Date:
December 14th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 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 3890)
---------------------------------------
Vector Time (GMT): 2007/346/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1688145
76 A = 6718822
45 meter
Y = 5828901
30 meter E =
0003538
Z = -2885169
38 I = 51
32629
XDOT = -4455
050877 Wp = 109
66651
YDOT = -3773
433698 meter/sec RA = 263
78474 deg
ZDOT = -5022
923575 TA = 103
69923
MA = 103
65984
Ha = 184
571 n
mi
Hp = 178
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5538535
95 X = -1739184
28
Y = 19123691
94 feet Y = 5809738
60 meter
Z = -9465778
80 Z = -2893493
44
XDOT = -14616
308650 XDOT = -4388
124136
YDOT = -12380
031817 feet/sec YDOT = -3822
877582 meter/sec
ZDOT = -16479
408056 ZDOT = -5044
404325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17890846
17 X = -5453129
91
Y = -8701630
95 feet Y = -2652257
11 meter
Z = -9496903
91 Z = -2894656
31
XDOT = 14065
154574 XDOT = 4287
059114
YDOT = -10865
157834 feet/sec YDOT = -3311
700108 meter/sec
ZDOT = -16561
649180 ZDOT = -5047
990670
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
52584167
00020000 00000-0 20000-3 0 9007
2 25544 51
6399 264
3976 0001108 311
5355 48
5715 15
77413310 38918
Satellite: ISS
Catalog Number: 25544
Epoch time: 07346
52584167 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 264
3976 deg
Eccentricity:
0001108
Arg of perigee: 311
5355 deg
Mean anomaly: 48
5715 deg
Mean motion: 15
77413310 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3891
Checksum: 297
Coasting Arc #2 (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 = 3813215
49 A = 6716513
65 meter
Y = 4156746
44 meter E =
0011208
Z = 3637942
04 I = 51
32263
XDOT = -2331
813414 Wp = 80
83793
YDOT = 5937
878119 meter/sec RA = 258
55028 deg
ZDOT = -4327
435221 TA = 55
19424
MA = 55
08883
Ha = 184
466 n
mi
Hp = 178
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12510549
51 X = 3748778
25
Y = 13637619
54 feet Y = 4199027
16 meter
Z = 11935505
36 Z = 3656310
72
XDOT = -7650
306475 XDOT = -2377
016472
YDOT = 19481
227424 feet/sec YDOT = 5911
550345 meter/sec
ZDOT = -14197
622115 ZDOT = -4338
872106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15406938
72 X = -4696034
92
Y = 10170471
08 feet Y = 3099959
59 meter
Z = 12005938
59 Z = 3659410
08
XDOT = -17325
134599 XDOT = -5280
701026
YDOT = -9384
359160 feet/sec YDOT = -2860
352672 meter/sec
ZDOT = -14240
594141 ZDOT = -4340
533094
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
53946030
00020000 00000-0 20000-3 0 9011
2 25544 51
6391 259
1659 0001062 312
4948 47
6127 15
77455377 39071
Satellite: ISS
Catalog Number: 25544
Epoch time: 07347
53946030 = yrday
fracday
Element set: 901
Inclination: 51
6391 deg
RA of node: 259
1659 deg
Eccentricity:
0001062
Arg of perigee: 312
4948 deg
Mean anomaly: 47
6127 deg
Mean motion: 15
77455377 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3907
Checksum: 304
Coasting Arc #3 (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 = 2442518
99 A = 6713349
29 meter
Y = -4359361
79 meter E =
0007866
Z = 4478281
57 I = 51
31965
XDOT = 4274
962886 Wp = 110
29879
YDOT = 5606
321983 meter/sec RA = 253
41450 deg
ZDOT = 3118
708828 TA = 308
45338
MA = 308
52395
Ha = 184
365 n
mi
Hp = 178
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8013513
73 X = 2469329
85
Y = -14302368
06 feet Y = -4331898
80 meter
Z = 14692524
83 Z = 4490211
89
XDOT = 14025
468787 XDOT = 4196
