Date:
September 26th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 5 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 898)
---------------------------------------
Vector Time (GMT): 2006/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5932954
06 A = 6722031
98 meter
Y = -636412
61 meter E =
0020461
Z = 3091468
38 I = 51
80035
XDOT = -1969
753264 Wp = 61
37944
YDOT = -5606
637815 meter/sec RA = 30
18272 deg
ZDOT = -4900
435896 TA = 82
79128
MA = 82
55872
Ha = 190
471 n
mi
Hp = 177
802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19465072
37 X = -5940414
71
Y = -2087967
87 feet Y = -702799
71 meter
Z = 10142612
78 Z = 3062627
51
XDOT = -6462
445093 XDOT = -1883
106825
YDOT = -18394
481021 feet/sec YDOT = -5628
180527 meter/sec
ZDOT = -16077
545592 ZDOT = -4909
794306
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19610835
44 X = 5977382
64
Y = 912835
61 feet Y = 278232
30 meter
Z = 10035093
96 Z = 3058696
64
XDOT = 7532
652930 XDOT = 2295
952613
YDOT = 16548
590988 feet/sec YDOT = 5044
010533 meter/sec
ZDOT = -16113
155837 ZDOT = -4911
289899
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 06268
53801820
00020000 00000-0 20000-3 0 9008
2 25544 51
6359 30
5221 0012015 24
2426 335
9302 15
76137541 8994
Satellite: ISS
Catalog Number: 25544
Epoch time: 06268
53801820 = yrday
fracday
Element set: 900
Inclination: 51
6359 deg
RA of node: 30
5221 deg
Eccentricity:
0012015
Arg of perigee: 24
2426 deg
Mean anomaly: 335
9302 deg
Mean motion: 15
76137541 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 899
Checksum: 264
Coasting Arc #2 (Orbit 914)
---------------------------------------
Vector Time (GMT): 2006/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1295776
17 A = 6716355
80 meter
Y = 4654364
19 meter E =
0014488
Z = 4651530
18 I = 51
75814
XDOT = -7120
169545 Wp = 60
30926
YDOT = -858
986197 meter/sec RA = 25
08690 deg
ZDOT = 2843
453465 TA = 1
70638
MA = 1
70144
Ha = 190
392 n
mi
Hp = 177
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4251234
14 X = 1221037
40
Y = 15270223
72 feet Y = 4668436
59 meter
Z = 15260925
80 Z = 4657643
44
XDOT = -23360
136302 XDOT = -7123
848297
YDOT = -2818
196184 feet/sec YDOT = -938
628324 meter/sec
ZDOT = 9328
915566 ZDOT = 2808
854134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5333033
89 X = -1625508
73
Y = -14902920
61 feet Y = -4542410
20 meter
Z = 15284315
08 Z = 4658659
24
XDOT = 22472
167642 XDOT = 6849
516697
YDOT = 1392
050759 feet/sec YDOT = 424
297071 meter/sec
ZDOT = 9199
918078 ZDOT = 2804
135030
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 06269
55244982
00020000 00000-0 20000-3 0 9012
2 25544 51
6369 25
2954 0012081 27
5332 332
6469 15
76224223 9155
Satellite: ISS
Catalog Number: 25544
Epoch time: 06269
55244982 = yrday
fracday
Element set: 901
Inclination: 51
6369 deg
RA of node: 25
2954 deg
Eccentricity:
0012081
Arg of perigee: 27
5332 deg
Mean anomaly: 332
6469 deg
Mean motion: 15
76224223 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 915
Checksum: 289
Coasting Arc #3 (Orbit 929)
---------------------------------------
Vector Time (GMT): 2006/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6418125
90 A = 6724534
42 meter
Y = 809852
28 meter E =
0019777
Z = -1806569
70 I = 51
75932
XDOT = 944
198325 Wp = 33
10655
YDOT = 5112
099623 meter/sec RA = 19
90548 deg
ZDOT = 5691
364260 TA = 306
86669
MA = 307
04783
Ha = 190
636 n
mi
Hp = 177
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21056843
52 X = 6417369
17
Y = 2656995
66 feet Y = 881619
04 meter
Z = -5927065
96 Z = -1775391
