Date:
October 11th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 63 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 2397)
---------------------------------------
Vector Time (GMT): 2009/282/14:00:34
905
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1949088
26 A = 6724031
37 meter
Y = 5231464
82 meter E =
0014876
Z = 3746297
61 I = 51
96917
XDOT = -4345
990396 Wp = 130
55460
YDOT = -4699
237617 meter/sec RA = 78
77495 deg
ZDOT = 4280
601758 TA = 274
47040
MA = 274
64033
Ha = 190
666 n
mi
Hp = 182
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6394646
51 X = -2025641
73
Y = 17163598
50 feet Y = 5209240
91 meter
Z = 12291002
67 Z = 3736642
85
XDOT = -14258
498673 XDOT = -4313
914492
YDOT = -15417
446251 feet/sec YDOT = -4747
657731 meter/sec
ZDOT = 14043
969021 ZDOT = 4259
566402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8342486
67 X = -2542789
94
Y = -16334378
48 feet Y = -4978718
56 meter
Z = 12253177
54 Z = 3734768
51
XDOT = 19863
066077 XDOT = 6054
262540
YDOT = 378
533091 feet/sec YDOT = 115
376886 meter/sec
ZDOT = 13960
797392 ZDOT = 4255
251045
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 09282
63923984
00020000 00000-0 20000-3 0 9004
2 25544 51
6410 79
1788 0008354 182
4965 177
6159 15
74733075 23984
Satellite: ISS
Catalog Number: 25544
Epoch time: 09282
63923984 = yrday
fracday
Element set: 900
Inclination: 51
6410 deg
RA of node: 79
1788 deg
Eccentricity:
0008354
Arg of perigee: 182
4965 deg
Mean anomaly: 177
6159 deg
Mean motion: 15
74733075 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2398
Checksum: 330
Coasting Arc #2 (Orbit 2412)
---------------------------------------
Vector Time (GMT): 2009/283/14:00:34
905
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4076060
12 A = 6724757
12 meter
Y = 4009387
97 meter E =
0009662
Z = -3552072
71 I = 51
96454
XDOT = -1919
458957 Wp = 153
23234
YDOT = 5938
162602 meter/sec RA = 73
60597 deg
ZDOT = 4496
348308 TA = 164
70012
MA = 164
67089
Ha = 190
492 n
mi
Hp = 182
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13372900
66 X = 4048179
08
Y = 13154160
02 feet Y = 4054813
01 meter
Z = -11653781
85 Z = -3532338
62
XDOT = -6297
437522 XDOT = -2007
560619
YDOT = 19482
160767 feet/sec YDOT = 5916
205445 meter/sec
ZDOT = 14751
798912 ZDOT = 4486
809488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18753368
64 X = -5716026
76
Y = 1410551
50 feet Y = 429936
10 meter
Z = -11575773
77 Z = -3528295
84
XDOT = -10315
511163 XDOT = -3144
167802
YDOT = -16289
500297 feet/sec YDOT = -4965
039691 meter/sec
ZDOT = 14714
454554 ZDOT = 4484
965748
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 09283
59115196
00020000 00000-0 20000-3 0 9019
2 25544 51
6413 74
2858 0008130 186
2339 173
8724 15
74706730 24132
Satellite: ISS
Catalog Number: 25544
Epoch time: 09283
59115196 = yrday
fracday
Element set: 901
Inclination: 51
6413 deg
RA of node: 74
2858 deg
Eccentricity:
0008130
Arg of perigee: 186
2339 deg
Mean anomaly: 173
8724 deg
Mean motion: 15
74706730 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2413
Checksum: 293
Coasting Arc #3 (Orbit 2428)
---------------------------------------
Vector Time (GMT): 2009/284/14:00:34
905
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1440387
83 A = 6722763
77 meter
Y = -5124033
28 meter E =
0007975
Z = -4107847
16 I = 51
94896
XDOT = 4973
272015 Wp = 133
43541
YDOT = 4459
430559 meter/sec RA = 68
53821 deg
ZDOT = -3828
713345 TA = 97
44909
MA = 97
35846
Ha = 190
383 n
mi
Hp = 182
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4725681
84 X = 1517533
98
Y = -16811132
82 feet Y = -5107494
70 meter
Z = -13477188
84 Z = -4100662
26
XDOT = 16316
509234 XDOT = 4941
635644
YDOT = 14630
677687 feet/sec YDOT = 4514
867702 meter/sec
