Date:
April 17th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7803 84 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
575 -2
0 3
1 3
1
N/A 2
4 0
1 186
4
000/00:04:57
149 -0
2 0
2 178
0
Coasting Arc #1 (Orbit 1880)
---------------------------------------
Vector Time (GMT): 2008/107/13:01:22
930
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6205228
31 A = 6721923
06 meter
Y = -2471806
59 meter E =
0014374
Z = 683803
65 I = 51
51403
XDOT = 1209
329828 Wp = 45
75785
YDOT = 4709
539873 meter/sec RA = 333
61195 deg
ZDOT = 5982
509086 TA = 321
71791
MA = 321
81987
Ha = 184
666 n
mi
Hp = 178
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20358360
61 X = 6229085
46
Y = -8109601
68 feet Y = -2402282
75 meter
Z = 2243450
30 Z = 714006
75
XDOT = 3967
617545 XDOT = 1127
515159
YDOT = 15451
246304 feet/sec YDOT = 4722
606149 meter/sec
ZDOT = 19627
654481 ZDOT = 5988
185045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10493141
14 X = 3198309
42
Y = -19224732
82 feet Y = -5859698
56 meter
Z = 2359066
05 Z = 719043
33
XDOT = 11425
059033 XDOT = 3482
357993
YDOT = 8672
981882 feet/sec YDOT = 2643
524878 meter/sec
ZDOT = 19649
897244 ZDOT = 5989
288680
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
60459587
00020000 00000-0 20000-3 0 9009
2 25544 51
6397 333
8006 0001810 350
0206 10
0923 15
77534721 18817
Satellite: ISS
Catalog Number: 25544
Epoch time: 08107
60459587 = yrday
fracday
Element set: 900
Inclination: 51
6397 deg
RA of node: 333
8006 deg
Eccentricity:
0001810
Arg of perigee: 350
0206 deg
Mean anomaly: 10
0923 deg
Mean motion: 15
77534721 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1881
Checksum: 268
Coasting Arc #2 (Orbit 1895)
---------------------------------------
Vector Time (GMT): 2008/108/13:01:22
930
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -49752
30 A = 6711515
97 meter
Y = -4573686
60 meter E =
0012093
Z = -4922351
24 I = 51
45213
XDOT = 7021
723717 Wp = 97
43390
YDOT = -2344
035042 meter/sec RA = 328
41297 deg
ZDOT = 2109
904879 TA = 193
06694
MA = 193
09830
Ha = 184
681 n
mi
Hp = 178
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -163229
33 X = 25307
11
Y = -15005533
48 feet Y = -4573823
55 meter
Z = -16149446
32 Z = -4922410
37
XDOT = 23037
151303 XDOT = 7037
163613
YDOT = -7690
403681 feet/sec YDOT = -2265
427670 meter/sec
ZDOT = 6922
260101 ZDOT = 2144
054241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9824836
22 X = -2994610
08
Y = -11342097
57 feet Y = -3457071
34 meter
Z = -16150130
38 Z = -4922559
74
XDOT = 11619
665916 XDOT = 3541
674171
YDOT = -20094
707032 feet/sec YDOT = -6124
866703 meter/sec
ZDOT = 7053
021089 ZDOT = 2149
760828
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
55480541
00020000 00000-0 20000-3 0 9019
2 25544 51
6384 328
8941 0001824 353
6633 6
4509 15
77554443 18961
Satellite: ISS
Catalog Number: 25544
Epoch time: 08108
55480541 = yrday
fracday
Element set: 901
Inclination: 51
6384 deg
RA of node: 328
8941 deg
Eccentricity:
0001824
Arg of perigee: 353
6633 deg
Mean anomaly: 6
4509 deg
Mean motion: 15
77554443 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1896
Checksum: 302
Coasting Arc #3 (Orbit 1911)
---------------------------------------
Vector Time (GMT): 2008/109/13:01:22
930
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5870668
