Date:
February 28th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5597 23 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 15 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
059/05:22:06
064 -8
2 10
5 10
5
N/A -6
5 0
0 187
3
000/00:02:12
128 -0
9 0
0 181
6
Coasting Arc #1 (Orbit 1076)
---------------------------------------
Vector Time (GMT): 2008/056/13:59:38
150
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2571933
83 A = 6721258
16 meter
Y = -6004514
29 meter E =
0021238
Z = 1544043
80 I = 51
38334
XDOT = 5086
615552 Wp = 67
62731
YDOT = -684
716151 meter/sec RA = 235
92965 deg
ZDOT = 5755
234645 TA = 309
49506
MA = 309
68268
Ha = 187
366 n
mi
Hp = 175
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8438103
11 X = -2512099
88
Y = -19699850
04 feet Y = -6032940
48 meter
Z = 5065760
50 Z = 1531695
17
XDOT = 16688
371233 XDOT = 5065
936516
YDOT = -2246
444064 feet/sec YDOT = -627
949995 meter/sec
ZDOT = 18882
003427 ZDOT = 5779
894966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9813116
78 X = -2991037
99
Y = -19064945
04 feet Y = -5810995
25 meter
Z = 5017789
83 Z = 1529422
34
XDOT = 14994
986882 XDOT = 4570
472002
YDOT = -2675
934616 feet/sec YDOT = -815
624871 meter/sec
ZDOT = 18976
309327 ZDOT = 5783
979083
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 08056
64346141
00020000 00000-0 20000-3 0 9007
2 25544 51
6357 236
4928 0007302 77
6872 282
5110 15
77489427 10770
Satellite: ISS
Catalog Number: 25544
Epoch time: 08056
64346141 = yrday
fracday
Element set: 900
Inclination: 51
6357 deg
RA of node: 236
4928 deg
Eccentricity:
0007302
Arg of perigee: 77
6872 deg
Mean anomaly: 282
5110 deg
Mean motion: 15
77489427 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1077
Checksum: 299
Coasting Arc #2 (Orbit 1091)
---------------------------------------
Vector Time (GMT): 2008/057/13:59:38
150
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4942078
33 A = 6713168
72 meter
Y = -300103
43 meter E =
0017146
Z = -4549270
84 I = 51
37417
XDOT = -2357
031559 Wp = 98
06238
YDOT = -6676
968033 meter/sec RA = 230
71185 deg
ZDOT = 3008
306500 TA = 201
93543
MA = 202
00891
Ha = 187
384 n
mi
Hp = 175
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16214167
76 X = -4916255
89
Y = -984591
29 feet Y = -355224
37 meter
Z = -14925429
25 Z = -4573216
50
XDOT = -7733
043172 XDOT = -2296
807169
YDOT = -21906
063099 feet/sec YDOT = -6702
988847 meter/sec
ZDOT = 9869
771980 ZDOT = 2997
002706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16153980
56 X = -4923733
27
Y = 414843
91 feet Y = 126444
42 meter
Z = -15017120
60 Z = -4577218
36
XDOT = -9624
998134 XDOT = -2933
699431
YDOT = -19971
959572 feet/sec YDOT = -6087
453278 meter/sec
ZDOT = 9825
717994 ZDOT = 2994
878844
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 08057
59370397
00020000 00000-0 20000-3 0 9013
2 25544 51
6363 231
5879 0007331 80
2890 279
9103 15
77479526 10928
Satellite: ISS
Catalog Number: 25544
Epoch time: 08057
59370397 = yrday
fracday
Element set: 901
Inclination: 51
6363 deg
RA of node: 231
5879 deg
Eccentricity:
0007331
Arg of perigee: 80
2890 deg
Mean anomaly: 279
9103 deg
Mean motion: 15
77479526 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1092
Checksum: 313
Coasting Arc #3 (Orbit 1107)
---------------------------------------
