Date:
March 8th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 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
077/02:55:34
912 -0
4 0
8 0
8
N/A -0
3 -0
0 186
1
000/00:05:09
824 0
7 -0
1 180
9
Coasting Arc #1 (Orbit 1248)
---------------------------------------
Vector Time (GMT): 2008/067/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6066602
22 A = 6724182
55 meter
Y = 1760281
32 meter E =
0006873
Z = -2296107
68 I = 51
65393
XDOT = -3311
606568 Wp = 156
18595
YDOT = 4333
567668 meter/sec RA = 179
46968 deg
ZDOT = -5439
205602 TA = 49
63679
MA = 49
57680
Ha = 186
734 n
mi
Hp = 181
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19903550
59 X = 6057621
48
Y = 5775201
19 feet Y = 1828071
09 meter
Z = -7533161
67 Z = -2266658
65
XDOT = -10864
850946 XDOT = -3333
396858
YDOT = 14217
741692 feet/sec YDOT = 4296
413005 meter/sec
ZDOT = -17845
162736 ZDOT = -5455
346465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18999626
76 X = 5791086
24
Y = 8379067
44 feet Y = 2553939
76 meter
Z = -7420122
08 Z = -2261653
21
XDOT = -11949
342546 XDOT = -3642
159608
YDOT = 11272
928192 feet/sec YDOT = 3435
988513 meter/sec
ZDOT = -17906
461063 ZDOT = -5457
889332
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
54809357
00020000 00000-0 20000-3 0 9001
2 25544 51
6386 180
3116 0002341 213
2993 146
8024 15
76027442 12499
Satellite: ISS
Catalog Number: 25544
Epoch time: 08067
54809357 = yrday
fracday
Element set: 900
Inclination: 51
6386 deg
RA of node: 180
3116 deg
Eccentricity:
0002341
Arg of perigee: 213
2993 deg
Mean anomaly: 146
8024 deg
Mean motion: 15
76027442 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1249
Checksum: 282
Coasting Arc #2 (Orbit 1264)
---------------------------------------
Vector Time (GMT): 2008/068/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3329763
01 A = 6717786
81 meter
Y = -3828604
98 meter E =
0007503
Z = 4397255
01 I = 51
66243
XDOT = 6667
308207 Wp = 77
64230
YDOT = 1973
593449 meter/sec RA = 174
27616 deg
ZDOT = -3324
040161 TA = 45
74674
MA = 45
68518
Ha = 186
513 n
mi
Hp = 181
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10924419
33 X = 3350966
77
Y = -12561039
94 feet Y = -3791250
63 meter
Z = 14426689
65 Z = 4413482
72
XDOT = 21874
370758 XDOT = 6660
891052
YDOT = 6475
044123 feet/sec YDOT = 2048
114854 meter/sec
ZDOT = -10905
643573 ZDOT = -3291
666563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12226910
65 X = 3726762
36
Y = -11217904
48 feet Y = -3419217
29 meter
Z = 14488385
41 Z = 4416059
87
XDOT = 20218
175990 XDOT = 6162
500042
YDOT = 8085
471477 feet/sec YDOT = 2464
451706 meter/sec
ZDOT = -10781
367597 ZDOT = -3286
160843
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
56260503
00020000 00000-0 20000-3 0 9019
2 25544 51
6389 175
0860 0002112 217
6492 142
4525 15
76068214 12655
Satellite: ISS
Catalog Number: 25544
Epoch time: 08068
56260503 = yrday
fracday
Element set: 901
Inclination: 51
6389 deg
RA of node: 175
0860 deg
Eccentricity:
0002112
Arg of perigee: 217
6492 deg
Mean anomaly: 142
4525 deg
Mean motion: 15
76068214 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1265
Checksum: 276
Coasting Arc #3 (Orbit 1280)
---------------------------------------
Vector Time (GMT): 2008/069/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5490745
