Date:
July 22nd 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9149 32 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 2886)
---------------------------------------
Vector Time (GMT): 2010/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5176963
19 A = 6735515
30 meter
Y = 2842849
52 meter E =
0011109
Z = -3251642
51 I = 51
92710
XDOT = -299
594034 Wp = 113
89867
YDOT = 6007
503723 meter/sec RA = 54
32069 deg
ZDOT = 4783
667546 TA = 208
32045
MA = 208
38088
Ha = 196
831 n
mi
Hp = 185
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16984787
37 X = 5160584
92
Y = 9326934
12 feet Y = 2900650
33 meter
Z = -10668118
46 Z = -3226532
37
XDOT = -982
920060 XDOT = -389
986762
YDOT = 19709
657885 feet/sec YDOT = 6003
647339 meter/sec
ZDOT = 15694
447328 ZDOT = 4781
993488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 106141
52 X = 32351
93
Y = -19431807
11 feet Y = -5922814
81 meter
Z = -10567736
74 Z = -3221046
16
XDOT = 16437
162960 XDOT = 5010
047270
YDOT = -8426
627726 feet/sec YDOT = -2568
436131 meter/sec
ZDOT = 15687
701634 ZDOT = 4781
611458
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 10202
50664778
00016717 00000-0 10270-3 0 9005
2 25544 51
6455 54
9326 0007633 133
0604 227
1198 15
71252106 28878
Satellite: ISS
Catalog Number: 25544
Epoch time: 10202
50664778 = yrday
fracday
Element set: 900
Inclination: 51
6455 deg
RA of node: 54
9326 deg
Eccentricity:
0007633
Arg of perigee: 133
0604 deg
Mean anomaly: 227
1198 deg
Mean motion: 15
71252106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2887
Checksum: 297
Coasting Arc #2 (Orbit 2902)
---------------------------------------
Vector Time (GMT): 2010/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1089897
37 A = 6734364
49 meter
Y = -5590145
48 meter E =
0011615
Z = -3598390
99 I = 51
90397
XDOT = 6044
917049 Wp = 113
65121
YDOT = 1675
307250 meter/sec RA = 49
27615 deg
ZDOT = -4449
332741 TA = 109
09177
MA = 108
96596
Ha = 196
755 n
mi
Hp = 185
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3575778
78 X = -1009826
23
Y = -18340372
30 feet Y = -5601885
09 meter
Z = -11805744
72 Z = -3603492
03
XDOT = 19832
405016 XDOT = 6047
347964
YDOT = 5496
414863 feet/sec YDOT = 1742
919413 meter/sec
ZDOT = -14597
548364 ZDOT = -4419
960732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14267098
22 X = -4348611
54
Y = 12046766
92 feet Y = 3671854
56 meter
Z = -11826088
68 Z = -3604591
83
XDOT = -4095
791751 XDOT = -1248
397326
YDOT = -19014
711869 feet/sec YDOT = -5795
684178 meter/sec
ZDOT = -14480
111310 ZDOT = -4413
537927
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 10203
52425666
00016717 00000-0 10270-3 0 9010
2 25544 51
6446 49
7285 0007607 136
8743 223
3016 15
71256406 29033
Satellite: ISS
Catalog Number: 25544
Epoch time: 10203
52425666 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 49
7285 deg
Eccentricity:
0007607
Arg of perigee: 136
8743 deg
Mean anomaly: 223
3016 deg
Mean motion: 15
71256406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2903
Checksum: 297
Coasting Arc #3 (Orbit 2918)
---------------------------------------
Vector Time (GMT): 2010/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5051008
39 A = 6731452
18 meter
Y = -48693
27 meter E =
0013636
Z = 4436584
58 I = 51
87401
XDOT = -2839
462704 Wp = 100
46083
YDOT = -6358
870966 meter/sec RA = 44
12950 deg
ZDOT = -3296
402652 TA = 22
51645
MA = 22
45667
Ha = 196
743 n
mi
Hp = 185
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16571549
84 X = -5071640
25
Y = -159754
82 feet Y = -105292
70 meter
Z = 14555723
68 Z = 4411997
07
XDOT = -9315
822521 XDOT = -2752
132559
YDOT = -20862
437552 feet/sec YDOT = -6390
134742 meter/sec
ZDOT = -10814
