
05
Y = -15066399
91 feet Y = -4592238
69 meter
Z = 7471240
90 Z = 2277234
23
XDOT = 6600
695756 XDOT = 2011
892066
YDOT = -15111
766179 feet/sec YDOT = -4606
066331 meter/sec
ZDOT = -17881
392214 ZDOT = -5450
248347
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 07219
53622824
00020000 00000-0 20000-3 0 9011
2 25544 51
6286 198
6768 0008458 216
6178 143
4409 15
76114850 18889
Satellite: ISS
Catalog Number: 25544
Epoch time: 07219
53622824 = yrday
fracday
Element set: 901
Inclination: 51
6286 deg
RA of node: 198
6768 deg
Eccentricity:
0008458
Arg of perigee: 216
6178 deg
Mean anomaly: 143
4409 deg
Mean motion: 15
76114850 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1888
Checksum: 322
Coasting Arc #3 (Orbit 1903)
---------------------------------------
Vector Time (GMT): 2007/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1093010
80 A = 6715226
82 meter
Y = -4332267
34 meter E =
0009694
Z = 5016587
02 I = 51
54054
XDOT = 7482
613211 Wp = 186
19373
YDOT = 218
162909 meter/sec RA = 192
73973 deg
ZDOT = 1809
552191 TA = 246
29399
MA = 246
39574
Ha = 187
205 n
mi
Hp = 181
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3585993
44 X = -1068854
91
Y = -14213475
51 feet Y = -4344355
62 meter
Z = 16458618
85 Z = 5011335
32
XDOT = 24549
255943 XDOT = 7470
827182
YDOT = 715
757577 feet/sec YDOT = 301
771558 meter/sec
ZDOT = 5936
851020 ZDOT = 1845
873725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7254453
40 X = -2211157
40
Y = 12764312
12 feet Y = 3890562
33 meter
Z = 16438175
43 Z = 5010355
87
XDOT = -16170
141859 XDOT = -4928
659239
YDOT = -17051
753296 feet/sec YDOT = -5197
374405 meter/sec
ZDOT = 6074
509644 ZDOT = 1851
510540
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 07220
55070171
00020000 00000-0 20000-3 0 9028
2 25544 51
6284 193
4498 0008516 220
8574 139
1952 15
76114936 19041
Satellite: ISS
Catalog Number: 25544
Epoch time: 07220
55070171 = yrday
fracday
Element set: 902
Inclination: 51
6284 deg
RA of node: 193
4498 deg
Eccentricity:
0008516
Arg of perigee: 220
8574 deg
Mean anomaly: 139
1952 deg
Mean motion: 15
76114936 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1904
Checksum: 291
Coasting Arc #4 (Orbit 1918)
---------------------------------------
Vector Time (GMT): 2007/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6664716
36 A = 6725744
90 meter
Y = -183489
50 meter E =
0001809
Z = -876792
87 I = 51
60466
XDOT = -648
894067 Wp = 15
99751
YDOT = -4842
982891 meter/sec RA = 187
55894 deg
ZDOT = 5950
521810 TA = 334
42614
MA = 334
43509
Ha = 187
018 n
mi
Hp = 182
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21865867
31 X = -6657909
99
Y = -601999
66 feet Y = -257979
94 meter
Z = -2876617
04 Z = -909153
01
XDOT = -2128
917544 XDOT = -623
596955
YDOT = -15889
051481 feet/sec YDOT = -4850
098523 meter/sec
ZDOT = 19522
709351 ZDOT = 5947
430350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15532945
41 X = 4734441
76
Y = 15378082
48 feet Y = 4687239
54 meter
Z = -2999277
99 Z = -914179
93
XDOT = -8108
785451 XDOT = -2471
557805
YDOT = 11992
838606 feet/sec YDOT = 3655
417207 meter/sec
ZDOT = 19510
384140 ZDOT = 5946
765086
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 07221
50176405
00020000 00000-0 20000-3 0 9032
2 25544 51
6282 188
5490 0008457 223
4080 136
6418 15
76132049 19191
Satellite: ISS
Catalog Number: 25544
Epoch time: 07221
50176405 = yrday
fracday
Element set: 903
Inclination: 51
6282 deg
RA of node: 188
5490 deg
Eccentricity:
0008457
Arg of perigee: 223
4080 deg
Mean anomaly: 136
6418 deg
Mean motion: 15
76132049 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1919
Checksum: 285
Coasting Arc #5 (Orbit 1934)
---------------------------------------
Vector Time (GMT): 2007/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 11458
46 A = 6714075
43 meter
Y = 4177035
40 meter E =
0010125
Z = -5263836
60 I = 51
