Date:
April 10th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5381 96 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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
There are no maneuvers
Coasting Arc #1 (Orbit 3992)
---------------------------------------
Vector Time (GMT): 2007/099/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3760166
98 A = 6707741
44 meter
Y = 2161423
15 meter E =
0026549
Z = -5136818
25 I = 51
92856
XDOT = -2172
573073 Wp = 72
41381
YDOT = 7230
902156 meter/sec RA = 97
97386 deg
ZDOT = 1466
225333 TA = 211
52024
MA = 211
67956
Ha = 188
468 n
mi
Hp = 171
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12336505
85 X = 3760671
98
Y = 7091283
30 feet Y = 2203474
38 meter
Z = -16853078
23 Z = -5118550
03
XDOT = -7127
864412 XDOT = -2260
391272
YDOT = 23723
432271 feet/sec YDOT = 7206
116181 meter/sec
ZDOT = 4810
450568 ZDOT = 1455
457787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14243373
44 X = 4341380
23
Y = 1387448
37 feet Y = 422894
26 meter
Z = -16784016
84 Z = -5115768
33
XDOT = 3274
851217 XDOT = 998
174651
YDOT = 23536
034387 feet/sec YDOT = 7173
783281 meter/sec
ZDOT = 4770
861703 ZDOT = 1454
158647
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 07099
53423300
00020000 00000-0 20000-3 0 9004
2 25544 51
6303 98
6849 0015778 47
2274 313
0215 15
78593111 39938
Satellite: ISS
Catalog Number: 25544
Epoch time: 07099
53423300 = yrday
fracday
Element set: 900
Inclination: 51
6303 deg
RA of node: 98
6849 deg
Eccentricity:
0015778
Arg of perigee: 47
2274 deg
Mean anomaly: 313
0215 deg
Mean motion: 15
78593111 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3993
Checksum: 294
Coasting Arc #2 (Orbit 4008)
---------------------------------------
Vector Time (GMT): 2007/100/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2428843
59 A = 6715708
21 meter
Y = -5641224
64 meter E =
0017990
Z = -2740710
65 I = 51
95865
XDOT = 3855
871056 Wp = 65
83363
YDOT = 4171
125467 meter/sec RA = 92
85881 deg
ZDOT = -5187
697805 TA = 145
32568
MA = 145
20827
Ha = 188
445 n
mi
Hp = 171
596
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7968646
94 X = 2505057
92
Y = -18507954
85 feet Y = -5613637
77 meter
Z = -8991832
85 Z = -2728726
31
XDOT = 12650
495592 XDOT = 3834
143232
YDOT = 13684
794838 feet/sec YDOT = 4214
122577 meter/sec
ZDOT = -17020
005921 ZDOT = -5169
018703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -599001
43 X = -182575
64
Y = -20161378
35 feet Y = -6145188
12 meter
Z = -8947446
85 Z = -2727181
80
XDOT = 15879
807651 XDOT = 4840
165372
YDOT = 7021
771990 feet/sec YDOT = 2140
236103 meter/sec
ZDOT = -16949
130653 ZDOT = -5166
095023
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 07100
54707838
00020000 00000-0 20000-3 0 9010
2 25544 51
6302 93
4458 0015870 51
2275 309
0305 15
78656098 40093
Satellite: ISS
Catalog Number: 25544
Epoch time: 07100
54707838 = yrday
fracday
Element set: 901
Inclination: 51
6302 deg
RA of node: 93
4458 deg
Eccentricity:
0015870
Arg of perigee: 51
2275 deg
Mean anomaly: 309
0305 deg
Mean motion: 15
78656098 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4009
Checksum: 285
Coasting Arc #3 (Orbit 4024)
---------------------------------------
Vector Time (GMT): 2007/101/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2950341
97 A = 6713485
36 meter
Y = -4894046
29 meter E =
0026904
Z = 3511260
39 I = 51
95134
XDOT = 3330
263005 Wp = 68
90117
YDOT = -5282
179982 meter/sec RA = 87
66047 deg
ZDOT = -4527
046294 TA = 69
43259
MA = 69
14415
Ha = 188
417 n
mi
Hp = 171
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9679599
