Date:
July 29th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8880 23 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 2996)
---------------------------------------
Vector Time (GMT): 2010/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6516113
77 A = 6739113
74 meter
Y = 1075697
33 meter E =
0008112
Z = -1348545
43 I = 51
76930
XDOT = 379
902553 Wp = 90
86388
YDOT = 4984
838824 meter/sec RA = 18
63083 deg
ZDOT = 5841
971976 TA = 254
38104
MA = 254
47058
Ha = 196
328 n
mi
Hp = 186
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21378326
01 X = 6510151
69
Y = 3529190
72 feet Y = 1148531
16 meter
Z = -4424361
65 Z = -1316905
21
XDOT = 1246
399451 XDOT = 295
754282
YDOT = 16354
458084 feet/sec YDOT = 4988
616247 meter/sec
ZDOT = 19166
574723 ZDOT = 5843
613434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9477785
26 X = -2888828
95
Y = -19513152
93 feet Y = -5947609
01 meter
Z = -4297840
79 Z = -1309981
87
XDOT = 11276
028065 XDOT = 3436
933354
YDOT = -9677
510145 feet/sec YDOT = -2949
705092 meter/sec
ZDOT = 19173
089367 ZDOT = 5843
957639
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
50254265
00016717 00000-0 10270-3 0 9008
2 25544 51
6420 19
1528 0007751 159
6876 200
4595 15
71301570 29970
Satellite: ISS
Catalog Number: 25544
Epoch time: 10209
50254265 = yrday
fracday
Element set: 900
Inclination: 51
6420 deg
RA of node: 19
1528 deg
Eccentricity:
0007751
Arg of perigee: 159
6876 deg
Mean anomaly: 200
4595 deg
Mean motion: 15
71301570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2997
Checksum: 302
Coasting Arc #2 (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 = -1774311
45 A = 6729662
15 meter
Y = -4349633
23 meter E =
0014282
Z = -4829241
59 I = 51
70945
XDOT = 7278
280118 Wp = 104
82108
YDOT = -245
294757 meter/sec RA = 13
55506 deg
ZDOT = -2462
799354 TA = 141
14064
MA = 141
03787
Ha = 196
197 n
mi
Hp = 186
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5821231
80 X = -1702082
01
Y = -14270450
24 feet Y = -4369070
55 meter
Z = -15843968
46 Z = -4837685
82
XDOT = 23878
871778 XDOT = 7292
445737
YDOT = -804
772825 feet/sec YDOT = -163
825349 meter/sec
ZDOT = -8080
050375 ZDOT = -2427
407688
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8121069
96 X = -2475302
12
Y = 13057981
64 feet Y = 3980072
80 meter
Z = -15877693
94 Z = -4839521
11
XDOT = -13846
353559 XDOT = -4220
368565
YDOT = -18225
826072 feet/sec YDOT = -5555
231787 meter/sec
ZDOT = -7938
519472 ZDOT = -2419
660735
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
52011815
00016717 00000-0 10270-3 0 9015
2 25544 51
6427 13
9486 0007709 162
3543 197
7888 15
71326345 30137
Satellite: ISS
Catalog Number: 25544
Epoch time: 10210
52011815 = yrday
fracday
Element set: 901
Inclination: 51
6427 deg
RA of node: 13
9486 deg
Eccentricity:
0007709
Arg of perigee: 162
3543 deg
Mean anomaly: 197
7888 deg
Mean motion: 15
71326345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3013
Checksum: 296
Coasting Arc #3 (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 = -5881744
62 A = 6736240
36 meter
Y = 1459490
95 meter E =
0017719
Z = 2916437
15 I = 51
70098
XDOT = -3635
167120 Wp = 121
99076
YDOT = -4558
045636 meter/sec RA = 8
40128 deg
ZDOT = -5037
219711 TA = 24
46598
MA = 24
38199
Ha = 196
200 n
mi
Hp = 186
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19297062
39 X = -5911795
10
Y = 4788356
13 feet Y = 1393549
62 meter
Z = 9568363
34 Z = 2887791
09
XDOT = -11926
401311 XDOT = -3559
458478
YDOT = -14954
217967 feet/sec YDOT = -4598
272726 meter/sec
ZDOT = -16526
311388 ZDOT = -5054
695412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15524118
