Date:
April 15th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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
112/05:52:08
599 -2
1 3
1 3
1
N/A 2
3 0
1 186
3
000/00:04:57
197 -0
3 0
3 178
0
Coasting Arc #1 (Orbit 1848)
---------------------------------------
Vector Time (GMT): 2008/105/13:33:33
465
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 987492
35 A = 6711542
73 meter
Y = -4404658
13 meter E =
0012234
Z = -4977615
81 I = 51
53271
XDOT = 7425
739550 Wp = 97
25675
YDOT = -539
667655 meter/sec RA = 343
81246 deg
ZDOT = 1953
283590 TA = 191
64048
MA = 191
66879
Ha = 184
717 n
mi
Hp = 178
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3239804
30 X = 1060852
76
Y = -14450978
12 feet Y = -4393205
35 meter
Z = -16330760
53 Z = -4972640
32
XDOT = 24362
662566 XDOT = 7421
733654
YDOT = -1770
563172 feet/sec YDOT = -456
651149 meter/sec
ZDOT = 6408
410729 ZDOT = 1989
347914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8022836
00 X = -2445360
41
Y = -12472775
55 feet Y = -3801701
99 meter
Z = -16312106
32 Z = -4971930
01
XDOT = 14801
066042 XDOT = 4511
364930
YDOT = -18071
324451 feet/sec YDOT = -5508
139693 meter/sec
ZDOT = 6546
710688 ZDOT = 1995
437418
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 08105
57742470
00020000 00000-0 20000-3 0 9009
2 25544 51
6401 344
2633 0001752 345
4464 14
6650 15
77470414 18493
Satellite: ISS
Catalog Number: 25544
Epoch time: 08105
57742470 = yrday
fracday
Element set: 900
Inclination: 51
6401 deg
RA of node: 344
2633 deg
Eccentricity:
0001752
Arg of perigee: 345
4464 deg
Mean anomaly: 14
6650 deg
Mean motion: 15
77470414 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1849
Checksum: 274
Coasting Arc #2 (Orbit 1864)
---------------------------------------
Vector Time (GMT): 2008/106/13:33:33
465
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6122285
60 A = 6718838
27 meter
Y = 26330
17 meter E =
0003717
Z = -2770033
62 I = 51
52934
XDOT = 2294
244286 Wp = 98
26743
YDOT = -5268
493382 meter/sec RA = 338
68322 deg
ZDOT = -5127
151037 TA = 113
50242
MA = 113
46336
Ha = 184
686 n
mi
Hp = 178
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20086238
83 X = -6108668
72
Y = 86385
07 feet Y = -42056
70 meter
Z = -9088036
82 Z = -2799742
52
XDOT = 7527
048183 XDOT = 2377
893586
YDOT = -17285
083274 feet/sec YDOT = -5242
370327 meter/sec
ZDOT = -16821
361669 ZDOT = -5115
802241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13671435
78 X = -4167053
63
Y = 14644856
88 feet Y = 4463752
38 meter
Z = -9202003
95 Z = -2804770
80
XDOT = -6290
650082 XDOT = -1917
390145
YDOT = -16402
122905 feet/sec YDOT = -4999
367062 meter/sec
ZDOT = -16778
347220 ZDOT = -5114
040233
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 08106
59101675
00020000 00000-0 20000-3 0 9019
2 25544 51
6395 339
0317 0001768 346
2322 13
8795 15
77486549 18650
Satellite: ISS
Catalog Number: 25544
Epoch time: 08106
59101675 = yrday
fracday
Element set: 901
Inclination: 51
6395 deg
RA of node: 339
0317 deg
Eccentricity:
0001768
Arg of perigee: 346
2322 deg
Mean anomaly: 13
8795 deg
Mean motion: 15
77486549 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1865
Checksum: 311
Coasting Arc #3 (Orbit 1880)
---------------------------------------
Vector Time (GMT): 2008/107/13:33:33
465