89 A = 6718223
93 meter
Y = 1481229
76 meter E =
0004086
Z = -2915072
90 I = 51
45022
XDOT = 1034
075317 Wp = 87
23300
YDOT = -5754
192137 meter/sec RA = 323
27904 deg
ZDOT = -5012
227030 TA = 126
45595
MA = 126
41828
Ha = 184
673 n
mi
Hp = 178
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19260724
69 X = -5872634
85
Y = 4859677
68 feet Y = 1415569
45 meter
Z = -9563887
45 Z = -2943597
76
XDOT = 3392
635555 XDOT = 1122
691496
YDOT = -18878
583127 feet/sec YDOT = -5742
133266 meter/sec
ZDOT = -16444
314403 ZDOT = -5006
987924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11132161
06 X = -3393082
69
Y = 16387952
37 feet Y = 4995047
88 meter
Z = -9673155
30 Z = -2948377
73
XDOT = -8735
760388 XDOT = -2662
659766
YDOT = -15617
835684 feet/sec YDOT = -4760
316317 meter/sec
ZDOT = -16424
793604 ZDOT = -5006
277091
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
56834343
00020000 00000-0 20000-3 0 9025
2 25544 51
6377 323
6619 0001888 356
2078 3
9076 15
77576085 19126
Satellite: ISS
Catalog Number: 25544
Epoch time: 08109
56834343 = yrday
fracday
Element set: 902
Inclination: 51
6377 deg
RA of node: 323
6619 deg
Eccentricity:
0001888
Arg of perigee: 356
2078 deg
Mean anomaly: 3
9076 deg
Mean motion: 15
77576085 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1912
Checksum: 313
Coasting Arc #4 (Orbit 1927)
---------------------------------------
Vector Time (GMT): 2008/110/13:01:22
930
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1735245
86 A = 6716288
51 meter
Y = 5403523
62 meter E =
0012207
Z = 3583868
65 I = 51
42145
XDOT = -6264
842004 Wp = 76
99535
YDOT = 914
750911 meter/sec RA = 318
04994 deg
ZDOT = -4397
285665 TA = 59
92635
MA = 59
80535
Ha = 184
610 n
mi
Hp = 178
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5693063
85 X = -1812949
99
Y = 17728095
86 feet Y = 5383684
75 meter
Z = 11758099
26 Z = 3575249
79
XDOT = -20553
943582 XDOT = -6253
243731
YDOT = 3001
151282 feet/sec YDOT = 844
758581 meter/sec
ZDOT = -14426
790241 ZDOT = -4427
692578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7759464
07 X = 2365084
65
Y = 16948473
86 feet Y = 5165894
83 meter
Z = 11725579
23 Z = 3573956
55
XDOT = -11802
274474 XDOT = -3597
333260
YDOT = 15499
701201 feet/sec YDOT = 4724
308926 meter/sec
ZDOT = -14543
330715 ZDOT = -4432
807202
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
58186113
00020000 00000-0 20000-3 0 9035
2 25544 51
6379 318
4279 0001928 354
6001 5
5143 15
77630140 19288
Satellite: ISS
Catalog Number: 25544
Epoch time: 08110
58186113 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 318
4279 deg
Eccentricity:
0001928
Arg of perigee: 354
6001 deg
Mean anomaly: 5
5143 deg
Mean motion: 15
77630140 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1928
Checksum: 275
Coasting Arc #5 (Orbit 1943)
---------------------------------------
Vector Time (GMT): 2008/111/13:01:22
930
Vector Time (MET): N/A
Weight (LBS) : 630561
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4936078
78 A = 6712762
94 meter
Y = 20208
75 meter E =
0007903
Z = 4543433
54 I = 51
38747
XDOT = -2795
865767 Wp = 101
86287
YDOT = 6528
243395 meter/sec RA = 312
91787 deg
ZDOT = 3002
456989 TA = 318
21582
MA = 318
27613
Ha = 184
569 n
mi
Hp = 178
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16194484
20 X = 4913414
37