ZDOT = -12561
395490 ZDOT = -3804
629827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9706380
48 X = 2958504
77
Y = 14542667
58 feet Y = 4432605
08 meter
Z = -13449084
42 Z = -4099280
93
XDOT = -20699
928418 XDOT = -6309
338182
YDOT = 2317
518738 feet/sec YDOT = 706
379711 meter/sec
ZDOT = -12466
212277 ZDOT = -3799
701502
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 09284
60650761
00020000 00000-0 20000-3 0 9025
2 25544 51
6417 69
0657 0008177 190
2031 169
8968 15
74737095 24290
Satellite: ISS
Catalog Number: 25544
Epoch time: 09284
60650761 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 69
0657 deg
Eccentricity:
0008177
Arg of perigee: 190
2031 deg
Mean anomaly: 169
8968 deg
Mean motion: 15
74737095 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2429
Checksum: 317
Coasting Arc #4 (Orbit 2444)
---------------------------------------
Vector Time (GMT): 2009/285/14:00:34
905
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4616530
52 A = 6725835
88 meter
Y = -3743134
86 meter E =
0014377
Z = 3128583
85 I = 51
94728
XDOT = 1378
698349 Wp = 128
48439
YDOT = -5795
332836 meter/sec RA = 63
36920 deg
ZDOT = -4893
062869 TA = 15
24918
MA = 15
20589
Ha = 190
297 n
mi
Hp = 182
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15146097
49 X = -4589529
23
Y = -12280626
17 feet Y = -3794608
55 meter
Z = 10264382
72 Z = 3106222
28
XDOT = 4523
288548 XDOT = 1467
170094
YDOT = -19013
559173 feet/sec YDOT = -5779
420899 meter/sec
ZDOT = -16053
355871 ZDOT = -4886
150023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19137263
10 X = 5833037
79
Y = -3973581
23 feet Y = -1211147
56 meter
Z = 10176021
54 Z = 3101651
37
XDOT = 11487
379879 XDOT = 3501
353387
YDOT = 14229
497676 feet/sec YDOT = 4337
150892 meter/sec
ZDOT = -16026
350886 ZDOT = -4884
831750
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 09285
62184693
00020000 00000-0 20000-3 0 9035
2 25544 51
6418 63
8462 0008093 193
1171 166
9784 15
74756108 24459
Satellite: ISS
Catalog Number: 25544
Epoch time: 09285
62184693 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 63
8462 deg
Eccentricity:
0008093
Arg of perigee: 193
1171 deg
Mean anomaly: 166
9784 deg
Mean motion: 15
74756108 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2445
Checksum: 316
Coasting Arc #5 (Orbit 2460)
---------------------------------------
Vector Time (GMT): 2009/286/14:00:34
905
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1002303
48 A = 6721337
09 meter
Y = 4965400
17 meter E =
0012581
Z = 4418517
79 I = 51
91906
XDOT = -5600
732007 Wp = 150
09605
YDOT = -4105
055256 meter/sec RA = 58
29629 deg
ZDOT = 3327
949761 TA = 266
52978
MA = 266
67369
Ha = 189
894 n
mi
Hp = 182
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3288397
24 X = -1079217
49
Y = 16290682
96 feet Y = 4953762
02 meter
Z = 14496449
43 Z = 4413461
45
XDOT = -18375
105010 XDOT = -5570
579015
YDOT = -13468
029055 feet/sec YDOT = -4167
517156 meter/sec
ZDOT = 10918
470344 ZDOT = 3300
814668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10681034
08 X = -3255579
19
Y = -12754874
72 feet Y = -3887685
82 meter
Z = 14476727
39 Z = 4412506
51
XDOT = 21073
289497 XDOT = 6423
138639
YDOT = -5321
343799 feet/sec YDOT = -1621
945590 meter/sec
ZDOT = 10811
266378 ZDOT = 3295
273992
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 09286
63716657
00020000 00000-0 20000-3 0 9049
2 25544 51
6424 58
6255 0007986 197
8635 162
2249 15
74834070 24612
Satellite: ISS
Catalog Number: 25544
Epoch time: 09286
63716657 = yrday
fracday
Element set: 904
Inclination: 51
6424 deg
RA of node: 58
6255 deg
Eccentricity:
0007986
Arg of perigee: 197
8635 deg
Mean anomaly: 162
2249 deg
Mean motion: 15
74834070 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2461
