Date:
December 12th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10440 99 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 3874)
---------------------------------------
Vector Time (GMT): 2007/345/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3970027
52 A = 6712148
67 meter
Y = -2320053
62 meter E =
0011706
Z = -4900401
18 I = 51
30074
XDOT = 1580
086674 Wp = 103
91847
YDOT = -7222
667964 meter/sec RA = 268
92632 deg
ZDOT = 2140
911772 TA = 186
95211
MA = 186
96836
Ha = 184
693 n
mi
Hp = 178
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13025024
68 X = -3919983
84
Y = -7611724
46 feet Y = -2364168
07 meter
Z = -16077431
69 Z = -4919566
55
XDOT = 5184
011396 XDOT = 1650
333973
YDOT = -23696
417204 feet/sec YDOT = -7204
606132 meter/sec
ZDOT = 7023
988752 ZDOT = 2148
757288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9923883
50 X = 3024799
69
Y = -11258113
50 feet Y = -3431473
00 meter
Z = -16150691
74 Z = -4922730
84
XDOT = 21472
049406 XDOT = 6544
680659
YDOT = 8816
023957 feet/sec YDOT = 2687
124102 meter/sec
ZDOT = 7053
152736 ZDOT = 2149
800954
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
51218059
00020000 00000-0 20000-3 0 9009
2 25544 51
6395 269
6279 0001038 307
9436 52
1636 15
77332049 38753
Satellite: ISS
Catalog Number: 25544
Epoch time: 07345
51218059 = yrday
fracday
Element set: 900
Inclination: 51
6395 deg
RA of node: 269
6279 deg
Eccentricity:
0001038
Arg of perigee: 307
9436 deg
Mean anomaly: 52
1636 deg
Mean motion: 15
77332049 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3875
Checksum: 304
Coasting Arc #2 (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 = -1685321
74 A = 6718905
83 meter
Y = 5831312
05 meter E =
0003623
Z = -2882116
05 I = 51
32630
XDOT = -4456
475461 Wp = 110
21858
YDOT = -3768
569731 meter/sec RA = 263
78371 deg
ZDOT = -5025
256914 TA = 103
10683
MA = 103
06639
Ha = 184
635 n
mi
Hp = 178
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5529270
79 X = -1736402
26
Y = 19131601
20 feet Y = 5812180
68 meter
Z = -9455761
32 Z = -2890426
50
XDOT = -14620
982483 XDOT = -4389
591669
YDOT = -12364
073919 feet/sec YDOT = -3818
029785 meter/sec
ZDOT = -16487
063366 ZDOT = -5046
744688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17900225
34 X = -5455988
68
Y = -8693924
88 feet Y = -2649908
30 meter
Z = -9486834
30 Z = -2891587
09
XDOT = 14050
796604 XDOT = 4282
682805
YDOT = -10871
787765 feet/sec YDOT = -3313
720911 meter/sec
ZDOT = -16569
330761 ZDOT = -5050
332016
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
52584953
00020000 00000-0 20000-3 0 9011
2 25544 51
6398 264
3965 0001022 312
1015 48
0063 15
77386669 38917
Satellite: ISS
Catalog Number: 25544
Epoch time: 07346
52584953 = yrday
fracday
Element set: 901
Inclination: 51
6398 deg
RA of node: 264
3965 deg
Eccentricity:
0001022
Arg of perigee: 312
1015 deg
Mean anomaly: 48
0063 deg
Mean motion: 15
77386669 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3891
Checksum: 300
Coasting Arc #3 (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 = 3819113
68 A = 6716596
90 meter
Y = 4141914
65 meter E =
0011248
Z = 3648744
11 I = 51
32250
XDOT = -2319
182691 Wp = 80
85905
YDOT = 5951
538137 meter/sec RA = 258
54952 deg
ZDOT = -4315
427880 TA = 55
00908
MA = 54
90353
Ha = 184
553 n
mi
Hp = 178
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12529900
51 X = 3754789
38
Y = 13588958