969330 ZDOT = -3309
985378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8276924
91 X = 2522806
71
Y = 14456382
81 feet Y = 4406305
48 meter
Z = 14457399
07 Z = 4406615
24
XDOT = -12277
738241 XDOT = -3742
254616
YDOT = 17919
652823 feet/sec YDOT = 5461
910180 meter/sec
ZDOT = -10869
220370 ZDOT = -3312
938369
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 10204
54185587
00016717 00000-0 10270-3 0 9029
2 25544 51
6450 44
5237 0007514 141
2066 218
9636 15
71292119 29199
Satellite: ISS
Catalog Number: 25544
Epoch time: 10204
54185587 = yrday
fracday
Element set: 902
Inclination: 51
6450 deg
RA of node: 44
5237 deg
Eccentricity:
0007514
Arg of perigee: 141
2066 deg
Mean anomaly: 218
9636 deg
Mean motion: 15
71292119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2919
Checksum: 302
Coasting Arc #4 (Orbit 2934)
---------------------------------------
Vector Time (GMT): 2010/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3776268
82 A = 6737934
95 meter
Y = 5171884
84 meter E =
0017622
Z = 2083089
43 I = 51
87228
XDOT = -5110
258575 Wp = 94
31710
YDOT = 1474
308807 meter/sec RA = 39
07263 deg
ZDOT = 5562
108550 TA = 288
83903
MA = 289
03007
Ha = 196
547 n
mi
Hp = 185
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12389333
40 X = 3708036
14
Y = 16968126
12 feet Y = 5213731
53 meter
Z = 6834282
90 Z = 2101269
16
XDOT = -16765
940208 XDOT = -5153
383925
YDOT = 4836
971150 feet/sec YDOT = 1416
920938 meter/sec
ZDOT = 18248
387632 ZDOT = 5537
178873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8074430
80 X = 2461086
51
Y = -19370549
48 feet Y = -5904143
48 meter
Z = 6906930
50 Z = 2105232
42
XDOT = 11492
675652 XDOT = 3502
967539
YDOT = 11309
864676 feet/sec YDOT = 3447
246753 meter/sec
ZDOT = 18148
674911 ZDOT = 5531
716113
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 10205
55944709
00016717 00000-0 10270-3 0 9031
2 25544 51
6437 39
3185 0007639 145
3836 214
7824 15
71307578 29353
Satellite: ISS
Catalog Number: 25544
Epoch time: 10205
55944709 = yrday
fracday
Element set: 903
Inclination: 51
6437 deg
RA of node: 39
3185 deg
Eccentricity:
0007639
Arg of perigee: 145
3836 deg
Mean anomaly: 214
7824 deg
Mean motion: 15
71307578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2935
Checksum: 328
Coasting Arc #5 (Orbit 2949)
---------------------------------------
Vector Time (GMT): 2010/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3595234
50 A = 6728526
49 meter
Y = -2458634
81 meter E =
0019970
Z = -5145732
80 I = 51
81542
XDOT = 5557
324060 Wp = 117
15016
YDOT = 5104
444062 meter/sec RA = 33
94014 deg
ZDOT = 1439
255109 TA = 166
66617
MA = 166
61331
Ha = 196
539 n
mi
Hp = 186
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11795388
77 X = 3647456
66
Y = -8066387
16 feet Y = -2418138
13 meter
Z = -16882325
45 Z = -5128141
00
XDOT = 18232
690484 XDOT = 5492
840722
YDOT = 16746
863722 feet/sec YDOT = 5166
228658 meter/sec
ZDOT = 4721
965581 ZDOT = 1466
095980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13176072
32 X = -4016066
84
Y = -5741106
70 feet Y = -1749889
32 meter
Z = -16811945
84 Z = -5124281
09
XDOT = 4004
246659 XDOT = 1220
494382
YDOT = -23376
435340 feet/sec YDOT = -7125
137492 meter/sec
ZDOT = 4829
252987 ZDOT = 1471
956310
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 10206
51343190
00016717 00000-0 10270-3 0 9046
2 25544 51
6429 34
4379 0007696 147
9750 212
1881 15
71303243 29508
Satellite: ISS
Catalog Number: 25544
Epoch time: 10206
51343190 = yrday
fracday
Element set: 904
Inclination: 51
6429 deg
RA of node: 34
4379 deg
Eccentricity:
0007696
Arg of perigee: 147
9750 deg
Mean anomaly: 212
1881 deg
Mean motion: 15
71303243 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2950