64 X = -2912453
77
Y = -16056582
31 feet Y = -4926826
84 meter
Z = 11519883
15 Z = 3497019
68
XDOT = 10926
059727 XDOT = 3411
073087
YDOT = -17329
986818 feet/sec YDOT = -5244
487262 meter/sec
ZDOT = -14852
514089 ZDOT = -4510
671674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15816201
99 X = -4820778
37
Y = -10129335
77 feet Y = -3087421
54 meter
Z = 11465622
72 Z = 3494721
80
XDOT = 1518
973353 XDOT = 462
983078
YDOT = -19252
981219 feet/sec YDOT = -5868
308676 meter/sec
ZDOT = -14791
544869 ZDOT = -4508
462876
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 07101
55989983
00020000 00000-0 20000-3 0 9026
2 25544 51
6299 88
2072 0015767 54
4134 305
8498 15
78704530 40256
Satellite: ISS
Catalog Number: 25544
Epoch time: 07101
55989983 = yrday
fracday
Element set: 902
Inclination: 51
6299 deg
RA of node: 88
2072 deg
Eccentricity:
0015767
Arg of perigee: 54
4134 deg
Mean anomaly: 305
8498 deg
Mean motion: 15
78704530 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4025
Checksum: 314
Coasting Arc #4 (Orbit 4040)
---------------------------------------
Vector Time (GMT): 2007/102/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3352746
85 A = 6708701
67 meter
Y = 3268873
15 meter E =
0020112
Z = 4785704
70 I = 51
93344
XDOT = -2886
414576 Wp = 76
67094
YDOT = -6695
640771 meter/sec RA = 82
55665 deg
ZDOT = 2546
994763 TA = 348
54262
MA = 348
58833
Ha = 188
425 n
mi
Hp = 171
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10999825
63 X = -3412298
66
Y = 10724649
43 feet Y = 3231047
95 meter
Z = 15701130
92 Z = 4769272
44
XDOT = -9469
864095 XDOT = -2823
701214
YDOT = -21967
325363 feet/sec YDOT = -6727
567593 meter/sec
ZDOT = 8356
282032 ZDOT = 2533
125046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4984966
18 X = -1519417
69
Y = 14597614
31 feet Y = 4449352
84 meter
Z = 15639678
71 Z = 4766974
07
XDOT = -17413
627942 XDOT = -5307
673797
YDOT = -14857
727306 feet/sec YDOT = -4528
635283 meter/sec
ZDOT = 8303
181757 ZDOT = 2530
809799
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 07102
57269816
00020000 00000-0 20000-3 0 9036
2 25544 51
6302 82
9691 0015641 58
3454 301
9235 15
78750328 40418
Satellite: ISS
Catalog Number: 25544
Epoch time: 07102
57269816 = yrday
fracday
Element set: 903
Inclination: 51
6302 deg
RA of node: 82
9691 deg
Eccentricity:
0015641
Arg of perigee: 58
3454 deg
Mean anomaly: 301
9235 deg
Mean motion: 15
78750328 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4041
Checksum: 286
Coasting Arc #5 (Orbit 4055)
---------------------------------------
Vector Time (GMT): 2007/103/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1994480
55 A = 6718412
16 meter
Y = 6367223
74 meter E =
0025977
Z = -709490
80 I = 51
96118
XDOT = -4374
448934 Wp = 53
25292
YDOT = 2022
738038 meter/sec RA = 77
37940 deg
ZDOT = 6021
021763 TA = 299
03158
MA = 299
29160
Ha = 188
381 n
mi
Hp = 171
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6543571
37 X = 1926579
67
Y = 20889841
67 feet Y = 6389147
46 meter
Z = -2327725
73 Z = -699966
81
XDOT = -14351
866580 XDOT = -4425
991301
YDOT = 6636
279652 feet/sec YDOT = 1973
532527 meter/sec
ZDOT = 19754
008408 ZDOT = 5999
645496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15618576
14 X = 4760542
01
Y = 15343838
16 feet Y = 4676801
87 meter
Z = -2291032
08 Z = -698306
58
XDOT = -8516
156501 XDOT = -2595
724501
YDOT = 11523
840310 feet/sec YDOT = 3512
466527 meter/sec
ZDOT = 19673
774125 ZDOT = 5996
566353
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 07103
52217605
00020000 00000-0 20000-3 0 9042
2 25544 51
