Date:
December 3rd 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 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
There are no maneuvers
Coasting Arc #1 (Orbit 1486)
---------------------------------------
Vector Time (GMT): 2008/336/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4863965
47 A = 6736022
49 meter
Y = 3899566
24 meter E =
0018205
Z = 2537216
02 I = 51
37387
XDOT = -1563
607685 Wp = 86
81080
YDOT = 5396
518026 meter/sec RA = 237
69753 deg
ZDOT = -5263
164343 TA = 64
33907
MA = 64
15115
Ha = 195
763 n
mi
Hp = 185
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15957891
96 X = 4807672
92
Y = 12793852
49 feet Y = 3953642
83 meter
Z = 8324199
53 Z = 2560709
20
XDOT = -5129
946474 XDOT = -1598
268450
YDOT = 17705
111633 feet/sec YDOT = 5378
839763 meter/sec
ZDOT = -17267
599552 ZDOT = -5270
843904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14131829
04 X = -4307381
49
Y = 14734232
26 feet Y = 4490993
99 meter
Z = 8415645
12 Z = 2565088
63
XDOT = -16124
703543 XDOT = -4914
809640
YDOT = -5523
996000 feet/sec YDOT = -1683
713981 meter/sec
ZDOT = -17296
974948 ZDOT = -5272
117964
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 08336
57865414
00020000 00000-0 20000-3 0 9009
2 25544 51
6421 238
4243 0006420 48
2346 311
9364 15
71651545 14873
Satellite: ISS
Catalog Number: 25544
Epoch time: 08336
57865414 = yrday
fracday
Element set: 900
Inclination: 51
6421 deg
RA of node: 238
4243 deg
Eccentricity:
0006420
Arg of perigee: 48
2346 deg
Mean anomaly: 311
9364 deg
Mean motion: 15
71651545 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1487
Checksum: 284
Coasting Arc #2 (Orbit 1502)
---------------------------------------
Vector Time (GMT): 2008/337/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 187144
70 A = 6731183
04 meter
Y = -5259297
94 meter E =
0014860
Z = 4183285
22 I = 51
37459
XDOT = 6037
095186 Wp = 85
17519
YDOT = 3114
571177 meter/sec RA = 232
60746 deg
ZDOT = 3635
773871 TA = 327
62187
MA = 327
71298
Ha = 195
774 n
mi
Hp = 185
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 613991
80 X = 225619
31
Y = -17254914
50 feet Y = -5256990
56 meter
Z = 13724689
05 Z = 4184287
20
XDOT = 19806
742736 XDOT = 5984
156773
YDOT = 10218
409373 feet/sec YDOT = 3181
785036 meter/sec
ZDOT = 11928
391965 ZDOT = 3664
974112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17174988
49 X = 5234936
49
Y = 1741678
96 feet Y = 530863
75 meter
Z = 13728163
56 Z = 4184344
25
XDOT = -11448
172878 XDOT = -3489
403093
YDOT = 17721
683190 feet/sec YDOT = 5401
569036 meter/sec
ZDOT = 12041
932775 ZDOT = 3670
381110
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 08337
59598839
00020000 00000-0 20000-3 0 9017
2 25544 51
6422 233
2176 0006453 50
7882 309
3852 15
71679152 15037
Satellite: ISS
Catalog Number: 25544
Epoch time: 08337
59598839 = yrday
fracday
Element set: 901
Inclination: 51
6422 deg
RA of node: 233
2176 deg
Eccentricity:
0006453
Arg of perigee: 50
7882 deg
Mean anomaly: 309
3852 deg
Mean motion: 15
71679152 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1503
Checksum: 306
Coasting Arc #3 (Orbit 1517)
---------------------------------------
Vector Time (GMT): 2008/338/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5405846
76 A = 6732533
14 meter
Y = -1467037
01 meter E =
0011192
Z = -3742646
61 I = 51
39817
XDOT = -1208
446047 Wp = 78
08284
YDOT = -6306
725209 meter/sec RA = 227
42038 deg
ZDOT = 4230
512649 TA = 236
60958
MA = 236
71671
Ha = 195
673 n
mi
Hp = 185
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17735717
72 X = -5370859
10
