Date:
February 26th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7642 38 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 3250)
---------------------------------------
Vector Time (GMT): 2007/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6433465
84 A = 6717671
19 meter
Y = -616339
60 meter E =
0007838
Z = 1851416
46 I = 51
54677
XDOT = -1133
381800 Wp = 209
08948
YDOT = 5110
500547 meter/sec RA = 341
37860 deg
ZDOT = 5642
910457 TA = 171
49939
MA = 171
48610
Ha = 186
074 n
mi
Hp = 175
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21107171
39 X = 6430885
95
Y = -2022111
53 feet Y = -544411
31 meter
Z = 6074200
98 Z = 1882663
62
XDOT = -3718
444225 XDOT = -1217
855819
YDOT = 16766
734077 feet/sec YDOT = 5097
354424 meter/sec
ZDOT = 18513
485751 ZDOT = 5637
199096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19306138
46 X = 5884511
00
Y = 8685402
38 feet Y = 2647310
65 meter
Z = 6191473
17 Z = 1887161
02
XDOT = -10993
846542 XDOT = -3350
924426
YDOT = 11262
160623 feet/sec YDOT = 3432
706558 meter/sec
ZDOT = 18492
677139 ZDOT = 5636
567992
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 07052
55960910
00020000 00000-0 20000-3 0 9008
2 25544 51
6345 341
5457 0020932 233
9551 125
9675 15
78562240 32515
Satellite: ISS
Catalog Number: 25544
Epoch time: 07052
55960910 = yrday
fracday
Element set: 900
Inclination: 51
6345 deg
RA of node: 341
5457 deg
Eccentricity:
0020932
Arg of perigee: 233
9551 deg
Mean anomaly: 125
9675 deg
Mean motion: 15
78562240 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3251
Checksum: 285
Coasting Arc #2 (Orbit 3265)
---------------------------------------
Vector Time (GMT): 2007/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2396500
88 A = 6711548
72 meter
Y = -4683670
25 meter E =
0017242
Z = -4167702
21 I = 51
49981
XDOT = 6777
457939 Wp = 215
60912
YDOT = 189
770084 meter/sec RA = 336
15636 deg
ZDOT = 3662
503795 TA = 91
88388
MA = 91
68640
Ha = 185
755 n
mi
Hp = 175
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7862535
70 X = 2468941
98
Y = -15366372
22 feet Y = -4656466
32 meter
Z = -13673563
69 Z = -4155884
04
XDOT = 22235
754394 XDOT = 6757
040586
YDOT = 622
605263 feet/sec YDOT = 265
445349 meter/sec
ZDOT = 12016
088565 ZDOT = 3695
378754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14345395
59 X = 4372476
58
Y = -9661797
10 feet Y = -2944915
76 meter
Z = -13629765
55 Z = -4154352
54
XDOT = 18438
157978 XDOT = 5619
950552
YDOT = 10151
697904 feet/sec YDOT = 3094
237521 meter/sec
ZDOT = 12139
574074 ZDOT = 3700
142178
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 07053
50918354
00020000 00000-0 20000-3 0 9010
2 25544 51
6348 336
6352 0020905 237
5594 122
3550 15
78608697 32660
Satellite: ISS
Catalog Number: 25544
Epoch time: 07053
50918354 = yrday
fracday
Element set: 901
Inclination: 51
6348 deg
RA of node: 336
6352 deg
Eccentricity:
0020905
Arg of perigee: 237
5594 deg
Mean anomaly: 122
3550 deg
Mean motion: 15
78608697 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3266
Checksum: 302
Coasting Arc #3 (Orbit 3281)
---------------------------------------
Vector Time (GMT): 2007/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5068166
71 A = 6710905
76 meter
Y = -1065957
12 meter E =
0012251
Z = -4254812
42 I = 51
47317
XDOT = 4116
893754 Wp = 235
60340
YDOT = -5490
551097 meter/sec RA = 331
02514 deg
ZDOT = -3527
981876 TA = 358
63210
MA = 358
63545
Ha = 185
248 n
mi
Hp = 175
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16627843
54 X = -5035201
46
Y = -3497234
65 feet Y = -1122447
89 meter