05 X = 4731751
18
Y = 12509434
54 feet Y = 3812875
65 meter
Z = 9453801
07 Z = 2881518
56
XDOT = -3835
340678 XDOT = -1169
011839
YDOT = 17334
564542 feet/sec YDOT = 5283
575272 meter/sec
ZDOT = -16596
148045 ZDOT = -5058
505924
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
53768462
00016717 00000-0 10270-3 0 9025
2 25544 51
6422 8
7430 0007710 167
4197 192
7159 15
71310320 30295
Satellite: ISS
Catalog Number: 25544
Epoch time: 10211
53768462 = yrday
fracday
Element set: 902
Inclination: 51
6422 deg
RA of node: 8
7430 deg
Eccentricity:
0007710
Arg of perigee: 167
4197 deg
Mean anomaly: 192
7159 deg
Mean motion: 15
71310320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3029
Checksum: 284
Coasting Arc #4 (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 = 4419500
56 A = 6733190
74 meter
Y = 3308687
31 meter E =
0015535
Z = 3851289
51 I = 51
66224
XDOT = -5802
149592 Wp = 127
10210
YDOT = 2927
361394 meter/sec RA = 3
33869 deg
ZDOT = 4122
665932 TA = 279
73611
MA = 279
91153
Ha = 195
907 n
mi
Hp = 186
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14499673
74 X = 4363465
06
Y = 10855273
34 feet Y = 3357795
34 meter
Z = 12635464
26 Z = 3872623
26
XDOT = -19035
923857 XDOT = -5854
479622
YDOT = 9604
204047 feet/sec YDOT = 2862
185523 meter/sec
ZDOT = 13525
806862 ZDOT = 4094
352376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -397417
09 X = -121132
73
Y = -18048750
29 feet Y = -5501259
09 meter
Z = 12720736
13 Z = 3877280
37
XDOT = 18057
107948 XDOT = 5503
806503
YDOT = 9102
850259 feet/sec YDOT = 2774
548759 meter/sec
ZDOT = 13412
564880 ZDOT = 4088
149775
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
55524169
00016717 00000-0 10270-3 0 9033
2 25544 51
6430 3
5383 0007738 171
3522 188
7775 15
71359169 30451
Satellite: ISS
Catalog Number: 25544
Epoch time: 10212
55524169 = yrday
fracday
Element set: 903
Inclination: 51
6430 deg
RA of node: 3
5383 deg
Eccentricity:
0007738
Arg of perigee: 171
3522 deg
Mean anomaly: 188
7775 deg
Mean motion: 15
71359169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3045
Checksum: 308
Coasting Arc #5 (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 = 4010554
86 A = 6732257
00 meter
Y = -3442258
01 meter E =
0013189
Z = -4184015
30 I = 51
62949
XDOT = 6175
097768 Wp = 141
00469
YDOT = 2717
752384 meter/sec RA = 358
17383 deg
ZDOT = 3679
377107 TA = 166
65207
MA = 166
61715
Ha = 195
878 n
mi
Hp = 187
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13157988
39 X = 4069073
80
Y = -11293497
41 feet Y = -3397082
19 meter
Z = -13727084
32 Z = -4164390
17
XDOT = 20259
507112 XDOT = 6126
374782
YDOT = 8916
510446 feet/sec YDOT = 2786
533419 meter/sec
ZDOT = 12071
447202 ZDOT = 3709
257324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17120247
58 X = -5218251
46
Y = -3118003
69 feet Y = -950367
52 meter
Z = -13648580
95 Z = -4160087
47
XDOT = -6080
709696 XDOT = -1853
400315
YDOT = -20030
485295 feet/sec YDOT = -6105
291918 meter/sec
ZDOT = 12190
892595 ZDOT = 3715
784063
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
50919489
00016717 00000-0 10270-3 0 9043
2 25544 51
6441 358
6595 0007670 174
1104 186
0150 15
71346623 30600
Satellite: ISS
Catalog Number: 25544
Epoch time: 10213
50919489 = yrday
fracday
Element set: 904
Inclination: 51
6441 deg
RA of node: 358
6595 deg
Eccentricity:
0007670
Arg of perigee: 174
1104 deg
Mean anomaly: 186
0150 deg
Mean motion: 15
71346623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3060
Checksum: 297
Coasting Arc #6 (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 = -6114171
14 A = 6736845
84 meter