6300 78
0576 0015778 62
4772 297
7994 15
78773303 40562
Satellite: ISS
Catalog Number: 25544
Epoch time: 07103
52217605 = yrday
fracday
Element set: 904
Inclination: 51
6300 deg
RA of node: 78
0576 deg
Eccentricity:
0015778
Arg of perigee: 62
4772 deg
Mean anomaly: 297
7994 deg
Mean motion: 15
78773303 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4056
Checksum: 306
Coasting Arc #6 (Orbit 4071)
---------------------------------------
Vector Time (GMT): 2007/104/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4243882
33 A = 6706870
45 meter
Y = -149192
80 meter E =
0029003
Z = -5215040
53 I = 51
91543
XDOT = 1533
116535 Wp = 81
12147
YDOT = 7461
034482 meter/sec RA = 72
22550 deg
ZDOT = 1043
439579 TA = 198
75426
MA = 198
86133
Ha = 188
348 n
mi
Hp = 171
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13923498
46 X = 4270568
95
Y = -489477
69 feet Y = -101586
41 meter
Z = -17109713
02 Z = -5194358
91
XDOT = 5029
909892 XDOT = 1444
503383
YDOT = 24478
459585 feet/sec YDOT = 7477
683246 meter/sec
ZDOT = 3423
358200 ZDOT = 1050
671807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12015026
05 X = 3662179
94
Y = -7238846
48 feet Y = -2206400
41 meter
Z = -17031850
40 Z = -5191308
00
XDOT = 15744
905460 XDOT = 4799
047184
YDOT = 18084
283415 feet/sec YDOT = 5512
089585 meter/sec
ZDOT = 3451
562227 ZDOT = 1052
036167
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 07104
53492830
00020000 00000-0 20000-3 0 9050
2 25544 51
6308 72
8178 0015688 65
7663 294
5140 15
78785611 40726
Satellite: ISS
Catalog Number: 25544
Epoch time: 07104
53492830 = yrday
fracday
Element set: 905
Inclination: 51
6308 deg
RA of node: 72
8178 deg
Eccentricity:
0015688
Arg of perigee: 65
7663 deg
Mean anomaly: 294
5140 deg
Mean motion: 15
78785611 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4072
Checksum: 308
Coasting Arc #7 (Orbit 4087)
---------------------------------------
Vector Time (GMT): 2007/105/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -535877
26 A = 6715749
74 meter
Y = -6231293
81 meter E =
0018805
Z = -2465681
22 I = 51
93688
XDOT = 5261
642341 Wp = 83
84751
YDOT = 1657
887457 meter/sec RA = 67
10312 deg
ZDOT = -5366
144309 TA = 123
91662
MA = 123
73766
Ha = 188
274 n
mi
Hp = 170
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1758127
49 X = -454180
29
Y = -20443877
33 feet Y = -6236829
66 meter
Z = -8089505
30 Z = -2468085
68
XDOT = 17262
606105 XDOT = 5268
780473
YDOT = 5439
263309 feet/sec YDOT = 1716
765656 meter/sec
ZDOT = -17605
460333 ZDOT = -5340
565860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11721509
11 X = -3572715
98
Y = -16837153
47 feet Y = -5131964
38 meter
Z = -8099365
13 Z = -2468686
49
XDOT = 16522
726152 XDOT = 5036
126931
YDOT = -3131
769257 feet/sec YDOT = -954
563270 meter/sec
ZDOT = -17508
924935 ZDOT = -5336
720320
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 07105
54765600
00020000 00000-0 20000-3 0 9061
2 25544 51
6316 67
5780 0015685 69
4494 290
8353 15
78846831 40889
Satellite: ISS
Catalog Number: 25544
Epoch time: 07105
54765600 = yrday
fracday
Element set: 906
Inclination: 51
6316 deg
RA of node: 67
5780 deg
Eccentricity:
0015685
Arg of perigee: 69
4494 deg
Mean anomaly: 290
8353 deg
Mean motion: 15
78846831 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4088
Checksum: 322
Coasting Arc #8 (Orbit 4103)
---------------------------------------
Vector Time (GMT): 2007/106/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4807734
89 A = 6712406
11 meter
Y = -2854314
15 meter E =
0027347
Z = 3696343
53 I = 51
91390
XDOT = 436
801935 Wp = 77
80585