Z = -13959358
32 Z = -4279353
23
XDOT = 13506
869271 XDOT = 4195
122021
YDOT = -18013
619084 feet/sec YDOT = -5444
076308 meter/sec
ZDOT = -11574
743687 ZDOT = -3507
792187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13021583
95 X = -3968978
79
Y = -10796705
26 feet Y = -3290835
76 meter
Z = -14051655
52 Z = -4282944
60
XDOT = 19607
224425 XDOT = 5976
282005
YDOT = -8679
721202 feet/sec YDOT = -2645
579022 meter/sec
ZDOT = -11499
603415 ZDOT = -3505
079121
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 07054
52203852
00020000 00000-0 20000-3 0 9024
2 25544 51
6353 331
3976 0020845 241
6048 118
3016 15
78657794 32825
Satellite: ISS
Catalog Number: 25544
Epoch time: 07054
52203852 = yrday
fracday
Element set: 902
Inclination: 51
6353 deg
RA of node: 331
3976 deg
Eccentricity:
0020845
Arg of perigee: 241
6048 deg
Mean anomaly: 118
3016 deg
Mean motion: 15
78657794 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3282
Checksum: 291
Coasting Arc #4 (Orbit 3297)
---------------------------------------
Vector Time (GMT): 2007/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4491019
27 A = 6717717
56 meter
Y = 4686689
20 meter E =
0016231
Z = 1698011
98 I = 51
47132
XDOT = -4613
087069 Wp = 202
37504
YDOT = -2363
158796 meter/sec RA = 325
80095 deg
ZDOT = -5711
020994 TA = 318
75005
MA = 318
87257
Ha = 185
154 n
mi
Hp = 175
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14734315
19 X = -4551341
24
Y = 15376276
92 feet Y = 4636130
82 meter
Z = 5570905
46 Z = 1676048
46
XDOT = -15134
800096 XDOT = -4558
576306
YDOT = -7753
145655 feet/sec YDOT = -2414
440037 meter/sec
ZDOT = -18736
945518 ZDOT = -5733
298698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20105271
29 X = -6128086
69
Y = 7086174
96 feet Y = 2159866
13 meter
Z = 5488999
40 Z = 1673047
02
XDOT = -9416
307325 XDOT = -2870
090473
YDOT = -12221
659121 feet/sec YDOT = -3725
161700 meter/sec
ZDOT = -18820
907547 ZDOT = -5736
612620
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 07055
53486910
00020000 00000-0 20000-3 0 9035
2 25544 51
6351 326
1596 0020909 245
3082 114
5906 15
78663233 32981
Satellite: ISS
Catalog Number: 25544
Epoch time: 07055
53486910 = yrday
fracday
Element set: 903
Inclination: 51
6351 deg
RA of node: 326
1596 deg
Eccentricity:
0020909
Arg of perigee: 245
3082 deg
Mean anomaly: 114
5906 deg
Mean motion: 15
78663233 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3298
Checksum: 298
Coasting Arc #5 (Orbit 3313)
---------------------------------------
Vector Time (GMT): 2007/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2804976
41 A = 6706619
21 meter
Y = 3116643
55 meter E =
0018914
Z = 5249232
87 I = 51
41184
XDOT = -5862
709927 Wp = 245
67172
YDOT = 4982
730077 meter/sec RA = 320
63218 deg
ZDOT = 167
181400 TA = 202
69384
MA = 202
77757
Ha = 184
764 n
mi
Hp = 175
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9202678
52 X = 2744417
83
Y = 10225208
51 feet Y = 3147671
64 meter
Z = 17221892
63 Z = 5262712
18
XDOT = -19234
612620 XDOT = -5918
803922
YDOT = 16347
539622 feet/sec YDOT = 4916
856340 meter/sec
ZDOT = 548
495406 ZDOT = 138
564738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3757715
03 X = 1145351
54
Y = 13166776
92 feet Y = 4013233
60 meter
Z = 17272907
40 Z = 5264782
18
XDOT = -23470
232839 XDOT = -7153
726969
YDOT = 6087
997941 feet/sec YDOT = 1855
621773 meter/sec
ZDOT = 441
634377 ZDOT = 134
610158
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 07056
54767234
00020000 00000-0 20000-3 0 9049
2 25544 51
6352 320
9210 0021012 249
5270 110
3639 15
78747998 33145