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2897544
62 A = 6716007
77 meter
Y = 4766861
15 meter E =
0011648
Z = 3732904
94 I = 51
49374
XDOT = -6412
895280 Wp = 73
97762
YDOT = -567
304455 meter/sec RA = 333
46120 deg
ZDOT = -4239
284139 TA = 60
73173
MA = 60
61534
Ha = 184
622 n
mi
Hp = 178
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9506379
98 X = -2968766
85
Y = 15639308
22 feet Y = 4734061
11 meter
Z = 12247063
45 Z = 3718655
41
XDOT = -21039
682678 XDOT = -6385
481272
YDOT = -1861
235090 feet/sec YDOT = -638
864057 meter/sec
ZDOT = -13908
412529 ZDOT = -4270
371397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5124944
33 X = 1562083
03
Y = 17607342
41 feet Y = 5366717
97 meter
Z = 12192875
95 Z = 3716388
59
XDOT = -14197
388628 XDOT = -4327
364054
YDOT = 13878
567343 feet/sec YDOT = 4230
187326 meter/sec
ZDOT = -14027
722690 ZDOT = -4275
649876
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 08107
60458371
00020000 00000-0 20000-3 0 9021
2 25544 51
6398 333
7985 0001903 346
2878 13
8235 15
77569028 18813
Satellite: ISS
Catalog Number: 25544
Epoch time: 08107
60458371 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 333
7985 deg
Eccentricity:
0001903
Arg of perigee: 346
2878 deg
Mean anomaly: 13
8235 deg
Mean motion: 15
77569028 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1881
Checksum: 316
Coasting Arc #4 (Orbit 1896)
---------------------------------------
Vector Time (GMT): 2008/108/13:33:33
465
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4912338
83 A = 6713419
47 meter
Y = 1117741
95 meter E =
0008261
Z = 4431149
84 I = 51
45788
XDOT = -4193
414031 Wp = 100
58446
YDOT = 5607
338772 meter/sec RA = 328
33612 deg
ZDOT = 3227
784825 TA = 317
02260
MA = 317
08710
Ha = 184
583 n
mi
Hp = 178
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16116597
23 X = 4877949
12
Y = 3667132
38 feet Y = 1172482
49 meter
Z = 14537893
18 Z = 4454930
53
XDOT = -13757
920048 XDOT = -4271
484595
YDOT = 18396
780747 feet/sec YDOT = 5560
009275 meter/sec
ZDOT = 10589
845225 ZDOT = 3207
223164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13338443
39 X = 4065557
54
Y = -9623646
17 feet Y = -2933287
35 meter
Z = 14629226
45 Z = 4458988
22
XDOT = 3996
505065 XDOT = 1218
134744
YDOT = 21550
681097 feet/sec YDOT = 6568
647598 meter/sec
ZDOT = 10511
532277 ZDOT = 3203
915038
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 08108
61813088
00020000 00000-0 20000-3 0 9034
2 25544 51
6383 328
5651 0001871 352
9826 7
1313 15
77543242 18970
Satellite: ISS
Catalog Number: 25544
Epoch time: 08108
61813088 = yrday
fracday
Element set: 903
Inclination: 51
6383 deg
RA of node: 328
5651 deg
Eccentricity:
0001871
Arg of perigee: 352
9826 deg
Mean anomaly: 7
1313 deg
Mean motion: 15
77543242 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1897
Checksum: 296
Coasting Arc #5 (Orbit 1911)
---------------------------------------
Vector Time (GMT): 2008/109/13:33:33
465
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4242638
75 A = 6720673
74 meter
Y = -4909990
60 meter E =
0009027
Z = -1733800
27 I = 51
45761
XDOT = 4751
057359 Wp = 29
84450
YDOT = 2102
996525 meter/sec RA = 323
11938 deg
ZDOT = 5690
752843 TA = 310
88485
MA = 310
96302
Ha = 184
642 n
mi
Hp = 178
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13919418
48 X = 4305650
29
Y = -16108893