42 A = 6720991
57 meter
Y = -1732031
41 meter E =
0011132
Z = 3459883
52 I = 51
70240
XDOT = 4296
880279 Wp = 99
45125
YDOT = -4486
654074 meter/sec RA = 169
17738 deg
ZDOT = 4558
820833 TA = 301
56923
MA = 301
67786
Ha = 186
470 n
mi
Hp = 181
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18014256
64 X = -5487776
89
Y = -5682517
75 feet Y = -1793415
11 meter
Z = 11351323
90 Z = 3433217
02
XDOT = 14097
376245 XDOT = 4324
585578
YDOT = -14719
993680 feet/sec YDOT = -4438
448530 meter/sec
ZDOT = 14956
761263 ZDOT = 4579
762714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17427333
54 X = -5311851
26
Y = -7443548
30 feet Y = -2268793
52 meter
Z = 11248939
45 Z = 3428676
74
XDOT = 14857
320596 XDOT = 4528
511318
YDOT = -11990
434478 feet/sec YDOT = -3654
684429 meter/sec
ZDOT = 15036
441203 ZDOT = 4583
107279
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 08069
57708638
00020000 00000-0 20000-3 0 9028
2 25544 51
6388 169
8596 0002136 223
6238 136
4757 15
76133834 12811
Satellite: ISS
Catalog Number: 25544
Epoch time: 08069
57708638 = yrday
fracday
Element set: 902
Inclination: 51
6388 deg
RA of node: 169
8596 deg
Eccentricity:
0002136
Arg of perigee: 223
6238 deg
Mean anomaly: 136
4757 deg
Mean motion: 15
76133834 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1281
Checksum: 321
Coasting Arc #4 (Orbit 1295)
---------------------------------------
Vector Time (GMT): 2008/070/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4120977
01 A = 6720735
81 meter
Y = 4026825
44 meter E =
0003919
Z = -3464561
98 I = 51
73002
XDOT = -5848
834698 Wp = 116
31776
YDOT = -2063
829125 meter/sec RA = 163
98037 deg
ZDOT = 4560
475717 TA = 202
65860
MA = 202
67590
Ha = 186
270 n
mi
Hp = 180
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13520265
78 X = -4148869
11
Y = 13211369
56 feet Y = 3980586
08 meter
Z = -11366673
15 Z = -3484649
74
XDOT = -19189
090216 XDOT = -5847
475891
YDOT = -6771
092930 feet/sec YDOT = -2129
226160 meter/sec
ZDOT = 14962
190673 ZDOT = 4532
065579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14491415
09 X = -4416983
32
Y = 12066169
36 feet Y = 3677768
42 meter
Z = -11443145
40 Z = -3487870
72
XDOT = -17775
137390 XDOT = -5417
861876
YDOT = -7268
676103 feet/sec YDOT = -2215
492476 meter/sec
ZDOT = 14853
080468 ZDOT = 4527
218927
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 08070
52813879
00020000 00000-0 20000-3 0 9030
2 25544 51
6383 164
9609 0002060 230
9243 129
1738 15
76159338 12961
Satellite: ISS
Catalog Number: 25544
Epoch time: 08070
52813879 = yrday
fracday
Element set: 903
Inclination: 51
6383 deg
RA of node: 164
9609 deg
Eccentricity:
0002060
Arg of perigee: 230
9243 deg
Mean anomaly: 129
1738 deg
Mean motion: 15
76159338 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1296
Checksum: 303
Coasting Arc #5 (Orbit 1311)
---------------------------------------
Vector Time (GMT): 2008/071/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4663301
61 A = 6717511
00 meter
Y = 1946299
50 meter E =
0007432
Z = -4433389
35 I = 51
74578
XDOT = -5097
629314 Wp = 73
26867
YDOT = 4742
743119 meter/sec RA = 158
88507 deg
ZDOT = -3282
293839 TA = 163
85482
MA = 163
83112
Ha = 186
228 n
mi
Hp = 181
112
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15299545
