Date:
October 18th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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
293/19:22:12
506 1
2 1
9 1
9
N/A -1
4 -0
0 195
5
000/00:04:21
013 0
2 0
1 185
1
Coasting Arc #1 (Orbit 239)
---------------------------------------
Vector Time (GMT): 2010/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 546575
65 A = 6726215
65 meter
Y = 4281005
80 meter E =
0010699
Z = 5150280
91 I = 51
48086
XDOT = -7228
545686 Wp = 81
39340
YDOT = 2380
839436 meter/sec RA = 334
51054 deg
ZDOT = -1208
155859 TA = 20
18745
MA = 20
14517
Ha = 195
740 n
mi
Hp = 184
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1793227
21 X = 473644
70
Y = 14045294
62 feet Y = 4286710
34 meter
Z = 16897247
09 Z = 5152758
90
XDOT = -23715
701069 XDOT = -7248
762379
YDOT = 7811
153004 feet/sec YDOT = 2299
892415 meter/sec
ZDOT = -3963
765940 ZDOT = -1243
321592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7074764
42 X = -2156388
20
Y = -12251517
79 feet Y = -3734262
62 meter
Z = 16907127
02 Z = 5153292
32
XDOT = 17824
931434 XDOT = 5433
039101
YDOT = -15974
557375 feet/sec YDOT = -4869
045088 meter/sec
ZDOT = -4104
766630 ZDOT = -1251
132869
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 10288
54560345
00016717 00000-0 10270-3 0 9008
2 25544 51
6448 334
8221 0007249 96
7931 263
4056 15
72033690 2408
Satellite: ISS
Catalog Number: 25544
Epoch time: 10288
54560345 = yrday
fracday
Element set: 900
Inclination: 51
6448 deg
RA of node: 334
8221 deg
Eccentricity:
0007249
Arg of perigee: 96
7931 deg
Mean anomaly: 263
4056 deg
Mean motion: 15
72033690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 240
Checksum: 300
Coasting Arc #2 (Orbit 255)
---------------------------------------
Vector Time (GMT): 2010/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5942599
15 A = 6737815
78 meter
Y = -3136107
25 meter E =
0018805
Z = 410191
72 I = 51
49254
XDOT = 1905
693899 Wp = 66
51184
YDOT = 4423
954283 meter/sec RA = 329
39386 deg
ZDOT = 6005
031730 TA = 297
95412
MA = 298
14434
Ha = 195
889 n
mi
Hp = 184
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19496716
36 X = 5975233
36
Y = -10289065
79 feet Y = -3069471
05 meter
Z = 1345773
37 Z = 439140
52
XDOT = 6252
276573 XDOT = 1826
911198
YDOT = 14514
285705 feet/sec YDOT = 4444
824705 meter/sec
ZDOT = 19701
547671 ZDOT = 6014
098073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13582908
25 X = -4140070
44
Y = 17354120
77 feet Y = 5289536
01 meter
Z = 1461856
76 Z = 445573
94
XDOT = -10265
182850 XDOT = -3128
827733
YDOT = -9750
461769 feet/sec YDOT = -2971
940747 meter/sec
ZDOT = 19737
840094 ZDOT = 6016
093661
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 10289
56271850
00016717 00000-0 10270-3 0 9012
2 25544 51
6447 329
6143 0007432 98
3322 261
8683 15
71991798 2564
Satellite: ISS
Catalog Number: 25544
Epoch time: 10289
56271850 = yrday
fracday
Element set: 901
Inclination: 51
6447 deg
RA of node: 329
6143 deg
Eccentricity:
0007432
Arg of perigee: 98
3322 deg
Mean anomaly: 261
8683 deg
Mean motion: 15
71991798 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 256
Checksum: 330
Coasting Arc #3 (Orbit 270)
---------------------------------------
Vector Time (GMT): 2010/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2656393
63 A = 6725715
35 meter
Y = -3262722
49 meter E =
0022233
Z = -5266309
19 I = 51
42749
XDOT = 6125
867151 Wp = 93
01014
YDOT = -4628
910700 meter/sec RA = 324
25788 deg
ZDOT = -224
102670 TA = 174
86271
MA = 174