73
XDOT = 3097
763532 XDOT = 859
315813
YDOT = 16771
980391 feet/sec YDOT = 5122
183692 meter/sec
ZDOT = 18672
454922 ZDOT = 5695
744967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21245802
48 X = -6475720
60
Y = -656239
80 feet Y = -200021
89 meter
Z = -5810819
39 Z = -1771137
75
XDOT = -4611
034198 XDOT = -1405
443223
YDOT = -14865
299493 feet/sec YDOT = -4530
943286 meter/sec
ZDOT = 18689
445785 ZDOT = 5696
543075
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 06270
50345897
00020000 00000-0 20000-3 0 9027
2 25544 51
6371 20
3959 0012326 30
7623 329
4261 15
76205574 9309
Satellite: ISS
Catalog Number: 25544
Epoch time: 06270
50345897 = yrday
fracday
Element set: 902
Inclination: 51
6371 deg
RA of node: 20
3959 deg
Eccentricity:
0012326
Arg of perigee: 30
7623 deg
Mean anomaly: 329
4261 deg
Mean motion: 15
76205574 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 930
Checksum: 278
Coasting Arc #4 (Orbit 945)
---------------------------------------
Vector Time (GMT): 2006/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -264941
25 A = 6714136
07 meter
Y = -4295855
58 meter E =
0024454
Z = -5173342
66 I = 51
69782
XDOT = 7525
656816 Wp = 59
22517
YDOT = 999
925075 meter/sec RA = 14
78627 deg
ZDOT = -1207
677784 TA = 199
18049
MA = 199
27272
Ha = 190
544 n
mi
Hp = 177
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -869229
81 X = -191753
13
Y = -14094014
36 feet Y = -4298409
10 meter
Z = -16972908
98 Z = -5174451
97
XDOT = 24690
475119 XDOT = 7519
782967
YDOT = 3280
594079 feet/sec YDOT = 1084
048290 meter/sec
ZDOT = -3962
197455 ZDOT = -1171
131818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2341158
34 X = 713585
06
Y = 13919641
66 feet Y = 4242706
78 meter
Z = -16977602
72 Z = -5174773
31
XDOT = -23908
574648 XDOT = -7287
333553
YDOT = -677
440841 feet/sec YDOT = -206
483968 meter/sec
ZDOT = -3825
927228 ZDOT = -1166
142619
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 06271
51784253
00020000 00000-0 20000-3 0 9033
2 25544 51
6373 15
1692 0012265 34
4352 325
7605 15
76258820 9469
Satellite: ISS
Catalog Number: 25544
Epoch time: 06271
51784253 = yrday
fracday
Element set: 903
Inclination: 51
6373 deg
RA of node: 15
1692 deg
Eccentricity:
0012265
Arg of perigee: 34
4352 deg
Mean anomaly: 325
7605 deg
Mean motion: 15
76258820 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 946
Checksum: 284
Coasting Arc #5 (Orbit 961)
---------------------------------------
Vector Time (GMT): 2006/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6657568
76 A = 6725605
51 meter
Y = -918801
99 meter E =
0017081
Z = 262567
82 I = 51
70871
XDOT = 406
090208 Wp = 86
09024
YDOT = -4763
119356 meter/sec RA = 9
62524 deg
ZDOT = -6034
113360 TA = 91
05873
MA = 90
86303
Ha = 190
582 n
mi
Hp = 176
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21842417
21 X = -6648075
31
Y = -3014442
23 feet Y = -993197
53 meter
Z = 861442
98 Z = 230247
99
XDOT = 1332
316955 XDOT = 488
634890
YDOT = -15627
032008 feet/sec YDOT = -4758
116652 meter/sec
ZDOT = -19796
959841 ZDOT = -6031
940083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22053072
41 X = 6721776
47
Y = 182117
35 feet Y = 55509
37 meter
Z = 740922
46 Z = 225833
17
XDOT = 591
804116 XDOT = 180
381894
YDOT = 14074
353876 feet/sec YDOT = 4289
863062 meter/sec
ZDOT = -19789
483468 ZDOT = -6031
834561
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 06272
53220063
00020000 00000-0 20000-3 0 9041
2 25544 51
6368 9
9418 0012333 38
7222 321
4824 15
76303048 9626
Satellite: ISS
Catalog Number: 25544
Epoch time: 06272