Checksum: 323
Coasting Arc #6 (Orbit 2475)
---------------------------------------
Vector Time (GMT): 2009/287/14:00:34
905
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5159018
31 A = 6726884
82 meter
Y = 3406585
93 meter E =
0004334
Z = -2658648
56 I = 51
92067
XDOT = -965
794445 Wp = 165
79075
YDOT = 5552
679972 meter/sec RA = 53
12848 deg
ZDOT = 5238
365527 TA = 164
08446
MA = 164
07083
Ha = 189
692 n
mi
Hp = 183
121
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16925913
08 X = 5133457
22
Y = 11176463
03 feet Y = 3464133
99 meter
Z = -8722600
26 Z = -2633648
13
XDOT = -3168
616944 XDOT = -1053
261014
YDOT = 18217
453978 feet/sec YDOT = 5541
391249 meter/sec
ZDOT = 17186
238607 ZDOT = 5233
460752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19186701
35 X = -5848106
57
Y = 6706961
28 feet Y = 2044281
80 meter
Z = -8623849
30 Z = -2628549
27
XDOT = -12004
176601 XDOT = -3658
873028
YDOT = -12257
035684 feet/sec YDOT = -3735
944476 meter/sec
ZDOT = 17167
138019 ZDOT = 5232
543668
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 09287
58901595
00020000 00000-0 20000-3 0 9052
2 25544 51
6425 53
7319 0007772 202
6128 157
4694 15
74802669 24760
Satellite: ISS
Catalog Number: 25544
Epoch time: 09287
58901595 = yrday
fracday
Element set: 905
Inclination: 51
6425 deg
RA of node: 53
7319 deg
Eccentricity:
0007772
Arg of perigee: 202
6128 deg
Mean anomaly: 157
4694 deg
Mean motion: 15
74802669 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2476
Checksum: 324
Coasting Arc #7 (Orbit 2491)
---------------------------------------
Vector Time (GMT): 2009/288/14:00:34
905
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 728718
79 A = 6720106
24 meter
Y = -4731078
23 meter E =
0007969
Z = -4721260
14 I = 51
87931
XDOT = 6187
213217 Wp = 114
88602
YDOT = 3674
321484 meter/sec RA = 48
04837 deg
ZDOT = -2733
834260 TA = 128
31440
MA = 128
24272
Ha = 189
561 n
mi
Hp = 183
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2390809
67 X = 804503
77
Y = -15521910
19 feet Y = -4722505
94 meter
Z = -15489698
63 Z = -4717535
47
XDOT = 20299
255962 XDOT = 6158
947155
YDOT = 12054
860513 feet/sec YDOT = 3743
352267 meter/sec
ZDOT = -8969
272505 ZDOT = -2703
845276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11023634
38 X = 3360003
76
Y = 11205966
65 feet Y = 3415578
63 meter
Z = -15475213
30 Z = -4716845
01
XDOT = -20960
528842 XDOT = -6388
769191
YDOT = 8427
748723 feet/sec YDOT = 2568
777811 meter/sec
ZDOT = -8850
841404 ZDOT = -2697
736460
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 09288
60430434
00020000 00000-0 20000-3 0 9066
2 25544 51
6425 48
5117 0007837 206
1927 153
8841 15
74839725 24921
Satellite: ISS
Catalog Number: 25544
Epoch time: 09288
60430434 = yrday
fracday
Element set: 906
Inclination: 51
6425 deg
RA of node: 48
5117 deg
Eccentricity:
0007837
Arg of perigee: 206
1927 deg
Mean anomaly: 153
8841 deg
Mean motion: 15
74839725 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2492
Checksum: 309
Coasting Arc #8 (Orbit 2507)
---------------------------------------
Vector Time (GMT): 2009/289/14:00:34
905
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5639899
71 A = 6727819
10 meter
Y = -2978403
18 meter E =
0014993
Z = 2110403
25 I = 51
88441
XDOT = 710
772761 Wp = 140
47474
YDOT = -5292
194142 meter/sec RA = 42
88424 deg
ZDOT = -5559
241254 TA = 15
99244
MA = 15
94516
Ha = 189
398 n
mi
Hp = 183
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18503607
96 X = -5616427
69
Y = -9771663
98 feet Y = -3041340
45 meter
Z = 6923895
18 Z = 2083061
29
XDOT = 2331
931630 XDOT = 796
904552
YDOT = -17362
841672 feet/sec YDOT = -5283
764741 meter/sec
ZDOT = -18238
980491 ZDOT = -5555
578580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18707503