83986
Ha = 195
774 n
mi
Hp = 184
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8715202
20 X = -2594128
81
Y = -10704470
10 feet Y = -3292080
08 meter
Z = -17277917
28 Z = -5279062
61
XDOT = 20097
989340 XDOT = 6178
261857
YDOT = -15186
714895 feet/sec YDOT = -4560
114631 meter/sec
ZDOT = -735
244981 ZDOT = -194
215354
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12340621
01 X = 3761421
29
Y = 6039991
72 feet Y = 1840989
48 meter
Z = -17329005
40 Z = -5281880
85
XDOT = -11319
714904 XDOT = -3450
249103
YDOT = 21380
728172 feet/sec YDOT = 6516
845947 meter/sec
ZDOT = -615
389448 ZDOT = -187
570704
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 10290
51624470
00016717 00000-0 10270-3 0 9020
2 25544 51
6455 324
7318 0007374 103
2851 256
9134 15
72038851 2717
Satellite: ISS
Catalog Number: 25544
Epoch time: 10290
51624470 = yrday
fracday
Element set: 902
Inclination: 51
6455 deg
RA of node: 324
7318 deg
Eccentricity:
0007374
Arg of perigee: 103
2851 deg
Mean anomaly: 256
9134 deg
Mean motion: 15
72038851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 271
Checksum: 291
Coasting Arc #4 (Orbit 286)
---------------------------------------
Vector Time (GMT): 2010/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4614409
40 A = 6737366
77 meter
Y = 4832549
86 meter E =
0020646
Z = 794134
27 I = 51
44244
XDOT = -3993
485465 Wp = 119
15986
YDOT = -2817
670801 meter/sec RA = 319
11317 deg
ZDOT = -5951
961727 TA = 52
15967
MA = 51
97301
Ha = 195
715 n
mi
Hp = 184
075
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15139138
46 X = -4671962
72
Y = 15854822
38 feet Y = 4780627
02 meter
Z = 2605427
39 Z = 771577
02
XDOT = -13101
986435 XDOT = -3932
767019
YDOT = -9244
326776 feet/sec YDOT = -2861
989322 meter/sec
ZDOT = -19527
433486 ZDOT = -5971
214617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6637775
55 X = 2023193
99
Y = -20903876
87 feet Y = -6371501
67 meter
Z = 2514960
29 Z = 766559
90
XDOT = 14204
013784 XDOT = 4329
383401
YDOT = 2108
221283 feet/sec YDOT = 642
585847 meter/sec
ZDOT = -19604
579762 ZDOT = -5975
475912
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 10291
53332487
00016717 00000-0 10270-3 0 9038
2 25544 51
6447 319
5238 0007495 106
2585 253
9402 15
72090493 2874
Satellite: ISS
Catalog Number: 25544
Epoch time: 10291
53332487 = yrday
fracday
Element set: 903
Inclination: 51
6447 deg
RA of node: 319
5238 deg
Eccentricity:
0007495
Arg of perigee: 106
2585 deg
Mean anomaly: 253
9402 deg
Mean motion: 15
72090493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 287
Checksum: 316
Coasting Arc #5 (Orbit 302)
---------------------------------------
Vector Time (GMT): 2010/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4158710
29 A = 6726308
45 meter
Y = 1509775
08 meter E =
0012338
Z = 5058139
76 I = 51
38247
XDOT = -4231
926770 Wp = 115
53707
YDOT = 6234
441387 meter/sec RA = 313
99712 deg
ZDOT = 1610
235624 TA = 318
90290
MA = 318
99577
Ha = 195
572 n
mi
Hp = 184
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13644062
62 X = 4116946
67
Y = 4953330
32 feet Y = 1556047
19 meter
Z = 16594946
71 Z = 5078241
53
XDOT = -13884
274181 XDOT = -4309
149284
YDOT = 20454
204024 feet/sec YDOT = 6186
685797 meter/sec
ZDOT = 5282
925277 ZDOT = 1589
488488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14315674
74 X = -4363417
66
Y = 1754171
26 feet Y = 534671
40 meter
Z = 16675506
65 Z = 5082694
43
XDOT = 3208
500596 XDOT = 977
950982
YDOT = -23502
568309 feet/sec YDOT = -7163