Satellite: ISS
Catalog Number: 25544
Epoch time: 07056
54767234 = yrday
fracday
Element set: 904
Inclination: 51
6352 deg
RA of node: 320
9210 deg
Eccentricity:
0021012
Arg of perigee: 249
5270 deg
Mean anomaly: 110
3639 deg
Mean motion: 15
78747998 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3314
Checksum: 286
Coasting Arc #6 (Orbit 3329)
---------------------------------------
Vector Time (GMT): 2007/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5409725
35 A = 6717756
15 meter
Y = -3716236
43 meter E =
0007726
Z = 1437073
49 I = 51
42850
XDOT = 1742
867349 Wp = 275
53010
YDOT = 4766
703910 meter/sec RA = 315
45646 deg
ZDOT = 5793
093599 TA = 100
34722
MA = 100
26011
Ha = 184
518 n
mi
Hp = 175
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17748442
74 X = 5443897
89
Y = -12192376
74 feet Y = -3655550
82 meter
Z = 4714808
04 Z = 1463436
26
XDOT = 5718
068729 XDOT = 1661
294696
YDOT = 15638
792357 feet/sec YDOT = 4785
737412 meter/sec
ZDOT = 19006
212594 ZDOT = 5801
362216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21200135
97 X = 6461801
44
Y = -3643685
34 feet Y = -1110595
29 meter
Z = 4813364
45 Z = 1467113
49
XDOT = -1723
513419 XDOT = -525
326890
YDOT = 15005
154375 feet/sec YDOT = 4573
571054 meter/sec
ZDOT = 19037
866714 ZDOT = 5802
741774
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 07057
56045341
00020000 00000-0 20000-3 0 9051
2 25544 51
6355 315
6819 0020915 253
6711 106
2154 15
78749485 33308
Satellite: ISS
Catalog Number: 25544
Epoch time: 07057
56045341 = yrday
fracday
Element set: 905
Inclination: 51
6355 deg
RA of node: 315
6819 deg
Eccentricity:
0020915
Arg of perigee: 253
6711 deg
Mean anomaly: 106
2154 deg
Mean motion: 15
78749485 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3330
Checksum: 291
Coasting Arc #7 (Orbit 3344)
---------------------------------------
Vector Time (GMT): 2007/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -285317
30 A = 6710155
49 meter
Y = -5074310
48 meter E =
0014221
Z = -4375674
61 I = 51
38393
XDOT = 6180
085067 Wp = 236
11116
YDOT = -3213
818330 meter/sec RA = 310
22931 deg
ZDOT = 3308
479808 TA = 67
26853
MA = 67
11830
Ha = 184
288 n
mi
Hp = 175
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -936080
40 X = -207298
77
Y = -16648000
28 feet Y = -5077064
81 meter
Z = -14355887
82 Z = -4376871
17
XDOT = 20275
869644 XDOT = 6199
491569
YDOT = -10544
023394 feet/sec YDOT = -3144
600684 meter/sec
ZDOT = 10854
592545 ZDOT = 3338
548962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5931947
34 X = 1808057
55
Y = -15578725
89 feet Y = -4748395
65 meter
Z = -14361022
78 Z = -4377239
74
XDOT = 21614
801706 XDOT = 6588
191560
YDOT = -1926
420002 feet/sec YDOT = -587
172817 meter/sec
ZDOT = 10967
135818 ZDOT = 3342
782997
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 07058
50991101
00020000 00000-0 20000-3 0 9061
2 25544 51
6358 310
7710 0021015 257
3951 102
4864 15
78800839 33459
Satellite: ISS
Catalog Number: 25544
Epoch time: 07058
50991101 = yrday
fracday
Element set: 906
Inclination: 51
6358 deg
RA of node: 310
7710 deg
Eccentricity:
0021015
Arg of perigee: 257
3951 deg
Mean anomaly: 102
4864 deg
Mean motion: 15
78800839 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3345
Checksum: 282
Coasting Arc #8 (Orbit 3360)
---------------------------------------
Vector Time (GMT): 2007/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5089463
46 A = 6711127
90 meter
Y = 1603334
44 meter E =
0013686
Z = -4057923
66 I = 51
37011
XDOT = 950
007123 Wp = 267
23921
YDOT = -6643
509141 meter/sec RA = 305