04 feet Y = -4862194
75 meter
Z = -5688321
10 Z = -1713036
03
XDOT = 15587
458526 XDOT = 4699
543259
YDOT = 6899
594897 feet/sec YDOT = 2155
837794 meter/sec
ZDOT = 18670
448959 ZDOT = 5713
708506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3254185
52 X = -991875
75
Y = -21060655
10 feet Y = -6419287
67 meter
Z = -5609164
48 Z = -1709673
33
XDOT = 13742
098677 XDOT = 4188
591677
YDOT = -7101
396247 feet/sec YDOT = -2164
505576 meter/sec
ZDOT = 18758
712742 ZDOT = 5717
655644
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 08109
56830703
00020000 00000-0 20000-3 0 9043
2 25544 51
6374 323
6584 0001725 354
7229 5
3917 15
77598520 19123
Satellite: ISS
Catalog Number: 25544
Epoch time: 08109
56830703 = yrday
fracday
Element set: 904
Inclination: 51
6374 deg
RA of node: 323
6584 deg
Eccentricity:
0001725
Arg of perigee: 354
7229 deg
Mean anomaly: 5
3917 deg
Mean motion: 15
77598520 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1912
Checksum: 298
Coasting Arc #6 (Orbit 1927)
---------------------------------------
Vector Time (GMT): 2008/110/13:33:33
465
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3304751
45 A = 6709866
69 meter
Y = -2635766
45 meter E =
0015196
Z = -5223982
84 I = 51
39818
XDOT = 5356
203842 Wp = 78
75033
YDOT = -5491
540680 meter/sec RA = 317
96219 deg
ZDOT = -616
225358 TA = 185
36067
MA = 185
37695
Ha = 184
632 n
mi
Hp = 178
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10842360
42 X = -3249654
74
Y = -8647527
72 feet Y = -2672414
16 meter
Z = -17139051
33 Z = -5239903
66
XDOT = 17572
847251 XDOT = 5420
206577
YDOT = -18016
865747 feet/sec YDOT = -5431
286706 meter/sec
ZDOT = -2021
736738 ZDOT = -590
048900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13499120
36 X = -4114531
88
Y = 2829171
12 feet Y = 862331
36 meter
Z = -17200381
85 Z = -5242676
39
XDOT = -2582
848722 XDOT = -787
252291
YDOT = -24036
156630 feet/sec YDOT = -7326
220541 meter/sec
ZDOT = -1921
879812 ZDOT = -585
788967
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 08110
58180686
00020000 00000-0 20000-3 0 9056
2 25544 51
6366 318
4249 0001700 2
1847 357
9325 15
77638633 19283
Satellite: ISS
Catalog Number: 25544
Epoch time: 08110
58180686 = yrday
fracday
Element set: 905
Inclination: 51
6366 deg
RA of node: 318
4249 deg
Eccentricity:
0001700
Arg of perigee: 2
1847 deg
Mean anomaly: 357
9325 deg
Mean motion: 15
77638633 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1928
Checksum: 301
Coasting Arc #7 (Orbit 1943)
---------------------------------------
Vector Time (GMT): 2008/111/13:33:33
465
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4931857
73 A = 6721397
46 meter
Y = 4507513
06 meter E =
0009267
Z = -699378
30 I = 51
41728
XDOT = -2802
516684 Wp = 131
89715
YDOT = -3983
842606 meter/sec RA = 312
78365 deg
ZDOT = -5969
932224 TA = 55
75616
MA = 55
66841
Ha = 184
550 n
mi
Hp = 178
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16180635
60 X = -4978497
38
Y = 14788428
67 feet Y = 4452101
42 meter
Z = -2294548
23 Z = -723451
03
XDOT = -9194
608543 XDOT = -2728
759071
YDOT = -13070
349757 feet/sec YDOT = -4014
769608 meter/sec
ZDOT = -19586
391812 ZDOT = -5983
367894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1566303
76 X = 477409
39
Y = 21854682
94 feet Y = 6661307
36 meter
Z = -2386434
31 Z = -727385