582821 meter/sec
ZDOT = 5199
708092 ZDOT = 1584
871027
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 10292
55038885
00016717 00000-0 10270-3 0 9047
2 25544 51
6438 314
3159 0007547 109
7129 250
4848 15
72112774 3031
Satellite: ISS
Catalog Number: 25544
Epoch time: 10292
55038885 = yrday
fracday
Element set: 904
Inclination: 51
6438 deg
RA of node: 314
3159 deg
Eccentricity:
0007547
Arg of perigee: 109
7129 deg
Mean anomaly: 250
4848 deg
Mean motion: 15
72112774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 303
Checksum: 312
Coasting Arc #6 (Orbit 317)
---------------------------------------
Vector Time (GMT): 2010/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 827156
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2677659
82 A = 6735690
03 meter
Y = -5854811
00 meter E =
0011541
Z = -1984933
01 I = 51
39513
XDOT = 5277
131016 Wp = 78
43109
YDOT = 535
345922 meter/sec RA = 308
82738 deg
ZDOT = 5569
360259 TA = 259
41985
MA = 259
54987
Ha = 195
594 n
mi
Hp = 183
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8784973
15 X = 2752573
03
Y = -19208697
51 feet Y = -5824449
10 meter
Z = -6512247
41 Z = -1971742
21
XDOT = 17313
421968 XDOT = 5243
696950
YDOT = 1756
384260 feet/sec YDOT = 594
171501 meter/sec
ZDOT = 18272
179327 ZDOT = 5594
915837
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1249603
56 X = 380879
17
Y = 21101534
65 feet Y = 6431747
76 meter
Z = -6459327
07 Z = -1968802
89
XDOT = -14470
000459 XDOT = -4410
456140
YDOT = 6451
496957 feet/sec YDOT = 1966
416273 meter/sec
ZDOT = 18374
604751 ZDOT = 5600
579528
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 10293
50387128
00016717 00000-0 10270-3 0 9051
2 25544 51
6446 309
4339 0007585 113
5581 246
6378 15
72173351 3181
Satellite: ISS
Catalog Number: 25544
Epoch time: 10293
50387128 = yrday
fracday
Element set: 905
Inclination: 51
6446 deg
RA of node: 309
4339 deg
Eccentricity:
0007585
Arg of perigee: 113
5581 deg
Mean anomaly: 246
6378 deg
Mean motion: 15
72173351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 318
Checksum: 316
Coasting Arc #7 (Orbit 322)
---------------------------------------
Vector Time (GMT): 2010/293/19:24:23
013
Vector Time (MET): N/A
Weight (LBS) : 826971
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2117902
10 A = 6727321
18 meter
Y = -3907767
63 meter E =
0019251
Z = -5067059
85 I = 51
35806
XDOT = 5511
549063 Wp = 106
52854
YDOT = -5098
570844 meter/sec RA = 307
24545 deg
ZDOT = 1628
112209 TA = 179
21596
MA = 179
21293
Ha = 195
505 n
mi
Hp = 185
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6948497
70 X = -2049431
90
Y = -12820759
93 feet Y = -3931068
86 meter
Z = -16624212
10 Z = -5077182
20
XDOT = 18082
510048 XDOT = 5560
243339
YDOT = -16727
594633 feet/sec YDOT = -5036
664990 meter/sec
ZDOT = 5341
575490 ZDOT = 1655
006610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3128058
29 X = 953432
17
Y = -14195748
41 feet Y = -4326864
12 meter
Z = -16664750
58 Z = -5079415
98
XDOT = 23554
785050 XDOT = 7179
498483
YDOT = -1207
902792 feet/sec YDOT = -368
168771 meter/sec
ZDOT = 5449
413280 ZDOT = 1660
981168
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 10293
82169646
00016717 00000-0 10270-3 0 9060
2 25544 51
6453 307
8062 0005787 116
8339 243
3416 15
71792133 3230
Satellite: ISS
Catalog Number: 25544
Epoch time: 10293
82169646 = yrday
fracday
Element set: 906
Inclination: 51
6453 deg
RA of node: 307
8062 deg
Eccentricity:
0005787
Arg of perigee: 116
8339 deg
Mean anomaly: 243
