Date:
December 10th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8234 39 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 3811)
---------------------------------------
Vector Time (GMT): 2007/341/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4549470
03 A = 6713576
05 meter
Y = 1557173
73 meter E =
0010552
Z = -4695164
17 I = 51
32127
XDOT = 299
624139 Wp = 67
54620
YDOT = -7208
668964 meter/sec RA = 289
69237 deg
ZDOT = -2681
938226 TA = 175
94997
MA = 175
94142
Ha = 184
949 n
mi
Hp = 179
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14926082
76 X = -4543735
70
Y = 5108837
70 feet Y = 1506331
65 meter
Z = -15404081
91 Z = -4717251
84
XDOT = 983
018829 XDOT = 393
238954
YDOT = -23650
488726 feet/sec YDOT = -7204
794622 meter/sec
ZDOT = -8799
009928 ZDOT = -2680
256159
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1132060
60 X = -345052
07
Y = -15652870
96 feet Y = -4770995
07 meter
Z = -15488059
21 Z = -4720760
45
XDOT = 21453
090869 XDOT = 6538
902097
YDOT = 7146
532852 feet/sec YDOT = 2178
263213 meter/sec
ZDOT = -8793
322303 ZDOT = -2680
204638
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
52050458
00020000 00000-0 20000-3 0 9003
2 25544 51
6383 290
2214 0001014 290
5067 69
5989 15
77129070 38122
Satellite: ISS
Catalog Number: 25544
Epoch time: 07341
52050458 = yrday
fracday
Element set: 900
Inclination: 51
6383 deg
RA of node: 290
2214 deg
Eccentricity:
0001014
Arg of perigee: 290
5067 deg
Mean anomaly: 69
5989 deg
Mean motion: 15
77129070 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3812
Checksum: 277
Coasting Arc #2 (Orbit 3827)
---------------------------------------
Vector Time (GMT): 2007/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -582767
85 A = 6722432
08 meter
Y = 6554677
41 meter E =
0013008
Z = 1343093
27 I = 51
34334
XDOT = -5000
168869 Wp = 120
58363
YDOT = 754
508576 meter/sec RA = 284
47704 deg
ZDOT = -5816
632852 TA = 44
57844
MA = 44
47389
Ha = 184
918 n
mi
Hp = 179
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1911968
00 X = -662544
56
Y = 21504847
14 feet Y = 6547714
32 meter
Z = 4406473
97 Z = 1340069
31
XDOT = -16404
753507 XDOT = -4979
977570
YDOT = 2475
421836 feet/sec YDOT = 698
707608 meter/sec
ZDOT = -19083
441115 ZDOT = -5840
874996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20412826
08 X = -6221829
39
Y = -7037488
30 feet Y = -2145026
44 meter
Z = 4395608
58 Z = 1339781
49
XDOT = 991
870389 XDOT = 302
322095
YDOT = -14926
354011 feet/sec YDOT = -4549
552703 meter/sec
ZDOT = -19175
710737 ZDOT = -5844
756633
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
53430974
00020000 00000-0 20000-3 0 9011
2 25544 51
6388 284
9907 0001008 294
0230 66
0830 15
77156271 38287
Satellite: ISS
Catalog Number: 25544
Epoch time: 07342
53430974 = yrday
fracday
Element set: 901
Inclination: 51
6388 deg
RA of node: 284
9907 deg
Eccentricity:
0001008
Arg of perigee: 294
0230 deg
Mean anomaly: 66
0830 deg
Mean motion: 15
77156271 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3828
Checksum: 290
Coasting Arc #3 (Orbit 3843)
---------------------------------------
Vector Time (GMT): 2007/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4194284
76 A = 6710949
20 meter
Y = 308180
96 meter E =
0001403
Z = 5228520
60 I = 51
29966
XDOT = -979
850568 Wp = 97
66839
YDOT = 7638
012054 meter/sec RA = 279
31103 deg
ZDOT = 335
566112 TA = 349
13225
MA = 349
13528
Ha = 184
641 n
mi
Hp = 179
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13760776
77 X = 4165127
29
Y = 1011092
38 feet Y = 354919
95 meter
Z = 17153938