Y = -1267695
63 meter E =
0011658
Z = -2515463
39 I = 51
61507
XDOT = 3132
189428 Wp = 157
99540
YDOT = -4613
299231 meter/sec RA = 353
10384 deg
ZDOT = -5306
794511 TA = 50
47485
MA = 50
37187
Ha = 195
629 n
mi
Hp = 187
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20059616
60 X = -6087321
50
Y = -4159106
41 feet Y = -1335917
68 meter
Z = -8252832
65 Z = -2545100
77
XDOT = 10276
212035 XDOT = 3209
322730
YDOT = -15135
496166 feet/sec YDOT = -4577
841622 meter/sec
ZDOT = -17410
743147 ZDOT = -5291
391319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9738019
52 X = 2968148
35
Y = 17969074
85 feet Y = 5476974
01 meter
Z = -8371317
45 Z = -2551577
56
XDOT = -16949
907476 XDOT = -5166
331799
YDOT = 1131
101307 feet/sec YDOT = 344
759678 meter/sec
ZDOT = -17349
109246 ZDOT = -5288
008498
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
52673505
00016717 00000-0 10270-3 0 9053
2 25544 51
6439 353
4544 0007593 178
1416 181
9766 15
71369601 30763
Satellite: ISS
Catalog Number: 25544
Epoch time: 10214
52673505 = yrday
fracday
Element set: 905
Inclination: 51
6439 deg
RA of node: 353
4544 deg
Eccentricity:
0007593
Arg of perigee: 178
1416 deg
Mean anomaly: 181
9766 deg
Mean motion: 15
71369601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3076
Checksum: 320
Coasting Arc #7 (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 = -1322709
43 A = 6729012
82 meter
Y = 4323254
72 meter E =
0006416
Z = 4978522
94 I = 51
55880
XDOT = -7444
497362 Wp = 131
13838
YDOT = -10
479641 meter/sec RA = 347
94741 deg
ZDOT = -1971
283858 TA = 337
92325
MA = 337
95087
Ha = 195
679 n
mi
Hp = 187
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4339597
86 X = -1395139
22
Y = 14183906
55 feet Y = 4308058
03 meter
Z = 16333736
67 Z = 4971921
64
XDOT = -24424
203942 XDOT = -7434
250777
YDOT = -34
382024 feet/sec YDOT = -93
671020 meter/sec
ZDOT = -6467
466727 ZDOT = -2007
424212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13596498
05 X = 4144212
61
Y = -6001131
00 feet Y = -1829144
73 meter
Z = 16307297
02 Z = 4970464
13
XDOT = 15593
251658 XDOT = 4752
823105
YDOT = 17384
177102 feet/sec YDOT = 5298
697181 meter/sec
ZDOT = -6611
962626 ZDOT = -2015
326208
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
54426839
00016717 00000-0 10270-3 0 9063
2 25544 51
6444 348
2500 0007585 181
1250 178
9896 15
71343549 30925
Satellite: ISS
Catalog Number: 25544
Epoch time: 10215
54426839 = yrday
fracday
Element set: 906
Inclination: 51
6444 deg
RA of node: 348
2500 deg
Eccentricity:
0007585
Arg of perigee: 181
1250 deg
Mean anomaly: 178
9896 deg
Mean motion: 15
71343549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3092
Checksum: 322
Coasting Arc #8 (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 = 6554450
82 A = 6739193
01 meter
Y = -1276112
99 meter E =
0010474
Z = 898718
08 I = 51
56537
XDOT = 129
990087 Wp = 87
88706
YDOT = 4890
130543 meter/sec RA = 342
85144 deg
ZDOT = 5936
504210 TA = 281
91723
MA = 282
03464
Ha = 195
430 n
mi
Hp = 187
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21504103
73 X = 6563867
62
Y = -4186722
40 feet Y = -1202764
63 meter
Z = 2948550
15 Z = 930582
21
XDOT = 426
476662 XDOT = 46
459769
YDOT = 16043
735376 feet/sec YDOT = 4891
116576 meter/sec
ZDOT = 19476
719850 ZDOT = 5936
933259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17526971
96 X = -5342221
05
Y = -13114601
60 feet Y = -3997330
57 meter
Z = 3075963
04 Z = 937553
54
XDOT = 10726
507000 XDOT = 3269
439334
YDOT = -9723
270816 feet/sec YDOT = -2963
652945 meter/sec
ZDOT = 19478
381513 ZDOT = 5937
010685
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