53220063 = yrday
fracday
Element set: 904
Inclination: 51
6368 deg
RA of node: 9
9418 deg
Eccentricity:
0012333
Arg of perigee: 38
7222 deg
Mean anomaly: 321
4824 deg
Mean motion: 15
76303048 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 962
Checksum: 269
Coasting Arc #6 (Orbit 977)
---------------------------------------
Vector Time (GMT): 2006/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -986465
82 A = 6713429
14 meter
Y = 4077197
52 meter E =
0015165
Z = 5233163
04 I = 51
64079
XDOT = -7615
764322 Wp = 45
44082
YDOT = -1066
427881 meter/sec RA = 4
47107 deg
ZDOT = -593
215599 TA = 50
25484
MA = 50
12132
Ha = 190
584 n
mi
Hp = 176
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3236436
41 X = -1057406
26
Y = 13376632
29 feet Y = 4065769
61 meter
Z = 17169170
09 Z = 5228198
48
XDOT = -24986
103417 XDOT = -7600
391598
YDOT = -3498
779136 feet/sec YDOT = -1151
505615 meter/sec
ZDOT = -1946
245405 ZDOT = -630
175963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1348806
43 X = 411116
20
Y = -13718823
22 feet Y = -4181497
32 meter
Z = 17151204
75 Z = 5227687
21
XDOT = 24217
879733 XDOT = 7381
609743
YDOT = -271
732998 feet/sec YDOT = -82
824218 meter/sec
ZDOT = -2084
078337 ZDOT = -635
227077
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 06273
54653110
00020000 00000-0 20000-3 0 9057
2 25544 51
6374 4
7139 0012417 41
7769 318
4342 15
76388021 9781
Satellite: ISS
Catalog Number: 25544
Epoch time: 06273
54653110 = yrday
fracday
Element set: 905
Inclination: 51
6374 deg
RA of node: 4
7139 deg
Eccentricity:
0012417
Arg of perigee: 41
7769 deg
Mean anomaly: 318
4342 deg
Mean motion: 15
76388021 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 978
Checksum: 290
Coasting Arc #7 (Orbit 993)
---------------------------------------
Vector Time (GMT): 2006/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6518514
71 A = 6724661
95 meter
Y = 942374
82 meter E =
0026382
Z = 1286460
50 I = 51
65020
XDOT = -1844
243497 Wp = 52
56814
YDOT = 4661
354468 meter/sec RA = 359
33645 deg
ZDOT = 5864
371993 TA = 321
58080
MA = 321
76838
Ha = 190
640 n
mi
Hp = 176
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21386203
12 X = 6501243
06
Y = 3091780
89 feet Y = 1015171
88 meter
Z = 4220670
95 Z = 1318085
63
XDOT = -6050
667641 XDOT = -1924
718522
YDOT = 15293
157704 feet/sec YDOT = 4640
281151 meter/sec
ZDOT = 19240
065593 ZDOT = 5855
217150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21581045
23 X = -6577902
59
Y = 421600
84 feet Y = 128503
94 meter
Z = 4338616
78 Z = 1322410
39
XDOT = 3619
910842 XDOT = 1103
348825
YDOT = -14516
564970 feet/sec YDOT = -4424
649003 meter/sec
ZDOT = 19206
565421 ZDOT = 5854
161140
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 06274
56083868
00020000 00000-0 20000-3 0 9068
2 25544 51
6374 359
4869 0012579 45
8012 314
4184 15
76382184 9948
Satellite: ISS
Catalog Number: 25544
Epoch time: 06274
56083868 = yrday
fracday
Element set: 906
Inclination: 51
6374 deg
RA of node: 359
4869 deg
Eccentricity:
0012579
Arg of perigee: 45
8012 deg
Mean anomaly: 314
4184 deg
Mean motion: 15
76382184 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 994
Checksum: 328
Coasting Arc #8 (Orbit 1008)
---------------------------------------
Vector Time (GMT): 2006/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2229934
13 A = 6715053
78 meter
Y = -4093759
54 meter E =
0021583
Z = -4849533
17 I = 51
58932
XDOT = 7226
882481 Wp = 77
08338
YDOT = 1147
177609 meter/sec RA = 354
15021 deg
ZDOT = 2368
253778 TA = 215
98328
MA = 216
12879
Ha = 190
656 n
mi