Y = 66301
67 feet Y = 75280
13 meter
Z = 14906278
03 Z = 4567358
39
XDOT = -9172
787950 XDOT = -2883
243463
YDOT = 21418
121374 feet/sec YDOT = 6496
489902 meter/sec
ZDOT = 9850
580673 ZDOT = 2988
662120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11714889
41 X = 3570698
29
Y = -11058154
69 feet Y = -3370525
55 meter
Z = 14998047
21 Z = 4571404
79
XDOT = 7274
744732 XDOT = 2217
342194
YDOT = 21022
628712 feet/sec YDOT = 6407
697231 meter/sec
ZDOT = 9798
317758 ZDOT = 2986
527253
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
59536293
00020000 00000-0 20000-3 0 9046
2 25544 51
6367 313
1939 0001913 2
0677 358
0496 15
77617392 19446
Satellite: ISS
Catalog Number: 25544
Epoch time: 08111
59536293 = yrday
fracday
Element set: 904
Inclination: 51
6367 deg
RA of node: 313
1939 deg
Eccentricity:
0001913
Arg of perigee: 2
0677 deg
Mean anomaly: 358
0496 deg
Mean motion: 15
77617392 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1944
Checksum: 304
Coasting Arc #6 (Orbit 1954)
---------------------------------------
Vector Time (GMT): 2008/112/05:54:37
149
Vector Time (MET): N/A
Weight (LBS) : 630355
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2523347
01 A = 6711644
70 meter
Y = 3446042
97 meter E =
0006906
Z = 5172875
64 I = 51
36732
XDOT = -5409
645292 Wp = 55
56423
YDOT = 5409
512656 meter/sec RA = 309
24432 deg
ZDOT = -960
077905 TA = 43
63522
MA = 43
58063
Ha = 186
363 n
mi
Hp = 178
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8278697
55 X = 2459495
91
Y = 11305915
25 feet Y = 3473903
44 meter
Z = 16971376
76 Z = 5184979
21
XDOT = -17748
180092 XDOT = -5465
069275
YDOT = 17747
744936 feet/sec YDOT = 5348
709023 meter/sec
ZDOT = -3149
861892 ZDOT = -986
493058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6231486
99 X = -1899357
23
Y = 12487575
60 feet Y = 3806213
04 meter
Z = 17018143
48 Z = 5187130
13
XDOT = -23030
004108 XDOT = -7019
545252
YDOT = -7041
082161 feet/sec YDOT = -2146
121843 meter/sec
ZDOT = -3250
644413 ZDOT = -990
796417
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
29215612
00020000 00000-0 20000-3 0 9054
2 25544 51
6390 309
5991 0003331 54
4273 305
7202 15
77083741 19559
Satellite: ISS
Catalog Number: 25544
Epoch time: 08112
29215612 = yrday
fracday
Element set: 905
Inclination: 51
6390 deg
RA of node: 309
5991 deg
Eccentricity:
0003331
Arg of perigee: 54
4273 deg
Mean anomaly: 305
7202 deg
Mean motion: 15
77083741 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1955
Checksum: 275
Coasting Arc #7 (Orbit 1970)
---------------------------------------
Vector Time (GMT): 2008/113/05:54:37
149
Vector Time (MET): N/A
Weight (LBS) : 630355
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4735815
38 A = 6721920
39 meter
Y = -4393770
61 meter E =
0017505
Z = 1826863
93 I = 51
38462
XDOT = 2223
734179 Wp = 64
50625
YDOT = 4758
173958 meter/sec RA = 304
09137 deg
ZDOT = 5644
714236 TA = 315
87510
MA = 316
01463
Ha = 186
438 n
mi
Hp = 177
945
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15537452
05 X = 4775720
49
Y = -14415257
91 feet Y = -4340588
94 meter
Z = 5993648
08 Z = 1849967
78
XDOT = 7295
715812 XDOT = 2142
940738
YDOT = 15610
806950 feet/sec YDOT = 4782
589135 meter/sec
ZDOT = 18519
403660 ZDOT = 5655
321218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20074334
04 X = 6118657