96 Z = 5248825
99
XDOT = -3214
732835 XDOT = -1066
817299
YDOT = 25059
094664 feet/sec YDOT = 7626
568499 meter/sec
ZDOT = 1100
938689 ZDOT = 330
595913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4033743
57 X = -1229485
04
Y = 13093863
91 feet Y = 3991009
72 meter
Z = 17231324
61 Z = 5252107
74
XDOT = -22754
263536 XDOT = -6935
499526
YDOT = -8435
791162 feet/sec YDOT = -2571
229146 meter/sec
ZDOT = 1082
767076 ZDOT = 330
027405
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
54808932
00020000 00000-0 20000-3 0 9027
2 25544 51
6392 279
7605 0001154 295
0423 65
0622 15
77227181 38441
Satellite: ISS
Catalog Number: 25544
Epoch time: 07343
54808932 = yrday
fracday
Element set: 902
Inclination: 51
6392 deg
RA of node: 279
7605 deg
Eccentricity:
0001154
Arg of perigee: 295
0423 deg
Mean anomaly: 65
0622 deg
Mean motion: 15
77227181 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3844
Checksum: 290
Coasting Arc #4 (Orbit 3859)
---------------------------------------
Vector Time (GMT): 2007/344/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1102621
77 A = 6722724
28 meter
Y = -6578525
99 meter E =
0013152
Z = 782003
59 I = 51
33579
XDOT = 4665
379466 Wp = 48
85731
YDOT = 1495
979542 meter/sec RA = 274
13236 deg
ZDOT = 5950
378195 TA = 319
71887
MA = 319
81624
Ha = 184
792 n
mi
Hp = 179
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3617525
50 X = 1172303
02
Y = -21583090
53 feet Y = -6565806
38 meter
Z = 2565628
59 Z = 787528
33
XDOT = 15306
363079 XDOT = 4619
398257
YDOT = 4908
069364 feet/sec YDOT = 1547
892351 meter/sec
ZDOT = 19522
238171 ZDOT = 5972
931443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20375676
16 X = 6210506
09
Y = 7977660
75 feet Y = 2431591
00 meter
Z = 2586017
70 Z = 788218
19
XDOT = -7355
402081 XDOT = -2241
926554
YDOT = 12370
858089 feet/sec YDOT = 3770
637545 meter/sec
ZDOT = 19608
314188 ZDOT = 5976
614164
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 07344
56184728
00020000 00000-0 20000-3 0 9031
2 25544 51
6389 274
5291 0001102 301
0297 59
0760 15
77235775 38603
Satellite: ISS
Catalog Number: 25544
Epoch time: 07344
56184728 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 274
5291 deg
Eccentricity:
0001102
Arg of perigee: 301
0297 deg
Mean anomaly: 59
0760 deg
Mean motion: 15
77235775 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3860
Checksum: 296
Coasting Arc #5 (Orbit 3874)
---------------------------------------
Vector Time (GMT): 2007/345/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3975892
64 A = 6712290
06 meter
Y = -2293766
64 meter E =
0011671
Z = -4908180
31 I = 51
30060
XDOT = 1560
887351 Wp = 103
83532
YDOT = -7233
647492 meter/sec RA = 268
92379 deg
ZDOT = 2117
593862 TA = 186
79782
MA = 186
81366
Ha = 184
756 n
mi
Hp = 178
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13044267
19 X = -3926104
68
Y = -7525481
11 feet Y = -2337948
11 meter
Z = -16102953
79 Z = -4927374
80
XDOT = 5121
021494 XDOT = 1631
372128
YDOT = -23732
439277 feet/sec YDOT = -7215
799026 meter/sec
ZDOT = 6947
486424 ZDOT = 2125
346682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9842819
00 X = 3000091
23
Y = -11293201
97 feet Y = -3442167
96 meter
Z = -16176322
10 Z = -4930542
98
XDOT = 21516
710160 XDOT = 6558
293257
YDOT = 8767
333948 feet/sec YDOT = 2672
283387 meter/sec
ZDOT = 6976
296097 ZDOT = 2126
375050
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 07345
51222277
00020000 00000-0 20000-3 0 9040
2 25544 51
6394 269
6249 0001113 305
4339 54
6722 15
77270617 38753
Satellite: ISS
Catalog Number: 25544