59478
XDOT = -7694
274881 Wp = 120
98203
YDOT = -188
282654 meter/sec RA = 182
41404 deg
ZDOT = -171
520444 TA = 147
42003
MA = 147
35752
Ha = 186
782 n
mi
Hp = 182
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 37593
36 X = -9680
42
Y = 13704184
39 feet Y = 4177045
94 meter
Z = -17269805
12 Z = -5263831
81
XDOT = -25243
683993 XDOT = -7690
764428
YDOT = -617
725242 feet/sec YDOT = -274
304720 meter/sec
ZDOT = -562
731114 ZDOT = -208
889917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9096694
17 X = 2772672
38
Y = -10250615
36 feet Y = -3124387
56 meter
Z = -17269258
57 Z = -5263670
01
XDOT = 17551
026516 XDOT = 5349
552882
YDOT = 16732
349810 feet/sec YDOT = 5100
020222 meter/sec
ZDOT = -704
396337 ZDOT = -214
700003
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 07222
51622366
00020000 00000-0 20000-3 0 9047
2 25544 51
6291 183
3211 0008436 228
5970 131
4470 15
76121803 19351
Satellite: ISS
Catalog Number: 25544
Epoch time: 07222
51622366 = yrday
fracday
Element set: 904
Inclination: 51
6291 deg
RA of node: 183
3211 deg
Eccentricity:
0008436
Arg of perigee: 228
5970 deg
Mean anomaly: 131
4470 deg
Mean motion: 15
76121803 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1935
Checksum: 270
Coasting Arc #6 (Orbit 1950)
---------------------------------------
Vector Time (GMT): 2007/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6690672
48 A = 6725970
80 meter
Y = 137984
33 meter E =
0013461
Z = -577970
66 I = 51
66488
XDOT = -616
450828 Wp = 178
19605
YDOT = 4787
384525 meter/sec RA = 177
26547 deg
ZDOT = -6010
159640 TA = 8
10180
MA = 8
08008
Ha = 186
589 n
mi
Hp = 182
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21951025
18 X = 6691439
86
Y = 452704
49 feet Y = 212807
54 meter
Z = -1896229
21 Z = -545466
30
XDOT = -2022
476470 XDOT = -640
742707
YDOT = 15706
642142 feet/sec YDOT = 4780
355734 meter/sec
ZDOT = -19718
371523 ZDOT = -6013
212864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16235248
77 X = -4948503
82
Y = -14795989
92 feet Y = -4509817
73 meter
Z = -1772995
44 Z = -540409
01
XDOT = 10698
647487 XDOT = 3260
947754
YDOT = -9382
323864 feet/sec YDOT = -2859
732314 meter/sec
ZDOT = -19729
335335 ZDOT = -6013
501410
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 07223
53067614
00020000 00000-0 20000-3 0 9050
2 25544 51
6300 178
0940 0008422 233
0665 126
9729 15
76140784 19512
Satellite: ISS
Catalog Number: 25544
Epoch time: 07223
53067614 = yrday
fracday
Element set: 905
Inclination: 51
6300 deg
RA of node: 178
0940 deg
Eccentricity:
0008422
Arg of perigee: 233
0665 deg
Mean anomaly: 126
9729 deg
Mean motion: 15
76140784 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1951
Checksum: 284
Coasting Arc #7 (Orbit 1966)
---------------------------------------
Vector Time (GMT): 2007/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1076723
45 A = 6714672
16 meter
Y = -4227625
91 meter E =
0003849
Z = 5106830
28 I = 51
65636
XDOT = 7557
126200 Wp = 240
39838
YDOT = 135
829114 meter/sec RA = 172
09781 deg
ZDOT = -1483
598865 TA = 223
80256
MA = 223
83310
Ha = 186
371 n
mi
Hp = 182
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3532557
24 X = 1099109
93
Y = -13870163
75 feet Y = -4215460
53 meter
Z = 16754692
52 Z = 5112114
99
XDOT = 24793
721128 XDOT = 7562
252554
YDOT = 445
633576 feet/sec YDOT = 220
365911 meter/sec
ZDOT = -4867
450344 ZDOT = -1446
874808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11575713
76 X = -3528277
55
Y = 8379123
61 feet Y = 2553956
88 meter
Z = 16774184
42 Z = 5112771
41
XDOT = -18065
548773 XDOT = -5506
379266
YDOT = -15509
762345 feet/sec YDOT = -4727
375563 meter/sec
ZDOT = -4728
206695 ZDOT = -1441
157401
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 07224
54512179
00020000 00000-0 20000-3 0 9064
2 25544 51
6306 172
8673 0008405 237
1425 122
8931 15
76148006 19675
Satellite: ISS
Catalog Number: 25544