88 X = 5702047
18
Y = -9454178
47 feet Y = -2881633
60 meter
Z = 6815941
38 Z = 2077498
93
XDOT = 12050
749662 XDOT = 3673
068497
YDOT = 10682
117312 feet/sec YDOT = 3255
909357 meter/sec
ZDOT = -18224
758551 ZDOT = -5554
906406
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 09289
61957598
00020000 00000-0 20000-3 0 9074
2 25544 51
6425 43
2917 0007647 209
2274 150
8463 15
74873240 25084
Satellite: ISS
Catalog Number: 25544
Epoch time: 09289
61957598 = yrday
fracday
Element set: 907
Inclination: 51
6425 deg
RA of node: 43
2917 deg
Eccentricity:
0007647
Arg of perigee: 209
2274 deg
Mean anomaly: 150
8463 deg
Mean motion: 15
74873240 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2508
Checksum: 320
Coasting Arc #9 (Orbit 2523)
---------------------------------------
Vector Time (GMT): 2009/290/14:00:34
905
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -551552
89 A = 6718847
72 meter
Y = 4503547
65 meter E =
0009718
Z = 4957844
66 I = 51
83279
XDOT = -6717
413603 Wp = 175
33042
YDOT = -3132
238153 meter/sec RA = 37
79271 deg
ZDOT = 2088
148184 TA = 254
43925
MA = 254
54655
Ha = 189
033 n
mi
Hp = 183
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1809556
72 X = -625956
31
Y = 14775418
80 feet Y = 4496964
20 meter
Z = 16265894
54 Z = 4954984
09
XDOT = -22038
758539 XDOT = -6692
033233
YDOT = -10276
371894 feet/sec YDOT = -3207
214176 meter/sec
ZDOT = 6850
879868 ZDOT = 2055
575986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11112732
77 X = -3387160
95
Y = -9922478
34 feet Y = -3024371
40 meter
Z = 16254796
69 Z = 4954462
03
XDOT = 20232
742074 XDOT = 6166
939784
YDOT = -11594
861830 feet/sec YDOT = -3534
113886 meter/sec
ZDOT = 6722
302795 ZDOT = 2048
957892
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 09290
63482824
00020000 00000-0 20000-3 0 9084
2 25544 51
6432 38
0708 0007640 214
4157 145
6513 15
74930600 25243
Satellite: ISS
Catalog Number: 25544
Epoch time: 09290
63482824 = yrday
fracday
Element set: 908
Inclination: 51
6432 deg
RA of node: 38
0708 deg
Eccentricity:
0007640
Arg of perigee: 214
4157 deg
Mean anomaly: 145
6513 deg
Mean motion: 15
74930600 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2524
Checksum: 279
Coasting Arc #10 (Orbit 2538)
---------------------------------------
Vector Time (GMT): 2009/291/14:00:34
905
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6070575
98 A = 6728663
78 meter
Y = 2474274
31 meter E =
0001051
Z = -1514459
42 I = 51
84070
XDOT = -602
126424 Wp = 22
31817
YDOT = 5025
503598 meter/sec RA = 32
63404 deg
ZDOT = 5799
193204 TA = 321
04696
MA = 321
05454
Ha = 188
817 n
mi
Hp = 183
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19916587
86 X = 6049814
22
Y = 8117697
87 feet Y = 2542042
91 meter
Z = -4968698
89 Z = -1485018
24
XDOT = -1975
480393 XDOT = -686
450005
YDOT = 16487
872698 feet/sec YDOT = 5018
299078 meter/sec
ZDOT = 19026
224421 ZDOT = 5796
062906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17763110
15 X = -5414195
97
Y = 12172944
86 feet Y = 3710313
59 meter
Z = -4852503
52 Z = -1479043
07
XDOT = -11722
980966 XDOT = -3573
164598
YDOT = -9529
951285 feet/sec YDOT = -2904
729152 meter/sec
ZDOT = 19014
075946 ZDOT = 5795
490348
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 09291
58661379
00020000 00000-0 20000-3 0 9094
2 25544 51
6429 33
1772 0007399 219
2559 140
8068 15
74898115 25398
Satellite: ISS
Catalog Number: 25544
Epoch time: 09291
58661379 = yrday
fracday
Element set: 909
Inclination: 51
6429 deg
RA of node: 33
1772 deg
Eccentricity:
0007399
Arg of perigee: 219
2559 deg
Mean anomaly: 140
8068 deg
Mean motion: 15
74898115 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2539
Checksum: 334
Coasting Arc #11 (Orbit 2554)