Epoch time: 07345
51222277 = yrday
fracday
Element set: 904
Inclination: 51
6394 deg
RA of node: 269
6249 deg
Eccentricity:
0001113
Arg of perigee: 305
4339 deg
Mean anomaly: 54
6722 deg
Mean motion: 15
77270617 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3875
Checksum: 295
Coasting Arc #6 (Orbit 3890)
---------------------------------------
Vector Time (GMT): 2007/346/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1652860
17 A = 6719195
60 meter
Y = 5858556
28 meter E =
0003561
Z = -2845804
67 I = 51
32659
XDOT = -4472
417961 Wp = 112
72330
YDOT = -3712
918971 meter/sec RA = 263
78133 deg
ZDOT = -5052
422043 TA = 100
12774
MA = 100
08756
Ha = 184
712 n
mi
Hp = 178
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5422769
58 X = -1704424
15
Y = 19220985
18 feet Y = 5839785
21 meter
Z = -9336629
51 Z = -2853958
59
XDOT = -14673
287273 XDOT = -4406
023315
YDOT = -12181
492686 feet/sec YDOT = -3762
560034 meter/sec
ZDOT = -16576
187804 ZDOT = -5073
988444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18006524
66 X = -5488388
72
Y = -8605103
06 feet Y = -2622835
41 meter
Z = -9367103
22 Z = -2855093
06
XDOT = 13886
365059 XDOT = 4232
564070
YDOT = -10946
555925 feet/sec YDOT = -3336
510246 meter/sec
ZDOT = -16658
749143 ZDOT = -5077
586739
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 07346
52593391
00020000 00000-0 20000-3 0 9051
2 25544 51
6398 264
3937 0001101 309
8827 50
2241 15
77316845 38910
Satellite: ISS
Catalog Number: 25544
Epoch time: 07346
52593391 = yrday
fracday
Element set: 905
Inclination: 51
6398 deg
RA of node: 264
3937 deg
Eccentricity:
0001101
Arg of perigee: 309
8827 deg
Mean anomaly: 50
2241 deg
Mean motion: 15
77316845 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3891
Checksum: 303
Coasting Arc #7 (Orbit 3906)
---------------------------------------
Vector Time (GMT): 2007/347/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3845189
08 A = 6716660
36 meter
Y = 4074680
25 meter E =
0011056
Z = 3697099
94 I = 51
32195
XDOT = -2262
163286 Wp = 79
57294
YDOT = 6012
293998 meter/sec RA = 258
54787 deg
ZDOT = -4260
794495 TA = 55
55508
MA = 55
45065
Ha = 184
644 n
mi
Hp = 178
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12615449
74 X = 3781379
76
Y = 13368373
53 feet Y = 4117322
02 meter
Z = 12129592
96 Z = 3715625
46
XDOT = -7421
795557 XDOT = -2308
527379
YDOT = 19725
374008 feet/sec YDOT = 5986
738589 meter/sec
ZDOT = -13978
984565 ZDOT = -4271
895830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15157113
84 X = -4619888
30
Y = 10314886
89 feet Y = 3143977
53 meter
Z = 12200615
42 Z = 3718747
58
XDOT = -17591
127334 XDOT = -5361
775612
YDOT = -9216
041876 feet/sec YDOT = -2809
049564 meter/sec
ZDOT = -14020
670104 ZDOT = -4273
500248
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 07347
53962221
00020000 00000-0 20000-3 0 9066
2 25544 51
6390 259
1625 0001066 312
1528 47
9547 15
77336384 39073
Satellite: ISS
Catalog Number: 25544
Epoch time: 07347
53962221 = yrday
fracday
Element set: 906
Inclination: 51
6390 deg
RA of node: 259
1625 deg
Eccentricity:
0001066
Arg of perigee: 312
1528 deg
Mean anomaly: 47
9547 deg
Mean motion: 15
77336384 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3907
Checksum: 301
Coasting Arc #8 (Orbit 3922)
---------------------------------------
Vector Time (GMT): 2007/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2352521
88 A = 6714016
64 meter
Y = -4475501
60 meter E =
0008193
Z = 4412158
33 I = 51
32051
XDOT = 4341
015705 Wp = 108
47997
YDOT = 5484
511941 meter/sec RA = 253
41363 deg
ZDOT = 3241