02
Y = 6720737
41 feet Y = 2048480
76 meter
Z = 6081833
23 Z = 1853742
77
XDOT = -9780
629208 XDOT = -2981
135783
YDOT = 12316
982954 feet/sec YDOT = 3754
216404 meter/sec
ZDOT = 18560
558924 ZDOT = 5657
258360
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
30600453
00020000 00000-0 20000-3 0 9069
2 25544 51
6391 304
3679 0003386 57
7681 302
3811 15
77086409 19716
Satellite: ISS
Catalog Number: 25544
Epoch time: 08113
30600453 = yrday
fracday
Element set: 906
Inclination: 51
6391 deg
RA of node: 304
3679 deg
Eccentricity:
0003386
Arg of perigee: 57
7681 deg
Mean anomaly: 302
3811 deg
Mean motion: 15
77086409 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1971
Checksum: 287
Coasting Arc #8 (Orbit 1985)
---------------------------------------
Vector Time (GMT): 2008/114/05:54:37
149
Vector Time (MET): N/A
Weight (LBS) : 630355
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1407417
63 A = 6714614
14 meter
Y = -4831007
53 meter E =
0012163
Z = -4457233
14 I = 51
34558
XDOT = 5379
830627 Wp = 98
03945
YDOT = -4493
622555 meter/sec RA = 298
87117 deg
ZDOT = 3177
425188 TA = 203
84835
MA = 203
90475
Ha = 186
425 n
mi
Hp = 177
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4617511
89 X = -1331639
13
Y = -15849762
24 feet Y = -4846322
18 meter
Z = -14623468
30 Z = -4463886
65
XDOT = 17650
362949 XDOT = 5414
243545
YDOT = -14742
856150 feet/sec YDOT = -4433
269947 meter/sec
ZDOT = 10424
623321 ZDOT = 3203
644250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11550232
69 X = 3520510
92
Y = -11762970
21 feet Y = -3585353
32 meter
Z = -14649466
24 Z = -4465157
31
XDOT = 20644
029015 XDOT = 6292
300044
YDOT = 7186
576709 feet/sec YDOT = 2190
468581 meter/sec
ZDOT = 10524
751776 ZDOT = 3207
944341
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
25646929
00020000 00000-0 20000-3 0 9073
2 25544 51
6397 299
4639 0003385 60
3839 299
7663 15
77123481 19868
Satellite: ISS
Catalog Number: 25544
Epoch time: 08114
25646929 = yrday
fracday
Element set: 907
Inclination: 51
6397 deg
RA of node: 299
4639 deg
Eccentricity:
0003385
Arg of perigee: 60
3839 deg
Mean anomaly: 299
7663 deg
Mean motion: 15
77123481 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1986
Checksum: 343
Coasting Arc #9 (Orbit 2001)
---------------------------------------
Vector Time (GMT): 2008/115/05:54:37
149
Vector Time (MET): N/A
Weight (LBS) : 630355
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4610825
38 A = 6717397
46 meter
Y = 3290484
49 meter E =
0008938
Z = -3620309
79 I = 51
34317
XDOT = -1052
544220 Wp = 73
10074
YDOT = -6259
061205 meter/sec RA = 293
74023 deg
ZDOT = -4354
610313 TA = 150
49944
MA = 150
44897
Ha = 186
380 n
mi
Hp = 177
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15127379
87 X = -4629690
33
Y = 10795552
78 feet Y = 3238818
34 meter
Z = -11877656
81 Z = -3642755
15
XDOT = -3453
229068 XDOT = -961
321965
YDOT = -20534
977707 feet/sec YDOT = -6270
321044 meter/sec
ZDOT = -14286
779243 ZDOT = -4359
502444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16950793
23 X = -5166601
78
Y = -7483796
00 feet Y = -2281061
02 meter
Z = -11963432
58 Z = -3646454
25
XDOT = 15426
272307 XDOT = 4701
927799
YDOT = -12103
760400 feet/sec YDOT = -3689
226170 meter/sec
ZDOT = -14306
162574 ZDOT = -4360
518353
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