56178918
00016717 00000-0 10270-3 0 9079
2 25544 51
6453 343
0452 0007540 185
6751 174
4326 15
71404114 31083
Satellite: ISS
Catalog Number: 25544
Epoch time: 10216
56178918 = yrday
fracday
Element set: 907
Inclination: 51
6453 deg
RA of node: 343
0452 deg
Eccentricity:
0007540
Arg of perigee: 185
6751 deg
Mean anomaly: 174
4326 deg
Mean motion: 15
71404114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3108
Checksum: 296
Coasting Arc #9 (Orbit 3122)
---------------------------------------
Vector Time (GMT): 2010/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1496796
08 A = 6727457
31 meter
Y = -3918621
57 meter E =
0015736
Z = -5271540
75 I = 51
49749
XDOT = 7137
823361 Wp = 118
29976
YDOT = -2851
102041 meter/sec RA = 337
71922 deg
ZDOT = 85
537640 TA = 152
55661
MA = 152
47341
Ha = 195
219 n
mi
Hp = 187
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4910748
30 X = -1427258
10
Y = -12856369
98 feet Y = -3934970
27 meter
Z = -17295081
20 Z = -5278643
64
XDOT = 23418
055646 XDOT = 7168
758882
YDOT = -9354
009320 feet/sec YDOT = -2771
109672 meter/sec
ZDOT = 280
635302 ZDOT = 120
287756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6090738
55 X = -1856457
11
Y = 12301339
34 feet Y = 3749448
23 meter
Z = -17323437
47 Z = -5280183
74
XDOT = -21942
487771 XDOT = -6688
070273
YDOT = -10240
519835 feet/sec YDOT = -3121
310446 meter/sec
ZDOT = 419
606633 ZDOT = 127
896102
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 10217
51570882
00016717 00000-0 10270-3 0 9082
2 25544 51
6454 338
1665 0007393 189
5722 170
5300 15
71425065 31236
Satellite: ISS
Catalog Number: 25544
Epoch time: 10217
51570882 = yrday
fracday
Element set: 908
Inclination: 51
6454 deg
RA of node: 338
1665 deg
Eccentricity:
0007393
Arg of perigee: 189
5722 deg
Mean anomaly: 170
5300 deg
Mean motion: 15
71425065 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3123
Checksum: 302
Coasting Arc #10 (Orbit 3138)
---------------------------------------
Vector Time (GMT): 2010/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5634666
80 A = 6739330
60 meter
Y = 3598580
54 meter E =
0017768
Z = 754981
09 I = 51
50999
XDOT = -3169
172308 Wp = 149
53391
YDOT = -3700
840956 meter/sec RA = 332
58728 deg
ZDOT = -5966
615392 TA = 22
22373
MA = 22
14681
Ha = 195
121 n
mi
Hp = 187
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18486439
62 X = -5678155
52
Y = 11806366
61 feet Y = 3535327
09 meter
Z = 2476972
09 Z = 727502
99
XDOT = -10397
546942 XDOT = -3098
568909
YDOT = -12141
866655 feet/sec YDOT = -3735
885099 meter/sec
ZDOT = -19575
509815 ZDOT = -5981
839966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21356937
60 X = 6509594
58
Y = 5054933
03 feet Y = 1540743
59 meter
Z = 2367065
97 Z = 721481
71
XDOT = -1185
350720 XDOT = -361
294899
YDOT = 14277
199512 feet/sec YDOT = 4351
690411 meter/sec
ZDOT = -19636
344463 ZDOT = -5985
157792
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 10218
53321460
00016717 00000-0 10270-3 0 9092
2 25544 51
6456 332
9611 0007446 193
6726 166
4235 15
71412878 31396
Satellite: ISS
Catalog Number: 25544
Epoch time: 10218
53321460 = yrday
fracday
Element set: 909
Inclination: 51
6456 deg
RA of node: 332
9611 deg
Eccentricity:
0007446
Arg of perigee: 193
6726 deg
Mean anomaly: 166
4235 deg
Mean motion: 15
71412878 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3139
Checksum: 312
Coasting Arc #11 (Orbit 3154)
---------------------------------------
Vector Time (GMT): 2010/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3852425
73 A = 6728364
79 meter
Y = 2288407
10 meter E =
0010291
Z = 5020088
