Date:
March 11th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11505 0 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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
There are no maneuvers
Coasting Arc #1 (Orbit 3035)
---------------------------------------
Vector Time (GMT): 2009/069/01:20:10
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1388778
44 A = 6736767
04 meter
Y = -6160386
67 meter E =
0023187
Z = 2315782
09 I = 51
97974
XDOT = 4487
580831 Wp = 106
50150
YDOT = -3076
443981 meter/sec RA = 93
95722 deg
ZDOT = -5454
426210 TA = 47
58372
MA = 47
38779
Ha = 197
171 n
mi
Hp = 184
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4556359
72 X = -1331038
17
Y = -20211242
34 feet Y = -6175593
72 meter
Z = 7597710
25 Z = 2309176
40
XDOT = 14723
034222 XDOT = 4548
144683
YDOT = -10093
320148 feet/sec YDOT = -3025
923148 meter/sec
ZDOT = -17895
099115 ZDOT = -5432
478589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7076131
19 X = 2156804
79
Y = 19482860
37 feet Y = 5938375
84 meter
Z = 7571423
32 Z = 2307769
83
XDOT = -12036
262752 XDOT = -3668
652887
YDOT = 11341
652355 feet/sec YDOT = 3456
935638 meter/sec
ZDOT = -17809
641321 ZDOT = -5428
378675
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 09069
09211766
00010596 00000-0 82463-4 0 9006
2 25544 51
6369 94
5678 0009224 105
4475 254
7706 15
71580313 30361
Satellite: ISS
Catalog Number: 25544
Epoch time: 09069
09211766 = yrday
fracday
Element set: 900
Inclination: 51
6369 deg
RA of node: 94
5678 deg
Eccentricity:
0009224
Arg of perigee: 105
4475 deg
Mean anomaly: 254
7706 deg
Mean motion: 15
71580313 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3036
Checksum: 317
Coasting Arc #2 (Orbit 3051)
---------------------------------------
Vector Time (GMT): 2009/070/01:20:10
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3325024
83 A = 6730953
58 meter
Y = 3908581
30 meter E =
0019042
Z = 4344223
01 I = 51
95985
XDOT = -2828
648741 Wp = 109
49994
YDOT = -6274
283956 meter/sec RA = 88
90689 deg
ZDOT = 3461
639778 TA = 305
62467
MA = 305
80189
Ha = 197
270 n
mi
Hp = 184
237
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10908874
12 X = -3389587
25
Y = 12823429
46 feet Y = 3871038
43 meter
Z = 14252700
17 Z = 4327913
03
XDOT = -9280
343639 XDOT = -2775
094187
YDOT = -20584
921114 feet/sec YDOT = -6305
615726 meter/sec
ZDOT = 11357
085885 ZDOT = 3448
029202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9068554
14 X = 2764095
30
Y = -14248081
75 feet Y = -4342815
32 meter
Z = 14189321
06 Z = 4324905
06
XDOT = 11122
034806 XDOT = 3389
996209
YDOT = 18396
227746 feet/sec YDOT = 5607
170217 meter/sec
ZDOT = 11303
439968 ZDOT = 3445
288502
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 09070
10953154
00010596 00000-0 82463-4 0 9015
2 25544 51
6358 89
3606 0009406 110
3195 249
8978 15
71577277 30527
Satellite: ISS
Catalog Number: 25544
Epoch time: 09070
10953154 = yrday
fracday
Element set: 901
Inclination: 51
6358 deg
RA of node: 89
3606 deg
Eccentricity:
0009406
Arg of perigee: 110
3195 deg
Mean anomaly: 249
8978 deg
Mean motion: 15
71577277 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3052
Checksum: 322
Coasting Arc #3 (Orbit 3066)
---------------------------------------
Vector Time (GMT): 2009/071/01:20:10
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3367536