804318
YDOT = 18393
444826 feet/sec YDOT = 5653
689649 meter/sec
ZDOT = 10231
984345 ZDOT = 3139
287417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13065997
84 X = 3982516
14
Y = 9835094
97 feet Y = 2997736
95 meter
Z = 14737538
04 Z = 4492001
59
XDOT = -19433
673801 XDOT = -5923
383775
YDOT = 10332
252028 feet/sec YDOT = 3149
270418 meter/sec
ZDOT = 10311
003950 ZDOT = 3142
794004
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
55304012
00020000 00000-0 20000-3 0 9023
2 25544 51
6392 253
9332 0001083 314
8075 45
3002 15
77523261 39235
Satellite: ISS
Catalog Number: 25544
Epoch time: 07348
55304012 = yrday
fracday
Element set: 902
Inclination: 51
6392 deg
RA of node: 253
9332 deg
Eccentricity:
0001083
Arg of perigee: 314
8075 deg
Mean anomaly: 45
3002 deg
Mean motion: 15
77523261 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3923
Checksum: 260
Coasting Arc #4 (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 = -3588073
40 A = 6720781
31 meter
Y = -5436438
63 meter E =
0008088
Z = -1640303
62 I = 51
35530
XDOT = 3350
971076 Wp = 29
50271
YDOT = -3931
093951 meter/sec RA = 248
19081 deg
ZDOT = 5717
585485 TA = 312
27772
MA = 312
34627
Ha = 184
297 n
mi
Hp = 178
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11771894
34 X = -3519047
35
Y = -17836084
75 feet Y = -5476176
39 meter
Z = -5381573
56 Z = -1657567
36
XDOT = 10993
999592 XDOT = 3366
905142
YDOT = -12897
289866 feet/sec YDOT = -3893
532986 meter/sec
ZDOT = 18758
482563 ZDOT = 5733
902793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19130136
12 X = 5830865
49
Y = -9488015
72 feet Y = -2891947
19 meter
Z = -5447953
67 Z = -1660536
28
XDOT = 10787
475205 XDOT = 3288
022442
YDOT = 10978
814770 feet/sec YDOT = 3346
342742 meter/sec
ZDOT = 18820
259570 ZDOT = 5736
415117
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
50323729
00020000 00000-0 20000-3 0 9036
2 25544 51
6394 249
0274 0001155 315
5346 44
5726 15
77586117 39386
Satellite: ISS
Catalog Number: 25544
Epoch time: 07349
50323729 = yrday
fracday
Element set: 903
Inclination: 51
6394 deg
RA of node: 249
0274 deg
Eccentricity:
0001155
Arg of perigee: 315
5346 deg
Mean anomaly: 44
5726 deg
Mean motion: 15
77586117 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3938
Checksum: 304
Coasting Arc #5 (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 = -3468992
48 A = 6709799
44 meter
Y = 2406545
75 meter E =
0014264
Z = -5227273
81 I = 51
33109
XDOT = -3842
444355 Wp = 82
14085
YDOT = -6649
194760 meter/sec RA = 243
02640 deg
ZDOT = -510
464528 TA = 182
98193
MA = 182
99044
Ha = 184
242 n
mi
Hp = 178
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11381208
94 X = -3470251
82
Y = 7895491
30 feet Y = 2367746
91 meter
Z = -17149848
47 Z = -5244129
07
XDOT = -12606
444734 XDOT = -3765
326719
YDOT = -21814
943439 feet/sec YDOT = -6691
731923 meter/sec
ZDOT = -1674
752389 ZDOT = -528
944410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6674660
31 X = -2034436
46
Y = -12046603
95 feet Y = -3671804
88 meter
Z = -17213838
78 Z = -5246778
06
XDOT = 22132
059129 XDOT = 6745
851622
YDOT = -9764
479458 feet/sec YDOT = -2976
213339 meter/sec
ZDOT = -1745
908933 ZDOT = -532
153043
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
51674483
00020000 00000-0 20000-3 0 9046
2 25544 51
6397 243
7943 0001201 319
8460 40
2616 15
77654625 39548
Satellite: ISS
Catalog Number: 25544
Epoch time: 07350
51674483 = yrday
fracday
Element set: 904
Inclination: 51
6397 deg