3416 deg
Mean motion: 15
71792133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 323
Checksum: 314
Coasting Arc #8 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2010/294/19:24:23
013
Vector Time (MET): N/A
Weight (LBS) : 826971
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4053282
89 A = 6738222
79 meter
Y = 5321793
64 meter E =
0016058
Z = -753962
63 I = 51
37738
XDOT = -3446
512088 Wp = 133
64709
YDOT = -3455
731482 meter/sec RA = 302
12806 deg
ZDOT = -5953
570913 TA = 54
59482
MA = 54
44494
Ha = 195
448 n
mi
Hp = 185
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13298172
21 X = -4108828
21
Y = 17459952
89 feet Y = 5276156
77 meter
Z = -2473630
67 Z = -773789
30
XDOT = -11307
454357 XDOT = -3378
691167
YDOT = -11337
701712 feet/sec YDOT = -3493
893681 meter/sec
ZDOT = -19532
712968 ZDOT = -5970
149512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21360243
33 X = -6510602
17
Y = 5003166
73 feet Y = 1524965
22 meter
Z = -2553138
32 Z = -778196
56
XDOT = -1043
596841 XDOT = -318
088317
YDOT = -14311
200100 feet/sec YDOT = -4362
053791 meter/sec
ZDOT = -19599
131326 ZDOT = -5973
815228
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 10294
83895069
00016717 00000-0 10270-3 0 9078
2 25544 51
6453 302
5991 0005817 121
9507 238
2221 15
71785508 3393
Satellite: ISS
Catalog Number: 25544
Epoch time: 10294
83895069 = yrday
fracday
Element set: 907
Inclination: 51
6453 deg
RA of node: 302
5991 deg
Eccentricity:
0005817
Arg of perigee: 121
9507 deg
Mean anomaly: 238
2221 deg
Mean motion: 15
71785508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 325
Coasting Arc #9 (Orbit 354)
---------------------------------------
Vector Time (GMT): 2010/295/19:24:23
013
Vector Time (MET): N/A
Weight (LBS) : 826971
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3717865
93 A = 6726158
99 meter
Y = 1955300
49 meter E =
0007691
Z = 5247042
98 I = 51
32237
XDOT = -3531
748064 Wp = 113
50767
YDOT = 6846
115684 meter/sec RA = 296
98037 deg
ZDOT = -51
689555 TA = 336
96755
MA = 337
00202
Ha = 195
151 n
mi
Hp = 185
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12197722
86 X = 3670235
14
Y = 6415027
86 feet Y = 1996609
88 meter
Z = 17214707
93 Z = 5264989
09
XDOT = -11587
099949 XDOT = -3607
789002
YDOT = 22461
009462 feet/sec YDOT = 6806
196383 meter/sec
ZDOT = -169
585154 ZDOT = -69
032386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5457083
03 X = 1663318
91
Y = 12556920
90 feet Y = 3827349
49 meter
Z = 17286618
43 Z = 5268961
30
XDOT = -22146
194828 XDOT = -6750
160184
YDOT = 9940
342280 feet/sec YDOT = 3029
816327 meter/sec
ZDOT = -239
147943 ZDOT = -72
892293
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 10295
85618607
00016717 00000-0 10270-3 0 9083
2 25544 51
6452 297
3921 0005680 124
9276 235
2420 15
71872824 3554
Satellite: ISS
Catalog Number: 25544
Epoch time: 10295
85618607 = yrday
fracday
Element set: 908
Inclination: 51
6452 deg
RA of node: 297
3921 deg
Eccentricity:
0005680
Arg of perigee: 124
9276 deg
Mean anomaly: 235
2420 deg
Mean motion: 15
71872824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 355
Checksum: 321
Coasting Arc #10 (Orbit 369)
---------------------------------------
Vector Time (GMT): 2010/296/19:24:23
013
Vector Time (MET): N/A
Weight (LBS) : 826971
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2002218
11 A = 6738027
36 meter
Y = -6398245
94 meter E =
0012399
Z = -651423
95 I = 51
35001
XDOT = 4777
904550 Wp = 67
37619
YDOT = 897