97 X = 4662727
83
Y = 6385497
03 feet Y = 1998443
75 meter
Z = -14545240
65 Z = -4410736
51
XDOT = -16724
505622 XDOT = -5134
339728
YDOT = 15560
180835 feet/sec YDOT = 4685
533080 meter/sec
ZDOT = -10768
680574 ZDOT = -3307
147572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14936700
09 X = 4552706
19
Y = 7366826
38 feet Y = 2245408
68 meter
Z = -14458200
59 Z = -4406859
54
XDOT = -17097
268820 XDOT = -5211
247536
YDOT = 13360
929137 feet/sec YDOT = 4072
411201 meter/sec
ZDOT = -10863
338553 ZDOT = -3311
145591
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 08071
54256685
00020000 00000-0 20000-3 0 9040
2 25544 51
6373 159
7343 0002001 235
8108 124
2867 15
76183993 13128
Satellite: ISS
Catalog Number: 25544
Epoch time: 08071
54256685 = yrday
fracday
Element set: 904
Inclination: 51
6373 deg
RA of node: 159
7343 deg
Eccentricity:
0002001
Arg of perigee: 235
8108 deg
Mean anomaly: 124
2867 deg
Mean motion: 15
76183993 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1312
Checksum: 290
Coasting Arc #6 (Orbit 1327)
---------------------------------------
Vector Time (GMT): 2008/072/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4706839
59 A = 6723615
95 meter
Y = -4257595
27 meter E =
0012849
Z = 2199513
09 I = 51
79387
XDOT = 4803
716203 Wp = 114
37420
YDOT = 2457
377399 meter/sec RA = 153
69827 deg
ZDOT = -5503
130998 TA = 40
99848
MA = 40
90196
Ha = 186
067 n
mi
Hp = 180
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15442387
11 X = 4743414
02
Y = -13968488
41 feet Y = -4204756
14 meter
Z = 7216250
30 Z = 2222467
86
XDOT = 15760
223763 XDOT = 4802
613615
YDOT = 8062
261808 feet/sec YDOT = 2511
088987 meter/sec
ZDOT = -18054
891726 ZDOT = -5479
797295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16047182
01 X = 4891181
08
Y = -13221350
27 feet Y = -4029867
56 meter
Z = 7303704
74 Z = 2226169
20
XDOT = 14497
506782 XDOT = 4418
840067
YDOT = 7636
326609 feet/sec YDOT = 2327
552351 meter/sec
ZDOT = -17965
174956 ZDOT = -5475
785327
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 08072
55696646
00020000 00000-0 20000-3 0 9058
2 25544 51
6372 154
5075 0001774 243
5440 116
5542 15
76253457 13287
Satellite: ISS
Catalog Number: 25544
Epoch time: 08072
55696646 = yrday
fracday
Element set: 905
Inclination: 51
6372 deg
RA of node: 154
5075 deg
Eccentricity:
0001774
Arg of perigee: 243
5440 deg
Mean anomaly: 116
5542 deg
Mean motion: 15
76253457 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1328
Checksum: 297
Coasting Arc #7 (Orbit 1343)
---------------------------------------
Vector Time (GMT): 2008/073/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3691746
34 A = 6714544
73 meter
Y = -2414099
66 meter E =
0004528
Z = 5061191
81 I = 51
78913
XDOT = 5611
435680 Wp = 145
70410
YDOT = -4998
712167 meter/sec RA = 148
59005 deg
ZDOT = 1704
405132 TA = 287
92168
MA = 287
97104
Ha = 186
068 n
mi
Hp = 180
865
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12112028
66 X = -3689063
38
Y = -7920274
48 feet Y = -2455367
85 meter
Z = 16604960
01 Z = 5043263
91
XDOT = 18410
222046 XDOT = 5658
635341
YDOT = -16399
974300 feet/sec YDOT = -4935
697977 meter/sec
ZDOT = 5591
880354 ZDOT = 1731
780045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11960444
93 X = -3645543