Epoch time: 07224
54512179 = yrday
fracday
Element set: 906
Inclination: 51
6306 deg
RA of node: 172
8673 deg
Eccentricity:
0008405
Arg of perigee: 237
1425 deg
Mean anomaly: 122
8931 deg
Mean motion: 15
76148006 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1967
Checksum: 291
Coasting Arc #8 (Orbit 1982)
---------------------------------------
Vector Time (GMT): 2007/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6418048
98 A = 6724336
19 meter
Y = -131615
28 meter E =
0005821
Z = 1994635
20 I = 51
71781
XDOT = 1844
726899 Wp = 78
21303
YDOT = -4959
712139 meter/sec RA = 166
97908 deg
ZDOT = 5595
908298 TA = 303
99743
MA = 304
05272
Ha = 186
154 n
mi
Hp = 183
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21056591
14 X = -6425789
59
Y = -431808
66 feet Y = -203428
87 meter
Z = 6544078
74 Z = 1963438
24
XDOT = 6052
253606 XDOT = 1872
866760
YDOT = -16272
021452 feet/sec YDOT = -4938
926230 meter/sec
ZDOT = 18359
279194 ZDOT = 5604
937939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16074793
95 X = 4899597
20
Y = 13663886
95 feet Y = 4164752
74 meter
Z = 6425779
97 Z = 1958577
74
XDOT = -13897
110284 XDOT = -4235
839214
YDOT = 7679
789076 feet/sec YDOT = 2340
799710 meter/sec
ZDOT = 18392
872757 ZDOT = 5606
147616
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 07225
55955928
00020000 00000-0 20000-3 0 9070
2 25544 51
6310 167
6397 0008457 241
2386 118
7929 15
76172591 19839
Satellite: ISS
Catalog Number: 25544
Epoch time: 07225
55955928 = yrday
fracday
Element set: 907
Inclination: 51
6310 deg
RA of node: 167
6397 deg
Eccentricity:
0008457
Arg of perigee: 241
2386 deg
Mean anomaly: 118
7929 deg
Mean motion: 15
76172591 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1983
Checksum: 331
Coasting Arc #9 (Orbit 1997)
---------------------------------------
Vector Time (GMT): 2007/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2101337
86 A = 6716912
98 meter
Y = 4473903
06 meter E =
0007347
Z = -4553364
88 I = 51
72138
XDOT = -7066
478751 Wp = 164
38061
YDOT = -209
147797 meter/sec RA = 161
79175 deg
ZDOT = 3049
812142 TA = 135
95326
MA = 135
89470
Ha = 185
899 n
mi
Hp = 183
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6894153
10 X = -2129090
56
Y = 14678159
64 feet Y = 4450249
62 meter
Z = -14938861
15 Z = -4563640
31
XDOT = -23183
985405 XDOT = -7078
429975
YDOT = -686
180436 feet/sec YDOT = -288
236020 meter/sec
ZDOT = 10005
945348 ZDOT = 3015
454846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14429839
96 X = 4398215
22
Y = -7321835
61 feet Y = -2231695
49 meter
Z = -14977240
46 Z = -4565062
89
XDOT = 17303
111483 XDOT = 5273
988380
YDOT = 13860
807762 feet/sec YDOT = 4224
774206 meter/sec
ZDOT = 9875
645880 ZDOT = 3010
096864
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 07226
51058869
00020000 00000-0 20000-3 0 9086
2 25544 51
6315 162
7391 0008437 245
4383 114
5903 15
76175341 19983
Satellite: ISS
Catalog Number: 25544
Epoch time: 07226
51058869 = yrday
fracday
Element set: 908
Inclination: 51
6315 deg
RA of node: 162
7391 deg
Eccentricity:
0008437
Arg of perigee: 245
4383 deg
Mean anomaly: 114
5903 deg
Mean motion: 15
76175341 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1998
Checksum: 311
Coasting Arc #10 (Orbit 2013)
---------------------------------------
Vector Time (GMT): 2007/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5857458
32 A = 6721337
90 meter
Y = 288485
33 meter E =
0004746
Z = -3277292
78 I = 51
76406
XDOT = -2916
346123 Wp = 223
55919
YDOT = 5325
380269 meter/sec RA = 156
69504 deg
ZDOT = -4742
899845 TA = 354
83463
MA = 354
83953
Ha = 185
781 n
mi
Hp = 183
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19217382
95 X = 5869717
35
Y = 946474
17 feet Y = 354055
29 meter
Z = -10752272
89 Z = -3248807
91
XDOT = -9568
064707 XDOT = -2952
638779
YDOT = 17471
720044 feet/sec YDOT = 5292
565140 meter/sec
