Date:
August 10th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20451 43 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
230/20:37:31
569 1
8 4
0 4
0
N/A -2
7 -0
0 191
6
000/00:10:59
139 2
3 0
2 191
0
Coasting Arc #1 (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 = -5020659
51 A = 6730089
51 meter
Y = -226249
46 meter E =
0006726
Z = -4479937
14 I = 51
40862
XDOT = 3095
350667 Wp = 114
47543
YDOT = -6295
348378 meter/sec RA = 317
23351 deg
ZDOT = -3157
480333 TA = 123
88076
MA = 123
81676
Ha = 194
133 n
mi
Hp = 188
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16471980
03 X = -4995994
23
Y = -742288
27 feet Y = -282255
32 meter
Z = -14697956
50 Z = -4504267
00
XDOT = 10155
349957 XDOT = 3180
854434
YDOT = -20654
030110 feet/sec YDOT = -6260
256059 meter/sec
ZDOT = -10359
187444 ZDOT = -3142
236169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11496075
55 X = 3504003
83
Y = 11698206
09 feet Y = 3565613
22 meter
Z = -14795244
66 Z = -4509590
57
XDOT = -20691
383481 XDOT = -6306
733685
YDOT = 7335
902070 feet/sec YDOT = 2235
982951 meter/sec
ZDOT = -10298
188773 ZDOT = -3138
887938
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
52145784
00016717 00000-0 10270-3 0 9009
2 25544 51
6476 317
6784 0007048 206
9846 153
0950 15
71638261 31862
Satellite: ISS
Catalog Number: 25544
Epoch time: 10221
52145784 = yrday
fracday
Element set: 900
Inclination: 51
6476 deg
RA of node: 317
6784 deg
Eccentricity:
0007048
Arg of perigee: 206
9846 deg
Mean anomaly: 153
0950 deg
Mean motion: 15
71638261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3186
Checksum: 315
Coasting Arc #2 (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 = -1460011
79 A = 6733895
68 meter
Y = 5635535
48 meter E =
0010979
Z = 3370367
97 I = 51
39978
XDOT = -6045
985008 Wp = 122
91799
YDOT = 1198
533071 meter/sec RA = 312
05150 deg
ZDOT = -4618
123158 TA = 17
20791
MA = 17
17072
Ha = 194
003 n
mi
Hp = 188
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4790064
93 X = -1539293
11
Y = 18489289
64 feet Y = 5618765
39 meter
Z = 11057637
71 Z = 3363082
98
XDOT = -19835
908819 XDOT = -6036
504418
YDOT = 3932
195116 feet/sec YDOT = 1130
976370 meter/sec
ZDOT = -15151
322698 ZDOT = -4647
470776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15965294
35 X = 4866221
72
Y = -10514365
94 feet Y = -3204778
74 meter
Z = 11028480
87 Z = 3361480
97
XDOT = 16552
799205 XDOT = 5045
293198
YDOT = 9101
736214 feet/sec YDOT = 2774
209198 meter/sec
ZDOT = -15268
682953 ZDOT = -4653
894564
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
53879921
00016717 00000-0 10270-3 0 9019
2 25544 51
6472 312
4734 0006833 209
9717 150
1054 15
71675004 32025
Satellite: ISS
Catalog Number: 25544
Epoch time: 10222
53879921 = yrday
fracday
Element set: 901
Inclination: 51
6472 deg
RA of node: 312
4734 deg
Eccentricity:
0006833
Arg of perigee: 209
9717 deg
Mean anomaly: 150
1054 deg
Mean motion: 15
71675004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3202
Checksum: 288
Coasting Arc #3 (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 = 5255486
58 A = 6733184
70 meter
Y = -2309683
53 meter E =
0010362
Z = 3517464
26 I = 51
37852
XDOT = -247
316602 Wp = 126
87023
YDOT = 6261
461249 meter/sec RA = 306
96683 deg
ZDOT = 4465
801955 TA = 275
09752
MA = 275
21579
Ha = 193
720 n
mi
Hp = 188
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17242410
04 X = 5263836
43
Y = -7577701