Vector Time (GMT): 2008/058/13:59:38
150
Vector Time (MET): N/A
Weight (LBS) : 569213
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1391432
23 A = 6716621
13 meter
Y = 5512295
06 meter E =
0012727
Z = -3588792
41 I = 51
40559
XDOT = -6182
204479 Wp = 83
10446
YDOT = -1294
518878 meter/sec RA = 225
58003 deg
ZDOT = -4397
101469 TA = 139
97158
MA = 139
87771
Ha = 187
362 n
mi
Hp = 175
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4565066
38 X = 1347123
04
Y = 18084957
55 feet Y = 5527607
02 meter
Z = -11774253
32 Z = -3582140
65
XDOT = -20282
823095 XDOT = -6145
909358
YDOT = -4247
109180 feet/sec YDOT = -1363
448982 meter/sec
ZDOT = -14426
185921 ZDOT = -4427
046161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6481426
76 X = 1975538
88
Y = 17507451
41 feet Y = 5336271
19 meter
Z = -11748140
88 Z = -3580833
34
XDOT = -19255
457788 XDOT = -5869
063534
YDOT = -2602
898429 feet/sec YDOT = -793
363441 meter/sec
ZDOT = -14540
964677 ZDOT = -4432
086033
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 08058
60728128
00020000 00000-0 20000-3 0 9026
2 25544 51
6364 226
3546 0007312 83
6747 276
5251 15
77507757 11082
Satellite: ISS
Catalog Number: 25544
Epoch time: 08058
60728128 = yrday
fracday
Element set: 902
Inclination: 51
6364 deg
RA of node: 226
3546 deg
Eccentricity:
0007312
Arg of perigee: 83
6747 deg
Mean anomaly: 276
5251 deg
Mean motion: 15
77507757 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1108
Checksum: 300
Coasting Arc #4 (Orbit 1117)
---------------------------------------
Vector Time (GMT): 2008/059/05:23:12
128
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2626505
85 A = 6715633
87 meter
Y = 3278181
69 meter E =
0014115
Z = -5251869
61 I = 51
39948
XDOT = -5815
750563 Wp = 87
54512
YDOT = -5030
922146 meter/sec RA = 222
23979 deg
ZDOT = -231
700352 TA = 180
24598
MA = 180
24668
Ha = 187
342 n
mi
Hp = 181
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8617145
17 X = -2637455
38
Y = 10755189
28 feet Y = 3248749
31 meter
Z = -17230543
35 Z = -5264655
70
XDOT = -19080
546465 XDOT = -5757
936227
YDOT = -16505
650086 feet/sec YDOT = -5095
633932 meter/sec
ZDOT = -760
171757 ZDOT = -259
812502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4487443
02 X = -1367772
63
Y = -12965968
97 feet Y = -3952027
34 meter
Z = -17279103
43 Z = -5266670
73
XDOT = 23228
058080 XDOT = 7079
912103
YDOT = -6881
579057 feet/sec YDOT = -2097
505297 meter/sec
ZDOT = -868
382277 ZDOT = -264
682918
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 08059
24076454
00020000 00000-0 20000-3 0 9036
2 25544 51
6385 223
0895 0000933 278
6800 81
4258 15
75577551 11182
Satellite: ISS
Catalog Number: 25544
Epoch time: 08059
24076454 = yrday
fracday
Element set: 903
Inclination: 51
6385 deg
RA of node: 223
0895 deg
Eccentricity:
0000933
Arg of perigee: 278
6800 deg
Mean anomaly: 81
4258 deg
Mean motion: 15
75577551 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1118
Checksum: 300
Coasting Arc #5 (Orbit 1133)
---------------------------------------
Vector Time (GMT): 2008/060/05:23:12
128
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5184559
64 A = 6727724
33 meter
Y = 4264908
08 meter E =
0010866
Z = -347488
40 I = 51
46243
XDOT = -3289
071493 Wp = 141
19046
YDOT = 3517
331040 meter/sec RA = 217
07845 deg
ZDOT = -6012
718159 TA = 42