RA of node: 243
7943 deg
Eccentricity:
0001201
Arg of perigee: 319
8460 deg
Mean anomaly: 40
2616 deg
Mean motion: 15
77654625 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3954
Checksum: 296
Coasting Arc #6 (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 = 2998576
12 A = 6721522
37 meter
Y = 5958426
44 meter E =
0009331
Z = -791824
73 I = 51
38517
XDOT = -4641
120661 Wp = 141
72231
YDOT = 1550
509125 meter/sec RA = 237
84563 deg
ZDOT = -5952
621217 TA = 46
95473
MA = 46
87663
Ha = 184
213 n
mi
Hp = 178
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9837848
16 X = 2935571
79
Y = 19548643
19 feet Y = 5991606
01 meter
Z = -2597850
18 Z = -777410
14
XDOT = -15226
773823 XDOT = -4629
196816
YDOT = 5086
972196 feet/sec YDOT = 1498
676609 meter/sec
ZDOT = -19529
597169 ZDOT = -5975
138840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20333675
40 X = -6197704
26
Y = 8109260
80 feet Y = 2471702
69 meter
Z = -2542256
14 Z = -774879
67
XDOT = -3157
414390 XDOT = -962
379906
YDOT = -14019
673338 feet/sec YDOT = -4273
196434 meter/sec
ZDOT = -19615
266335 ZDOT = -5978
733179
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
53021673
00020000 00000-0 20000-3 0 9057
2 25544 51
6398 238
5609 0001156 314
0339 46
0731 15
77659163 39703
Satellite: ISS
Catalog Number: 25544
Epoch time: 07351
53021673 = yrday
fracday
Element set: 905
Inclination: 51
6398 deg
RA of node: 238
5609 deg
Eccentricity:
0001156
Arg of perigee: 314
0339 deg
Mean anomaly: 46
0731 deg
Mean motion: 15
77659163 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3970
Checksum: 292
Coasting Arc #7 (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 = 4625679
09 A = 6711010
79 meter
Y = -327366
14 meter E =
0006587
Z = 4848731
03 I = 51
36776
XDOT = 2879
132124 Wp = 45
50542
YDOT = 6776
860803 meter/sec RA = 232
63639 deg
ZDOT = -2282
684213 TA = 66
80499
MA = 66
73563
Ha = 183
881 n
mi
Hp = 178
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15176112
50 X = 4605441
45
Y = -1074035
90 feet Y = -275752
72 meter
Z = 15907910
20 Z = 4871153
64
XDOT = 9445
971536 XDOT = 2814
227237
YDOT = 22233
795287 feet/sec YDOT = 6808
694176 meter/sec
ZDOT = -7489
121435 ZDOT = -2268
854343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13909
71 X = 4239
68
Y = 15124218
39 feet Y = 4609861
76 meter
Z = 15993354
11 Z = 4874774
33
XDOT = -21741
315524 XDOT = -6626
752972
YDOT = 7905
238726 feet/sec YDOT = 2409
516764 meter/sec
ZDOT = -7435
662312 ZDOT = -2266
389873
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
54364965
00020000 00000-0 20000-3 0 9064
2 25544 51
6399 233
3273 0001427 321
2112 38
8951 15
77793234 39862
Satellite: ISS
Catalog Number: 25544
Epoch time: 07352
54364965 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 233
3273 deg
Eccentricity:
0001427
Arg of perigee: 321
2112 deg
Mean anomaly: 38
8951 deg
Mean motion: 15
77793234 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3986
Checksum: 308
Coasting Arc #8 (Orbit 4001)
---------------------------------------
Vector Time (GMT): 2007/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1850478
10 A = 6717293
50 meter
Y = -5664806
42 meter E =
0012585
Z = 3086245
02 I = 51
40730
XDOT = 5933
912350 Wp = 79
24013
YDOT = 722
601235 meter/sec RA = 227
49682 deg
ZDOT = 4869
812276 TA = 316
80129
MA = 316
89995
Ha = 184
087 n
mi
Hp = 178
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6071122
36 X = -1801988
47
Y = -18585322
90 feet Y = -5685228
70 meter