ZDOT = -15560
695029 ZDOT = -4757
155362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14778211
78 X = -4504398
95
Y = -12414505
43 feet Y = -3783941
25 meter
Z = -10644224
01 Z = -3244359
48
XDOT = 17212
727702 XDOT = 5246
439404
YDOT = -7100
567517 feet/sec YDOT = -2164
252979 meter/sec
ZDOT = -15614
055908 ZDOT = -4759
164241
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 07227
52501272
00020000 00000-0 20000-3 0 9090
2 25544 51
6322 157
5121 0008388 249
6520 110
3743 15
76198000 20141
Satellite: ISS
Catalog Number: 25544
Epoch time: 07227
52501272 = yrday
fracday
Element set: 909
Inclination: 51
6322 deg
RA of node: 157
5121 deg
Eccentricity:
0008388
Arg of perigee: 249
6520 deg
Mean anomaly: 110
3743 deg
Mean motion: 15
76198000 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2014
Checksum: 263
Coasting Arc #11 (Orbit 2029)
---------------------------------------
Vector Time (GMT): 2007/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2917087
60 A = 6720123
58 meter
Y = -4838933
56 meter E =
0004052
Z = 3633531
71 I = 51
78606
XDOT = 6311
112624 Wp = 110
27908
YDOT = 506
310782 meter/sec RA = 151
50135 deg
ZDOT = -4389
889630 TA = 26
21628
MA = 26
19577
Ha = 185
465 n
mi
Hp = 183
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9570497
39 X = 2953329
63
Y = -15875766
29 feet Y = -4806110
41 meter
Z = 11921035
79 Z = 3647790
79
XDOT = 20705
750079 XDOT = 6326
306981
YDOT = 1661
124614 feet/sec YDOT = 576
970156 meter/sec
ZDOT = -14402
525033 ZDOT = -4359
193681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17049703
14 X = -5196749
52
Y = 7187837
28 feet Y = 2190852
80 meter
Z = 11974476
51 Z = 3649820
44
XDOT = -15259
996849 XDOT = -4651
247039
YDOT = -12383
510957 feet/sec YDOT = -3774
494140 meter/sec
ZDOT = -14286
058332 ZDOT = -4354
390579
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 07228
53942960
00020000 00000-0 20000-3 0 9107
2 25544 51
6321 152
2852 0008421 253
4670 106
5570 15
76197120 20305
Satellite: ISS
Catalog Number: 25544
Epoch time: 07228
53942960 = yrday
fracday
Element set: 910
Inclination: 51
6321 deg
RA of node: 152
2852 deg
Eccentricity:
0008421
Arg of perigee: 253
4670 deg
Mean anomaly: 106
5570 deg
Mean motion: 15
76197120 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2030
Checksum: 264
Coasting Arc #12 (Orbit 2045)
---------------------------------------
Vector Time (GMT): 2007/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5114640
95 A = 6717916
66 meter
Y = -670106
50 meter E =
0005027
Z = 4305700
49 I = 51
80323
XDOT = 3708
484136 Wp = 166
98866
YDOT = -5770
392587 meter/sec RA = 146
41010 deg
ZDOT = 3501
572816 TA = 247
63693
MA = 247
69022
Ha = 185
249 n
mi
Hp = 183
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16780318
07 X = -5127683
75
Y = -2198512
13 feet Y = -727374
23 meter
Z = 14126313
94 Z = 4280822
06
XDOT = 12166
942702 XDOT = 3755
724010
YDOT = -18931
734210 feet/sec YDOT = -5728
658105 meter/sec
ZDOT = 11488
099790 ZDOT = 3519
703234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12499166
09 X = 3809745
82
Y = 11525727
84 feet Y = 3513041
85 meter
Z = 14031882
28 Z = 4276917
72
XDOT = -19969
119794 XDOT = -6086
587713
YDOT = 7564
330995 feet/sec YDOT = 2305
608087 meter/sec
ZDOT = 11556
105195 ZDOT = 3522
300864
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 07229
55383856
00020000 00000-0 20000-3 0 9114
2 25544 51
6321 147
0574 0008418 257
4685 102
5538 15
76213843 20462
Satellite: ISS
Catalog Number: 25544
Epoch time: 07229
55383856 = yrday
fracday
Element set: 911
Inclination: 51
6321 deg
RA of node: 147
0574 deg
Eccentricity:
0008418
Arg of perigee: 257
4685 deg
Mean anomaly: 102
5538 deg
Mean motion: 15
76213843 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2046
Checksum: 298
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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