59869
MA = 42
51446
Ha = 187
370 n
mi
Hp = 181
733
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17009710
10 X = 5138171
47
Y = 13992480
57 feet Y = 4322625
41 meter
Z = -1140053
80 Z = -322414
78
XDOT = -10790
916973 XDOT = -3298
950013
YDOT = 11539
800000 feet/sec YDOT = 3480
495519 meter/sec
ZDOT = -19726
765615 ZDOT = -6028
720292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20826470
31 X = -6347908
15
Y = 7182520
39 feet Y = 2189232
22 meter
Z = -1043555
70 Z = -318075
78
XDOT = -3725
063760 XDOT = -1135
399434
YDOT = -13619
143384 feet/sec YDOT = -4151
114904 meter/sec
ZDOT = -19787
613951 ZDOT = -6031
264732
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 08060
25558393
00020000 00000-0 20000-3 0 9047
2 25544 51
6385 217
8655 0000992 276
7233 83
3818 15
75551183 11345
Satellite: ISS
Catalog Number: 25544
Epoch time: 08060
25558393 = yrday
fracday
Element set: 904
Inclination: 51
6385 deg
RA of node: 217
8655 deg
Eccentricity:
0000992
Arg of perigee: 276
7233 deg
Mean anomaly: 83
3818 deg
Mean motion: 15
75551183 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1134
Checksum: 304
Coasting Arc #6 (Orbit 1149)
---------------------------------------
Vector Time (GMT): 2008/061/05:23:12
128
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3141124
96 A = 6715742
86 meter
Y = -2903495
07 meter E =
0003009
Z = 5175973
63 I = 51
44693
XDOT = 6020
579510 Wp = 39
64361
YDOT = 4700
513379 meter/sec RA = 211
90568 deg
ZDOT = -1014
299481 TA = 60
06192
MA = 60
03204
Ha = 187
094 n
mi
Hp = 181
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10305528
08 X = 3148215
25
Y = -9525902
46 feet Y = -2868329
59 meter
Z = 16981540
77 Z = 5191250
21
XDOT = 19752
557449 XDOT = 5972
497396
YDOT = 15421
631822 feet/sec YDOT = 4767
570094 meter/sec
ZDOT = -3327
754202 ZDOT = -985
168697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3013175
55 X = 918415
91
Y = 13634119
89 feet Y = 4155679
74 meter
Z = 17039689
00 Z = 5193697
21
XDOT = -22336
990796 XDOT = -6808
314795
YDOT = 8966
055321 feet/sec YDOT = 2732
853662 meter/sec
ZDOT = -3215
658299 ZDOT = -980
132650
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 08061
27038793
00020000 00000-0 20000-3 0 9058
2 25544 51
6384 212
6414 0001170 291
0069 69
0970 15
75640766 11500
Satellite: ISS
Catalog Number: 25544
Epoch time: 08061
27038793 = yrday
fracday
Element set: 905
Inclination: 51
6384 deg
RA of node: 212
6414 deg
Eccentricity:
0001170
Arg of perigee: 291
0069 deg
Mean anomaly: 69
0970 deg
Mean motion: 15
75640766 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1150
Checksum: 280
Coasting Arc #7 (Orbit 1165)
---------------------------------------
Vector Time (GMT): 2008/062/05:23:12
128
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5269660
34 A = 6726745
14 meter
Y = -3921236
13 meter E =
0013481
Z = 1418174
25 I = 51
50911
XDOT = 3940
327839 Wp = 56
37750
YDOT = -3183
711989 meter/sec RA = 206
76786 deg
ZDOT = 5806
476319 TA = 319
26480
MA = 319
36553
Ha = 187
271 n
mi
Hp = 181
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17288911
87 X = -5232309
93
Y = -12864947
93 feet Y = -3979955
64 meter
Z = 4652802
66 Z = 1392665
41
XDOT = 12927
584775 XDOT = 3947
429432
YDOT = -10445
249309 feet/sec YDOT = -3139
609295 meter/sec
ZDOT = 19050
119157 ZDOT = 5825