Z = 10125475
78 Z = 3077372
49
XDOT = 19468
216371 XDOT = 5901
734079
YDOT = 2370
738960 feet/sec YDOT = 788
777210 meter/sec
ZDOT = 15977
074397 ZDOT = 4898
561554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18883621
04 X = 5755727
69
Y = -5135941
69 feet Y = -1565435
03 meter
Z = 10091034
30 Z = 3075747
25
XDOT = -3767
549918 XDOT = -1148
349215
YDOT = 17848
028614 feet/sec YDOT = 5440
079121 meter/sec
ZDOT = 16086
757937 ZDOT = 4903
243819
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 07353
55705056
00020000 00000-0 20000-3 0 9077
2 25544 51
6397 228
0932 0001430 328
6960 31
4120 15
77787285 40025
Satellite: ISS
Catalog Number: 25544
Epoch time: 07353
55705056 = yrday
fracday
Element set: 907
Inclination: 51
6397 deg
RA of node: 228
0932 deg
Eccentricity:
0001430
Arg of perigee: 328
6960 deg
Mean anomaly: 31
4120 deg
Mean motion: 15
77787285 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4002
Checksum: 284
Coasting Arc #9 (Orbit 4016)
---------------------------------------
Vector Time (GMT): 2007/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5620801
61 A = 6716178
21 meter
Y = -1478422
10 meter E =
0004202
Z = -3367969
56 I = 51
42475
XDOT = -1174
814497 Wp = 73
95262
YDOT = -6048
817963 meter/sec RA = 222
26499 deg
ZDOT = 4621
774037 TA = 246
15624
MA = 246
20029
Ha = 183
880 n
mi
Hp = 178
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18440950
17 X = -5587490
67
Y = -4850466
20 feet Y = -1541090
41 meter
Z = -11049768
91 Z = -3395195
14
XDOT = -3854
378272 XDOT = -1129
540482
YDOT = -19845
203291 feet/sec YDOT = -6061
702856 meter/sec
ZDOT = 15163
300646 ZDOT = 4616
175895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5504255
66 X = 1677697
13
Y = -18193142
90 feet Y = -5545269
95 meter
Z = -11153733
89 Z = -3399658
09
XDOT = 18646
673593 XDOT = 5683
506111
YDOT = -3629
494305 feet/sec YDOT = -1106
269864 meter/sec
ZDOT = 15141
301687 ZDOT = 4615
068754
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 07354
50707875
00020000 00000-0 20000-3 0 9085
2 25544 51
6394 223
1864 0001550 324
7685 35
3377 15
77854521 40177
Satellite: ISS
Catalog Number: 25544
Epoch time: 07354
50707875 = yrday
fracday
Element set: 908
Inclination: 51
6394 deg
RA of node: 223
1864 deg
Eccentricity:
0001550
Arg of perigee: 324
7685 deg
Mean anomaly: 35
3377 deg
Mean motion: 15
77854521 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4017
Checksum: 304
Coasting Arc #10 (Orbit 4032)
---------------------------------------
Vector Time (GMT): 2007/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 29843
56 A = 6711267
03 meter
Y = 4762626
79 meter E =
0011146
Z = -4738993
02 I = 51
42997
XDOT = -6786
732887 Wp = 63
68061
YDOT = -2541
347333 meter/sec RA = 217
13086 deg
ZDOT = -2596
598629 TA = 180
76082
MA = 180
76251
Ha = 183
844 n
mi
Hp = 178
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 97911
93 X = -393
57
Y = 15625415
96 feet Y = 4762792
21 meter
Z = -15547877
37 Z = -4738920
72
XDOT = -22266
184012 XDOT = -6745
196758
YDOT = -8337
753717 feet/sec YDOT = -2617
007771 meter/sec
ZDOT = -8519
024374 ZDOT = -2629
468579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15626160
17 X = -4762853
62
Y = -104110
27 feet Y = -31732
81 meter
Z = -15547089
15 Z = -4738752
77
XDOT = 8740
801865 XDOT = 2664
196408
YDOT = -20919
776826 feet/sec YDOT = -6376
347976 meter/sec
ZDOT = -8644
637985 ZDOT = -2634
885658
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 07355