82 I = 51
44828
XDOT = -5421
943077 Wp = 167
77085
YDOT = 5157
095545 meter/sec RA = 327
48205 deg
ZDOT = 1799
375050 TA = 264
77519
MA = 264
89263
Ha = 194
794 n
mi
Hp = 187
945
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12639192
01 X = 3802163
77
Y = 7507897
32 feet Y = 2331205
67 meter
Z = 16470107
69 Z = 5038681
74
XDOT = -17788
527156 XDOT = -5487
948576
YDOT = 16919
604806 feet/sec YDOT = 5096
094888 meter/sec
ZDOT = 5903
461449 ZDOT = 1772
875937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3589803
16 X = -1094172
00
Y = -14169590
19 feet Y = -4318891
09 meter
Z = 16544430
22 Z = 5042742
33
XDOT = 23535
064409 XDOT = 7173
487632
YDOT = 846
928604 feet/sec YDOT = 258
143838 meter/sec
ZDOT = 5797
453857 ZDOT = 1767
063936
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 10219
55070986
00016717 00000-0 10270-3 0 9101
2 25544 51
6465 327
7563 0007346 198
1419 161
9482 15
71467617 31555
Satellite: ISS
Catalog Number: 25544
Epoch time: 10219
55070986 = yrday
fracday
Element set: 910
Inclination: 51
6465 deg
RA of node: 327
7563 deg
Eccentricity:
0007346
Arg of perigee: 198
1419 deg
Mean anomaly: 161
9482 deg
Mean motion: 15
71467617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3155
Checksum: 330
Coasting Arc #12 (Orbit 3169)
---------------------------------------
Vector Time (GMT): 2010/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3639647
56 A = 6737196
89 meter
Y = -5166686
31 meter E =
0002833
Z = -2339622
53 I = 51
45268
XDOT = 5326
149311 Wp = 150
86546
YDOT = 1311
796888 meter/sec RA = 322
31817 deg
ZDOT = 5389
064192 TA = 182
78157
MA = 182
78315
Ha = 194
744 n
mi
Hp = 188
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11941100
90 X = 3708517
09
Y = -16951070
57 feet Y = -5125600
32 meter
Z = -7675926
94 Z = -2321774
69
XDOT = 17474
243146 XDOT = 5284
906197
YDOT = 4303
795564 feet/sec YDOT = 1371
126005 meter/sec
ZDOT = 17680
656799 ZDOT = 5414
837984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20390127
25 X = -6214910
79
Y = 3906734
97 feet Y = 1190772
82 meter
Z = -7604516
49 Z = -2317856
63
XDOT = -9248
690870 XDOT = -2819
000977
YDOT = -13656
713544 feet/sec YDOT = -4162
566288 meter/sec
ZDOT = 17783
707220 ZDOT = 5420
473961
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 10220
50460613
00016717 00000-0 10270-3 0 9119
2 25544 51
6466 322
8773 0007135 202
3950 157
6901 15
71419937 31706
Satellite: ISS
Catalog Number: 25544
Epoch time: 10220
50460613 = yrday
fracday
Element set: 911
Inclination: 51
6466 deg
RA of node: 322
8773 deg
Eccentricity:
0007135
Arg of perigee: 202
3950 deg
Mean anomaly: 157
6901 deg
Mean motion: 15
71419937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3170
Checksum: 289
Coasting Arc #13 (Orbit 3185)
---------------------------------------
Vector Time (GMT): 2010/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5178556
93 A = 6731316
08 meter
Y = 114342
49 meter E =
0006174
Z = -4301250
23 I = 51
41004
XDOT = 2735
329701 Wp = 123
11274
YDOT = -6299
404364 meter/sec RA = 317
23280 deg
ZDOT = -3467
612429 TA = 111
70513
MA = 111
63939
Ha = 194
517 n
mi
Hp = 188
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16990016
16 X = -5158556
47
Y = 375139
40 feet Y = 56544
84 meter
Z = -14111713
37 Z = -4326358
45
XDOT = 8974
178808 XDOT = 2822
412108
YDOT = -20667
337152 feet/sec YDOT = -6268
329171 meter/sec
ZDOT = -11376
681196 ZDOT = -3454
113368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12638795
32 X = 3852304
81
Y = 11234697
99 feet Y = 3424335
95 meter
Z = -14212116
20 Z = -4331853
02
XDOT = -19873
487666 XDOT = -6057
439041
YDOT = 8062
