Date:
October 2nd 2008
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) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
276/11:35:20
275 -0
2 2
2 2
2
N/A 1
5 -0
1 195
0
000/00:04:40
551 -1
7 -0
1 186
2
Coasting Arc #1 (Orbit 526)
---------------------------------------
Vector Time (GMT): 2008/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628687
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6131363
95 A = 6735950
00 meter
Y = -2330551
17 meter E =
0013243
Z = 1519028
54 I = 51
59911
XDOT = 3002
496498 Wp = 87
11303
YDOT = -4108
198254 meter/sec RA = 190
23503 deg
ZDOT = 5773
705237 TA = 289
61839
MA = 289
76129
Ha = 193
894 n
mi
Hp = 185
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20116023
46 X = -6112226
98
Y = -7646165
25 feet Y = -2399008
52 meter
Z = 4983689
43 Z = 1489288
37
XDOT = 9850
710296 XDOT = 3020
163654
YDOT = -13478
340729 feet/sec YDOT = -4074
523446 meter/sec
ZDOT = 18942
602482 ZDOT = 5788
334862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21154381
50 X = 6447855
48
Y = 4092252
23 feet Y = 1247318
48 meter
Z = 4868369
18 Z = 1483878
92
XDOT = -6997
716194 XDOT = -2132
903896
YDOT = 13401
874005 feet/sec YDOT = 4084
891197 meter/sec
ZDOT = 18998
776519 ZDOT = 5790
827083
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 08275
56067464
00020000 00000-0 20000-3 0 9009
2 25544 51
6413 190
9185 0005976 171
8792 188
2468 15
72342544 5275
Satellite: ISS
Catalog Number: 25544
Epoch time: 08275
56067464 = yrday
fracday
Element set: 900
Inclination: 51
6413 deg
RA of node: 190
9185 deg
Eccentricity:
0005976
Arg of perigee: 171
8792 deg
Mean anomaly: 188
2468 deg
Mean motion: 15
72342544 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 527
Checksum: 316
Coasting Arc #2 (Orbit 541)
---------------------------------------
Vector Time (GMT): 2008/276/11:37:40
551
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6428231
44 A = 6737440
94 meter
Y = 1561088
06 meter E =
0016302
Z = -1229753
66 I = 51
62902
XDOT = -2201
574909 Wp = 158
77067
YDOT = 4469
631095 meter/sec RA = 185
18581 deg
ZDOT = -5873
361288 TA = 34
71035
MA = 34
60408
Ha = 194
967 n
mi
Hp = 186
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21089998
15 X = 6416271
39
Y = 5121679
99 feet Y = 1632905
33 meter
Z = -4034624
88 Z = -1198553
74
XDOT = -7223
014792 XDOT = -2222
859046
YDOT = 14664
144014 feet/sec YDOT = 4444
892536 meter/sec
ZDOT = -19269
558031 ZDOT = -5884
108686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21491517
26 X = -6550614
46
Y = -3177299
70 feet Y = -968440
95 meter
Z = -3913729
47 Z = -1192904
74
XDOT = 5515
530890 XDOT = 1681
133815
YDOT = -13683
782045 feet/sec YDOT = -4170
816767 meter/sec
ZDOT = -19310
678965 ZDOT = -5885
894948
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 08276
51401835
00020000 00000-0 20000-3 0 9010
2 25544 51
6414 186
0346 0007817 177
4923 182
6279 15
71936842 5429
Satellite: ISS
Catalog Number: 25544
Epoch time: 08276
51401835 = yrday
fracday
Element set: 901
Inclination: 51
6414 deg
RA of node: 186
0346 deg
Eccentricity:
0007817
Arg of perigee: 177
4923 deg
Mean anomaly: 182
6279 deg
Mean motion: 15
71936842 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 542
Checksum: 301
Coasting Arc #3 (Orbit 557)
---------------------------------------