52040872
00020000 00000-0 20000-3 0 9096
2 25544 51
6384 217
9520 0001611 326
7065 33
3999 15
77914535 40336
Satellite: ISS
Catalog Number: 25544
Epoch time: 07355
52040872 = yrday
fracday
Element set: 909
Inclination: 51
6384 deg
RA of node: 217
9520 deg
Eccentricity:
0001611
Arg of perigee: 326
7065 deg
Mean anomaly: 33
3999 deg
Mean motion: 15
77914535 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4033
Checksum: 294
Coasting Arc #11 (Orbit 4048)
---------------------------------------
Vector Time (GMT): 2007/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6017227
64 A = 6720489
51 meter
Y = 2805490
08 meter E =
0012499
Z = 1005829
69 I = 51
48545
XDOT = -1232
166616 Wp = 120
88770
YDOT = 4781
761399 meter/sec RA = 211
92206 deg
ZDOT = -5918
363274 TA = 48
07553
MA = 47
96903
Ha = 183
844 n
mi
Hp = 177
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19741560
50 X = 5980522
82
Y = 9204363
77 feet Y = 2872572
71 meter
Z = 3299966
17 Z = 1034973
04
XDOT = -4042
541392 XDOT = -1256
794811
YDOT = 15688
193565 feet/sec YDOT = 4767
846020 meter/sec
ZDOT = -19417
202343 ZDOT = -5924
408124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9230899
09 X = -2813578
04
Y = 19710202
11 feet Y = 6007669
60 meter
Z = 3411412
48 Z = 1039798
52
XDOT = -14245
575719 XDOT = -4342
051479
YDOT = -3280
779887 feet/sec YDOT = -999
981710 meter/sec
ZDOT = -19439
743366 ZDOT = -5925
233778
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 07356
53370471
00020000 00000-0 20000-3 0 9101
2 25544 51
6382 212
7180 0001500 332
3692 27
7393 15
77950972 40492
Satellite: ISS
Catalog Number: 25544
Epoch time: 07356
53370471 = yrday
fracday
Element set: 910
Inclination: 51
6382 deg
RA of node: 212
7180 deg
Eccentricity:
0001500
Arg of perigee: 332
3692 deg
Mean anomaly: 27
7393 deg
Mean motion: 15
77950972 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4049
Checksum: 285
Coasting Arc #12 (Orbit 4064)
---------------------------------------
Vector Time (GMT): 2007/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2245385
18 A = 6708713
80 meter
Y = -3538431
78 meter E =
0002719
Z = 5237395
08 I = 51
47064
XDOT = 6738
903044 Wp = 39
20553
YDOT = 3726
245897 meter/sec RA = 206
75080 deg
ZDOT = -369
448203 TA = 54
31919
MA = 54
29388
Ha = 183
680 n
mi
Hp = 177
862
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7366749
28 X = 2259343
21
Y = -11609028
16 feet Y = -3513245
62 meter
Z = 17183054
71 Z = 5248336
38
XDOT = 22109
261954 XDOT = 6698
529460
YDOT = 12225
216196 feet/sec YDOT = 3801
378464 meter/sec
ZDOT = -1212
100404 ZDOT = -336
807848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11722813
10 X = 3573113
43
Y = 7084578
77 feet Y = 2159379
61 meter
Z = 17224409
88 Z = 5250000
13
XDOT = -11356
398262 XDOT = -3461
430190
YDOT = 21451
976360 feet/sec YDOT = 6538
562394 meter/sec
ZDOT = -1087
198876 ZDOT = -331
378217
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 07357
54696381
00020000 00000-0 20000-3 0 9115
2 25544 51
6372 207
4825 0001620 333
2546 26
8535 15
78014724 40652
Satellite: ISS
Catalog Number: 25544
Epoch time: 07357
54696381 = yrday
fracday
Element set: 911
Inclination: 51
6372 deg
RA of node: 207
4825 deg
Eccentricity:
0001620
Arg of perigee: 333
2546 deg
Mean anomaly: 26
8535 deg
Mean motion: 15
78014724 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4065
Checksum: 289
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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