635340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19734022
21 X = 6014929
97
Y = -8711224
15 feet Y = -2655181
12 meter
Z = 4554653
95 Z = 1388258
52
XDOT = 2123
510289 XDOT = 647
245936
YDOT = 14865
232083 feet/sec YDOT = 4530
922739 meter/sec
ZDOT = 19123
105784 ZDOT = 5828
722643
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 08062
28518233
00020000 00000-0 20000-3 0 9063
2 25544 51
6384 207
4168 0001190 301
2231 58
8816 15
75618795 11664
Satellite: ISS
Catalog Number: 25544
Epoch time: 08062
28518233 = yrday
fracday
Element set: 906
Inclination: 51
6384 deg
RA of node: 207
4168 deg
Eccentricity:
0001190
Arg of perigee: 301
2231 deg
Mean anomaly: 58
8816 deg
Mean motion: 15
75618795 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1166
Checksum: 289
Coasting Arc #8 (Orbit 1180)
---------------------------------------
Vector Time (GMT): 2008/063/05:23:12
128
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3753232
34 A = 6717003
04 meter
Y = 2694473
31 meter E =
0011301
Z = -4885939
93 I = 51
50334
XDOT = -5987
600891 Wp = 104
59630
YDOT = -4283
066218 meter/sec RA = 201
57871 deg
ZDOT = 2238
997712 TA = 187
22145
MA = 187
23774
Ha = 187
184 n
mi
Hp = 181
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12313754
40 X = -3759348
90
Y = 8840135
53 feet Y = 2652468
28 meter
Z = -16029986
66 Z = -4904187
63
XDOT = -19644
359878 XDOT = -5950
138390
YDOT = -14052
054521 feet/sec YDOT = -4349
813502 meter/sec
ZDOT = 7345
793020 ZDOT = 2210
001596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1914799
24 X = -583630
81
Y = -14962457
48 feet Y = -4560557
04 meter
Z = -16099547
40 Z = -4907142
05
XDOT = 20666
850150 XDOT = 6299
255926
YDOT = -10423
522422 feet/sec YDOT = -3177
089634 meter/sec
ZDOT = 7234
231297 ZDOT = 2204
993699
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 08063
23653860
00020000 00000-0 20000-3 0 9076
2 25544 51
6383 202
5187 0001286 303
6183 56
4858 15
75652806 11816
Satellite: ISS
Catalog Number: 25544
Epoch time: 08063
23653860 = yrday
fracday
Element set: 907
Inclination: 51
6383 deg
RA of node: 202
5187 deg
Eccentricity:
0001286
Arg of perigee: 303
6183 deg
Mean anomaly: 56
4858 deg
Mean motion: 15
75652806 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1181
Checksum: 294
Coasting Arc #9 (Orbit 1196)
---------------------------------------
Vector Time (GMT): 2008/064/05:23:12
128
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5130493
49 A = 6724911
53 meter
Y = 3569181
89 meter E =
0004098
Z = -2480392
18 I = 51
55722
XDOT = -4672
197327 Wp = 135
44999
YDOT = 3023
823617 meter/sec RA = 196
46244 deg
ZDOT = -5321
073247 TA = 72
64762
MA = 72
60281
Ha = 187
221 n
mi
Hp = 181
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16832327
73 X = 5102250
05
Y = 11709914
33 feet Y = 3626396
01 meter
Z = -8137769
62 Z = -2455537
53
XDOT = -15328
731387 XDOT = -4679
814745
YDOT = 9920
681157 feet/sec YDOT = 2971
533706 meter/sec
ZDOT = -17457
589392 ZDOT = -5343
788825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18196737
86 X = -5546365
70
Y = 9532856
29 feet Y = 2905614
60 meter
Z = -8042140
69 Z = -2451244
48
XDOT = -1041
367119 XDOT = -317
408698
YDOT = -16765
666825 feet/sec YDOT = -5110
175248 meter/sec
ZDOT = -17544
227341 ZDOT = -5347
480494
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 08064