61
Y = -8286523
75 feet Y = -2525732
44 meter
Z = 16535959
74 Z = 5040160
53
XDOT = 18262
428306 XDOT = 5566
388148
YDOT = -14963
417316 feet/sec YDOT = -4560
849598 meter/sec
ZDOT = 5696
201913 ZDOT = 1736
202343
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 08073
57133728
00020000 00000-0 20000-3 0 9069
2 25544 51
6372 149
2800 0001853 248
9898 111
1068 15
76302321 13445
Satellite: ISS
Catalog Number: 25544
Epoch time: 08073
57133728 = yrday
fracday
Element set: 906
Inclination: 51
6372 deg
RA of node: 149
2800 deg
Eccentricity:
0001853
Arg of perigee: 248
9898 deg
Mean anomaly: 111
1068 deg
Mean motion: 15
76302321 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1344
Checksum: 286
Coasting Arc #8 (Orbit 1358)
---------------------------------------
Vector Time (GMT): 2008/074/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5006417
49 A = 6725440
88 meter
Y = 4424472
42 meter E =
0009369
Z = -726117
04 I = 51
84948
XDOT = -3655
194963 Wp = 32
93888
YDOT = -3158
206909 meter/sec RA = 143
42832 deg
ZDOT = 6001
415900 TA = 319
16426
MA = 319
23443
Ha = 185
986 n
mi
Hp = 180
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16425254
25 X = -5051993
23
Y = 14515985
65 feet Y = 4368232
98 meter
Z = -2382273
76 Z = -750548
67
XDOT = -11992
109459 XDOT = -3648
761264
YDOT = -10361
571225 feet/sec YDOT = -3199
045435 meter/sec
ZDOT = 19689
684711 ZDOT = 5983
674744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16600262
33 X = -5059759
96
Y = 14299711
12 feet Y = 4358551
95 meter
Z = -2475398
35 Z = -754501
42
XDOT = -10924
076664 XDOT = -3329
658567
YDOT = -9308
802247 feet/sec YDOT = -2837
322925 meter/sec
ZDOT = 19621
305317 ZDOT = 5980
573861
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 08074
52228630
00020000 00000-0 20000-3 0 9073
2 25544 51
6366 144
3796 0001663 261
9607 98
1368 15
76281109 13593
Satellite: ISS
Catalog Number: 25544
Epoch time: 08074
52228630 = yrday
fracday
Element set: 907
Inclination: 51
6366 deg
RA of node: 144
3796 deg
Eccentricity:
0001663
Arg of perigee: 261
9607 deg
Mean anomaly: 98
1368 deg
Mean motion: 15
76281109 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1359
Checksum: 308
Coasting Arc #9 (Orbit 1374)
---------------------------------------
Vector Time (GMT): 2008/075/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2689183
32 A = 6713425
76 meter
Y = 3167364
90 meter E =
0013444
Z = -5284640
93 I = 51
83221
XDOT = -5791
179947 Wp = 91
67075
YDOT = 5066
407314 meter/sec RA = 138
29554 deg
ZDOT = 89
432070 TA = 179
17736
MA = 179
17514
Ha = 185
906 n
mi
Hp = 180
833
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8822779
92 X = 2679236
94
Y = 10391617
14 feet Y = 3197381
26 meter
Z = -17338060
80 Z = -5271601
24
XDOT = -18999
934208 XDOT = -5847
837326
YDOT = 16622
071241 feet/sec YDOT = 5001
330248 meter/sec
ZDOT = 293
412303 ZDOT = 61
161300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8963540
22 X = 2732087
06
Y = 10354998
03 feet Y = 3156203
40 meter
Z = -17287696
99 Z = -5269290
04
XDOT = -18177
898794 XDOT = -5540
623552
YDOT = 16046
188729 feet/sec YDOT = 4890
878325 meter/sec
ZDOT = 185
632814 ZDOT = 56
580882
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 08075
53660476
00020000 00000-0 20000-3 0 9084
2 25544 51
6367 139