18
XDOT = -14292
331287 XDOT = -4356
302576
YDOT = -1100
580518 feet/sec YDOT = -335
456942 meter/sec
ZDOT = -19638
322377 ZDOT = -5985
760661
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 08111
59528175
00020000 00000-0 20000-3 0 9068
2 25544 51
6369 313
1913 0001950 3
2205 356
8973 15
77713897 19444
Satellite: ISS
Catalog Number: 25544
Epoch time: 08111
59528175 = yrday
fracday
Element set: 906
Inclination: 51
6369 deg
RA of node: 313
1913 deg
Eccentricity:
0001950
Arg of perigee: 3
2205 deg
Mean anomaly: 356
8973 deg
Mean motion: 15
77713897 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1944
Checksum: 304
Coasting Arc #8 (Orbit 1954)
---------------------------------------
Vector Time (GMT): 2008/112/05:54:37
197
Vector Time (MET): N/A
Weight (LBS) : 630355
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2477391
11 A = 6711555
37 meter
Y = 3491656
69 meter E =
0006954
Z = 5164418
65 I = 51
36759
XDOT = -5437
418068 Wp = 55
16541
YDOT = 5370
952051 meter/sec RA = 309
24110 deg
ZDOT = -1018
056504 TA = 44
59378
MA = 44
53786
Ha = 186
269 n
mi
Hp = 177
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8127923
59 X = 2413074
44
Y = 11455566
58 feet Y = 3519000
66 meter
Z = 16943630
75 Z = 5176297
84
XDOT = -17839
298124 XDOT = -5492
127141
YDOT = 17621
233762 feet/sec YDOT = 5309
841844 meter/sec
ZDOT = -3340
080395 ZDOT = -1044
604844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6433828
97 X = -1961031
07
Y = 12423409
40 feet Y = 3786655
18 meter
Z = 16989541
33 Z = 5178412
20
XDOT = -22964
276377 XDOT = -6999
511440
YDOT = -7164
629388 feet/sec YDOT = -2183
779037 meter/sec
ZDOT = -3441
377591 ZDOT = -1048
931890
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 08112
29205689
00020000 00000-0 20000-3 0 9079
2 25544 51
6392 309
5969 0003258 54
2609 305
8859 15
77129058 19556
Satellite: ISS
Catalog Number: 25544
Epoch time: 08112
29205689 = yrday
fracday
Element set: 907
Inclination: 51
6392 deg
RA of node: 309
5969 deg
Eccentricity:
0003258
Arg of perigee: 54
2609 deg
Mean anomaly: 305
8859 deg
Mean motion: 15
77129058 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1955
Checksum: 327
Coasting Arc #9 (Orbit 1970)
---------------------------------------
Vector Time (GMT): 2008/113/05:54:37
197
Vector Time (MET): N/A
Weight (LBS) : 630355
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4760123
80 A = 6721665
64 meter
Y = -4340104
35 meter E =
0017413
Z = 1890069
19 I = 51
38440
XDOT = 2153
668402 Wp = 65
17413
YDOT = 4822
732845 meter/sec RA = 304
08877 deg
ZDOT = 5617
171512 TA = 315
94628
MA = 316
08489
Ha = 186
325 n
mi
Hp = 177
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15617204
05 X = 4799119
95
Y = -14239187
51 feet Y = -4286655
94 meter
Z = 6201014
40 Z = 1913288
92
XDOT = 7065
841214 XDOT = 2072
292061
YDOT = 15822
614320 feet/sec YDOT = 4846
361248 meter/sec
ZDOT = 18429
040394 ZDOT = 5627
436694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19957309
21 X = 6082987
85
Y = 6873879
75 feet Y = 2095158
55 meter
Z = 6289649
36 Z = 1917085
12
XDOT = -10065
120449 XDOT = -3067
848713
YDOT = 12225
429075 feet/sec YDOT = 3726
310782 meter/sec
ZDOT = 18468
890997 ZDOT = 5629
317976
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 08113
30587310
00020000 00000-0 20000-3 0 9087
2 25544 51
6392 304