684291 meter/sec RA = 291
83330 deg
ZDOT = 5963
394678 TA = 285
51041
MA = 285
64729
Ha = 195
229 n
mi
Hp = 185
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6568957
06 X = 2076780
27
Y = -20991620
52 feet Y = -6375439
05 meter
Z = -2137217
69 Z = -641515
54
XDOT = 15675
539862 XDOT = 4738
541381
YDOT = 2945
158434 feet/sec YDOT = 950
893811 meter/sec
ZDOT = 19564
943170 ZDOT = 5986
510803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18018654
90 X = 5492086
01
Y = -12621243
49 feet Y = -3846955
02 meter
Z = -2097454
90 Z = -639304
25
XDOT = 9613
125630 XDOT = 2930
080692
YDOT = 10510
132575 feet/sec YDOT = 3203
488409 meter/sec
ZDOT = 19657
582889 ZDOT = 5991
631264
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 10296
80983144
00016717 00000-0 10270-3 0 9091
2 25544 51
6455 292
5102 0005678 128
0786 232
0889 15
71881726 3705
Satellite: ISS
Catalog Number: 25544
Epoch time: 10296
80983144 = yrday
fracday
Element set: 909
Inclination: 51
6455 deg
RA of node: 292
5102 deg
Eccentricity:
0005678
Arg of perigee: 128
0786 deg
Mean anomaly: 232
0889 deg
Mean motion: 15
71881726 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 370
Checksum: 330
Coasting Arc #11 (Orbit 385)
---------------------------------------
Vector Time (GMT): 2010/297/19:24:23
013
Vector Time (MET): N/A
Weight (LBS) : 826971
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4388253
62 A = 6726779
65 meter
Y = 418802
38 meter E =
0017839
Z = -5096238
76 I = 51
30218
XDOT = 1002
938242 Wp = 93
00321
YDOT = -7473
199829 meter/sec RA = 286
70971 deg
ZDOT = -1483
141219 TA = 162
70993
MA = 162
64909
Ha = 195
085 n
mi
Hp = 185
205
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14397157
56 X = -4367853
24
Y = 1374023
56 feet Y = 369844
29 meter
Z = -16719943
45 Z = -5117508
00
XDOT = 3290
479797 XDOT = 1093
635459
YDOT = -24518
372144 feet/sec YDOT = -7461
477274 meter/sec
ZDOT = -4865
948880 ZDOT = -1478
048396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12297628
94 X = -3748317
30
Y = -7421347
27 feet Y = -2262026
65 meter
Z = -16805193
33 Z = -5122222
93
XDOT = 16741
304006 XDOT = 5102
749461
YDOT = -16808
965465 feet/sec YDOT = -5123
372674 meter/sec
ZDOT = -4845
477594 ZDOT = -1476
901571
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 10297
82703530
00016717 00000-0 10270-3 0 9105
2 25544 51
6455 287
3026 0005569 131
4636 228
7005 15
71912601 3869
Satellite: ISS
Catalog Number: 25544
Epoch time: 10297
82703530 = yrday
fracday
Element set: 910
Inclination: 51
6455 deg
RA of node: 287
3026 deg
Eccentricity:
0005569
Arg of perigee: 131
4636 deg
Mean anomaly: 228
7005 deg
Mean motion: 15
71912601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 386
Checksum: 298
Coasting Arc #12 (Orbit 401)
---------------------------------------
Vector Time (GMT): 2010/298/19:24:23
013
Vector Time (MET): N/A
Weight (LBS) : 826971
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 259676
73 A = 6736554
55 meter
Y = 6439244
20 meter E =
0019508
Z = 1926994
37 I = 51
32748
XDOT = -4952
579709 Wp = 118
92192
YDOT = 1883
239826 meter/sec RA = 281
53712 deg
ZDOT = -5592
282911 TA = 39
55101
MA = 39
40882
Ha = 195
104 n
mi
Hp = 185
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 851957
79 X = 178291
35
Y = 21126129
25 feet Y = 6441692
99 meter
Z = 6322160
01 Z = 1928058
28
XDOT = -16248
621092 XDOT = -4946
103275
YDOT = 6178
608354 feet/sec YDOT = 1827
893364 meter/sec
ZDOT = -18347
384877 ZDOT = -5616
327484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11639489