82 feet Y = 4184261
96 meter
Z = 11970945
23 Z = 3667141
72
XDOT = -7608
867098 XDOT = -2364
597766
YDOT = 19526
043757 feet/sec YDOT = 5925
350420 meter/sec
ZDOT = -14158
227953 ZDOT = -4326
803919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15361848
69 X = -4682291
48
Y = 10196956
92 feet Y = 3108032
47 meter
Z = 12041487
15 Z = 3670245
28
XDOT = -17373
884626 XDOT = -5295
560034
YDOT = -9353
902770 feet/sec YDOT = -2851
069564 meter/sec
ZDOT = -14200
966677 ZDOT = -4328
454643
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
53949037
00020000 00000-0 20000-3 0 9022
2 25544 51
6391 259
1650 0000983 313
4760 46
6323 15
77413839 39070
Satellite: ISS
Catalog Number: 25544
Epoch time: 07347
53949037 = yrday
fracday
Element set: 902
Inclination: 51
6391 deg
RA of node: 259
1650 deg
Eccentricity:
0000983
Arg of perigee: 313
4760 deg
Mean anomaly: 46
6323 deg
Mean motion: 15
77413839 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3907
Checksum: 304
Coasting Arc #4 (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 = 2420296
12 A = 6713574
39 meter
Y = -4388474
89 meter E =
0008029
Z = 4462111
08 I = 51
31986
XDOT = 4291
592214 Wp = 109
89222
YDOT = 5576
386451 meter/sec RA = 253
41425 deg
ZDOT = 3149
277338 TA = 308
51825
MA = 308
59022
Ha = 184
478 n
mi
Hp = 178
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7940604
08 X = 2447512
74
Y = -14397883
50 feet Y = -4361258
14 meter
Z = 14639472
06 Z = 4473934
43
XDOT = 14080
026950 XDOT = 4213
618658
YDOT = 18295
231138 feet/sec YDOT = 5623
941106 meter/sec
ZDOT = 10332
274732 ZDOT = 3169
937158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13170650
06 X = 4014414
14
Y = 9776416
40 feet Y = 2979851
72 meter
Z = 14684074
50 Z = 4475705
91
XDOT = -19348
164452 XDOT = -5897
320525
YDOT = 10391
695453 feet/sec YDOT = 3167
388774 meter/sec
ZDOT = 10411
600795 ZDOT = 3173
455922
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
55310208
00020000 00000-0 20000-3 0 9038
2 25544 51
6391 253
9325 0001010 316
6987 43
4099 15
77466635 39234
Satellite: ISS
Catalog Number: 25544
Epoch time: 07348
55310208 = yrday
fracday
Element set: 903
Inclination: 51
6391 deg
RA of node: 253
9325 deg
Eccentricity:
0001010
Arg of perigee: 316
6987 deg
Mean anomaly: 43
4099 deg
Mean motion: 15
77466635 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3923
Checksum: 294
Coasting Arc #5 (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 = -3617123
24 A = 6720907
81 meter
Y = -5402235
51 meter E =
0007946
Z = -1689868
40 I = 51
35505
XDOT = 3309
770136 Wp = 30
09949
YDOT = -3992
875556 meter/sec RA = 248
19049 deg
ZDOT = 5698
418178 TA = 311
11085
MA = 311
17942
Ha = 184
432 n
mi
Hp = 178
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11867202
25 X = -3548236
73
Y = -17723869
77 feet Y = -5442298
89 meter
Z = -5544187
65 Z = -1707273
60
XDOT = 10858
825906 XDOT = 3326
491227
YDOT = -13099
985421 feet/sec YDOT = -3955
770921 meter/sec
ZDOT = 18695
597698 ZDOT = 5714
537237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19030216
38 X = 5800409
95
Y = -9595334
78 feet Y = -2924658
04 meter
Z = -5611103
31 Z = -1710264
29
XDOT = 10997
219082 XDOT = 3351
952376
YDOT = 10876
902166 feet/sec YDOT = 3315
279780 meter/sec
ZDOT = 18756
612497 ZDOT = 5717
015489
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
50333784
00020000 00000-0 20000-3 0 9049
2 25544 51
6394 249