188991 TA = 308
89699
MA = 308
97003
Ha = 184
590 n
mi
Hp = 178
851
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7718247
64 X = 2380959
34
Y = -14683404
20 feet Y = -4449035
91 meter
Z = 14475585
08 Z = 4423655
39
XDOT = 14242
177510 XDOT = 4263
619340
YDOT = 17993
805580 feet/sec YDOT = 5532
622493 meter/sec
ZDOT = 10633
822148 ZDOT = 3262
090300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13484089
75 X = 4109950
56
Y = 9596672
60 feet Y = 2925065
81 meter
Z = 14518934
79 Z = 4425371
32
XDOT = -19084
976095 XDOT = -5817
100714
YDOT = 10569
490192 feet/sec YDOT = 3221
580611 meter/sec
ZDOT = 10714
058972 ZDOT = 3265
645175
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 07348
55328659
00020000 00000-0 20000-3 0 9071
2 25544 51
6391 253
9303 0001097 315
7520 44
3557 15
77380224 39236
Satellite: ISS
Catalog Number: 25544
Epoch time: 07348
55328659 = yrday
fracday
Element set: 907
Inclination: 51
6391 deg
RA of node: 253
9303 deg
Eccentricity:
0001097
Arg of perigee: 315
7520 deg
Mean anomaly: 44
3557 deg
Mean motion: 15
77380224 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3923
Checksum: 299
Coasting Arc #9 (Orbit 3937)
---------------------------------------
Vector Time (GMT): 2007/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3684532
26 A = 6720988
63 meter
Y = -5318571
82 meter E =
0007577
Z = -1806794
99 I = 51
35444
XDOT = 3210
633512 Wp = 29
66232
YDOT = -4138
252149 meter/sec RA = 248
18919 deg
ZDOT = 5650
806679 TA = 310
19441
MA = 310
26070
Ha = 184
552 n
mi
Hp = 178
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12088360
44 X = -3616008
27
Y = -17449382
61 feet Y = -5359391
03 meter
Z = -5927805
10 Z = -1824528
54
XDOT = 10533
574515 XDOT = 3229
218882
YDOT = -13576
942747 feet/sec YDOT = -4102
245687 meter/sec
ZDOT = 18539
391991 ZDOT = 5666
448646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18784359
90 X = 5725472
90
Y = -9846041
40 feet Y = -3001073
42 meter
Z = -5995963
38 Z = -1827569
64
XDOT = 11491
760722 XDOT = 3502
688668
YDOT = 10630
798946 feet/sec YDOT = 3240
267519 meter/sec
ZDOT = 18598
572860 ZDOT = 5668
845008
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 07349
50357636
00020000 00000-0 20000-3 0 9085
2 25544 51
6394 249
0252 0001169 317
0799 43
0275 15
77423301 39384
Satellite: ISS
Catalog Number: 25544
Epoch time: 07349
50357636 = yrday
fracday
Element set: 908
Inclination: 51
6394 deg
RA of node: 249
0252 deg
Eccentricity:
0001169
Arg of perigee: 317
0799 deg
Mean anomaly: 43
0275 deg
Mean motion: 15
77423301 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3938
Checksum: 301
Coasting Arc #10 (Orbit 3953)
---------------------------------------
Vector Time (GMT): 2007/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3316407
68 A = 6710444
58 meter
Y = 2662919
10 meter E =
0014148
Z = -5202664
52 I = 51
33148
XDOT = -4015
238617 Wp = 79
74789
YDOT = -6519
720554 meter/sec RA = 243
02977 deg
ZDOT = -776
854856 TA = 182
82006
MA = 182
82805
Ha = 184
540 n
mi
Hp = 178
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10880602
62 X = -3320664
71
Y = 8736611
21 feet Y = 2625809
79 meter
Z = -17069109
30 Z = -5218785
77
XDOT = -13173
355044 XDOT = -3938
261861
YDOT = -21390
159299 feet/sec YDOT = -6564
190765 meter/sec
ZDOT = -2548
736404 ZDOT = -796
174505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7563385
65 X = -2305319
95
Y = -11636979
20 feet Y = -3546951
26 meter
Z = -17130274
19 Z = -5221307
57
XDOT = 21798
116615 XDOT = 6644
065944
YDOT = -10302
903858 feet/sec YDOT = -3140
325096 meter/sec