27028051
00020000 00000-0 20000-3 0 9087
2 25544 51
6404 294
2330 0003387 62
8331 297
3178 15
77161753 20023
Satellite: ISS
Catalog Number: 25544
Epoch time: 08115
27028051 = yrday
fracday
Element set: 908
Inclination: 51
6404 deg
RA of node: 294
2330 deg
Eccentricity:
0003387
Arg of perigee: 62
8331 deg
Mean anomaly: 297
3178 deg
Mean motion: 15
77161753 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2002
Checksum: 272
Coasting Arc #10 (Orbit 2017)
---------------------------------------
Vector Time (GMT): 2008/116/05:54:37
149
Vector Time (MET): N/A
Weight (LBS) : 630355
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 509906
78 A = 6719300
71 meter
Y = 5992565
85 meter E =
0016318
Z = 2982084
93 I = 51
33841
XDOT = -5147
454005 Wp = 90
65156
YDOT = 2910
852819 meter/sec RA = 288
50824 deg
ZDOT = -4946
176417 TA = 54
67457
MA = 54
52211
Ha = 186
398 n
mi
Hp = 177
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1672922
50 X = 428372
47
Y = 19660649
10 feet Y = 5997811
83 meter
Z = 9783743
20 Z = 2984364
44
XDOT = -16887
972456 XDOT = -5155
593132
YDOT = 9550
042057 feet/sec YDOT = 2853
245872 meter/sec
ZDOT = -16227
612918 ZDOT = -4971
202618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15912502
72 X = -4850130
83
Y = 11659727
76 feet Y = 3553885
02 meter
Z = 9793080
69 Z = 2984931
00
XDOT = -16072
856416 XDOT = -4899
006636
YDOT = -8161
658622 feet/sec YDOT = -2487
673548 meter/sec
ZDOT = -16323
330701 ZDOT = -4975
351198
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
28407388
00020000 00000-0 20000-3 0 9094
2 25544 51
6399 289
0021 0003389 66
9548 293
1974 15
77164655 20181
Satellite: ISS
Catalog Number: 25544
Epoch time: 08116
28407388 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 289
0021 deg
Eccentricity:
0003389
Arg of perigee: 66
9548 deg
Mean anomaly: 293
1974 deg
Mean motion: 15
77164655 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2018
Checksum: 327
Coasting Arc #11 (Orbit 2033)
---------------------------------------
Vector Time (GMT): 2008/117/05:54:37
149
Vector Time (MET): N/A
Weight (LBS) : 630355
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4361047
63 A = 6712794
63 meter
Y = -1666361
35 meter E =
0009232
Z = 4816669
58 I = 51
30948
XDOT = 195
329819 Wp = 104
65336
YDOT = 7339
977669 meter/sec RA = 283
36896 deg
ZDOT = 2356
401490 TA = 322
26692
MA = 322
33163
Ha = 186
208 n
mi
Hp = 177
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14307899
03 X = 4355958
31
Y = -5467064
79 feet Y = -1617622
40 meter
Z = 15802721
71 Z = 4837843
25
XDOT = 640
845862 XDOT = 101
791456
YDOT = 24081
291565 feet/sec YDOT = 7341
638801 meter/sec
ZDOT = 7730
976018 ZDOT = 2357
123696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12252444
85 X = 3734545
19
Y = 9050617
35 feet Y = 2758628
17 meter
Z = 15883787
53 Z = 4841378
44
XDOT = -19325
804577 XDOT = -5890
505235
YDOT = 12553
972041 feet/sec YDOT = 3826
450678 meter/sec
ZDOT = 7734
477468 ZDOT = 2357
468732
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
29784681
00020000 00000-0 20000-3 0 9102
2 25544 51
6404 283
7710 0003345 68
6839 291
4683 15
77213072 20342
Satellite: ISS
Catalog Number: 25544
Epoch time: 08117
29784681 = yrday
fracday
Element set: 910
Inclination: 51
6404 deg
RA of node: 283
7710 deg
Eccentricity:
0003345