331633 feet/sec YDOT = 2457
398682 meter/sec
ZDOT = -11322
660776 ZDOT = -3451
147004
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 10221
52208609
00016717 00000-0 10270-3 0 9128
2 25544 51
6465 317
6729 0007254 205
8198 154
2602 15
71447118 31862
Satellite: ISS
Catalog Number: 25544
Epoch time: 10221
52208609 = yrday
fracday
Element set: 912
Inclination: 51
6465 deg
RA of node: 317
6729 deg
Eccentricity:
0007254
Arg of perigee: 205
8198 deg
Mean anomaly: 154
2602 deg
Mean motion: 15
71447118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3186
Checksum: 304
Coasting Arc #14 (Orbit 3201)
---------------------------------------
Vector Time (GMT): 2010/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1062265
70 A = 6733589
46 meter
Y = 5542441
95 meter E =
0009896
Z = 3661620
69 I = 51
39600
XDOT = -6153
257976 Wp = 120
96690
YDOT = 1675
330307 meter/sec RA = 312
05045 deg
ZDOT = -4317
393796 TA = 14
88559
MA = 14
85648
Ha = 194
405 n
mi
Hp = 188
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3485123
70 X = -1141950
41
Y = 18183864
67 feet Y = 5530117
43 meter
Z = 12013191
26 Z = 3656266
92
XDOT = -20187
854253 XDOT = -6150
561900
YDOT = 5496
490509 feet/sec YDOT = 1606
536074 meter/sec
ZDOT = -14164
677810 ZDOT = -4347
279001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14794491
51 X = 4509361
01
Y = -11155113
70 feet Y = -3400078
65 meter
Z = 11991757
39 Z = 3655087
65
XDOT = 17817
378026 XDOT = 5430
736822
YDOT = 8262
119505 feet/sec YDOT = 2518
294025 meter/sec
ZDOT = -14284
189939 ZDOT = -4353
821094
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 10222
53955771
00016717 00000-0 10270-3 0 9130
2 25544 51
6463 312
4685 0007040 208
9289 151
1483 15
71468869 32020
Satellite: ISS
Catalog Number: 25544
Epoch time: 10222
53955771 = yrday
fracday
Element set: 913
Inclination: 51
6463 deg
RA of node: 312
4685 deg
Eccentricity:
0007040
Arg of perigee: 208
9289 deg
Mean anomaly: 151
1483 deg
Mean motion: 15
71468869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3202
Checksum: 314
Coasting Arc #15 (Orbit 3217)
---------------------------------------
Vector Time (GMT): 2010/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5254637
81 A = 6734882
87 meter
Y = -2783503
44 meter E =
0010370
Z = 3160246
31 I = 51
38122
XDOT = 282
273681 Wp = 119
41242
YDOT = 6004
650423 meter/sec RA = 306
96700 deg
ZDOT = 4802
618807 TA = 277
50424
MA = 277
62204
Ha = 194
183 n
mi
Hp = 188
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17239625
35 X = 5270021
33
Y = -9132229
12 feet Y = -2724656
92 meter
Z = 10368262
18 Z = 3185810
18
XDOT = 926
094754 XDOT = 191
777833
YDOT = 19700
296665 feet/sec YDOT = 6007
300989 meter/sec
ZDOT = 15756
623382 ZDOT = 4803
770252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18960539
28 X = -5779172
37
Y = -4355442
62 feet Y = -1327538
91 meter
Z = 10470492
89 Z = 3191406
23
XDOT = 11960
626866 XDOT = 3645
599069
YDOT = -14046
562501 feet/sec YDOT = -4281
392250 meter/sec
ZDOT = 15761
210708 ZDOT = 4804
017024
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 10223
55701894
00016717 00000-0 10270-3 0 9149
2 25544 51
6460 307
2632 0007070 213
6446 146
4268 15
71502866 32183
Satellite: ISS
Catalog Number: 25544
Epoch time: 10223
55701894 = yrday
fracday
Element set: 914
Inclination: 51
6460 deg
RA of node: 307
2632 deg
Eccentricity:
0007070
Arg of perigee: 213
6446 deg
Mean anomaly: 146
4268 deg
Mean motion: 15
71502866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3218
Checksum: 296
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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