YDOT = -6377
218378 meter/sec RA = 61
90287 deg
ZDOT = -4324
042332 TA = 57
71384
MA = 57
44921
Ha = 188
294 n
mi
Hp = 170
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15773408
44 X = -4793416
62
Y = -9364547
73 feet Y = -2907996
67 meter
Z = 12127111
31 Z = 3673022
19
XDOT = 1433
077215 XDOT = 529
086138
YDOT = -20922
632474 feet/sec YDOT = -6371
818069 meter/sec
ZDOT = -14186
490591 ZDOT = -4321
695803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18401233
25 X = -5608695
89
Y = 144477
04 feet Y = 44036
60 meter
Z = 12038925
94 Z = 3669464
63
XDOT = -9482
388406 XDOT = -2890
231986
YDOT = -17364
366697 feet/sec YDOT = -5292
658969 meter/sec
ZDOT = -14178
470872 ZDOT = -4321
597922
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 07106
56035933
00020000 00000-0 20000-3 0 9074
2 25544 51
6321 62
3390 0015616 73
2235 287
0642 15
78888725 41041
Satellite: ISS
Catalog Number: 25544
Epoch time: 07106
56035933 = yrday
fracday
Element set: 907
Inclination: 51
6321 deg
RA of node: 62
3390 deg
Eccentricity:
0015616
Arg of perigee: 73
2235 deg
Mean anomaly: 287
0642 deg
Mean motion: 15
78888725 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4104
Checksum: 287
Coasting Arc #9 (Orbit 4119)
---------------------------------------
Vector Time (GMT): 2007/107/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1418872
40 A = 6708457
31 meter
Y = 4557619
14 meter E =
0021903
Z = 4695050
51 I = 51
88752
XDOT = -5576
678155 Wp = 90
51942
YDOT = -4580
932437 meter/sec RA = 56
79633 deg
ZDOT = 2750
422361 TA = 332
51093
MA = 332
62662
Ha = 188
130 n
mi
Hp = 170
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4655093
18 X = -1492539
02
Y = 14952818
70 feet Y = 4541340
77 meter
Z = 15403709
03 Z = 4687978
43
XDOT = -18296
188171 XDOT = -5538
400329
YDOT = -15029
305897 feet/sec YDOT = -4643
079871 meter/sec
ZDOT = 9023
695410 ZDOT = 2723
423490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3910112
83 X = 1191802
39
Y = 15191106
01 feet Y = 4630249
11 meter
Z = 15377654
15 Z = 4687108
98
XDOT = -22416
433716 XDOT = -6832
528997
YDOT = -3298
102331 feet/sec YDOT = -1005
261591 meter/sec
ZDOT = 8921
449184 ZDOT = 2719
257711
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 07107
57303678
00020000 00000-0 20000-3 0 9081
2 25544 51
6330 57
1004 0015428 77
5935 282
6956 15
78954581 41201
Satellite: ISS
Catalog Number: 25544
Epoch time: 07107
57303678 = yrday
fracday
Element set: 908
Inclination: 51
6330 deg
RA of node: 57
1004 deg
Eccentricity:
0015428
Arg of perigee: 77
5935 deg
Mean anomaly: 282
6956 deg
Mean motion: 15
78954581 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4120
Checksum: 304
Coasting Arc #10 (Orbit 4134)
---------------------------------------
Vector Time (GMT): 2007/108/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4632324
33 A = 6717847
25 meter
Y = 4785402
14 meter E =
0024276
Z = -840819
87 I = 51
90221
XDOT = -2930
891982 Wp = 63
98807
YDOT = 3864
692452 meter/sec RA = 51
61171 deg
ZDOT = 5991
062234 TA = 286
85389
MA = 287
11998
Ha = 188
149 n
mi
Hp = 170
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15197914
46 X = 4582553
62
Y = 15700138
25 feet Y = 4836925
11 meter
Z = -2758595
36 Z = -818436
46
XDOT = -9615
787343 XDOT = -3002
993773
YDOT = 12679
437180 feet/sec YDOT = 3831
514406 meter/sec
ZDOT = 19655
715991 ZDOT = 5976
648560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21310647
78 X = 6495485
44
Y = 4877330
28 feet Y = 1486610
27 meter
Z = -2673711
66 Z = -814947
31
XDOT = -891
725482 XDOT = -271
797927
YDOT = 14376
710409 feet/sec YDOT = 4382