88 feet Y = -2250866
85 meter
Z = 11540237
06 Z = 3543015
16
XDOT = -811
406175 XDOT = -339
008634
YDOT = 20542
851866 feet/sec YDOT = 6258
182931 meter/sec
ZDOT = 14651
581216 ZDOT = 4464
377798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17938895
68 X = -5467775
40
Y = -5527164
28 feet Y = -1684679
67 meter
Z = 11642414
61 Z = 3548607
97
XDOT = 13734
859340 XDOT = 4186
385127
YDOT = -13623
522803 feet/sec YDOT = -4152
449750 meter/sec
ZDOT = 14645
868701 ZDOT = 4464
060780
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
55611856
00016717 00000-0 10270-3 0 9024
2 25544 51
6470 307
2671 0006846 214
9220 145
1493 15
71731697 32183
Satellite: ISS
Catalog Number: 25544
Epoch time: 10223
55611856 = yrday
fracday
Element set: 902
Inclination: 51
6470 deg
RA of node: 307
2671 deg
Eccentricity:
0006846
Arg of perigee: 214
9220 deg
Mean anomaly: 145
1493 deg
Mean motion: 15
71731697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3218
Checksum: 301
Coasting Arc #4 (Orbit 3232)
---------------------------------------
Vector Time (GMT): 2010/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -967465
92 A = 6730300
76 meter
Y = -5048374
91 meter E =
0009456
Z = -4353167
51 I = 51
35087
XDOT = 5642
754640 Wp = 152
79854
YDOT = -3991
527192 meter/sec RA = 301
78017 deg
ZDOT = 3369
513483 TA = 151
35870
MA = 151
30673
Ha = 193
512 n
mi
Hp = 188
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3174100
79 X = -889795
59
Y = -16562909
81 feet Y = -5058759
46 meter
Z = -14282045
64 Z = -4357678
67
XDOT = 18512
974542 XDOT = 5670
601010
YDOT = -13095
561652 feet/sec YDOT = -3928
270796 meter/sec
ZDOT = 11054
834263 ZDOT = 3396
993245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8266459
95 X = -2519616
99
Y = 14681797
14 feet Y = 4475011
77 meter
Z = -14300076
83 Z = -4358663
42
XDOT = -21479
855473 XDOT = -6547
059948
YDOT = -1202
378879 feet/sec YDOT = -366
485082 meter/sec
ZDOT = 11164
721164 ZDOT = 3403
007011
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 10224
50983940
00016717 00000-0 10270-3 0 9037
2 25544 51
6461 302
3872 0006684 218
3623 141
7064 15
71771455 32336
Satellite: ISS
Catalog Number: 25544
Epoch time: 10224
50983940 = yrday
fracday
Element set: 903
Inclination: 51
6461 deg
RA of node: 302
3872 deg
Eccentricity:
0006684
Arg of perigee: 218
3623 deg
Mean anomaly: 141
7064 deg
Mean motion: 15
71771455 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3233
Checksum: 297
Coasting Arc #5 (Orbit 3248)
---------------------------------------
Vector Time (GMT): 2010/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4375824
48 A = 6736132
57 meter
Y = 4550589
16 meter E =
0008838
Z = -2333741
89 I = 51
35467
XDOT = -2315
997155 Wp = 182
66039
YDOT = -4986
622466 meter/sec RA = 296
68617 deg
ZDOT = -5388
797891 TA = 23
69539
MA = 23
65471
Ha = 193
250 n
mi
Hp = 188
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14356379
51 X = -4415047
99
Y = 14929754
46 feet Y = 4501436
74 meter
Z = -7656633
49 Z = -2355094
73
XDOT = -7598
415863 XDOT = -2233
886158
YDOT = -16360
309928 feet/sec YDOT = -5012
062266 meter/sec
ZDOT = -17679
783107 ZDOT = -5399
849408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20515241
77 X = 6253045
69
Y = -2610227
03 feet Y = -795597
20 meter
Z = -7742015
70 Z = -2359766
39
XDOT = -4651
196339 XDOT = -1417
684644
YDOT = 15937
651572 feet/sec YDOT = 4857
796199 meter/sec
ZDOT = -17723
970440 ZDOT = -5402
266190