25130701
00020000 00000-0 20000-3 0 9084
2 25544 51
6383 197
2945 0001346 302
7483 57
3551 15
75634222 11977
Satellite: ISS
Catalog Number: 25544
Epoch time: 08064
25130701 = yrday
fracday
Element set: 908
Inclination: 51
6383 deg
RA of node: 197
2945 deg
Eccentricity:
0001346
Arg of perigee: 302
7483 deg
Mean anomaly: 57
3551 deg
Mean motion: 15
75634222 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1197
Checksum: 283
Coasting Arc #10 (Orbit 1212)
---------------------------------------
Vector Time (GMT): 2008/065/05:23:12
128
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4390430
32 A = 6718948
02 meter
Y = -2639814
06 meter E =
0008894
Z = 4343171
07 I = 51
56697
XDOT = 5714
632984 Wp = 61
45602
YDOT = 3890
935091 meter/sec RA = 191
26228 deg
ZDOT = -3402
443082 TA = 62
90145
MA = 62
81074
Ha = 187
012 n
mi
Hp = 181
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14404298
96 X = 4398525
01
Y = -8660807
28 feet Y = -2590672
28 meter
Z = 14249248
93 Z = 4364519
05
XDOT = 18748
795878 XDOT = 5687
227271
YDOT = 12765
535076 feet/sec YDOT = 3954
685972 meter/sec
ZDOT = -11162
871003 ZDOT = -3374
748847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1327026
88 X = 404477
79
Y = 16685459
20 feet Y = 5085727
97 meter
Z = 14330699
81 Z = 4367997
30
XDOT = -18623
309249 XDOT = -5676
384659
YDOT = 11003
546573 feet/sec YDOT = 3353
880995 meter/sec
ZDOT = -11056
312911 ZDOT = -3369
964175
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 08065
26606049
00020000 00000-0 20000-3 0 9090
2 25544 51
6387 192
0695 0001528 314
4830 45
6209 15
75726834 12134
Satellite: ISS
Catalog Number: 25544
Epoch time: 08065
26606049 = yrday
fracday
Element set: 909
Inclination: 51
6387 deg
RA of node: 192
0695 deg
Eccentricity:
0001528
Arg of perigee: 314
4830 deg
Mean anomaly: 45
6209 deg
Mean motion: 15
75726834 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1213
Checksum: 296
Coasting Arc #11 (Orbit 1228)
---------------------------------------
Vector Time (GMT): 2008/066/05:23:12
128
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4784105
20 A = 6722360
11 meter
Y = -3243407
03 meter E =
0011604
Z = 3421646
26 I = 51
60601
XDOT = 5374
922684 Wp = 84
82298
YDOT = -3075
999096 meter/sec RA = 186
15934 deg
ZDOT = 4587
140644 TA = 315
71623
MA = 315
80902
Ha = 187
281 n
mi
Hp = 181
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15695883
22 X = -4764102
72
Y = -10641099
18 feet Y = -3296793
53 meter
Z = 11225873
54 Z = 3398454
45
XDOT = 17634
260774 XDOT = 5386
636525
YDOT = -10091
860551 feet/sec YDOT = -3015
827799 meter/sec
ZDOT = 15049
674029 ZDOT = 4613
280093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16410458
42 X = 5001907
73
Y = -9606574
95 feet Y = -2928084
05 meter
Z = 11136631
03 Z = 3394445
14
XDOT = 808
584131 XDOT = 246
456443
YDOT = 18990
526269 feet/sec YDOT = 5788
312407 meter/sec
ZDOT = 15149
429493 ZDOT = 4617
546109
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 08066
28080431
00020000 00000-0 20000-3 0 9106
2 25544 51
6380 186
8442 0001548 320
7108 39
3944 15
75687881 12299
Satellite: ISS
Catalog Number: 25544
Epoch time: 08066
28080431 = yrday
fracday
Element set: 910
Inclination: 51
6380 deg
RA of node: 186
8442 deg
Eccentricity:
0001548
Arg of perigee: 320
7108 deg
Mean anomaly: 39
3944 deg
Mean motion: 15