Arg of perigee: 68
6839 deg
Mean anomaly: 291
4683 deg
Mean motion: 15
77213072 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2034
Checksum: 296
Coasting Arc #12 (Orbit 2048)
---------------------------------------
Vector Time (GMT): 2008/118/05:54:37
149
Vector Time (MET): N/A
Weight (LBS) : 630355
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 121952
32 A = 6722483
29 meter
Y = -6637879
92 meter E =
0012684
Z = -1026270
10 I = 51
33735
XDOT = 4886
869782 Wp = 45
89026
YDOT = -814
370494 meter/sec RA = 278
15696 deg
ZDOT = 5901
753671 TA = 302
82729
MA = 302
94936
Ha = 186
246 n
mi
Hp = 177
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 400106
04 X = 201154
53
Y = -21777821
27 feet Y = -6636073
28 meter
Z = -3367027
87 Z = -1025485
66
XDOT = 16033
037344 XDOT = 4866
943191
YDOT = -2671
819207 feet/sec YDOT = -759
834490 meter/sec
ZDOT = 19362
708895 ZDOT = 5925
445763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18391537
09 X = 5605740
51
Y = -11670506
28 feet Y = -3557170
31 meter
Z = -3364685
31 Z = -1025556
08
XDOT = 10165
370097 XDOT = 3098
404805
YDOT = 10461
864190 feet/sec YDOT = 3188
776205 meter/sec
ZDOT = 19453
526158 ZDOT = 5929
434773
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 08118
24824230
00020000 00000-0 20000-3 0 9114
2 25544 51
6408 278
8668 0003275 70
0264 290
1253 15
77248734 20492
Satellite: ISS
Catalog Number: 25544
Epoch time: 08118
24824230 = yrday
fracday
Element set: 911
Inclination: 51
6408 deg
RA of node: 278
8668 deg
Eccentricity:
0003275
Arg of perigee: 70
0264 deg
Mean anomaly: 290
1253 deg
Mean motion: 15
77248734 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2049
Checksum: 288
Coasting Arc #13 (Orbit 2064)
---------------------------------------
Vector Time (GMT): 2008/119/05:54:37
149
Vector Time (MET): N/A
Weight (LBS) : 630355
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4192780
39 A = 6710759
51 meter
Y = -314863
48 meter E =
0018180
Z = -5245886
42 I = 51
29510
XDOT = 469
564022 Wp = 87
28995
YDOT = -7678
156371 meter/sec RA = 272
98242 deg
ZDOT = 86
657044 TA = 183
53070
MA = 183
54354
Ha = 186
197 n
mi
Hp = 177
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13755841
18 X = -4163464
26
Y = -1033016
65 feet Y = -361585
38 meter
Z = -17210913
45 Z = -5266183
82
XDOT = 1540
564376 XDOT = 554
966502
YDOT = -25190
801742 feet/sec YDOT = -7672
427932 meter/sec
ZDOT = 284
307886 ZDOT = 89
145277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6881614
21 X = -2097516
01
Y = -11842540
13 feet Y = -3609606
23 meter
Z = -17288824
73 Z = -5269633
78
XDOT = 20771
665362 XDOT = 6331
203602
YDOT = -12492
848604 feet/sec YDOT = -3807
820255 meter/sec
ZDOT = 293
074460 ZDOT = 89
329095
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 08119
26197871
00020000 00000-0 20000-3 0 9122
2 25544 51
6406 273
6354 0003250 71
5443 288
6075 15
77285337 20655
Satellite: ISS
Catalog Number: 25544
Epoch time: 08119
26197871 = yrday
fracday
Element set: 912
Inclination: 51
6406 deg
RA of node: 273
6354 deg
Eccentricity:
0003250
Arg of perigee: 71
5443 deg
Mean anomaly: 288
6075 deg
Mean motion: 15
77285337 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2065
Checksum: 299
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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