1518 0001644 262
8649 97
2328 15
76345916 13754
Satellite: ISS
Catalog Number: 25544
Epoch time: 08075
53660476 = yrday
fracday
Element set: 908
Inclination: 51
6367 deg
RA of node: 139
1518 deg
Eccentricity:
0001644
Arg of perigee: 262
8649 deg
Mean anomaly: 97
2328 deg
Mean motion: 15
76345916 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1375
Checksum: 320
Coasting Arc #10 (Orbit 1390)
---------------------------------------
Vector Time (GMT): 2008/076/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5043020
72 A = 6724961
53 meter
Y = -4350749
37 meter E =
0009363
Z = -894764
03 I = 51
89356
XDOT = 2529
479034 Wp = 148
22628
YDOT = 4153
464965 meter/sec RA = 133
16682 deg
ZDOT = -5975
406986 TA = 41
51554
MA = 41
44446
Ha = 185
881 n
mi
Hp = 180
583
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16545343
58 X = 5095643
19
Y = -14274112
11 feet Y = -4294061
23 meter
Z = -2935577
54 Z = -870137
59
XDOT = 8298
815729 XDOT = 2511
873252
YDOT = 13626
853559 feet/sec YDOT = 4181
652477 meter/sec
ZDOT = -19604
353627 ZDOT = -5963
161860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16253943
61 X = 4954202
01
Y = -14623627
92 feet Y = -4457281
79 meter
Z = -2841673
73 Z = -866142
15
XDOT = 7631
899342 XDOT = 2326
202920
YDOT = 12259
420840 feet/sec YDOT = 3736
671472 meter/sec
ZDOT = -19556
914326 ZDOT = -5960
947486
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 08076
55089515
00020000 00000-0 20000-3 0 9097
2 25544 51
6374 133
9241 0001442 271
2134 88
8865 15
76423956 13917
Satellite: ISS
Catalog Number: 25544
Epoch time: 08076
55089515 = yrday
fracday
Element set: 909
Inclination: 51
6374 deg
RA of node: 133
9241 deg
Eccentricity:
0001442
Arg of perigee: 271
2134 deg
Mean anomaly: 88
8865 deg
Mean motion: 15
76423956 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1391
Checksum: 306
Coasting Arc #11 (Orbit 1400)
---------------------------------------
Vector Time (GMT): 2008/077/02:58:09
824
Vector Time (MET): N/A
Weight (LBS) : 567143
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4940918
54 A = 6725078
28 meter
Y = 4384838
30 meter E =
0013046
Z = 1222361
18 I = 51
90139
XDOT = -2388
725400 Wp = 51
34677
YDOT = -4345
682364 meter/sec RA = 130
07047 deg
ZDOT = 5899
315269 TA = 322
02141
MA = 322
11333
Ha = 186
054 n
mi
Hp = 180
891
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16210362
67 X = -4995521
16
Y = 14385952
42 feet Y = 4329280
87 meter
Z = 4010371
34 Z = 1198225
90
XDOT = -7837
025591 XDOT = -2368
611002
YDOT = -14257
488070 feet/sec YDOT = -4372
281776 meter/sec
ZDOT = 19354
708887 ZDOT = 5887
760090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3615834
95 X = 1102106
49
Y = -21386604
12 feet Y = -6518636
94 meter
Z = 3918349
78 Z = 1194313
01
XDOT = 13573
427462 XDOT = 4137
180691
YDOT = 5853
623219 feet/sec YDOT = 1784
184357 meter/sec
ZDOT = 19309
889397 ZDOT = 5885
654288
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 08077
18481792
00020000 00000-0 20000-3 0 9102
2 25544 51
6346 130
6544 0001850 296
9494 63
1481 15
76282470 14018
Satellite: ISS
Catalog Number: 25544
Epoch time: 08077
18481792 = yrday
fracday
Element set: 910
Inclination: 51
6346 deg
RA of node: 130
6544 deg
Eccentricity:
0001850
Arg of perigee: 296
9494 deg
Mean anomaly: 63