Hp = 176
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7316056
87 X = 2299103
58
Y = -13430969
62 feet Y = -4068436
52 meter
Z = -15910541
88 Z = -4838532
04
XDOT = 23710
244359 XDOT = 7202
012898
YDOT = 3763
706067 feet/sec YDOT = 1227
853602 meter/sec
ZDOT = 7769
861475 ZDOT = 2403
301595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4872850
27 X = -1485244
76
Y = 14541544
64 feet Y = 4432262
81 meter
Z = -15870090
91 Z = -4837203
71
XDOT = -22897
809231 XDOT = -6979
252253
YDOT = 900
733820 feet/sec YDOT = 274
543668 meter/sec
ZDOT = 7900
590474 ZDOT = 2408
099977
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 06275
51172671
00020000 00000-0 20000-3 0 9076
2 25544 51
6368 354
5865 0012652 49
2115 311
0145 15
76444672 10096
Satellite: ISS
Catalog Number: 25544
Epoch time: 06275
51172671 = yrday
fracday
Element set: 907
Inclination: 51
6368 deg
RA of node: 354
5865 deg
Eccentricity:
0012652
Arg of perigee: 49
2115 deg
Mean anomaly: 311
0145 deg
Mean motion: 15
76444672 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1009
Checksum: 284
Coasting Arc #9 (Orbit 1024)
---------------------------------------
Vector Time (GMT): 2006/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6004780
19 A = 6721630
62 meter
Y = -1118932
60 meter E =
0015272
Z = -2825369
64 I = 51
58314
XDOT = 3272
147788 Wp = 68
29423
YDOT = -4746
566521 meter/sec RA = 349
03455 deg
ZDOT = -5090
960469 TA = 144
10532
MA = 144
00262
Ha = 190
672 n
mi
Hp = 175
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19700722
39 X = -5978096
69
Y = -3671038
71 feet Y = -1185932
31 meter
Z = -9269585
44 Z = -2854476
02
XDOT = 10735
393006 XDOT = 3349
712346
YDOT = -15572
724806 feet/sec YDOT = -4709
542098 meter/sec
ZDOT = -16702
626211 ZDOT = -5074
875743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19987565
12 X = 6092209
85
Y = -259304
82 feet Y = -79036
11 meter
Z = -9378177
01 Z = -2858468
35
XDOT = -7577
297301 XDOT = -2309
560217
YDOT = 15938
076839 feet/sec YDOT = 4857
925820 meter/sec
ZDOT = -16643
324404 ZDOT = -5072
885278
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 06276
52598312
00020000 00000-0 20000-3 0 9083
2 25544 51
6361 349
3581 0012655 53
0232 307
2089 15
76457788 10256
Satellite: ISS
Catalog Number: 25544
Epoch time: 06276
52598312 = yrday
fracday
Element set: 908
Inclination: 51
6361 deg
RA of node: 349
3581 deg
Eccentricity:
0012655
Arg of perigee: 53
0232 deg
Mean anomaly: 307
2089 deg
Mean motion: 15
76457788 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1025
Checksum: 301
Coasting Arc #10 (Orbit 1040)
---------------------------------------
Vector Time (GMT): 2006/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3419190
44 A = 6718301
34 meter
Y = 4237005
24 meter E =
0023360
Z = 3924708
40 I = 51
54545
XDOT = -6426
264854 Wp = 66
59674
YDOT = -1448
859903 meter/sec RA = 343
82475 deg
ZDOT = -4006
478320 TA = 65
09602
MA = 64
85340
Ha = 190
666 n
mi
Hp = 175
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11217816
41 X = -3485380
68
Y = 13900935
83 feet Y = 4198400
16 meter
Z = 12876339
89 Z = 3907936
84
XDOT = -21083
546108 XDOT = -6390
123080
YDOT = -4753
477372 feet/sec YDOT = -1520
520176 meter/sec
ZDOT = -13144
613910 ZDOT = -4037
609308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8065190
87 X = 2458270
18
Y = -15988088
48 feet Y = -4873169
37 meter
Z = 12814416
64 Z = 3905834
19
XDOT = 20375
178861 XDOT = 6210
354517
YDOT = -423
982057 feet/sec YDOT = -129
229731 meter/sec
ZDOT = -13260
792505 ZDOT = -4041
889556