0270 0001083 317
6666 42
4415 15
77515686 39385
Satellite: ISS
Catalog Number: 25544
Epoch time: 07349
50333784 = yrday
fracday
Element set: 904
Inclination: 51
6394 deg
RA of node: 249
0270 deg
Eccentricity:
0001083
Arg of perigee: 317
6666 deg
Mean anomaly: 42
4415 deg
Mean motion: 15
77515686 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3938
Checksum: 306
Coasting Arc #6 (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 = -3419030
28 A = 6710075
30 meter
Y = 2492451
04 meter E =
0014303
Z = -5220323
37 I = 51
33120
XDOT = -3900
751857 Wp = 81
52285
YDOT = -6607
480332 meter/sec RA = 243
02785 deg
ZDOT = -599
288340 TA = 182
74957
MA = 182
75744
Ha = 184
402 n
mi
Hp = 178
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11217290
93 X = -3421287
70
Y = 8177332
80 feet Y = 2454205
33 meter
Z = -17127045
17 Z = -5236938
32
XDOT = -12797
742312 XDOT = -3823
664854
YDOT = -21678
085080 feet/sec YDOT = -6650
669686 meter/sec
ZDOT = -1966
169093 ZDOT = -618
051551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6972056
73 X = -2125082
89
Y = -11913127
12 feet Y = -3631121
15 meter
Z = -17190110
26 Z = -5239545
61
XDOT = 22025
474818 XDOT = 6713
364725
YDOT = -9945
689964 feet/sec YDOT = -3031
446301 meter/sec
ZDOT = -2038
401148 ZDOT = -621
304670
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
51689576
00020000 00000-0 20000-3 0 9056
2 25544 51
6397 243
7942 0001135 322
6137 37
4949 15
77569520 39542
Satellite: ISS
Catalog Number: 25544
Epoch time: 07350
51689576 = yrday
fracday
Element set: 905
Inclination: 51
6397 deg
RA of node: 243
7942 deg
Eccentricity:
0001135
Arg of perigee: 322
6137 deg
Mean anomaly: 37
4949 deg
Mean motion: 15
77569520 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3954
Checksum: 320
Coasting Arc #7 (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 = 3081610
63 A = 6721874
14 meter
Y = 5929498
63 meter E =
0009685
Z = -684487
69 I = 51
38540
XDOT = -4568
894615 Wp = 140
56304
YDOT = 1691
495165 meter/sec RA = 237
84599 deg
ZDOT = -5970
060875 TA = 46
93024
MA = 46
84921
Ha = 184
400 n
mi
Hp = 178
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10110271
08 X = 3018402
18
Y = 19453735
65 feet Y = 5963605
58 meter
Z = -2245694
53 Z = -669670
21
XDOT = -14989
811730 XDOT = -4558
467946
YDOT = 5549
524821 feet/sec YDOT = 1640
461952 meter/sec
ZDOT = -19586
813895 ZDOT = -5992
231248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20262723
54 X = -6176078
14
Y = 8386939
94 feet Y = 2556339
29 meter
Z = -2188567
82 Z = -667075
47
XDOT = -3618
656284 XDOT = -1102
966435
YDOT = -13828
826256 feet/sec YDOT = -4215
026243 meter/sec
ZDOT = -19671
144065 ZDOT = -5995
764711
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
53042750
00020000 00000-0 20000-3 0 9067
2 25544 51
6398 238
5612 0001078 317
0649 43
0432 15
77559127 39701
Satellite: ISS
Catalog Number: 25544
Epoch time: 07351
53042750 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 238
5612 deg
Eccentricity:
0001078
Arg of perigee: 317
0649 deg
Mean anomaly: 43
0432 deg
Mean motion: 15
77559127 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3970
Checksum: 290
Coasting Arc #8 (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 = 4555361
13 A = 6711110
63 meter
Y = -489054
10 meter E =
0006285
Z = 4901613
77 I = 51
36701
XDOT = 3023
381281 Wp = 44
34428
YDOT = 6763
962331 meter/sec RA = 232
63966 deg