Checksum: 298
Coasting Arc #6 (Orbit 2965)
---------------------------------------
Vector Time (GMT): 2010/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5722626
51 A = 6739654
99 meter
Y = -3518727
26 meter E =
0018639
Z = -407317
27 I = 51
82815
XDOT = 2801
261722 Wp = 143
05602
YDOT = -3875
081696 meter/sec RA = 28
85452 deg
ZDOT = -6036
982780 TA = 41
35913
MA = 41
21814
Ha = 196
305 n
mi
Hp = 186
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18775021
36 X = -5680875
52
Y = -11544380
76 feet Y = -3582487
60 meter
Z = -1336342
74 Z = -435016
09
XDOT = 9190
491215 XDOT = 2873
711277
YDOT = -12713
522625 feet/sec YDOT = -3843
350607 meter/sec
ZDOT = -19806
373951 ZDOT = -6023
198991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 653602
85 X = 199218
15
Y = 22023594
85 feet Y = 6712791
71 meter
Z = -1447079
51 Z = -441069
84
XDOT = -14130
648118 XDOT = -4307
021546
YDOT = -847
252974 feet/sec YDOT = -258
242706 meter/sec
ZDOT = -19751
208539 ZDOT = -6020
168363
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 10207
53100511
00016717 00000-0 10270-3 0 9058
2 25544 51
6434 29
2336 0007466 151
3112 208
8462 15
71347578 29668
Satellite: ISS
Catalog Number: 25544
Epoch time: 10207
53100511 = yrday
fracday
Element set: 905
Inclination: 51
6434 deg
RA of node: 29
2336 deg
Eccentricity:
0007466
Arg of perigee: 151
3112 deg
Mean anomaly: 208
8462 deg
Mean motion: 15
71347578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2966
Checksum: 290
Coasting Arc #7 (Orbit 2981)
---------------------------------------
Vector Time (GMT): 2010/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1103194
73 A = 6727939
31 meter
Y = 4042539
84 meter E =
0009884
Z = 5259224
33 I = 51
76040
XDOT = -7194
475218 Wp = 143
40898
YDOT = -2691
160804 meter/sec RA = 23
75009 deg
ZDOT = 551
128938 TA = 301
31485
MA = 301
41158
Ha = 196
461 n
mi
Hp = 186
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3619405
27 X = -1173864
93
Y = 13262925
98 feet Y = 4029807
68 meter
Z = 17254673
01 Z = 5253693
81
XDOT = -23603
921318 XDOT = -7166
524682
YDOT = -8829
267731 feet/sec YDOT = -2771
457492 meter/sec
ZDOT = 1808
165807 ZDOT = 516
246638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13055374
61 X = 3979278
18
Y = -4396213
50 feet Y = -1339965
88 meter
Z = 17232514
07 Z = 5252470
29
XDOT = 5685
731887 XDOT = 1733
011079
YDOT = 23532
885506 feet/sec YDOT = 7172
823502 meter/sec
ZDOT = 1668
692779 ZDOT = 508
617559
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 10208
54857273
00016717 00000-0 10270-3 0 9065
2 25544 51
6428 24
0281 0007685 154
8466 205
3071 15
71280956 29828
Satellite: ISS
Catalog Number: 25544
Epoch time: 10208
54857273 = yrday
fracday
Element set: 906
Inclination: 51
6428 deg
RA of node: 24
0281 deg
Eccentricity:
0007685
Arg of perigee: 154
8466 deg
Mean anomaly: 205
3071 deg
Mean motion: 15
71280956 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2982
Checksum: 317
Coasting Arc #8 (Orbit 2996)
---------------------------------------
Vector Time (GMT): 2010/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6516475
01 A = 6738999
33 meter
Y = 1080369
59 meter E =
0008214
Z = -1342464
91 I = 51
77058
XDOT = 371
444113 Wp = 90
70390
YDOT = 4983
251277 meter/sec RA = 18
62620 deg
ZDOT = 5843
960163 TA = 254
60906
MA = 254
69982
Ha = 196
285 n
mi
Hp = 186
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21379511
18 X = 6510431
12
Y = 3544519
65 feet Y = 1153207
00 meter
Z = -4404412
44 Z = -1310823
14
XDOT = 1218
648664 XDOT = 287
304565
YDOT = 16349
249597 feet/sec YDOT = 4986
934161 meter/sec
ZDOT = 19173
097649 ZDOT = 5845
560552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9465885
55 X = -2885201