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 10225
52712235
00016717 00000-0 10270-3 0 9048
2 25544 51
6451 297
1808 0006633 222
8481 137
2165 15
71763136 32497
Satellite: ISS
Catalog Number: 25544
Epoch time: 10225
52712235 = yrday
fracday
Element set: 904
Inclination: 51
6451 deg
RA of node: 297
1808 deg
Eccentricity:
0006633
Arg of perigee: 222
8481 deg
Mean anomaly: 137
2165 deg
Mean motion: 15
71763136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3249
Checksum: 299
Coasting Arc #6 (Orbit 3264)
---------------------------------------
Vector Time (GMT): 2010/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2923867
97 A = 6727508
28 meter
Y = 3453241
16 meter E =
0001165
Z = 4978352
21 I = 51
31425
XDOT = -4100
354078 Wp = 190
39465
YDOT = 6227
382069 meter/sec RA = 291
50923 deg
ZDOT = -1912
627139 TA = 278
15995
MA = 278
17317
Ha = 192
900 n
mi
Hp = 188
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9592742
68 X = 2860852
10
Y = 11329531
37 feet Y = 3485585
23 meter
Z = 16333176
55 Z = 4992403
23
XDOT = -13452
605242 XDOT = -4160
393919
YDOT = 20431
043533 feet/sec YDOT = 6181
193766 meter/sec
ZDOT = -6275
023423 ZDOT = -1932
692328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -513613
49 X = -156549
39
Y = -14774191
50 feet Y = -4503173
57 meter
Z = 16389359
84 Z = 4995476
88
XDOT = 22069
113347 XDOT = 6726
665748
YDOT = -7812
896388 feet/sec YDOT = -2381
370819 meter/sec
ZDOT = -6355
253121 ZDOT = -1937
081151
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 10226
54438332
00016717 00000-0 10270-3 0 9055
2 25544 51
6456 291
9740 0006633 228
5724 131
4869 15
71836256 32651
Satellite: ISS
Catalog Number: 25544
Epoch time: 10226
54438332 = yrday
fracday
Element set: 905
Inclination: 51
6456 deg
RA of node: 291
9740 deg
Eccentricity:
0006633
Arg of perigee: 228
5724 deg
Mean anomaly: 131
4869 deg
Mean motion: 15
71836256 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3265
Checksum: 320
Coasting Arc #7 (Orbit 3280)
---------------------------------------
Vector Time (GMT): 2010/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2630817
63 A = 6737999
34 meter
Y = -6118996
98 meter E =
0007444
Z = 996077
75 I = 51
33850
XDOT = 4115
372043 Wp = 59
04084
YDOT = 2734
394743 meter/sec RA = 286
39327 deg
ZDOT = 5899
388010 TA = 311
87771
MA = 311
94120
Ha = 192
850 n
mi
Hp = 188
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8631291
43 X = 2694207
10
Y = -20075449
40 feet Y = -6089223
19 meter
Z = 3267971
62 Z = 1009012
03
XDOT = 13501
876783 XDOT = 4055
831653
YDOT = 8971
111363 feet/sec YDOT = 2780
082246 meter/sec
ZDOT = 19354
947540 ZDOT = 5919
235835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18957426
30 X = -5778223
54
Y = 10853486
52 feet Y = 3308142
69 meter
Z = 3319686
32 Z = 1011840
39
XDOT = -4503
195979 XDOT = -1372
574134
YDOT = -13838
305515 feet/sec YDOT = -4217
915521 meter/sec
ZDOT = 19434
311193 ZDOT = 5923
578052
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 10227
56162899
00016717 00000-0 10270-3 0 9061
2 25544 51
6449 286
7670 0006301 232
2709 127
7883 15
71800920 32815
Satellite: ISS
Catalog Number: 25544
Epoch time: 10227
56162899 = yrday
fracday
Element set: 906
Inclination: 51
6449 deg
RA of node: 286
7670 deg
Eccentricity:
0006301
Arg of perigee: 232
2709 deg
Mean anomaly: 127
7883 deg
Mean motion: 15
71800920 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3281
Checksum: 320