ZDOT = -2128
864532 TA = 66
39208
MA = 66
32610
Ha = 184
087 n
mi
Hp = 178
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14945410
53 X = 4536679
83
Y = -1604508
19 feet Y = -438218
31 meter
Z = 16081410
02 Z = 4923698
54
XDOT = 9919
229923 XDOT = 2957
862669
YDOT = 22191
477463 feet/sec YDOT = 6797
405335 meter/sec
ZDOT = -6984
463687 ZDOT = -2114
335384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 559317
04 X = 170479
83
Y = 14930294
69 feet Y = 4550753
82 meter
Z = 16165548
42 Z = 4927259
16
XDOT = -21746
216580 XDOT = -6628
246813
YDOT = 8337
677350 feet/sec YDOT = 2541
324056 meter/sec
ZDOT = -6928
340181 ZDOT = -2111
758087
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
54392952
00020000 00000-0 20000-3 0 9072
2 25544 51
6399 233
3281 0001354 323
8371 36
2703 15
77678910 39865
Satellite: ISS
Catalog Number: 25544
Epoch time: 07352
54392952 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 233
3281 deg
Eccentricity:
0001354
Arg of perigee: 323
8371 deg
Mean anomaly: 36
2703 deg
Mean motion: 15
77678910 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3986
Checksum: 309
Coasting Arc #9 (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 = -2030572
67 A = 6718053
72 meter
Y = -5683721
12 meter E =
0012969
Z = 2935727
02 I = 51
40863
XDOT = 5855
600112 Wp = 76
88679
YDOT = 494
149855 meter/sec RA = 227
49933 deg
ZDOT = 4991
345621 TA = 317
14272
MA = 317
24372
Ha = 184
315 n
mi
Hp = 178
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6661983
82 X = -1981126
95
Y = -18647378
99 feet Y = -5706151
96 meter
Z = 9631650
31 Z = 2925981
89
XDOT = 19211
286457 XDOT = 5825
391844
YDOT = 1621
226560 feet/sec YDOT = 559
461101 meter/sec
ZDOT = 16375
805842 ZDOT = 5019
719214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18976714
96 X = 5784102
72
Y = -5719896
31 feet Y = -1743424
40 meter
Z = 9593880
07 Z = 2924214
65
XDOT = -3047
953191 XDOT = -929
016133
YDOT = 17622
095664 feet/sec YDOT = 5371
214758 meter/sec
ZDOT = 16484
032285 ZDOT = 5024
333041
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
55740884
00020000 00000-0 20000-3 0 9086
2 25544 51
6397 228
0945 0001374 331
8787 28
2304 15
77659771 40025
Satellite: ISS
Catalog Number: 25544
Epoch time: 07353
55740884 = yrday
fracday
Element set: 908
Inclination: 51
6397 deg
RA of node: 228
0945 deg
Eccentricity:
0001374
Arg of perigee: 331
8787 deg
Mean anomaly: 28
2304 deg
Mean motion: 15
77659771 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4002
Checksum: 313
Coasting Arc #10 (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 = -5571220
26 A = 6716055
09 meter
Y = -1247671
55 meter E =
0004595
Z = -3540460
64 I = 51
42297
XDOT = -1453
852181 Wp = 84
11221
YDOT = -6116
653339 meter/sec RA = 222
26888 deg
ZDOT = 4448
692312 TA = 233
50069
MA = 233
54302
Ha = 184
135 n
mi
Hp = 178
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18278281
68 X = -5539655
34
Y = -4093410
58 feet Y = -1309795
15 meter
Z = -11615684
52 Z = -3567449
56
XDOT = -4769
856236 XDOT = -1406
958067
YDOT = -20067
760298 feet/sec YDOT = -6132
649509 meter/sec
ZDOT = 14595
447219 ZDOT = 4441
742510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4741755
76 X = 1445287
16
Y = -18054446
00 feet Y = -5502995
14 meter
Z = -11718722
20 Z = -3571866
53
XDOT = 18911
808867 XDOT = 5764
319343
YDOT = -4477
610763 feet/sec YDOT = -1364
775761 meter/sec
ZDOT = 14568