23 X = -3547716
32
Y = 17649593
70 feet Y = 5379596
16 meter
Z = 6326374
07 Z = 1928278
82
XDOT = -15431
366744 XDOT = -4703
480583
YDOT = -3526
380368 feet/sec YDOT = -1074
840736 meter/sec
ZDOT = -18443
773413 ZDOT = -5621
662136
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 10298
84422390
00016717 00000-0 10270-3 0 9111
2 25544 51
6456 282
0956 0005721 135
2227 224
9398 15
71899148 4024
Satellite: ISS
Catalog Number: 25544
Epoch time: 10298
84422390 = yrday
fracday
Element set: 911
Inclination: 51
6456 deg
RA of node: 282
0956 deg
Eccentricity:
0005721
Arg of perigee: 135
2227 deg
Mean anomaly: 224
9398 deg
Mean motion: 15
71899148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 402
Checksum: 319
Coasting Arc #13 (Orbit 417)
---------------------------------------
Vector Time (GMT): 2010/299/19:24:23
013
Vector Time (MET): N/A
Weight (LBS) : 826971
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4020535
96 A = 6728833
03 meter
Y = -2824554
70 meter E =
0013569
Z = 4591280
59 I = 51
29671
XDOT = 1557
260597 Wp = 124
74974
YDOT = 6960
394863 meter/sec RA = 276
43320 deg
ZDOT = 2904
641437 TA = 296
27938
MA = 296
41873
Ha = 194
907 n
mi
Hp = 185
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13190734
78 X = 4029517
66
Y = -9266911
75 feet Y = -2779544
54 meter
Z = 15063256
54 Z = 4610834
61
XDOT = 5109
122693 XDOT = 1465
201849
YDOT = 22835
941150 feet/sec YDOT = 6977
294292 meter/sec
ZDOT = 9529
663506 ZDOT = 2911
983344
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16045881
90 X = 4890784
80
Y = -180903
53 feet Y = -55139
40 meter
Z = 15141657
21 Z = 4615177
12
XDOT = -8831
574107 XDOT = -2691
863788
YDOT = 20492
295594 feet/sec YDOT = 6246
051697 meter/sec
ZDOT = 9559
040924 ZDOT = 2913
595674
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 10299
86139353
00016717 00000-0 10270-3 0 9129
2 25544 51
6454 276
8879 0005565 138
5435 221
6150 15
71926136 4185
Satellite: ISS
Catalog Number: 25544
Epoch time: 10299
86139353 = yrday
fracday
Element set: 912
Inclination: 51
6454 deg
RA of node: 276
8879 deg
Eccentricity:
0005565
Arg of perigee: 138
5435 deg
Mean anomaly: 221
6150 deg
Mean motion: 15
71926136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 418
Checksum: 328
Coasting Arc #14 (Orbit 432)
---------------------------------------
Vector Time (GMT): 2010/300/19:24:23
013
Vector Time (MET): N/A
Weight (LBS) : 826971
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2358471
64 A = 6733773
84 meter
Y = -5502500
38 meter E =
0008255
Z = -3093251
28 I = 51
31089
XDOT = 3985
222743 Wp = 113
30427
YDOT = -4433
502807 meter/sec RA = 271
24211 deg
ZDOT = 4855
133679 TA = 210
67372
MA = 210
72200
Ha = 194
797 n
mi
Hp = 185
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7737767
85 X = -2281739
60
Y = -18052822
76 feet Y = -5528445
10 meter
Z = -10148462
19 Z = -3104522
74
XDOT = 13074
877767 XDOT = 4010
916938
YDOT = -14545
612884 feet/sec YDOT = -4388
794125 meter/sec
ZDOT = 15928
916269 ZDOT = 4874
556590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3609402
46 X = 1100145
87
Y = -19282927
70 feet Y = -5877436
36 meter
Z = -10193608
72 Z = -3107011
94
XDOT = 17457
784391 XDOT = 5321
132682
YDOT = -5181
782737 feet/sec YDOT = -1579
407378 meter/sec
ZDOT = 16006
805658 ZDOT = 4878
874364
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 10300
81497331
00016717 00000-0 10270-3 0 9131
2 25544 51
6447 272
0055 0005416 143
9304 216
2225 15
71969960 4333