Y = -4813113
55 feet Y = -1527292
30 meter
Z = -12279024
33 Z = -3768823
58
XDOT = -3964
718003 XDOT = -1158
384617
YDOT = -20691
355673 feet/sec YDOT = -6319
959281 meter/sec
ZDOT = 13879
634674 ZDOT = 4224
762922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5739816
16 X = 1749495
97
Y = -17385872
01 feet Y = -5299213
79 meter
Z = -12380716
80 Z = -3773642
48
XDOT = 19608
204991 XDOT = 5976
580881
YDOT = -3364
138218 feet/sec YDOT = -1025
389329 meter/sec
ZDOT = 13856
820991 ZDOT = 4223
559038
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 08338
54972666
00020000 00000-0 20000-3 0 9028
2 25544 51
6419 228
3364 0006304 52
7936 307
3800 15
71708692 15183
Satellite: ISS
Catalog Number: 25544
Epoch time: 08338
54972666 = yrday
fracday
Element set: 902
Inclination: 51
6419 deg
RA of node: 228
3364 deg
Eccentricity:
0006304
Arg of perigee: 52
7936 deg
Mean anomaly: 307
3800 deg
Mean motion: 15
71708692 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1518
Checksum: 303
Coasting Arc #4 (Orbit 1533)
---------------------------------------
Vector Time (GMT): 2008/339/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2280980
89 A = 6734398
57 meter
Y = 5494764
04 meter E =
0009908
Z = -3166488
06 I = 51
42468
XDOT = -5993
787769 Wp = 75
94656
YDOT = -275
474125 meter/sec RA = 222
33647 deg
ZDOT = -4805
865778 TA = 140
99309
MA = 140
92158
Ha = 195
717 n
mi
Hp = 185
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7483533
12 X = 2234750
37
Y = 18027441
08 feet Y = 5520013
07 meter
Z = -10388740
36 Z = -3155518
79
XDOT = -19664
658035 XDOT = -5966
915683
YDOT = -903
786498 feet/sec YDOT = -342
349462 meter/sec
ZDOT = -15767
276175 ZDOT = -4834
918590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18284784
74 X = -5573202
39
Y = 6895678
33 feet Y = 2101802
76 meter
Z = -10345728
28 Z = -3153377
98
XDOT = 2103
986602 XDOT = 641
295116
YDOT = -18195
686773 feet/sec YDOT = -5546
045328 meter/sec
ZDOT = -15880
042629 ZDOT = -4840
236993
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 08339
56703573
00020000 00000-0 20000-3 0 9031
2 25544 51
6415 223
1294 0006160 56
7785 303
3967 15
71708453 15343
Satellite: ISS
Catalog Number: 25544
Epoch time: 08339
56703573 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 223
1294 deg
Eccentricity:
0006160
Arg of perigee: 56
7785 deg
Mean anomaly: 303
3967 deg
Mean motion: 15
71708453 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1534
Checksum: 296
Coasting Arc #5 (Orbit 1549)
---------------------------------------
Vector Time (GMT): 2008/340/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4816038
06 A = 6729180
09 meter
Y = -948001
36 meter E =
0014425
Z = 4595360
41 I = 51
43090
XDOT = 3964
028165 Wp = 62
23791
YDOT = 5924
218602 meter/sec RA = 217
15591 deg
ZDOT = -2918
653406 TA = 56
82044
MA = 56
68217
Ha = 195
519 n
mi
Hp = 185
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15800649
80 X = 4803957
16
Y = -3110240
67 feet Y = -894213
51 meter
Z = 15076641
76 Z = 4618727
56
XDOT = 13005
341750 XDOT = 3911
666407
YDOT = 19436
412735 feet/sec YDOT = 5968
254100 meter/sec
ZDOT = -9575
634534 ZDOT = -2899
522711
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2819596
74 X = 859413
09
Y = 15768437
61 feet Y = 4806219
78 meter
Z = 15167251
16 Z = 4622978
15
XDOT = -18524
159256 XDOT = -5646
163741
YDOT = 12493
678643 feet/sec YDOT = 3808
073251 meter/sec
ZDOT = -9500
905211 ZDOT = -2895
875908
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 08340
58433034
00020000 00000-0 20000-3 0 9048
2 25544 51
6417 217
9221 0006229 59