1481 deg
Mean motion: 15
76282470 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1401
Checksum: 292
Coasting Arc #12 (Orbit 1415)
---------------------------------------
Vector Time (GMT): 2008/078/02:58:09
824
Vector Time (MET): N/A
Weight (LBS) : 567143
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1720527
15 A = 6715118
48 meter
Y = 4260919
49 meter E =
0010844
Z = -4906541
89 I = 51
88584
XDOT = -5540
233426 Wp = 104
30177
YDOT = 4839
646138 meter/sec RA = 124
90498 deg
ZDOT = 2261
606999 TA = 187
62143
MA = 187
63792
Ha = 186
039 n
mi
Hp = 180
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5644774
12 X = 1696587
63
Y = 13979394
67 feet Y = 4280025
25 meter
Z = -16097578
37 Z = -4898242
15
XDOT = -18176
618853 XDOT = -5604
925596
YDOT = 15878
104126 feet/sec YDOT = 4777
330512 meter/sec
ZDOT = 7419
970468 ZDOT = 2234
535660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13360361
00 X = -4072238
03
Y = -7058862
18 feet Y = -2151541
19 meter
Z = -16065248
15 Z = -4896687
63
XDOT = 3301
291679 XDOT = 1006
233704
YDOT = -22889
168198 feet/sec YDOT = -6976
618467 meter/sec
ZDOT = 7316
738202 ZDOT = 2230
141804
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 08078
13576680
00020000 00000-0 20000-3 0 9110
2 25544 51
6343 125
7529 0001684 301
0141 59
0858 15
76328554 14167
Satellite: ISS
Catalog Number: 25544
Epoch time: 08078
13576680 = yrday
fracday
Element set: 911
Inclination: 51
6343 deg
RA of node: 125
7529 deg
Eccentricity:
0001684
Arg of perigee: 301
0141 deg
Mean anomaly: 59
0858 deg
Mean motion: 15
76328554 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1416
Checksum: 289
Coasting Arc #13 (Orbit 1431)
---------------------------------------
Vector Time (GMT): 2008/079/02:58:09
824
Vector Time (MET): N/A
Weight (LBS) : 567143
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4709144
27 A = 6722278
59 meter
Y = -3965731
16 meter E =
0003195
Z = -2699145
07 I = 51
92618
XDOT = 1593
098810 Wp = 121
80409
YDOT = 5437
034697 meter/sec RA = 119
81148 deg
ZDOT = -5215
066565 TA = 88
86349
MA = 88
82689
Ha = 186
028 n
mi
Hp = 180
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15449948
38 X = 4766251
42
Y = -13010929
01 feet Y = -3912751
75 meter
Z = -8855462
84 Z = -2676129
42
XDOT = 5226
702131 XDOT = 1557
516038
YDOT = 17838
040344 feet/sec YDOT = 5454
650239 meter/sec
ZDOT = -17109
798443 ZDOT = -5207
414325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3222434
57 X = -982198
06
Y = 19978693
69 feet Y = 6089505
84 meter
Z = -8767674
41 Z = -2672387
16
XDOT = -14233
631497 XDOT = -4338
410880
YDOT = -9782
379990 feet/sec YDOT = -2981
669421 meter/sec
ZDOT = -17079
810021 ZDOT = -5205
926094
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 08079
15008518
00020000 00000-0 20000-3 0 9124
2 25544 51
6344 120
5256 0001727 310
4570 49
6443 15
76386766 14328
Satellite: ISS
Catalog Number: 25544
Epoch time: 08079
15008518 = yrday
fracday
Element set: 912
Inclination: 51
6344 deg
RA of node: 120
5256 deg
Eccentricity:
0001727
Arg of perigee: 310
4570 deg
Mean anomaly: 49
6443 deg
Mean motion: 15
76386766 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1432
Checksum: 284
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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