Satellite: ISS
Catalog Number: 25544
Epoch time: 10300
81497331 = yrday
fracday
Element set: 913
Inclination: 51
6447 deg
RA of node: 272
0055 deg
Eccentricity:
0005416
Arg of perigee: 143
9304 deg
Mean anomaly: 216
2225 deg
Mean motion: 15
71969960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 433
Checksum: 288
Coasting Arc #15 (Orbit 448)
---------------------------------------
Vector Time (GMT): 2010/301/19:24:23
013
Vector Time (MET): N/A
Weight (LBS) : 826971
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2772821
03 A = 6731413
10 meter
Y = 4776283
15 meter E =
0009547
Z = -3854026
94 I = 51
30267
XDOT = -3643
799307 Wp = 107
30279
YDOT = -5402
902930 meter/sec RA = 266
14878 deg
ZDOT = -4085
362957 TA = 119
85676
MA = 119
76185
Ha = 194
672 n
mi
Hp = 185
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9097181
87 X = -2807301
75
Y = 15670220
32 feet Y = 4745083
10 meter
Z = -12644445
34 Z = -3867581
18
XDOT = -11954
722136 XDOT = -3563
265933
YDOT = -17726
059482 feet/sec YDOT = -5443
199702 meter/sec
ZDOT = -13403
421774 ZDOT = -4102
869343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16050898
32 X = -4892313
81
Y = 8324985
91 feet Y = 2537455
71 meter
Z = -12698810
71 Z = -3870597
50
XDOT = 173
924094 XDOT = 53
012064
YDOT = -20161
579494 feet/sec YDOT = -6145
249430 meter/sec
ZDOT = -13473
573627 ZDOT = -4106
745242
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 10301
83210915
00016717 00000-0 10270-3 0 9146
2 25544 51
6438 266
7980 0005440 148
4209 211
7280 15
71987731 4495
Satellite: ISS
Catalog Number: 25544
Epoch time: 10301
83210915 = yrday
fracday
Element set: 914
Inclination: 51
6438 deg
RA of node: 266
7980 deg
Eccentricity:
0005440
Arg of perigee: 148
4209 deg
Mean anomaly: 211
7280 deg
Mean motion: 15
71987731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 449
Checksum: 305
Coasting Arc #16 (Orbit 464)
---------------------------------------
Vector Time (GMT): 2010/302/19:24:23
013
Vector Time (MET): N/A
Weight (LBS) : 826971
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3853107
30 A = 6730626
45 meter
Y = 3779353
77 meter E =
0013195
Z = 4008443
54 I = 51
30433
XDOT = -2141
073883 Wp = 100
43062
YDOT = 6304
041088 meter/sec RA = 260
95275 deg
ZDOT = -3877
198956 TA = 29
75684
MA = 29
68186
Ha = 194
385 n
mi
Hp = 185
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12641428
14 X = 3791086
92
Y = 12399454
63 feet Y = 3822094
72 meter
Z = 13151061
49 Z = 4027011
58
XDOT = -7024
520615 XDOT = -2192
572716
YDOT = 20682
549500 feet/sec YDOT = 6279
810402 meter/sec
ZDOT = -12720
469016 ZDOT = -3887
725472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4182268
07 X = 1274755
31
Y = 17149275
93 feet Y = 5227099
30 meter
Z = 13225489
32 Z = 4031129
14
XDOT = -15521
921092 XDOT = -4731
081549
YDOT = 13649
233567 feet/sec YDOT = 4160
286391 meter/sec
ZDOT = -12762
699537 ZDOT = -3890
070819
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 10302
84922585
00016717 00000-0 10270-3 0 9152
2 25544 51
6441 261
5900 0005321 152
4195 207
7251 15
72064206 4656
Satellite: ISS
Catalog Number: 25544
Epoch time: 10302
84922585 = yrday
fracday
Element set: 915
Inclination: 51
6441 deg
RA of node: 261
5900 deg
Eccentricity:
0005321
Arg of perigee: 152
4195 deg
Mean anomaly: 207
7251 deg
Mean motion: 15
72064206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 465
Checksum: 282
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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