ZDOT = -2623
080058 ZDOT = -799
514802
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 07350
51719685
00020000 00000-0 20000-3 0 9095
2 25544 51
6396 243
7929 0001226 322
3910 37
7169 15
77469049 39545
Satellite: ISS
Catalog Number: 25544
Epoch time: 07350
51719685 = yrday
fracday
Element set: 909
Inclination: 51
6396 deg
RA of node: 243
7929 deg
Eccentricity:
0001226
Arg of perigee: 322
3910 deg
Mean anomaly: 37
7169 deg
Mean motion: 15
77469049 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3954
Checksum: 322
Coasting Arc #11 (Orbit 3969)
---------------------------------------
Vector Time (GMT): 2007/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3224595
14 A = 6722278
79 meter
Y = 5872248
86 meter E =
0010076
Z = -494880
82 I = 51
38569
XDOT = -4437
138807 Wp = 138
98956
YDOT = 1937
782596 meter/sec RA = 237
84533 deg
ZDOT = -5994
560683 TA = 46
42048
MA = 46
33688
Ha = 184
556 n
mi
Hp = 178
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10579380
39 X = 3161095
16
Y = 19265908
34 feet Y = 5907953
10 meter
Z = -1623624
73 Z = -479369
43
XDOT = -14557
542018 XDOT = -4429
356937
YDOT = 6357
554449 feet/sec YDOT = 1888
207965 meter/sec
ZDOT = -19667
193841 ZDOT = -6016
097387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20116232
96 X = -6131427
81
Y = 8867140
85 feet Y = 2702704
53 meter
Z = -1563859
04 Z = -476664
23
XDOT = -4426
340554 XDOT = -1349
148601
YDOT = -13478
938783 feet/sec YDOT = -4108
380541 meter/sec
ZDOT = -19749
081781 ZDOT = -6019
520127
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 07351
53079627
00020000 00000-0 20000-3 0 9105
2 25544 51
6397 238
5604 0001161 318
0657 42
0419 15
77450119 39709
Satellite: ISS
Catalog Number: 25544
Epoch time: 07351
53079627 = yrday
fracday
Element set: 910
Inclination: 51
6397 deg
RA of node: 238
5604 deg
Eccentricity:
0001161
Arg of perigee: 318
0657 deg
Mean anomaly: 42
0419 deg
Mean motion: 15
77450119 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3970
Checksum: 286
Coasting Arc #12 (Orbit 3985)
---------------------------------------
Vector Time (GMT): 2007/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4436921
80 A = 6711116
23 meter
Y = -744569
74 meter E =
0005738
Z = 4977804
47 I = 51
36589
XDOT = 3247
376079 Wp = 40
84087
YDOT = 6733
000027 meter/sec RA = 232
64347 deg
ZDOT = -1881
908617 TA = 67
40148
MA = 67
34078
Ha = 184
257 n
mi
Hp = 178
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14556830
04 X = 4420736
39
Y = -2442814
10 feet Y = -695044
46 meter
Z = 16331379
49 Z = 4999319
90
XDOT = 10654
120993 XDOT = 3180
987365
YDOT = 22089
895101 feet/sec YDOT = 6768
942983 meter/sec
ZDOT = -6174
240869 ZDOT = -1866
293406
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1422897
65 X = 433699
20
Y = 14600030
74 feet Y = 4450089
37 meter
Z = 16413319
67 Z = 5002779
83
XDOT = -21720
159355 XDOT = -6620
304571
YDOT = 9010
332382 feet/sec YDOT = 2746
349310 meter/sec
ZDOT = -6113
980446 ZDOT = -1863
541240
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 07352
54437087
00020000 00000-0 20000-3 0 9116
2 25544 51
6398 233
3277 0001438 324
0625 36
0443 15
77561642 39869
Satellite: ISS
Catalog Number: 25544
Epoch time: 07352
54437087 = yrday
fracday
Element set: 911
Inclination: 51
6398 deg
RA of node: 233
3277 deg
Eccentricity:
0001438
Arg of perigee: 324
0625 deg
Mean anomaly: 36
0443 deg
Mean motion: 15
77561642 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3986
Checksum: 297
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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