Coasting Arc #8 (Orbit 3295)
---------------------------------------
Vector Time (GMT): 2010/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4041639
92 A = 6726310
45 meter
Y = -1223445
58 meter E =
0010572
Z = -5244160
33 I = 51
29194
XDOT = 1783
088165 Wp = 114
01336
YDOT = -7471
936734 meter/sec RA = 281
23788 deg
ZDOT = 365
304486 TA = 159
49776
MA = 159
45530
Ha = 192
567 n
mi
Hp = 188
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13259973
49 X = -4002183
69
Y = -4013929
07 feet Y = -1268420
79 meter
Z = -17205250
43 Z = -5263698
73
XDOT = 5850
026789 XDOT = 1864
733633
YDOT = -24514
228129 feet/sec YDOT = -7451
540685 meter/sec
ZDOT = 1198
505531 ZDOT = 374
164694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8284392
36 X = 2525082
79
Y = 10982386
50 feet Y = 3347431
41 meter
Z = -17283379
17 Z = -5267973
97
XDOT = -18336
435149 XDOT = -5588
945433
YDOT = 15792
490320 feet/sec YDOT = 4813
551049 meter/sec
ZDOT = 1233
926780 ZDOT = 376
100883
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 10228
51527566
00016717 00000-0 10270-3 0 9074
2 25544 51
6447 281
8854 0006377 236
2034 123
8521 15
71839852 32969
Satellite: ISS
Catalog Number: 25544
Epoch time: 10228
51527566 = yrday
fracday
Element set: 907
Inclination: 51
6447 deg
RA of node: 281
8854 deg
Eccentricity:
0006377
Arg of perigee: 236
2034 deg
Mean anomaly: 123
8521 deg
Mean motion: 15
71839852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3296
Checksum: 327
Coasting Arc #9 (Orbit 3311)
---------------------------------------
Vector Time (GMT): 2010/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -429750
89 A = 6738079
60 meter
Y = 6706948
99 meter E =
0012334
Z = 355836
70 I = 51
32804
XDOT = -4829
046229 Wp = 159
46129
YDOT = 11
531020 meter/sec RA = 276
09491 deg
ZDOT = -5998
048085 TA = 16
65561
MA = 16
61513
Ha = 192
254 n
mi
Hp = 188
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1409943
85 X = -506445
85
Y = 22004425
83 feet Y = 6701714
42 meter
Z = 1167443
23 Z = 353563
05
XDOT = -15843
327524 XDOT = -4799
679049
YDOT = 37
831429 feet/sec YDOT = -42
305747 meter/sec
ZDOT = -19678
635448 ZDOT = -6021
436085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13787491
11 X = 4202427
29
Y = -17207815
27 feet Y = -5244942
09 meter
Z = 1158362
60 Z = 353068
92
XDOT = 11645
930405 XDOT = 3549
679588
YDOT = 7988
687502 feet/sec YDOT = 2434
951951 meter/sec
ZDOT = -19772
160926 ZDOT = -6026
554650
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 10229
53248054
00016717 00000-0 10270-3 0 9080
2 25544 51
6453 276
6785 0006173 240
4222 119
6325 15
71910199 33129
Satellite: ISS
Catalog Number: 25544
Epoch time: 10229
53248054 = yrday
fracday
Element set: 908
Inclination: 51
6453 deg
RA of node: 276
6785 deg
Eccentricity:
0006173
Arg of perigee: 240
4222 deg
Mean anomaly: 119
6325 deg
Mean motion: 15
71910199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3312
Checksum: 303
Coasting Arc #10 (Orbit 3327)
---------------------------------------
Vector Time (GMT): 2010/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4148977
45 A = 6726460
46 meter
Y = -1242376
64 meter E =
0005437
Z = 5149398
21 I = 51
28637
XDOT = 809
158569 Wp = 204
23762
YDOT = 7563
167547 meter/sec RA = 270
96534 deg
ZDOT = 1168
328754 TA = 234
51743
MA = 234
56817
Ha = 192
029 n
mi
Hp = 189
059
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13612130
75 X = 4137547
00
Y = -4076038