Vector Time (GMT): 2008/277/11:37:40
551
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 727160
64 A = 6725877
11 meter
Y = -4149858
43 meter E =
0006904
Z = 5240274
07 I = 51
61961
XDOT = 7654
895157 Wp = 160
73703
YDOT = 523
995716 meter/sec RA = 180
04839 deg
ZDOT = -653
419907 TA = 295
44138
MA = 295
51280
Ha = 194
645 n
mi
Hp = 186
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2385697
64 X = 748054
12
Y = -13615021
08 feet Y = -4141609
93 meter
Z = 17192500
23 Z = 5243857
56
XDOT = 25114
485423 XDOT = 7651
641084
YDOT = 1719
146051 feet/sec YDOT = 609
578960 meter/sec
ZDOT = -2143
766098 ZDOT = -616
239535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -800542
98 X = -244005
50
Y = 13782498
20 feet Y = 4200905
45 meter
Z = 17205937
66 Z = 5244369
80
XDOT = -24159
817146 XDOT = -7363
912266
YDOT = 1068
060342 feet/sec YDOT = 325
544792 meter/sec
ZDOT = -1999
824280 ZDOT = -609
546440
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 08277
53116394
00020000 00000-0 20000-3 0 9027
2 25544 51
6408 180
8273 0007719 182
3335 177
7793 15
72016134 5583
Satellite: ISS
Catalog Number: 25544
Epoch time: 08277
53116394 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 180
8273 deg
Eccentricity:
0007719
Arg of perigee: 182
3335 deg
Mean anomaly: 177
7793 deg
Mean motion: 15
72016134 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 558
Checksum: 302
Coasting Arc #4 (Orbit 572)
---------------------------------------
Vector Time (GMT): 2008/278/11:37:40
551
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6704756
20 A = 6737866
20 meter
Y = 657001
26 meter E =
0007724
Z = -78849
70 I = 51
68926
XDOT = -529
488251 Wp = 83
28262
YDOT = -4739
786694 meter/sec RA = 174
93326 deg
ZDOT = 6035
044304 TA = 275
86276
MA = 275
95081
Ha = 194
551 n
mi
Hp = 186
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21997231
62 X = -6711221
53
Y = 2155515
96 feet Y = 581988
66 meter
Z = -258693
24 Z = -111437
77
XDOT = -1737
166177 XDOT = -505
765579
YDOT = -15550
481280 feet/sec YDOT = -4745
575020 meter/sec
ZDOT = 19800
014120 ZDOT = 6032
529683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21552020
12 X = 6569055
73
Y = -4894258
17 feet Y = -1491769
89 meter
Z = -384753
89 Z = -117272
98
XDOT = 3427
384293 XDOT = 1044
666733
YDOT = 13624
424091 feet/sec YDOT = 4152
724463 meter/sec
ZDOT = 19789
793153 ZDOT = 6031
928953
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 08278
48472501
00020000 00000-0 20000-3 0 9038
2 25544 51
6409 175
9446 0007670 185
4376 174
6704 15
71997818 5737
Satellite: ISS
Catalog Number: 25544
Epoch time: 08278
48472501 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 175
9446 deg
Eccentricity:
0007670
Arg of perigee: 185
4376 deg
Mean anomaly: 174
6704 deg
Mean motion: 15
71997818 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 573
Checksum: 327
Coasting Arc #5 (Orbit 588)
---------------------------------------
Vector Time (GMT): 2008/279/11:37:40
551
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1607851
33 A = 6725900
30 meter
Y = 3916539
77 meter E =
0014579
Z = -5236921
96 I = 51
67894
XDOT = -7388
521301 Wp = 114
23095
YDOT = 1970
518574 meter/sec RA = 169
82378 deg
ZDOT = -802
359180 TA = 148
16945
MA = 148
08125
Ha = 194
354 n