---------------------------------------
Vector Time (GMT): 2009/292/14:00:34
905
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 539754
64 A = 6717987
44 meter
Y = -4290613
21 meter E =
0009423
Z = -5148156
47 I = 51
77876
XDOT = 7144
895808 Wp = 108
14292
YDOT = 2519
852994 meter/sec RA = 27
52901 deg
ZDOT = -1355
905027 TA = 148
92676
MA = 148
87100
Ha = 188
651 n
mi
Hp = 183
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1770848
55 X = 612702
49
Y = -14076815
01 feet Y = -4284169
63 meter
Z = -16890277
14 Z = -5145356
95
XDOT = 23441
259212 XDOT = 7122
774288
YDOT = 8267
234231 feet/sec YDOT = 2599
627704 meter/sec
ZDOT = -4448
507307 ZDOT = -1321
247858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10876740
88 X = 3315230
62
Y = 9129980
31 feet Y = 2782818
00 meter
Z = -16879397
34 Z = -5144840
31
XDOT = -18900
850609 XDOT = -5760
979266
YDOT = 14575
175310 feet/sec YDOT = 4442
513435 meter/sec
ZDOT = -4311
747839 ZDOT = -1314
220741
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 09292
60183457
00020000 00000-0 20000-3 0 9106
2 25544 51
6423 27
9566 0007416 222
6138 137
4451 15
74940459 25550
Satellite: ISS
Catalog Number: 25544
Epoch time: 09292
60183457 = yrday
fracday
Element set: 910
Inclination: 51
6423 deg
RA of node: 27
9566 deg
Eccentricity:
0007416
Arg of perigee: 222
6138 deg
Mean anomaly: 137
4451 deg
Mean motion: 15
74940459 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2555
Checksum: 298
Coasting Arc #12 (Orbit 2570)
---------------------------------------
Vector Time (GMT): 2009/293/14:00:34
905
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6387294
29 A = 6729045
62 meter
Y = -1907757
44 meter E =
0014148
Z = 848066
73 I = 51
78983
XDOT = 644
034816 Wp = 155
91178
YDOT = -4822
994907 meter/sec RA = 22
37760 deg
ZDOT = -5976
790607 TA = 14
84559
MA = 14
80409
Ha = 188
338 n
mi
Hp = 183
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20955689
94 X = -6369606
57
Y = -6259046
72 feet Y = -1979085
03 meter
Z = 2782371
16 Z = 817079
31
XDOT = 2112
975119 XDOT = 726
953545
YDOT = -15823
474104 feet/sec YDOT = -4815
329343 meter/sec
ZDOT = -19608
893068 ZDOT = -5973
460349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16284117
90 X = 4963399
14
Y = -14622226
95 feet Y = -4456854
78 meter
Z = 2660108
84 Z = 810801
18
XDOT = 11269
023930 XDOT = 3434
798494
YDOT = 8971
069010 feet/sec YDOT = 2734
381834 meter/sec
ZDOT = -19595
932580 ZDOT = -5972
840250
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 09293
61703757
00020000 00000-0 20000-3 0 9110
2 25544 51
6428 22
7361 0007161 226
7661 133
2905 15
75002860 25716
Satellite: ISS
Catalog Number: 25544
Epoch time: 09293
61703757 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 22
7361 deg
Eccentricity:
0007161
Arg of perigee: 226
7661 deg
Mean anomaly: 133
2905 deg
Mean motion: 15
75002860 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2571
Checksum: 278
Coasting Arc #13 (Orbit 2586)
---------------------------------------
Vector Time (GMT): 2009/294/14:00:34
905
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -612362
87 A = 6717266
11 meter
Y = 4148459
32 meter E =
0006397
Z = 5250582
39 I = 51
72201
XDOT = -7455
500201 Wp = 207
76213
YDOT = -1838
431743 meter/sec RA = 17
25590 deg
ZDOT = 577
746384 TA = 236
72287
MA = 236
78417
Ha = 188
091 n
mi
Hp = 184
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2009064
53 X = -684213
21
Y = 13610430
85 feet Y = 4141209
73 meter
Z = 17226320
18 Z = 5247432
97
XDOT = -24460
302497 XDOT = -7437
195085
YDOT = -6031
600207 feet/sec YDOT = -1921
701196 meter/sec
ZDOT = 1895
493385 ZDOT = 541
571038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10660601
21 X = -3249351
25
Y = -8720926
97 feet Y = -2658138
54 meter