83 feet Y = -1196044
50 meter
Z = 16894351
08 Z = 5169525
88
XDOT = 2654
719714 XDOT = 718
850237
YDOT = 24813
541820 feet/sec YDOT = 7571
711033 meter/sec
ZDOT = 3833
099588 ZDOT = 1172
040690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13478345
56 X = -4108199
73
Y = -4184766
04 feet Y = -1275516
69 meter
Z = 16974841
05 Z = 5173931
55
XDOT = 11401
237495 XDOT = 3475
097188
YDOT = -21053
602498 feet/sec YDOT = -6417
138041 meter/sec
ZDOT = 3847
964158 ZDOT = 1172
859475
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 10230
54966596
00016717 00000-0 10270-3 0 9092
2 25544 51
6445 271
4716 0006141 243
9535 116
0995 15
71930141 33287
Satellite: ISS
Catalog Number: 25544
Epoch time: 10230
54966596 = yrday
fracday
Element set: 909
Inclination: 51
6445 deg
RA of node: 271
4716 deg
Eccentricity:
0006141
Arg of perigee: 243
9535 deg
Mean anomaly: 116
0995 deg
Mean motion: 15
71930141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3328
Checksum: 313
Coasting Arc #11 (Orbit 3332)
---------------------------------------
Vector Time (GMT): 2010/230/20:43:01
139
Vector Time (MET): N/A
Weight (LBS) : 828328
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1841420
51 A = 6738216
31 meter
Y = -6101390
84 meter E =
0005910
Z = -2175782
46 I = 51
31940
XDOT = 4325
625241 Wp = 320
16511
YDOT = -3256
901803 meter/sec RA = 269
06789 deg
ZDOT = 5468
475857 TA = 15
38658
MA = 15
36862
Ha = 191
606 n
mi
Hp = 191
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6041405
87 X = -1762487
35
Y = -20017686
49 feet Y = -6121541
24 meter
Z = -7138393
89 Z = -2184536
60
XDOT = 14191
683861 XDOT = 4335
158484
YDOT = -10685
373371 feet/sec YDOT = -3208
477090 meter/sec
ZDOT = 17941
193757 ZDOT = 5489
512453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19125940
45 X = 5829586
65
Y = -8420417
76 feet Y = -2566543
33 meter
Z = -7173422
56 Z = -2186459
20
XDOT = 11725
258538 XDOT = 3573
858802
YDOT = 11266
184309 feet/sec YDOT = 3433
932977 meter/sec
ZDOT = 18025
313999 ZDOT = 5494
115707
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 10230
86753260
00016717 00000-0 10270-3 0 9101
2 25544 51
6455 269
8447 0007945 269
8092 90
2159 15
71153189 33338
Satellite: ISS
Catalog Number: 25544
Epoch time: 10230
86753260 = yrday
fracday
Element set: 910
Inclination: 51
6455 deg
RA of node: 269
8447 deg
Eccentricity:
0007945
Arg of perigee: 269
8092 deg
Mean anomaly: 90
2159 deg
Mean motion: 15
71153189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3333
Checksum: 323
Coasting Arc #12 (Orbit 3348)
---------------------------------------
Vector Time (GMT): 2010/231/20:43:01
139
Vector Time (MET): N/A
Weight (LBS) : 828328
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3053610
09 A = 6731967
32 meter
Y = 4150945
51 meter E =
0003811
Z = -4334468
52 I = 51
30084
XDOT = -3369
662038 Wp = 7
58785
YDOT = -6025
803998 meter/sec RA = 263
97463 deg
ZDOT = -3393
375974 TA = 227
97944
MA = 228
01189
Ha = 192
035 n
mi
Hp = 191
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10018405
82 X = -3078744
05
Y = 13618587
62 feet Y = 4116657
91 meter
Z = -14220697
24 Z = -4349363
55
XDOT = -11055
321648 XDOT = -3285
545812
YDOT = -19769
698156 feet/sec YDOT = -6063
015076 meter/sec
ZDOT = -11133
123274 ZDOT = -3409
541534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14877160
69 X = -4534558
58
Y = -7925093
56 feet Y = -2415568
52 meter
Z = -14280251
94 Z = -4352620
79
XDOT = 17454