3654 0003307 57
4432 302
7052 15
77139362 19712
Satellite: ISS
Catalog Number: 25544
Epoch time: 08113
30587310 = yrday
fracday
Element set: 908
Inclination: 51
6392 deg
RA of node: 304
3654 deg
Eccentricity:
0003307
Arg of perigee: 57
4432 deg
Mean anomaly: 302
7052 deg
Mean motion: 15
77139362 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1971
Checksum: 271
Coasting Arc #10 (Orbit 1985)
---------------------------------------
Vector Time (GMT): 2008/114/05:54:37
197
Vector Time (MET): N/A
Weight (LBS) : 630355
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1330354
80 A = 6714622
16 meter
Y = -4894494
56 meter E =
0011806
Z = -4410993
45 I = 51
34632
XDOT = 5405
397536 Wp = 97
98039
YDOT = -4402
750913 meter/sec RA = 298
86729 deg
ZDOT = 3260
906463 TA = 204
84773
MA = 204
90462
Ha = 186
300 n
mi
Hp = 177
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4364681
12 X = -1254096
74
Y = -16058053
02 feet Y = -4908944
77 meter
Z = -14471763
29 Z = -4417271
42
XDOT = 17734
243884 XDOT = 5438
386868
YDOT = -14444
720844 feet/sec YDOT = -4342
120365 meter/sec
ZDOT = 10698
512019 ZDOT = 3287
246278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11855670
13 X = 3613608
26
Y = -11646588
79 feet Y = -3549880
26 meter
Z = -14496326
99 Z = -4418480
47
XDOT = 20433
819576 XDOT = 6228
228207
YDOT = 7382
909975 feet/sec YDOT = 2250
310960 meter/sec
ZDOT = 10799
112612 ZDOT = 3291
569524
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 08114
25630366
00020000 00000-0 20000-3 0 9093
2 25544 51
6399 299
4612 0003302 59
9198 300
2293 15
77183847 19861
Satellite: ISS
Catalog Number: 25544
Epoch time: 08114
25630366 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 299
4612 deg
Eccentricity:
0003302
Arg of perigee: 59
9198 deg
Mean anomaly: 300
2293 deg
Mean motion: 15
77183847 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1986
Checksum: 316
Coasting Arc #11 (Orbit 2001)
---------------------------------------
Vector Time (GMT): 2008/115/05:54:37
197
Vector Time (MET): N/A
Weight (LBS) : 630355
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4628241
00 A = 6716959
75 meter
Y = 3178713
72 meter E =
0009158
Z = -3696811
41 I = 51
34246
XDOT = -945
217059 Wp = 71
68482
YDOT = -6334
520155 meter/sec RA = 293
73628 deg
ZDOT = -4269
194031 TA = 153
08173
MA = 153
03419
Ha = 186
244 n
mi
Hp = 177
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15184517
72 X = -4645483
18
Y = 10428850
80 feet Y = 3126861
90 meter
Z = -12128646
35 Z = -3719337
43
XDOT = -3101
105835 XDOT = -853
573930
YDOT = -20782
546439 feet/sec YDOT = -6344
577452 meter/sec
ZDOT = -14006
542097 ZDOT = -4273
563741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16663312
25 X = -5078977
57
Y = -7718073
46 feet Y = -2352468
79 meter
Z = -12214742
60 Z = -3723053
54
XDOT = 15800
493569 XDOT = 4815
990440
YDOT = -11948
706290 feet/sec YDOT = -3641
965677 meter/sec
ZDOT = -14023
928870 ZDOT = -4274
493519
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 08115
27007407
00020000 00000-0 20000-3 0 9102
2 25544 51
6405 294
2300 0003304 62
1534 297
9965 15
77229354 20020
Satellite: ISS
Catalog Number: 25544
Epoch time: 08115
27007407 = yrday
fracday
Element set: 910
Inclination: 51
6405 deg
RA of node: 294
2300 deg
Eccentricity:
0003304
Arg of perigee: 62
1534 deg