mi
Hp = 186
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5275102
78 X = 1589376
91
Y = 12849539
93 feet Y = 3934416
38 meter
Z = -17181502
48 Z = -5229155
77
XDOT = -24240
555450 XDOT = -7406
109039
YDOT = 6464
955950 feet/sec YDOT = 1887
797523 meter/sec
ZDOT = -2632
412007 ZDOT = -838
295969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7147688
10 X = -2178615
33
Y = -11953819
63 feet Y = -3643524
22 meter
Z = -17151039
75 Z = -5227636
92
XDOT = 22186
561622 XDOT = 6762
463982
YDOT = -9325
954274 feet/sec YDOT = -2842
550863 meter/sec
ZDOT = -2771
314718 ZDOT = -844
696726
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 08279
50183864
00020000 00000-0 20000-3 0 9044
2 25544 51
6414 170
7363 0007652 189
3699 170
7322 15
72049899 5893
Satellite: ISS
Catalog Number: 25544
Epoch time: 08279
50183864 = yrday
fracday
Element set: 904
Inclination: 51
6414 deg
RA of node: 170
7363 deg
Eccentricity:
0007652
Arg of perigee: 189
3699 deg
Mean anomaly: 170
7322 deg
Mean motion: 15
72049899 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 589
Checksum: 329
Coasting Arc #6 (Orbit 604)
---------------------------------------
Vector Time (GMT): 2008/280/11:37:40
551
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6006287
92 A = 6737015
79 meter
Y = -2723523
45 meter E =
0017868
Z = 1320037
52 I = 51
74464
XDOT = 3081
417626 Wp = 144
99965
YDOT = 3944
746769 meter/sec RA = 164
68888 deg
ZDOT = -5857
301957 TA = 20
52648
MA = 20
45477
Ha = 194
277 n
mi
Hp = 186
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19705669
04 X = 6029883
80
Y = -8935444
38 feet Y = -2656225
74 meter
Z = 4330831
75 Z = 1349273
81
XDOT = 10109
637881 XDOT = 3065
531941
YDOT = 12942
082576 feet/sec YDOT = 3979
116128 meter/sec
ZDOT = -19216
869937 ZDOT = -5842
370806
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18005322
23 X = -5488022
22
Y = 11957142
41 feet Y = 3644537
01 meter
Z = 4443734
80 Z = 1354450
37
XDOT = -11279
280387 XDOT = -3437
924662
YDOT = -9835
306707 feet/sec YDOT = -2997
801484 meter/sec
ZDOT = -19158
664947 ZDOT = -5839
561076
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 08280
51893664
00020000 00000-0 20000-3 0 9054
2 25544 51
6412 165
5284 0007775 193
1253 166
9708 15
72025092 6053
Satellite: ISS
Catalog Number: 25544
Epoch time: 08280
51893664 = yrday
fracday
Element set: 905
Inclination: 51
6412 deg
RA of node: 165
5284 deg
Eccentricity:
0007775
Arg of perigee: 193
1253 deg
Mean anomaly: 166
9708 deg
Mean motion: 15
72025092 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 605
Checksum: 299
Coasting Arc #7 (Orbit 620)
---------------------------------------
Vector Time (GMT): 2008/281/11:37:40
551
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3652174
31 A = 6727237
10 meter
Y = -2780595
97 meter E =
0011215
Z = 4918815
81 I = 51
74046
XDOT = 6115
949517 Wp = 163
82469
YDOT = -4123
384724 meter/sec RA = 159
60557 deg
ZDOT = 2198
335749 TA = 264
78083
MA = 264
90882
Ha = 194
092 n
mi
Hp = 187
010
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11982199
18 X = -3644704
80
Y = -9122690
18 feet Y = -2821394
89 meter
Z = 16137847
14 Z = 4901091
50
XDOT = 20065
451172 XDOT = 6150
924073
YDOT = -13528
165106 feet/sec YDOT = -4054
797078 meter/sec
ZDOT = 7212
387628 ZDOT = 2228