1901 300
9873 15
71793277 15504
Satellite: ISS
Catalog Number: 25544
Epoch time: 08340
58433034 = yrday
fracday
Element set: 904
Inclination: 51
6417 deg
RA of node: 217
9221 deg
Eccentricity:
0006229
Arg of perigee: 59
1901 deg
Mean anomaly: 300
9873 deg
Mean motion: 15
71793277 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1550
Checksum: 284
Coasting Arc #6 (Orbit 1565)
---------------------------------------
Vector Time (GMT): 2008/341/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4529102
65 A = 6736998
31 meter
Y = -4604618
33 meter E =
0020262
Z = 1881885
60 I = 51
48028
XDOT = 4719
752270 Wp = 65
85010
YDOT = -2327
237176 meter/sec RA = 212
06295 deg
ZDOT = 5625
311906 TA = 315
09916
MA = 315
26288
Ha = 195
662 n
mi
Hp = 185
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14859260
67 X = -4486418
43
Y = -15107015
51 feet Y = -4655026
84 meter
Z = 6174165
34 Z = 1859986
29
XDOT = 15484
751542 XDOT = 4718
097898
YDOT = -7635
292573 feet/sec YDOT = -2274
467790 meter/sec
ZDOT = 18455
747722 ZDOT = 5648
236618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15125592
19 X = 4610280
50
Y = -14875582
42 feet Y = -4534077
52 meter
Z = 6088790
63 Z = 1855863
39
XDOT = 6531
108333 XDOT = 1990
681820
YDOT = 14284
972975 feet/sec YDOT = 4354
059763 meter/sec
ZDOT = 18544
532072 ZDOT = 5652
373375
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 08341
60161407
00020000 00000-0 20000-3 0 9055
2 25544 51
6409 212
7147 0006161 63
4983 296
6811 15
71787724 15668
Satellite: ISS
Catalog Number: 25544
Epoch time: 08341
60161407 = yrday
fracday
Element set: 905
Inclination: 51
6409 deg
RA of node: 212
7147 deg
Eccentricity:
0006161
Arg of perigee: 63
4983 deg
Mean anomaly: 296
6811 deg
Mean motion: 15
71787724 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1566
Checksum: 295
Coasting Arc #7 (Orbit 1580)
---------------------------------------
Vector Time (GMT): 2008/342/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3228139
23 A = 6726991
65 meter
Y = 2944201
78 meter E =
0019560
Z = -5131869
43 I = 51
47152
XDOT = -6170
167684 Wp = 90
61509
YDOT = -4364
421136 meter/sec RA = 206
90318 deg
ZDOT = 1381
689043 TA = 192
65054
MA = 192
69970
Ha = 195
663 n
mi
Hp = 184
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10591007
98 X = -3235891
70
Y = 9659454
66 feet Y = 2908059
85 meter
Z = -16836841
95 Z = -5147570
65
XDOT = -20243
332298 XDOT = -6127
617548
YDOT = -14318
966982 feet/sec YDOT = -4433
181703 meter/sec
ZDOT = 4533
100536 ZDOT = 1351
816885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9825434
98 X = -2994792
58
Y = -10338646
66 feet Y = -3151219
50 meter
Z = -16897543
43 Z = -5150371
24
XDOT = 13239
914477 XDOT = 4035
525933
YDOT = -19778
377023 feet/sec YDOT = -6028
449317 meter/sec
ZDOT = 4416
792801 ZDOT = 1346
238446
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 08342
55530628
00020000 00000-0 20000-3 0 9066
2 25544 51
6400 207
8322 0006196 66
9579 293
2236 15
71797454 15818
Satellite: ISS
Catalog Number: 25544
Epoch time: 08342
55530628 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 207
8322 deg
Eccentricity:
0006196
Arg of perigee: 66
9579 deg
Mean anomaly: 293
2236 deg
Mean motion: 15
71797454 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1581
Checksum: 306
Coasting Arc #8 (Orbit 1596)
---------------------------------------
Vector Time (GMT): 2008/343/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6065391
80 A = 6738367
51 meter
Y = 2878964
95 meter E =
0014649
Z = -530620
83 I = 51
53642
XDOT = -2477
354461 Wp = 116
21681
YDOT = 4138