08853 deg
ZDOT = -3806
081663 TA = 323
55384
MA = 323
64693
Ha = 184
020 n
mi
Hp = 175
020
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16697714
77 X = -5087301
84
Y = 5260283
58 feet Y = 1546433
24 meter
Z = -13313397
82 Z = -4082642
31
XDOT = 3116
821269 XDOT = 1042
713896
YDOT = -21796
289832 feet/sec YDOT = -6632
367335 meter/sec
ZDOT = -12487
144565 ZDOT = -3801
241393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17362862
96 X = -5292200
63
Y = -1593641
48 feet Y = -485741
92 meter
Z = -13406047
88 Z = -4086163
40
XDOT = 11268
734311 XDOT = 3434
710218
YDOT = -17591
464383 feet/sec YDOT = -5361
878344 meter/sec
ZDOT = -12469
809803 ZDOT = -3800
798028
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 07059
52264197
00020000 00000-0 20000-3 0 9073
2 25544 51
6357 305
5328 0021126 261
4945 98
3826 15
78836574 33611
Satellite: ISS
Catalog Number: 25544
Epoch time: 07059
52264197 = yrday
fracday
Element set: 907
Inclination: 51
6357 deg
RA of node: 305
5328 deg
Eccentricity:
0021126
Arg of perigee: 261
4945 deg
Mean anomaly: 98
3826 deg
Mean motion: 15
78836574 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3361
Checksum: 316
Coasting Arc #9 (Orbit 3376)
---------------------------------------
Vector Time (GMT): 2007/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1776348
97 A = 6716805
23 meter
Y = 6182600
35 meter E =
0010718
Z = 1923430
74 I = 51
37354
XDOT = -5286
408440 Wp = 226
73491
YDOT = 216
055937 meter/sec RA = 299
85294 deg
ZDOT = -5603
416062 TA = 291
75307
MA = 291
86712
Ha = 183
974 n
mi
Hp = 175
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5827916
55 X = -1854695
06
Y = 20284121
88 feet Y = 6162298
24 meter
Z = 6310468
29 Z = 1914610
96
XDOT = -17343
859710 XDOT = -5261
211950
YDOT = 708
844939 feet/sec YDOT = 157
081030 meter/sec
ZDOT = -18383
910965 ZDOT = -5629
035467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12981834
28 X = -3956863
09
Y = 16652003
64 feet Y = 5075530
71 meter
Z = 6278134
70 Z = 1913575
46
XDOT = -15055
487019 XDOT = -4588
912443
YDOT = -4803
106883 feet/sec YDOT = -1463
986978 meter/sec
ZDOT = -18480
123914 ZDOT = -5632
741769
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 07060
53534958
00020000 00000-0 20000-3 0 9082
2 25544 51
6354 300
2942 0020958 265
0958 94
7815 15
78850975 33774
Satellite: ISS
Catalog Number: 25544
Epoch time: 07060
53534958 = yrday
fracday
Element set: 908
Inclination: 51
6354 deg
RA of node: 300
2942 deg
Eccentricity:
0020958
Arg of perigee: 265
0958 deg
Mean anomaly: 94
7815 deg
Mean motion: 15
78850975 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3377
Checksum: 328
Coasting Arc #10 (Orbit 3392)
---------------------------------------
Vector Time (GMT): 2007/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3978292
74 A = 6706180
31 meter
Y = 1379211
06 meter E =
0018646
Z = 5235616
88 I = 51
32490
XDOT = -2941
849593 Wp = 266
70688
YDOT = 7101
341903 meter/sec RA = 294
67929 deg
ZDOT = 364
733540 TA = 179
81284
MA = 179
81214
Ha = 183
871 n
mi
Hp = 174
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13052141
54 X = 3937141
58
Y = 4524970
68 feet Y = 1423468
79 meter
Z = 17177220
74 Z = 5254842
84
XDOT = -9651
737511 XDOT = -3022
810931
YDOT = 23298
365823 feet/sec YDOT = 7067
991841 meter/sec
ZDOT = 1196
632348 ZDOT = 350
245360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10500102
68 X = 3200431
30
Y = 8836794
42 feet Y = 2693454
94 meter
Z = 17249625
47 Z = 5257685
84
XDOT = -16668
273859 XDOT = -5080
489872
YDOT = 17574
624589 feet/sec YDOT = 5356
745575 meter/sec