839132 XDOT = 5320
234967
YDOT = -12569
325449 feet/sec YDOT = -3831
130397 meter/sec
ZDOT = -11197
804822 ZDOT = -3413
090910
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 10231
88520191
00016717 00000-0 10270-3 0 9110
2 25544 51
6459 264
6413 0007930 274
4429 85
5827 15
71193742 33493
Satellite: ISS
Catalog Number: 25544
Epoch time: 10231
88520191 = yrday
fracday
Element set: 911
Inclination: 51
6459 deg
RA of node: 264
6413 deg
Eccentricity:
0007930
Arg of perigee: 274
4429 deg
Mean anomaly: 85
5827 deg
Mean motion: 15
71193742 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3349
Checksum: 317
Coasting Arc #13 (Orbit 3364)
---------------------------------------
Vector Time (GMT): 2010/232/20:43:01
139
Vector Time (MET): N/A
Weight (LBS) : 828328
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3819230
71 A = 6734247
52 meter
Y = 4158941
05 meter E =
0004553
Z = 3668318
97 I = 51
31224
XDOT = -2332
449582 Wp = 60
02933
YDOT = 5939
588006 meter/sec RA = 258
78701 deg
ZDOT = -4299
346732 TA = 75
70867
MA = 75
65811
Ha = 192
489 n
mi
Hp = 191
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12530284
47 X = 3754621
12
Y = 13644819
73 feet Y = 4201288
58 meter
Z = 12035167
21 Z = 3686715
67
XDOT = -7652
393642 XDOT = -2377
808743
YDOT = 19486
837291 feet/sec YDOT = 5913
251715 meter/sec
ZDOT = -14105
468280 ZDOT = -4310
787491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11515435
42 X = -3509904
72
Y = 14450144
18 feet Y = 4404403
95 meter
Z = 12108776
34 Z = 3690755
03
XDOT = -19380
669317 XDOT = -5907
228008
YDOT = -3569
318754 feet/sec YDOT = -1087
928356 meter/sec
ZDOT = -14151
193071 ZDOT = -4313
283648
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 10232
90285311
00016717 00000-0 10270-3 0 9127
2 25544 51
6451 259
4376 0007892 278
3520 81
6747 15
71202754 33657
Satellite: ISS
Catalog Number: 25544
Epoch time: 10232
90285311 = yrday
fracday
Element set: 912
Inclination: 51
6451 deg
RA of node: 259
4376 deg
Eccentricity:
0007892
Arg of perigee: 278
3520 deg
Mean anomaly: 81
6747 deg
Mean motion: 15
71202754 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3365
Checksum: 308
Coasting Arc #14 (Orbit 3380)
---------------------------------------
Vector Time (GMT): 2010/233/20:43:01
139
Vector Time (MET): N/A
Weight (LBS) : 828328
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 840147
06 A = 6735956
02 meter
Y = -5924608
07 meter E =
0006044
Z = 3084925
78 I = 51
32536
XDOT = 5005
218416 Wp = 61
41633
YDOT = 3244
746694 meter/sec RA = 253
69965 deg
ZDOT = 4864
061525 TA = 334
52391
MA = 334
55369
Ha = 192
710 n
mi
Hp = 191
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2756388
00 X = 891348
97
Y = -19437690
53 feet Y = -5914926
83 meter
Z = 10121147
58 Z = 3089131
37
XDOT = 16421
320261 XDOT = 4944
934827
YDOT = 10645
494403 feet/sec YDOT = 3300
380872 meter/sec
ZDOT = 15958
207104 ZDOT = 4888
230015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19609827
39 X = 5977075
39
Y = -732322
72 feet Y = -223211
97 meter
Z = 10137923
33 Z = 3090039
03
XDOT = -7691
225547 XDOT = -2344
285547
YDOT = 16501
961700 feet/sec YDOT = 5029
797926 meter/sec
ZDOT = 16054
909391 ZDOT = 4893
536382
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 10233
92048438
00016717 00000-0 10270-3 0 9138
2 25544 51
6454 254
2328 0007936 282
8693 77
1582 15
71222202 33815
Satellite: ISS
Catalog Number: 25544
Epoch time: 10233
92048438 = yrday