92
Y = -19522875
66 feet Y = -5950572
50 meter
Z = -4277885
42 Z = -1303899
47
XDOT = 11287
112515 XDOT = 3440
311895
YDOT = -9652
682268 feet/sec YDOT = -2942
137555 meter/sec
ZDOT = 19179
448065 ZDOT = 5845
895770
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 10209
50253056
00016717 00000-0 10270-3 0 9072
2 25544 51
6434 19
1480 0007776 159
0497 201
0985 15
71344041 29972
Satellite: ISS
Catalog Number: 25544
Epoch time: 10209
50253056 = yrday
fracday
Element set: 907
Inclination: 51
6434 deg
RA of node: 19
1480 deg
Eccentricity:
0007776
Arg of perigee: 159
0497 deg
Mean anomaly: 201
0985 deg
Mean motion: 15
71344041 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2997
Checksum: 308
Coasting Arc #9 (Orbit 3012)
---------------------------------------
Vector Time (GMT): 2010/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1749884
18 A = 6729505
18 meter
Y = -4350146
02 meter E =
0014428
Z = -4837625
38 I = 51
71060
XDOT = 7286
047699 Wp = 104
69153
YDOT = -226
595220 meter/sec RA = 13
55006 deg
ZDOT = -2441
403313 TA = 141
49295
MA = 141
38992
Ha = 196
155 n
mi
Hp = 186
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5741089
81 X = -1677610
09
Y = -14272132
61 feet Y = -4369309
92 meter
Z = -15871474
35 Z = -4845950
84
XDOT = 23904
355967 XDOT = 7299
899702
YDOT = -743
422639 feet/sec YDOT = -145
040705 meter/sec
ZDOT = -8009
853389 ZDOT = -2405
974673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8169916
67 X = -2490190
60
Y = 12994220
59 feet Y = 3960638
44 meter
Z = -15904724
84 Z = -4847760
13
XDOT = -13816
353299 XDOT = -4211
224486
YDOT = -18278
761267 feet/sec YDOT = -5571
366434 meter/sec
ZDOT = -7868
174821 ZDOT = -2398
219685
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 10210
52007847
00016717 00000-0 10270-3 0 9082
2 25544 51
6440 13
9437 0007736 161
7185 198
4256 15
71369195 30130
Satellite: ISS
Catalog Number: 25544
Epoch time: 10210
52007847 = yrday
fracday
Element set: 908
Inclination: 51
6440 deg
RA of node: 13
9437 deg
Eccentricity:
0007736
Arg of perigee: 161
7185 deg
Mean anomaly: 198
4256 deg
Mean motion: 15
71369195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3013
Checksum: 306
Coasting Arc #10 (Orbit 3028)
---------------------------------------
Vector Time (GMT): 2010/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5902349
09 A = 6736188
48 meter
Y = 1433516
03 meter E =
0017874
Z = 2887258
04 I = 51
70250
XDOT = -3591
052724 Wp = 122
11907
YDOT = -4568
640944 meter/sec RA = 8
39637 deg
ZDOT = -5059
389084 TA = 24
71698
MA = 24
63144
Ha = 196
154 n
mi
Hp = 186
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19364662
37 X = -5931965
84
Y = 4703136
58 feet Y = 1367346
72 meter
Z = 9472631
35 Z = 2858512
94
XDOT = -11781
669043 XDOT = -3515
121189
YDOT = -14988
979474 feet/sec YDOT = -4608
373473 meter/sec
ZDOT = -16599
045550 ZDOT = -5076
649939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15496836
78 X = 4723435
85
Y = 12614372
26 feet Y = 3844860
66 meter
Z = 9357673
29 Z = 2852218
82
XDOT = -3943
209043 XDOT = -1201
890116
YDOT = 17242
028546 feet/sec YDOT = 5255
370301 meter/sec
ZDOT = -16668
022984 ZDOT = -5080
413406
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 10211
53761705
00016717 00000-0 10270-3 0 9095
2 25544 51
6435 8
7382 0007733 166
7917 193
3448 15
71354049 30296
Satellite: ISS
Catalog Number: 25544
Epoch time: 10211
53761705 = yrday
fracday
Element set: 909
Inclination: 51
6435 deg
RA of node: 8
7382 deg
Eccentricity:
0007733
Arg of perigee: 166
7917 deg
Mean anomaly: 193
3448 deg
Mean motion: 15
71354049 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3029
Checksum: 315
Coasting Arc #11 (Orbit 3044)