132367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13493667
41 X = 4112869
83
Y = 6851040
79 feet Y = 2088197
23 meter
Z = 16068940
96 Z = 4897813
20
XDOT = -16825
595043 XDOT = -5128
441369
YDOT = 15862
404351 feet/sec YDOT = 4834
860846 meter/sec
ZDOT = 7327
330405 ZDOT = 2233
370307
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 08281
53601553
00020000 00000-0 20000-3 0 9062
2 25544 51
6416 160
3200 0007608 197
8283 162
2613 15
72081536 6214
Satellite: ISS
Catalog Number: 25544
Epoch time: 08281
53601553 = yrday
fracday
Element set: 906
Inclination: 51
6416 deg
RA of node: 160
3200 deg
Eccentricity:
0007608
Arg of perigee: 197
8283 deg
Mean anomaly: 162
2613 deg
Mean motion: 15
72081536 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 621
Checksum: 268
Coasting Arc #8 (Orbit 635)
---------------------------------------
Vector Time (GMT): 2008/282/11:37:40
551
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4527354
73 A = 6734822
90 meter
Y = 4328597
15 meter E =
0003711
Z = -2481361
99 I = 51
79370
XDOT = -5064
415026 Wp = 163
37776
YDOT = -2236
132141 meter/sec RA = 154
45407 deg
ZDOT = 5337
919373 TA = 168
67194
MA = 168
66359
Ha = 193
777 n
mi
Hp = 187
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14853526
02 X = -4563367
19
Y = 14201434
21 feet Y = 4277768
25 meter
Z = -8140951
40 Z = -2503443
65
XDOT = -16615
534861 XDOT = -5064
964738
YDOT = -7336
391539 feet/sec YDOT = -2292
768324 meter/sec
ZDOT = 17512
858835 ZDOT = 5313
314912
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11783893
60 X = 3591730
77
Y = -16794511
97 feet Y = -5118967
25 meter
Z = -8226012
28 Z = -2507288
54
XDOT = 16593
425561 XDOT = 5057
676111
YDOT = 3109
293896 feet/sec YDOT = 947
712779 meter/sec
ZDOT = 17417
360666 ZDOT = 5308
811531
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 08282
48951181
00020000 00000-0 20000-3 0 9073
2 25544 51
6417 155
4368 0007571 202
8740 157
2086 15
72113053 6363
Satellite: ISS
Catalog Number: 25544
Epoch time: 08282
48951181 = yrday
fracday
Element set: 907
Inclination: 51
6417 deg
RA of node: 155
4368 deg
Eccentricity:
0007571
Arg of perigee: 202
8740 deg
Mean anomaly: 157
2086 deg
Mean motion: 15
72113053 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 636
Checksum: 288
Coasting Arc #9 (Orbit 651)
---------------------------------------
Vector Time (GMT): 2008/283/11:37:40
551
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5022712
22 A = 6729344
47 meter
Y = 1017661
74 meter E =
0005962
Z = -4363213
98 I = 51
80083
XDOT = -4090
105755 Wp = 127
38418
YDOT = 5547
824947 meter/sec RA = 149
38953 deg
ZDOT = -3421
091435 TA = 108
19482
MA = 108
12991
Ha = 193
664 n
mi
Hp = 187
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16478714
62 X = 5032155
15
Y = 3338785
23 feet Y = 1073881
24 meter
Z = -14315006
49 Z = -4338790
52
XDOT = -13418
982137 XDOT = -4135
219250
YDOT = 18201
525416 feet/sec YDOT = 5501
834652 meter/sec
ZDOT = -11224
053265 ZDOT = -3441
071135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16892346
26 X = -5148787
14
Y = 214312
09 feet Y = 65322
33 meter
Z = -14220324
93 Z = -4334355
04
XDOT = 9248
869878 XDOT = 2819
055539
YDOT = -19368
720808 feet/sec YDOT = -5903
586102 meter/sec
ZDOT = -11300
857519 ZDOT = -3444
501372