Mean anomaly: 297
9965 deg
Mean motion: 15
77229354 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2002
Checksum: 264
Coasting Arc #12 (Orbit 2017)
---------------------------------------
Vector Time (GMT): 2008/116/05:54:37
197
Vector Time (MET): N/A
Weight (LBS) : 630355
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 398821
43 A = 6719371
25 meter
Y = 6053458
28 meter E =
0016328
Z = 2874196
14 I = 51
33949
XDOT = -5160
279211 Wp = 92
14989
YDOT = 2739
556970 meter/sec RA = 288
50421 deg
ZDOT = -5029
910944 TA = 54
59901
MA = 54
44660
Ha = 186
251 n
mi
Hp = 177
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1308469
25 X = 317138
58
Y = 19860427
42 feet Y = 6057461
22 meter
Z = 9429777
37 Z = 2875935
64
XDOT = -16930
049905 XDOT = -5166
095156
YDOT = 8988
047803 feet/sec YDOT = 2681
819600 meter/sec
ZDOT = -16502
332494 ZDOT = -5054
993818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16272277
67 X = -4959790
23
Y = 11455324
13 feet Y = 3491582
79 meter
Z = 9437049
28 Z = 2876412
62
XDOT = -15629
952792 XDOT = -4764
009611
YDOT = -8463
785112 feet/sec YDOT = -2579
761702 meter/sec
ZDOT = -16598
284632 ZDOT = -5059
157156
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 08116
28382215
00020000 00000-0 20000-3 0 9118
2 25544 51
6400 288
9989 0003296 66
1919 293
9591 15
77237778 20186
Satellite: ISS
Catalog Number: 25544
Epoch time: 08116
28382215 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 288
9989 deg
Eccentricity:
0003296
Arg of perigee: 66
1919 deg
Mean anomaly: 293
9591 deg
Mean motion: 15
77237778 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2018
Checksum: 326
Coasting Arc #13 (Orbit 2033)
---------------------------------------
Vector Time (GMT): 2008/117/05:54:37
197
Vector Time (MET): N/A
Weight (LBS) : 630355
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4363967
73 A = 6712309
03 meter
Y = -1476012
22 meter E =
0008667
Z = 4875375
86 I = 51
30876
XDOT = 47
109157 Wp = 104
88125
YDOT = 7393
568085 meter/sec RA = 283
36277 deg
ZDOT = 2190
789394 TA = 323
74463
MA = 323
80333
Ha = 186
039 n
mi
Hp = 177
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14317479
44 X = 4356464
50
Y = -4842559
78 feet Y = -1427254
12 meter
Z = 15995327
62 Z = 4896557
87
XDOT = 154
557601 XDOT = -46
212926
YDOT = 24257
113140 feet/sec YDOT = 7393
572949 meter/sec
ZDOT = 7187
629246 ZDOT = 2190
792067
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11730422
98 X = 3575432
92
Y = 9393413
73 feet Y = 2863112
51 meter
Z = 16076444
37 Z = 4900100
24
XDOT = -19708
747239 XDOT = -6007
226159
YDOT = 12279
163240 feet/sec YDOT = 3742
688955 meter/sec
ZDOT = 7188
375587 ZDOT = 2191
016879
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 08117
29754518
00020000 00000-0 20000-3 0 9120
2 25544 51
6406 283
7674 0003245 67
6671 292
4837 15
77295514 20348
Satellite: ISS
Catalog Number: 25544
Epoch time: 08117
29754518 = yrday
fracday
Element set: 912
Inclination: 51
6406 deg
RA of node: 283
7674 deg
Eccentricity:
0003245
Arg of perigee: 67
6671 deg
Mean anomaly: 292
4837 deg
Mean motion: 15
77295514 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2034
Checksum: 310
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics 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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