941868 meter/sec RA = 201
79198 deg
ZDOT = -5995
544023 TA = 69
55813
MA = 69
40089
Ha = 195
710 n
mi
Hp = 185
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19899579
39 X = 6035325
66
Y = 9445423
06 feet Y = 2946623
60 meter
Z = -1740881
99 Z = -501227
30
XDOT = -8127
803351 XDOT = -2494
326746
YDOT = 13579
205603 feet/sec YDOT = 4111
144234 meter/sec
ZDOT = -19670
420022 ZDOT = -6007
620178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8780298
27 X = -2676234
91
Y = 20211399
12 feet Y = 6160434
45 meter
Z = -1626546
81 Z = -495771
47
XDOT = -12363
361658 XDOT = -3768
352633
YDOT = -6919
818000 feet/sec YDOT = -2109
160526 meter/sec
ZDOT = -19716
957307 ZDOT = -6009
728587
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 08343
57256590
00020000 00000-0 20000-3 0 9073
2 25544 51
6399 202
6258 0006160 71
1468 289
0362 15
71789360 15979
Satellite: ISS
Catalog Number: 25544
Epoch time: 08343
57256590 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 202
6258 deg
Eccentricity:
0006160
Arg of perigee: 71
1468 deg
Mean anomaly: 289
0362 deg
Mean motion: 15
71789360 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1597
Checksum: 314
Coasting Arc #9 (Orbit 1612)
---------------------------------------
Vector Time (GMT): 2008/344/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 971308
73 A = 6726389
62 meter
Y = -4071479
83 meter E =
0008453
Z = 5258117
10 I = 51
52313
XDOT = 7424
947175 Wp = 82
72398
YDOT = 2045
446150 meter/sec RA = 196
66161 deg
ZDOT = 213
019798 TA = 5
25647
MA = 5
24760
Ha = 195
673 n
mi
Hp = 184
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3186708
44 X = 991220
88
Y = -13357873
46 feet Y = -4060507
31 meter
Z = 17251040
35 Z = 5262883
77
XDOT = 24360
062911 XDOT = 7400
487981
YDOT = 6710
781332 feet/sec YDOT = 2128
339425 meter/sec
ZDOT = 698
883851 ZDOT = 249
031888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13496166
64 X = 4113631
59
Y = 2411226
11 feet Y = 734941
72 meter
Z = 17269214
28 Z = 5263656
51
XDOT = -5300
555226 XDOT = -1615
609233
YDOT = 23678
391011 feet/sec YDOT = 7217
173580 meter/sec
ZDOT = 838
853783 ZDOT = 255
682633
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 08344
58981278
00020000 00000-0 20000-3 0 9084
2 25544 51
6391 197
4178 0006185 74
7094 285
4752 15
71800678 16132
Satellite: ISS
Catalog Number: 25544
Epoch time: 08344
58981278 = yrday
fracday
Element set: 908
Inclination: 51
6391 deg
RA of node: 197
4178 deg
Eccentricity:
0006185
Arg of perigee: 74
7094 deg
Mean anomaly: 285
4752 deg
Mean motion: 15
71800678 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1613
Checksum: 328
Coasting Arc #10 (Orbit 1627)
---------------------------------------
Vector Time (GMT): 2008/345/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6643736
60 A = 6737975
65 meter
Y = -629771
65 meter E =
0015235
Z = -895869
00 I = 51
58964
XDOT = -328
639337 Wp = 53
71794
YDOT = -4877
502769 meter/sec RA = 191
52505 deg
ZDOT = 5944
746661 TA = 296
50610
MA = 296
66225
Ha = 195
604 n
mi
Hp = 184
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21797036
09 X = -6631848
53
Y = -2066179
96 feet Y = -703999
16 meter
Z = -2939202
75 Z = -928116
28
XDOT = -1078
213048 XDOT = -302
953085
YDOT = -16002
305673 feet/sec YDOT = -4881
035006 meter/sec
ZDOT = 19503
762010 ZDOT = 5943
211811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 591247
82 X = 180212
34
Y = -21869575
43 feet Y = -6665846
59 meter
Z = -3064456
16 Z = -934046
24
XDOT = 14290
486814 XDOT = 4355
740381
YDOT = -2310
960435 feet/sec YDOT = -704
380741 meter/sec
ZDOT = 19497