021333 meter/sec
ZDOT = 19601
919674 ZDOT = 5974
665117
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 07108
52240216
00020000 00000-0 20000-3 0 9096
2 25544 51
6331 52
1885 0015512 80
7610 279
5310 15
78943948 41354
Satellite: ISS
Catalog Number: 25544
Epoch time: 07108
52240216 = yrday
fracday
Element set: 909
Inclination: 51
6331 deg
RA of node: 52
1885 deg
Eccentricity:
0015512
Arg of perigee: 80
7610 deg
Mean anomaly: 279
5310 deg
Mean motion: 15
78943948 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4135
Checksum: 282
Coasting Arc #11 (Orbit 4150)
---------------------------------------
Vector Time (GMT): 2007/109/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3712731
94 A = 6706275
73 meter
Y = -2047968
92 meter E =
0029822
Z = -5221228
87 I = 51
84550
XDOT = 4676
652460 Wp = 90
65059
YDOT = 6023
345032 meter/sec RA = 46
45416 deg
ZDOT = 967
296859 TA = 188
53254
MA = 188
58335
Ha = 188
049 n
mi
Hp = 170
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12180879
08 X = 3760720
92
Y = -6719058
12 feet Y = -2006182
54 meter
Z = -17130015
98 Z = -5203075
61
XDOT = 15343
347966 XDOT = 4604
251928
YDOT = 19761
630683 feet/sec YDOT = 6075
237129 meter/sec
ZDOT = 3173
546125 ZDOT = 989
840814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6420844
77 X = 1957073
49
Y = -12434675
14 feet Y = -3790088
98 meter
Z = -17061905
26 Z = -5200468
72
XDOT = 22848
764990 XDOT = 6964
303569
YDOT = 7346
193261 feet/sec YDOT = 2239
119706 meter/sec
ZDOT = 3259
180051 ZDOT = 993
398080
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 07109
53503299
00020000 00000-0 20000-3 0 9103
2 25544 51
6341 46
9487 0015445 84
6479 275
6448 15
78982482 41518
Satellite: ISS
Catalog Number: 25544
Epoch time: 07109
53503299 = yrday
fracday
Element set: 910
Inclination: 51
6341 deg
RA of node: 46
9487 deg
Eccentricity:
0015445
Arg of perigee: 84
6479 deg
Mean anomaly: 275
6448 deg
Mean motion: 15
78982482 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4151
Checksum: 323
Coasting Arc #12 (Orbit 4166)
---------------------------------------
Vector Time (GMT): 2007/110/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3190583
80 A = 6715195
88 meter
Y = -5377819
11 meter E =
0019721
Z = -2459778
80 I = 51
85624
XDOT = 5463
821617 Wp = 98
80492
YDOT = -805
793756 meter/sec RA = 41
32528 deg
ZDOT = -5364
685072 TA = 108
93508
MA = 108
72122
Ha = 187
961 n
mi
Hp = 170
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10467794
61 X = -3118261
80
Y = -17643763
48 feet Y = -5413093
48 meter
Z = -8070140
44 Z = -2475103
53
XDOT = 17925
923939 XDOT = 5498
487048
YDOT = -2643
680302 feet/sec YDOT = -744
500082 meter/sec
ZDOT = -17600
672810 ZDOT = -5338
057322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18655198
18 X = -5686104
41
Y = -8480288
14 feet Y = -2584791
82 meter
Z = -8128503
82 Z = -2477567
96
XDOT = 12633
283934 XDOT = 3850
624943
YDOT = -11139
137866 feet/sec YDOT = -3395
209222 meter/sec
ZDOT = -17500
489786 ZDOT = -5334
149287
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 07110
54763887
00020000 00000-0 20000-3 0 9118
2 25544 51
6348 41
7090 0015452 88
5863 271
7073 15
79035008 41678
Satellite: ISS
Catalog Number: 25544
Epoch time: 07110
54763887 = yrday
fracday
Element set: 911
Inclination: 51
6348 deg
RA of node: 41
7090 deg
Eccentricity:
0015452
Arg of perigee: 88
5863 deg
Mean anomaly: 271
7073 deg
Mean motion: 15
79035008 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4167
Checksum: 298
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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