75687881 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1229
Checksum: 297
Coasting Arc #12 (Orbit 1243)
---------------------------------------
Vector Time (GMT): 2008/067/05:23:12
128
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4959252
59 A = 6721535
54 meter
Y = 2767003
08 meter E =
0004525
Z = -3599309
86 I = 51
63265
XDOT = -5195
405655 Wp = 87
31828
YDOT = -3579
662241 meter/sec RA = 180
95693 deg
ZDOT = 4411
468217 TA = 229
62040
MA = 229
65991
Ha = 187
119 n
mi
Hp = 181
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16270513
73 X = -4972340
60
Y = 9078094
11 feet Y = 2711472
36 meter
Z = -11808759
38 Z = -3623433
50
XDOT = -17045
294143 XDOT = -5176
420888
YDOT = -11744
298691 feet/sec YDOT = -3637
653656 meter/sec
ZDOT = 14473
320923 ZDOT = 4386
275890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1495606
30 X = -455860
80
Y = -18512739
44 feet Y = -5642682
98 meter
Z = -11900833
92 Z = -3627374
18
XDOT = 16465
856974 XDOT = 5018
793206
YDOT = -10561
648705 feet/sec YDOT = -3219
190525 meter/sec
ZDOT = 14376
364956 ZDOT = 4381
916039
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 08067
23211249
00020000 00000-0 20000-3 0 9116
2 25544 51
6376 181
9456 0001537 320
6178 39
4874 15
75726037 12446
Satellite: ISS
Catalog Number: 25544
Epoch time: 08067
23211249 = yrday
fracday
Element set: 911
Inclination: 51
6376 deg
RA of node: 181
9456 deg
Eccentricity:
0001537
Arg of perigee: 320
6178 deg
Mean anomaly: 39
4874 deg
Mean motion: 15
75726037 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1244
Checksum: 294
Coasting Arc #13 (Orbit 1259)
---------------------------------------
Vector Time (GMT): 2008/068/05:23:12
128
Vector Time (MET): N/A
Weight (LBS) : 568540
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4232737
18 A = 6719509
32 meter
Y = 3055771
34 meter E =
0008029
Z = -4239125
42 I = 51
65394
XDOT = -5963
882675 Wp = 59
14704
YDOT = 3280
136538 meter/sec RA = 175
85970 deg
ZDOT = -3591
377625 TA = 174
34282
MA = 174
33375
Ha = 187
185 n
mi
Hp = 181
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13886933
00 X = 4218845
11
Y = 10025496
51 feet Y = 3103026
09 meter
Z = -13907891
78 Z = -4218597
13
XDOT = -19566
544210 XDOT = -5982
672394
YDOT = 10761
602816 feet/sec YDOT = 3213
339550 meter/sec
ZDOT = -11782
734989 ZDOT = -3620
395763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14786725
88 X = -4506994
05
Y = 8769389
61 feet Y = 2672909
95 meter
Z = -13828864
23 Z = -4215037
82
XDOT = -1393
848408 XDOT = -424
844995
YDOT = -21100
662689 feet/sec YDOT = -6431
481988 meter/sec
ZDOT = -11893
500515 ZDOT = -3625
138957
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 08068
24682959
00020000 00000-0 20000-3 0 9129
2 25544 51
6368 176
7209 0001567 325
8076 34
2986 15
75736473 12602
Satellite: ISS
Catalog Number: 25544
Epoch time: 08068
24682959 = yrday
fracday
Element set: 912
Inclination: 51
6368 deg
RA of node: 176
7209 deg
Eccentricity:
0001567
Arg of perigee: 325
8076 deg
Mean anomaly: 34
2986 deg
Mean motion: 15
75736473 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1260
Checksum: 323
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 may contain past, current and future orbital data 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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