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 08283
50655823
00020000 00000-0 20000-3 0 9082
2 25544 51
6415 150
2283 0007618 207
9704 152
1050 15
72132828 6522
Satellite: ISS
Catalog Number: 25544
Epoch time: 08283
50655823 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 150
2283 deg
Eccentricity:
0007618
Arg of perigee: 207
9704 deg
Mean anomaly: 152
1050 deg
Mean motion: 15
72132828 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 652
Checksum: 276
Coasting Arc #10 (Orbit 667)
---------------------------------------
Vector Time (GMT): 2008/284/11:37:40
551
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2526418
43 A = 6732052
08 meter
Y = -5178949
91 meter E =
0010283
Z = 3467783
03 I = 51
83561
XDOT = 6199
505267 Wp = 125
78848
YDOT = -38
686644 meter/sec RA = 144
23134 deg
ZDOT = -4570
851688 TA = 13
22977
MA = 13
20283
Ha = 193
282 n
mi
Hp = 187
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8288774
38 X = 2567296
49
Y = -16991305
47 feet Y = -5150469
27 meter
Z = 11377240
90 Z = 3480156
08
XDOT = 20339
584209 XDOT = 6221
681696
YDOT = -126
924685 feet/sec YDOT = 30
763533 meter/sec
ZDOT = -14996
232573 ZDOT = -4540
680329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4154791
75 X = -1266380
52
Y = 18413728
20 feet Y = 5612504
36 meter
Z = 11424630
07 Z = 3482227
24
XDOT = -18521
225841 XDOT = -5645
269636
YDOT = 5059
855380 feet/sec YDOT = 1542
243920 meter/sec
ZDOT = -14879
391883 ZDOT = -4535
238646
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 08284
52358763
00020000 00000-0 20000-3 0 9099
2 25544 51
6417 145
0200 0007470 211
9434 148
1276 15
72195203 6684
Satellite: ISS
Catalog Number: 25544
Epoch time: 08284
52358763 = yrday
fracday
Element set: 909
Inclination: 51
6417 deg
RA of node: 145
0200 deg
Eccentricity:
0007470
Arg of perigee: 211
9434 deg
Mean anomaly: 148
1276 deg
Mean motion: 15
72195203 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 668
Checksum: 285
Coasting Arc #11 (Orbit 683)
---------------------------------------
Vector Time (GMT): 2008/285/11:37:40
551
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5591108
06 A = 6731940
53 meter
Y = 1115910
45 meter E =
0010223
Z = 3579191
95 I = 51
85684
XDOT = 1653
569095 Wp = 130
94703
YDOT = -6052
300723 meter/sec RA = 139
17465 deg
ZDOT = 4455
244883 TA = 271
58829
MA = 271
70538
Ha = 193
200 n
mi
Hp = 187
851
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18343530
39 X = -5620558
10
Y = 3661123
52 feet Y = 1053223
06 meter
Z = 11742755
76 Z = 3551958
39
XDOT = 5425
095455 XDOT = 1699
480953
YDOT = -19856
629667 feet/sec YDOT = -6033
552507 meter/sec
ZDOT = 14616
945154 ZDOT = 4463
390011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16964434
33 X = 5170759
58
Y = -8034937
69 feet Y = -2449049
01 meter
Z = 11637396
16 Z = 3547078
35
XDOT = -930
073700 XDOT = -283
486464
YDOT = 19322
452815 feet/sec YDOT = 5889
483618 meter/sec
ZDOT = 14647
874479 ZDOT = 4464
672141
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 08285
54060125
00020000 00000-0 20000-3 0 9106
2 25544 51
6408 139
8104 0007470 216
3554 143
7102 15
72170248 6849
Satellite: ISS
Catalog Number: 25544
Epoch time: 08285
54060125 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 139
8104 deg
Eccentricity:
0007470