---------------------------------------
Vector Time (GMT): 2010/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4372240
82 A = 6732952
68 meter
Y = 3331847
66 meter E =
0015580
Z = 3884663
90 I = 51
66315
XDOT = -5848
756172 Wp = 127
53673
YDOT = 2892
474466 meter/sec RA = 3
33341 deg
ZDOT = 4081
531945 TA = 279
83519
MA = 280
01107
Ha = 195
861 n
mi
Hp = 186
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14344622
11 X = 4315787
72
Y = 10931258
72 feet Y = 3380424
86 meter
Z = 12744960
31 Z = 3905767
06
XDOT = -19188
832584 XDOT = -5900
492807
YDOT = 9489
745624 feet/sec YDOT = 2826
780733 meter/sec
ZDOT = 13390
852838 ZDOT = 4052
993416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -241382
38 X = -73573
35
Y = -17973457
00 feet Y = -5478309
69 meter
Z = 12829309
89 Z = 3910373
65
XDOT = 18066
797045 XDOT = 5506
759739
YDOT = 9281
789304 feet/sec YDOT = 2829
089380 meter/sec
ZDOT = 13276
711636 ZDOT = 4046
741707
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 10212
55514597
00016717 00000-0 10270-3 0 9105
2 25544 51
6444 3
5334 0007761 170
7294 189
4012 15
71403231 30459
Satellite: ISS
Catalog Number: 25544
Epoch time: 10212
55514597 = yrday
fracday
Element set: 910
Inclination: 51
6444 deg
RA of node: 3
5334 deg
Eccentricity:
0007761
Arg of perigee: 170
7294 deg
Mean anomaly: 189
4012 deg
Mean motion: 15
71403231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3045
Checksum: 278
Coasting Arc #12 (Orbit 3059)
---------------------------------------
Vector Time (GMT): 2010/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4075148
13 A = 6732270
89 meter
Y = -3413517
09 meter E =
0013057
Z = -4144884
78 I = 51
63128
XDOT = 6119
825168 Wp = 141
04571
YDOT = 2764
222361 meter/sec RA = 358
16825 deg
ZDOT = 3736
795374 TA = 167
30134
MA = 167
26842
Ha = 195
834 n
mi
Hp = 186
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13369908
57 X = 4133150
80
Y = -11199203
04 feet Y = -3367621
83 meter
Z = -13598703
34 Z = -4124947
11
XDOT = 20078
166561 XDOT = 6070
307729
YDOT = 9068
971000 feet/sec YDOT = 2832
380860 meter/sec
ZDOT = 12259
827343 ZDOT = 3766
405151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17180672
93 X = -5236669
11
Y = -3341225
59 feet Y = -1018405
56 meter
Z = -13518950
60 Z = -4120576
14
XDOT = -5863
509783 XDOT = -1787
197782
YDOT = -19981
098163 feet/sec YDOT = -6090
238720 meter/sec
ZDOT = 12378
190936 ZDOT = 3772
872597
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 10213
50907251
00016717 00000-0 10270-3 0 9115
2 25544 51
6455 358
6545 0007694 173
4631 186
6632 15
71391082 30603
Satellite: ISS
Catalog Number: 25544
Epoch time: 10213
50907251 = yrday
fracday
Element set: 911
Inclination: 51
6455 deg
RA of node: 358
6545 deg
Eccentricity:
0007694
Arg of perigee: 173
4631 deg
Mean anomaly: 186
6632 deg
Mean motion: 15
71391082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3060
Checksum: 302
Coasting Arc #13 (Orbit 3075)
---------------------------------------
Vector Time (GMT): 2010/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6072712
98 A = 6736565
83 meter
Y = -1327034
28 meter E =
0011472
Z = -2584292
16 I = 51
61589
XDOT = 3235
497569 Wp = 157
13650
YDOT = -4591
407443 meter/sec RA = 353
09865 deg
ZDOT = -5263
424041 TA = 52
18713
MA = 52
08332
Ha = 195
586 n
mi
Hp = 187
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19923599
02 X = -6044868
53
Y = -4353786
99 feet Y = -1394787
14 meter
Z = -8478648
82 Z = -2613725
72
XDOT = 10615
149505 XDOT = 3312
167710
YDOT = -15063
672713 feet/sec YDOT = -4554
797172 meter/sec
ZDOT = -17268
451578 ZDOT = -5247
520104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9500661
64 X = 2895801
67
Y = 17989816
24 feet Y = 5483295
99 meter