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 06277
54021170
00020000 00000-0 20000-3 0 9090
2 25544 51
6368 344
1297 0012717 55
7958 304
4410 15
76539925 10412
Satellite: ISS
Catalog Number: 25544
Epoch time: 06277
54021170 = yrday
fracday
Element set: 909
Inclination: 51
6368 deg
RA of node: 344
1297 deg
Eccentricity:
0012717
Arg of perigee: 55
7958 deg
Mean anomaly: 304
4410 deg
Mean motion: 15
76539925 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1041
Checksum: 294
Coasting Arc #11 (Orbit 1056)
---------------------------------------
Vector Time (GMT): 2006/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5127843
12 A = 6717572
89 meter
Y = 1468300
42 meter E =
0021591
Z = 4062538
59 I = 51
51595
XDOT = -4468
593255 Wp = 79
40428
YDOT = 5000
140701 meter/sec RA = 338
71424 deg
ZDOT = 3820
027532 TA = 331
31461
MA = 331
43320
Ha = 190
537 n
mi
Hp = 175
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16823632
29 X = 5091308
03
Y = 4817258
58 feet Y = 1525438
90 meter
Z = 13328538
70 Z = 4087360
97
XDOT = -14660
739025 XDOT = -4542
730560
YDOT = 16404
661093 feet/sec YDOT = 4949
756249 meter/sec
ZDOT = 12532
898726 ZDOT = 3798
138384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17408712
87 X = -5306175
68
Y = -835618
56 feet Y = -254696
54 meter
Z = 13421214
00 Z = 4090786
03
XDOT = 10500
938649 XDOT = 3200
686100
YDOT = -18083
000557 feet/sec YDOT = -5511
698570 meter/sec
ZDOT = 12452
016085 ZDOT = 3795
374503
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 06278
55441579
00020000 00000-0 20000-3 0 9103
2 25544 51
6362 338
9017 0012747 60
1251 300
1179 15
76562231 10574
Satellite: ISS
Catalog Number: 25544
Epoch time: 06278
55441579 = yrday
fracday
Element set: 910
Inclination: 51
6362 deg
RA of node: 338
9017 deg
Eccentricity:
0012747
Arg of perigee: 60
1251 deg
Mean anomaly: 300
1179 deg
Mean motion: 15
76562231 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1057
Checksum: 279
Coasting Arc #12 (Orbit 1071)
---------------------------------------
Vector Time (GMT): 2006/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465611
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4282673
83 A = 6721861
63 meter
Y = -4467156
41 meter E =
0017892
Z = -2624174
46 I = 51
50376
XDOT = 5282
449533 Wp = 60
05676
YDOT = 2013
361102 meter/sec RA = 333
50186 deg
ZDOT = 5228
929920 TA = 270
02174
MA = 270
22677
Ha = 190
706 n
mi
Hp = 175
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14050767
17 X = 4345055
85
Y = -14656024
95 feet Y = -4418916
63 meter
Z = -8609496
25 Z = -2603216
96
XDOT = 17330
871172 XDOT = 5234
141667
YDOT = 6605
515428 feet/sec YDOT = 2072
162783 meter/sec
ZDOT = 17155
281889 ZDOT = 5254
474904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10046710
25 X = -3062237
28
Y = 17680917
44 feet Y = 5389143
64 meter
Z = -8532017
52 Z = -2600558
94
XDOT = -17043
441100 XDOT = -5194
840847
YDOT = -1416
440978 feet/sec YDOT = -431
731210 meter/sec
ZDOT = 17250
718986 ZDOT = 5258
019147
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 06279
50520907
00020000 00000-0 20000-3 0 9113
2 25544 51
6355 334
0002 0012889 63
4562 296
7922 15
76588385 10726
Satellite: ISS
Catalog Number: 25544
Epoch time: 06279
50520907 = yrday
fracday
Element set: 911
Inclination: 51
6355 deg
RA of node: 334
0002 deg
Eccentricity:
0012889
Arg of perigee: 63
4562 deg
Mean anomaly: 296
7922 deg
Mean motion: 15
76588385 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1072
Checksum: 301
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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