Arg of perigee: 216
3554 deg
Mean anomaly: 143
7102 deg
Mean motion: 15
72170248 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 684
Checksum: 267
Coasting Arc #12 (Orbit 698)
---------------------------------------
Vector Time (GMT): 2008/286/11:37:40
551
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -367940
11 A = 6729347
13 meter
Y = 5198780
98 meter E =
0009298
Z = -4265043
49 I = 51
86924
XDOT = -6328
071238 Wp = 161
13399
YDOT = 2498
778383 meter/sec RA = 134
01747 deg
ZDOT = 3585
304361 TA = 145
24372
MA = 145
18295
Ha = 192
948 n
mi
Hp = 187
933
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1207152
60 X = -405327
20
Y = 17056368
03 feet Y = 5194457
04 meter
Z = -13992924
85 Z = -4266922
25
XDOT = -20761
388577 XDOT = -6372
959727
YDOT = 8198
091807 feet/sec YDOT = 2427
763568 meter/sec
ZDOT = 11762
809582 ZDOT = 3554
452804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3350033
96 X = -1021090
35
Y = -16762017
44 feet Y = -5109062
92 meter
Z = -13999674
91 Z = -4267100
91
XDOT = 16755
511475 XDOT = 5107
079898
YDOT = -13091
114376 feet/sec YDOT = -3990
171662 meter/sec
ZDOT = 11643
572540 ZDOT = 3548
960910
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 08286
49403358
00020000 00000-0 20000-3 0 9111
2 25544 51
6398 134
9263 0007608 220
2717 139
7882 15
72224204 6995
Satellite: ISS
Catalog Number: 25544
Epoch time: 08286
49403358 = yrday
fracday
Element set: 911
Inclination: 51
6398 deg
RA of node: 134
9263 deg
Eccentricity:
0007608
Arg of perigee: 220
2717 deg
Mean anomaly: 139
7882 deg
Mean motion: 15
72224204 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 699
Checksum: 308
Coasting Arc #13 (Orbit 713)
---------------------------------------
Vector Time (GMT): 2008/287/11:37:40
551
Vector Time (MET): N/A
Weight (LBS) : 628524
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5280508
81 A = 6734218
62 meter
Y = -3209516
21 meter E =
0008505
Z = -2663244
44 I = 51
90400
XDOT = 759
724430 Wp = 189
32255
YDOT = 5591
761680 meter/sec RA = 128
96023 deg
ZDOT = -5238
274526 TA = 20
87140
MA = 20
83670
Ha = 192
880 n
mi
Hp = 188
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17324503
95 X = 5328943
53
Y = -10529908
84 feet Y = -3150195
93 meter
Z = -8737678
62 Z = -2637473
21
XDOT = 2492
534218 XDOT = 722
587164
YDOT = 18345
674803 feet/sec YDOT = 5600
049251 meter/sec
ZDOT = -17185
940046 ZDOT = -5234
674401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13781153
03 X = -4200495
44
Y = 14927358
96 feet Y = 4549859
01 meter
Z = -8638183
87 Z = -2632918
44
XDOT = -6478
880012 XDOT = -1974
762628
YDOT = -15906
872402 feet/sec YDOT = -4848
414708 meter/sec
ZDOT = -17171
435126 ZDOT = -5233
853426
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 08287
51101245
00020000 00000-0 20000-3 0 9126
2 25544 51
6389 129
7177 0007655 224
6522 135
4025 15
72226715 7144
Satellite: ISS
Catalog Number: 25544
Epoch time: 08287
51101245 = yrday
fracday
Element set: 912
Inclination: 51
6389 deg
RA of node: 129
7177 deg
Eccentricity:
0007655
Arg of perigee: 224
6522 deg
Mean anomaly: 135
4025 deg
Mean motion: 15
72226715 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 714
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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