Z = 17214043
39 Z = 5246840
43
XDOT = 16972
961097 XDOT = 5173
358542
YDOT = -17254
085541 feet/sec YDOT = -5259
045273 meter/sec
ZDOT = 1752
776706 ZDOT = 534
246340
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 09294
63222280
00020000 00000-0 20000-3 0 9121
2 25544 51
6426 17
5152 0007203 230
9642 129
0881 15
75028277 25870
Satellite: ISS
Catalog Number: 25544
Epoch time: 09294
63222280 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 17
5152 deg
Eccentricity:
0007203
Arg of perigee: 230
9642 deg
Mean anomaly: 129
0881 deg
Mean motion: 15
75028277 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2587
Checksum: 283
Coasting Arc #14 (Orbit 2601)
---------------------------------------
Vector Time (GMT): 2009/295/14:00:34
905
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6597971
81 A = 6729334
47 meter
Y = 1298874
25 meter E =
0005478
Z = -145175
05 I = 51
73296
XDOT = -795
434730 Wp = 29
34865
YDOT = 4704
850150 meter/sec RA = 12
11259 deg
ZDOT = 6043
233536 TA = 329
07607
MA = 329
10832
Ha = 187
850 n
mi
Hp = 184
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21646889
13 X = 6583662
44
Y = 4261398
46 feet Y = 1372576
65 meter
Z = -476296
10 Z = -113156
09
XDOT = -2609
693995 XDOT = -877
343679
YDOT = 15435
860072 feet/sec YDOT = 4695
497028 meter/sec
ZDOT = 19826
881680 ZDOT = 6039
170361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14366307
99 X = -4378850
68
Y = 16746966
51 feet Y = 5104475
39 meter
Z = -349987
48 Z = -106676
18
XDOT = -10873
684872 XDOT = -3314
299149
YDOT = -8923
285957 feet/sec YDOT = -2719
817560 meter/sec
ZDOT = 19811
016122 ZDOT = 6038
397714
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 09295
58394467
00020000 00000-0 20000-3 0 9134
2 25544 51
6422 12
6201 0006893 235
9126 124
1384 15
74995628 26027
Satellite: ISS
Catalog Number: 25544
Epoch time: 09295
58394467 = yrday
fracday
Element set: 913
Inclination: 51
6422 deg
RA of node: 12
6201 deg
Eccentricity:
0006893
Arg of perigee: 235
9126 deg
Mean anomaly: 124
1384 deg
Mean motion: 15
74995628 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2602
Checksum: 303
Coasting Arc #15 (Orbit 2617)
---------------------------------------
Vector Time (GMT): 2009/296/14:00:34
905
Vector Time (MET): N/A
Weight (LBS) : 745632
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 798123
47 A = 6717144
94 meter
Y = -4099797
46 meter E =
0009962
Z = -5268589
24 I = 51
66332
XDOT = 7606
900488 Wp = 114
57763
YDOT = 1139
134067 meter/sec RA = 6
97181 deg
ZDOT = 262
241717 TA = 157
93361
MA = 157
89069
Ha = 187
667 n
mi
Hp = 184
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2618515
34 X = 869503
16
Y = -13450779
06 feet Y = -4090473
15 meter
Z = -17285397
76 Z = -5264538
58
XDOT = 24957
022599 XDOT = 7592
323178
YDOT = 3737
316492 feet/sec YDOT = 1224
117398 meter/sec
ZDOT = 860
373086 ZDOT = 299
161380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10522974
70 X = 3207402
69
Y = 8808767
72 feet Y = 2684912
40 meter
Z = -17269559
07 Z = -5263761
61
XDOT = -14549
106429 XDOT = -4434
567640
YDOT = 19376
348821 feet/sec YDOT = 5905
911121 meter/sec
ZDOT = 1006
003696 ZDOT = 306
629926
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 09296
59909755
00020000 00000-0 20000-3 0 9149
2 25544 51
6428 7
3986 0006969 239
0985 120
9494 15
75047826 26188
Satellite: ISS
Catalog Number: 25544
Epoch time: 09296
59909755 = yrday
fracday
Element set: 914
Inclination: 51
6428 deg
RA of node: 7
3986 deg
Eccentricity:
0006969
Arg of perigee: 239
0985 deg
Mean anomaly: 120
9494 deg
Mean motion: 15
75047826 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2618
Checksum: 349
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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