ZDOT = 1143
134290 ZDOT = 348
427332
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 07061
54802960
00020000 00000-0 20000-3 0 9096
2 25544 51
6352 295
0544 0021072 269
3619 90
5132 15
78915015 33931
Satellite: ISS
Catalog Number: 25544
Epoch time: 07061
54802960 = yrday
fracday
Element set: 909
Inclination: 51
6352 deg
RA of node: 295
0544 deg
Eccentricity:
0021072
Arg of perigee: 269
3619 deg
Mean anomaly: 90
5132 deg
Mean motion: 15
78915015 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3393
Checksum: 289
Coasting Arc #11 (Orbit 3408)
---------------------------------------
Vector Time (GMT): 2007/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3169404
73 A = 6717275
52 meter
Y = -5766954
77 meter E =
0012238
Z = 1329721
87 I = 51
35122
XDOT = 3741
126135 Wp = 311
98570
YDOT = 3389
257593 meter/sec RA = 289
49299 deg
ZDOT = 5824
372710 TA = 62
70556
MA = 62
58099
Ha = 183
835 n
mi
Hp = 174
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10398309
48 X = 3227196
70
Y = -18920455
29 feet Y = -5731189
48 meter
Z = 4362604
56 Z = 1345259
27
XDOT = 12274
035876 XDOT = 3674
655890
YDOT = 11119
611524 feet/sec YDOT = 3430
721763 meter/sec
ZDOT = 19108
834352 ZDOT = 5842
384918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16181411
33 X = 4932094
17
Y = -14274608
81 feet Y = -4350900
77 meter
Z = 4420210
14 Z = 1347280
05
XDOT = 6628
696459 XDOT = 2020
426681
YDOT = 13409
992831 feet/sec YDOT = 4087
365815 meter/sec
ZDOT = 19176
947220 ZDOT = 5845
133513
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 07062
56068465
00020000 00000-0 20000-3 0 9105
2 25544 51
6342 289
8140 0021241 273
3916 86
4820 15
78972349 34095
Satellite: ISS
Catalog Number: 25544
Epoch time: 07062
56068465 = yrday
fracday
Element set: 910
Inclination: 51
6342 deg
RA of node: 289
8140 deg
Eccentricity:
0021241
Arg of perigee: 273
3916 deg
Mean anomaly: 86
4820 deg
Mean motion: 15
78972349 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3409
Checksum: 302
Coasting Arc #12 (Orbit 3423)
---------------------------------------
Vector Time (GMT): 2007/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2518710
44 A = 6709434
74 meter
Y = -4386422
77 meter E =
0012260
Z = -4398060
58 I = 51
31570
XDOT = 4127
056306 Wp = 266
50826
YDOT = -5645
741710 meter/sec RA = 284
25929 deg
ZDOT = 3258
768473 TA = 36
29107
MA = 36
20798
Ha = 183
815 n
mi
Hp = 174
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8263485
68 X = -2448109
10
Y = -14391150
83 feet Y = -4414194
04 meter
Z = -14429332
61 Z = -4410124
34
XDOT = 13540
210978 XDOT = 4174
050890
YDOT = -18522
774640 feet/sec YDOT = -5599
327607 meter/sec
ZDOT = 10691
497616 ZDOT = 3278
931945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3091310
33 X = -942231
39
Y = -16263683
12 feet Y = -4957170
61 meter
Z = -14475236
41 Z = -4412052
06
XDOT = 17558
784382 XDOT = 5351
917479
YDOT = -12944
833354 feet/sec YDOT = -3945
585206 meter/sec
ZDOT = 10766
489942 ZDOT = 3281
626134
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 07063
51002738
00020000 00000-0 20000-3 0 9113
2 25544 51
6332 284
9012 0021276 277
1188 82
7559 15
79003246 34246
Satellite: ISS
Catalog Number: 25544
Epoch time: 07063
51002738 = yrday
fracday
Element set: 911
Inclination: 51
6332 deg
RA of node: 284
9012 deg
Eccentricity:
0021276
Arg of perigee: 277
1188 deg
Mean anomaly: 82
7559 deg
Mean motion: 15
79003246 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3424
Checksum: 281
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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