Z = -8596318
08 Z = -2620157
75
XDOT = -17111
739331 XDOT = -5215
658148
YDOT = 843
808117 feet/sec YDOT = 257
192714 meter/sec
ZDOT = -17204
815797 ZDOT = -5244
027855
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 10214
52658412
00016717 00000-0 10270-3 0 9121
2 25544 51
6453 353
4494 0007618 177
5095 182
6106 15
71413725 30760
Satellite: ISS
Catalog Number: 25544
Epoch time: 10214
52658412 = yrday
fracday
Element set: 912
Inclination: 51
6453 deg
RA of node: 353
4494 deg
Eccentricity:
0007618
Arg of perigee: 177
5095 deg
Mean anomaly: 182
6106 deg
Mean motion: 15
71413725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3076
Checksum: 305
Coasting Arc #14 (Orbit 3091)
---------------------------------------
Vector Time (GMT): 2010/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1437292
16 A = 6729022
08 meter
Y = 4322305
80 meter E =
0006634
Z = 4947196
41 I = 51
56058
XDOT = -7416
717265 Wp = 128
90470
YDOT = -97
239698 meter/sec RA = 347
94090 deg
ZDOT = -2072
036290 TA = 341
17308
MA = 341
19761
Ha = 195
641 n
mi
Hp = 187
236
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4715525
47 X = -1509550
65
Y = 14180793
32 feet Y = 4305828
75 meter
Z = 16230959
37 Z = 4940038
89
XDOT = -24333
061894 XDOT = -7405
013143
YDOT = -319
027880 feet/sec YDOT = -180
112266 meter/sec
ZDOT = -6798
019323 ZDOT = -2108
038154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13841281
20 X = 4218822
51
Y = -5716613
18 feet Y = -1742423
70 meter
Z = 16202295
82 Z = 4938459
77
XDOT = 15338
461211 XDOT = 4675
162977
YDOT = 17483
695981 feet/sec YDOT = 5329
030535 meter/sec
ZDOT = -6941
960574 ZDOT = -2115
909583
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 10215
54408826
00016717 00000-0 10270-3 0 9137
2 25544 51
6457 348
2450 0007615 180
4865 179
6291 15
71388215 30927
Satellite: ISS
Catalog Number: 25544
Epoch time: 10215
54408826 = yrday
fracday
Element set: 913
Inclination: 51
6457 deg
RA of node: 348
2450 deg
Eccentricity:
0007615
Arg of perigee: 180
4865 deg
Mean anomaly: 179
6291 deg
Mean motion: 15
71388215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3092
Checksum: 318
Coasting Arc #15 (Orbit 3107)
---------------------------------------
Vector Time (GMT): 2010/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6555178
76 A = 6738967
76 meter
Y = -1188670
91 meter E =
0010800
Z = 1005043
37 I = 51
56641
XDOT = -23
177958 Wp = 89
11337
YDOT = 4918
901064 meter/sec RA = 342
84644 deg
ZDOT = 5914
296268 TA = 281
86473
MA = 281
98582
Ha = 195
384 n
mi
Hp = 187
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21506491
99 X = 6563101
20
Y = -3899838
94 feet Y = -1115322
78 meter
Z = 3297386
38 Z = 1036907
41
XDOT = -76
043170 XDOT = -106
910728
YDOT = 16138
126850 feet/sec YDOT = 4918
173150 meter/sec
ZDOT = 19403
859146 ZDOT = 5913
980740
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17314548
83 X = -5277474
48
Y = -13307436
11 feet Y = -4056106
53 meter
Z = 3424797
97 Z = 1043878
42
XDOT = 11119
455242 XDOT = 3389
209958
YDOT = -9429
995493 feet/sec YDOT = -2874
262626 meter/sec
ZDOT = 19402
543535 ZDOT = 5913
895270
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 10216
56157967
00016717 00000-0 10270-3 0 9148
2 25544 51
6467 343
0401 0007569 185
0364 175
0723 15
71451189 31089
Satellite: ISS
Catalog Number: 25544
Epoch time: 10216
56157967 = yrday
fracday
Element set: 914
Inclination: 51
6467 deg
RA of node: 343
0401 deg
Eccentricity:
0007569
Arg of perigee: 185
0364 deg
Mean anomaly: 175
0723 deg
Mean motion: 15
71451189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3108
Checksum: 311
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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