287347 ZDOT = 4440
413983
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
50751901
00020000 00000-0 20000-3 0 9095
2 25544 51
6393 223
1883 0001468 327
8436 32
2639 15
77713680 40170
Satellite: ISS
Catalog Number: 25544
Epoch time: 07354
50751901 = yrday
fracday
Element set: 909
Inclination: 51
6393 deg
RA of node: 223
1883 deg
Eccentricity:
0001468
Arg of perigee: 327
8436 deg
Mean anomaly: 32
2639 deg
Mean motion: 15
77713680 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4017
Checksum: 297
Coasting Arc #11 (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 = 342639
54 A = 6712243
51 meter
Y = 4873579
22 meter E =
0010448
Z = -4612941
04 I = 51
43172
XDOT = -6775
069410 Wp = 62
22815
YDOT = -2249
869858 meter/sec RA = 217
13784 deg
ZDOT = -2880
396414 TA = 179
18115
MA = 179
17944
Ha = 184
124 n
mi
Hp = 178
267
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1124145
47 X = 310526
13
Y = 15989433
14 feet Y = 4877232
00 meter
Z = -15134320
99 Z = -4611353
69
XDOT = -22227
918011 XDOT = -6735
414835
YDOT = -7381
462788 feet/sec YDOT = -2325
410343 meter/sec
ZDOT = -9450
119467 ZDOT = -2913
214225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16009104
77 X = -4879575
13
Y = 912843
73 feet Y = 278234
77 meter
Z = -15127743
64 Z = -4610936
26
XDOT = 7858
026408 XDOT = 2395
126449
YDOT = -20866
071569 feet/sec YDOT = -6359
978614 meter/sec
ZDOT = -9575
502887 ZDOT = -2918
613280
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
52094532
00020000 00000-0 20000-3 0 9100
2 25544 51
6384 217
9546 0001527 329
4333 30
6743 15
77754254 40335
Satellite: ISS
Catalog Number: 25544
Epoch time: 07355
52094532 = yrday
fracday
Element set: 910
Inclination: 51
6384 deg
RA of node: 217
9546 deg
Eccentricity:
0001527
Arg of perigee: 329
4333 deg
Mean anomaly: 30
6743 deg
Mean motion: 15
77754254 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4033
Checksum: 287
Coasting Arc #12 (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 = 6073300
93 A = 6720610
52 meter
Y = 2537050
84 meter E =
0012901
Z = 1329831
81 I = 51
48433
XDOT = -793
028036 Wp = 116
35973
YDOT = 4975
696970 meter/sec RA = 211
92566 deg
ZDOT = -5833
041028 TA = 48
97874
MA = 48
86728
Ha = 184
134 n
mi
Hp = 178
115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19925527
98 X = 6038019
71
Y = 8323657
61 feet Y = 2604768
42 meter
Z = 4362965
27 Z = 1359250
98
XDOT = -2601
798019 XDOT = -820
271970
YDOT = 16324
465124 feet/sec YDOT = 4966
677647 meter/sec
ZDOT = -19137
273713 ZDOT = -5836
958838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8350434
34 X = -2545212
39
Y = 19889347
35 feet Y = 6062273
07 meter
Z = 4475434
69 Z = 1364112
49
XDOT = -14870
720130 XDOT = -4532
595496
YDOT = -1906
702669 feet/sec YDOT = -581
162974 meter/sec
ZDOT = -19151
681946 ZDOT = -5837
432657
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
53434660
00020000 00000-0 20000-3 0 9113
2 25544 51
6383 212
7212 0001451 337
1082 23
0018 15
77788321 40490
Satellite: ISS
Catalog Number: 25544
Epoch time: 07356
53434660 = yrday
fracday
Element set: 911
Inclination: 51
6383 deg
RA of node: 212
7212 deg
Eccentricity:
0001451
Arg of perigee: 337
1082 deg
Mean anomaly: 23
0018 deg
Mean motion: 15
77788321 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4049
Checksum: 265
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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