411161 ZDOT = 5942
810922
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 08345
54346940
00020000 00000-0 20000-3 0 9093
2 25544 51
6377 192
5351 0006099 77
9298 282
2547 15
71830115 16282
Satellite: ISS
Catalog Number: 25544
Epoch time: 08345
54346940 = yrday
fracday
Element set: 909
Inclination: 51
6377 deg
RA of node: 192
5351 deg
Eccentricity:
0006099
Arg of perigee: 77
9298 deg
Mean anomaly: 282
2547 deg
Mean motion: 15
71830115 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1628
Checksum: 317
Coasting Arc #11 (Orbit 1643)
---------------------------------------
Vector Time (GMT): 2008/346/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1520630
85 A = 6727304
52 meter
Y = 4199989
58 meter E =
0019494
Z = -5047781
58 I = 51
58176
XDOT = -7453
790333 Wp = 78
71740
YDOT = 573
500015 meter/sec RA = 186
42525 deg
ZDOT = -1770
284133 TA = 174
19014
MA = 174
16750
Ha = 195
645 n
mi
Hp = 184
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4988946
37 X = 1498074
57
Y = 13779493
39 feet Y = 4216868
90 meter
Z = -16560963
18 Z = -5040448
27
XDOT = -24454
692693 XDOT = -7451
049421
YDOT = 1881
561728 feet/sec YDOT = 490
163049 meter/sec
ZDOT = -5808
018810 ZDOT = -1806
488642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13299439
27 X = -4053669
09
Y = 6232361
61 feet Y = 1899623
82 meter
Z = -16532153
80 Z = -5039000
48
XDOT = -3487
681787 XDOT = -1063
045409
YDOT = -23204
130256 feet/sec YDOT = -7072
618902 meter/sec
ZDOT = -5948
560765 ZDOT = -1813
121321
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 08346
56069219
00020000 00000-0 20000-3 0 9109
2 25544 51
6366 187
3271 0006209 82
4987 277
6880 15
71860301 16448
Satellite: ISS
Catalog Number: 25544
Epoch time: 08346
56069219 = yrday
fracday
Element set: 910
Inclination: 51
6366 deg
RA of node: 187
3271 deg
Eccentricity:
0006209
Arg of perigee: 82
4987 deg
Mean anomaly: 277
6880 deg
Mean motion: 15
71860301 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1644
Checksum: 309
Coasting Arc #12 (Orbit 1659)
---------------------------------------
Vector Time (GMT): 2008/347/13:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6163355
60 A = 6735982
81 meter
Y = -1589534
70 meter E =
0019637
Z = 2180483
77 I = 51
64136
XDOT = 3096
971244 Wp = 101
77684
YDOT = 4418
645097 meter/sec RA = 181
26926 deg
ZDOT = -5495
166182 TA = 53
81104
MA = 53
62959
Ha = 195
443 n
mi
Hp = 184
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20220982
93 X = 6170079
42
Y = -5215008
84 feet Y = -1520575
31 meter
Z = 7153818
16 Z = 2210441
79
XDOT = 10160
666812 XDOT = 3074
025937
YDOT = 14496
867117 feet/sec YDOT = 4453
149979 meter/sec
ZDOT = -18028
760440 ZDOT = -5480
175778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7241805
10 X = 2207302
20
Y = 19543907
02 feet Y = 5956982
86 meter
Z = 7270043
99 Z = 2215909
41
XDOT = -11951
478286 XDOT = -3642
810582
YDOT = 11158
325652 feet/sec YDOT = 3401
057659 meter/sec
ZDOT = -17970
193376 ZDOT = -5477
314941
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 08347
57790032
00020000 00000-0 20000-3 0 9116
2 25544 51
6368 182
1188 0005996 84
4206 275
7640 15
71919122 16605
Satellite: ISS
Catalog Number: 25544
Epoch time: 08347
57790032 = yrday
fracday
Element set: 911
Inclination: 51
6368 deg
RA of node: 182
1188 deg
Eccentricity:
0005996
Arg of perigee: 84
4206 deg
Mean anomaly: 275
7640 deg
Mean motion: 15
71919122 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1660
Checksum: 303
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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