fracday
Element set: 913
Inclination: 51
6454 deg
RA of node: 254
2328 deg
Eccentricity:
0007936
Arg of perigee: 282
8693 deg
Mean anomaly: 77
1582 deg
Mean motion: 15
71222202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3381
Checksum: 307
Coasting Arc #15 (Orbit 3395)
---------------------------------------
Vector Time (GMT): 2010/234/20:43:01
139
Vector Time (MET): N/A
Weight (LBS) : 828328
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4602477
68 A = 6730209
76 meter
Y = -1391386
49 meter E =
0003299
Z = -4712414
33 I = 51
31613
XDOT = -545
620841 Wp = 114
90428
YDOT = -7198
707159 meter/sec RA = 248
51723 deg
ZDOT = 2658
467491 TA = 181
37013
MA = 181
37103
Ha = 192
793 n
mi
Hp = 191
026
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15099992
39 X = -4563685
30
Y = -4564916
30 feet Y = -1442637
24 meter
Z = -15460676
95 Z = -4734678
48
XDOT = -1790
094624 XDOT = -477
997110
YDOT = -23617
805639 feet/sec YDOT = -7204
430519 meter/sec
ZDOT = 8722
006205 ZDOT = 2655
981161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1611858
23 X = 491294
39
Y = -15604095
37 feet Y = -4756128
27 meter
Z = -15549755
10 Z = -4739565
36
XDOT = 21691
892258 XDOT = 6611
688760
YDOT = -6440
658029 feet/sec YDOT = -1963
112567 meter/sec
ZDOT = 8711
989066 ZDOT = 2655
414267
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 10234
87449493
00016717 00000-0 10270-3 0 9140
2 25544 51
6452 249
3538 0008082 286
2177 73
8095 15
71274069 33965
Satellite: ISS
Catalog Number: 25544
Epoch time: 10234
87449493 = yrday
fracday
Element set: 914
Inclination: 51
6452 deg
RA of node: 249
3538 deg
Eccentricity:
0008082
Arg of perigee: 286
2177 deg
Mean anomaly: 73
8095 deg
Mean motion: 15
71274069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3396
Checksum: 339
Coasting Arc #16 (Orbit 3411)
---------------------------------------
Vector Time (GMT): 2010/235/20:43:01
139
Vector Time (MET): N/A
Weight (LBS) : 828328
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1803223
07 A = 6738996
92 meter
Y = 6310671
02 meter E =
0004784
Z = -1515354
04 I = 51
35758
XDOT = -5106
769454 Wp = 213
47999
YDOT = 76
212691 meter/sec RA = 243
41574 deg
ZDOT = -5754
796112 TA = 343
25993
MA = 343
27572
Ha = 193
116 n
mi
Hp = 191
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5916086
19 X = 1739883
14
Y = 20704301
25 feet Y = 6330481
56 meter
Z = -4971633
99 Z = -1506748
11
XDOT = -16754
492960 XDOT = -5079
286919
YDOT = 250
041636 feet/sec YDOT = 19
259298 meter/sec
ZDOT = -18880
564673 ZDOT = -5779
537559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19014239
22 X = -5795540
11
Y = 10122684
91 feet Y = 3085394
36 meter
Z = -4937131
55 Z = -1504837
70
XDOT = -2968
119707 XDOT = -904
682887
YDOT = -14839
726024 feet/sec YDOT = -4523
148492 meter/sec
ZDOT = -18979
543412 ZDOT = -5784
964832
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 10235
89208863
00016717 00000-0 10270-3 0 9158
2 25544 51
6451 244
1496 0008098 288
9776 71
0508 15
71261973 34129
Satellite: ISS
Catalog Number: 25544
Epoch time: 10235
89208863 = yrday
fracday
Element set: 915
Inclination: 51
6451 deg
RA of node: 244
1496 deg
Eccentricity:
0008098
Arg of perigee: 288
9776 deg
Mean anomaly: 71
0508 deg
Mean motion: 15
71261973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3412
Checksum: 331
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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