22 A = 6733339
29 meter
Y = 4563776
02 meter E =
0015066
Z = -3645572
53 I = 51
96653
XDOT = -2851
603081 Wp = 108
68437
YDOT = 5613
893977 meter/sec RA = 83
76154 deg
ZDOT = 4403
787120 TA = 207
96398
MA = 208
04502
Ha = 197
225 n
mi
Hp = 184
237
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11048347
17 X = 3333962
40
Y = 14973018
43 feet Y = 4601245
63 meter
Z = -11960539
81 Z = -3629295
27
XDOT = -9355
653154 XDOT = -2935
559245
YDOT = 18418
287325 feet/sec YDOT = 5581
536769 meter/sec
ZDOT = 14448
120474 ZDOT = 4389
729597
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13347646
78 X = -4068362
74
Y = -13023919
79 feet Y = -3969690
75 meter
Z = -11896621
67 Z = -3626090
29
XDOT = 5454
109250 XDOT = 1662
412499
YDOT = -18707
199438 feet/sec YDOT = -5701
954389 meter/sec
ZDOT = 14393
666921 ZDOT = 4387
189677
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 09071
06334059
00010596 00000-0 82463-4 0 9029
2 25544 51
6361 84
4785 0009651 114
1102 246
1071 15
71594929 30670
Satellite: ISS
Catalog Number: 25544
Epoch time: 09071
06334059 = yrday
fracday
Element set: 902
Inclination: 51
6361 deg
RA of node: 84
4785 deg
Eccentricity:
0009651
Arg of perigee: 114
1102 deg
Mean anomaly: 246
1071 deg
Mean motion: 15
71594929 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3067
Checksum: 299
Coasting Arc #4 (Orbit 3082)
---------------------------------------
Vector Time (GMT): 2009/072/01:20:10
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1502358
16 A = 6734195
74 meter
Y = -5676490
01 meter E =
0014128
Z = -3303199
90 I = 51
96587
XDOT = 4575
359845 Wp = 109
59586
YDOT = 3960
170330 meter/sec RA = 78
71747 deg
ZDOT = -4745
495263 TA = 108
90118
MA = 108
74796
Ha = 197
152 n
mi
Hp = 184
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4928996
60 X = 1581768
24
Y = -18623654
88 feet Y = -5659246
11 meter
Z = -10837270
02 Z = -3295708
00
XDOT = 15011
023114 XDOT = 4553
789166
YDOT = 12992
684811 feet/sec YDOT = 4011
213563 meter/sec
ZDOT = -15569
210179 ZDOT = -4723
321080
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1649766
89 X = -502848
95
Y = 19210351
19 feet Y = 5855315
04 meter
Z = -10808451
63 Z = -3294416
06
XDOT = -15743
517334 XDOT = -4798
624083
YDOT = -10024
142038 feet/sec YDOT = -3055
358493 meter/sec
ZDOT = -15482
318810 ZDOT = -4719
010773
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 09072
08071866
00010596 00000-0 82463-4 0 9037
2 25544 51
6365 79
2716 0009668 117
1127 243
1022 15
71639217 30839
Satellite: ISS
Catalog Number: 25544
Epoch time: 09072
08071866 = yrday
fracday
Element set: 903
Inclination: 51
6365 deg
RA of node: 79
2716 deg
Eccentricity:
0009668
Arg of perigee: 117
1127 deg
Mean anomaly: 243
1022 deg
Mean motion: 15
71639217 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3083
Checksum: 306
Coasting Arc #5 (Orbit 3098)
---------------------------------------
Vector Time (GMT): 2009/073/01:20:10
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4390904
79 A = 6729914
29 meter
Y = -2213466
93 meter E =
0016144
Z = 4580312
45 I = 51
94379
XDOT = 391
860475 Wp = 95
53888
YDOT = -7073
659197 meter/sec RA = 73
57396 deg
ZDOT = -3035
176073 TA = 24
50801
MA = 24
43136
Ha = 197
264 n
mi
Hp = 184
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14405855
61 X = -4388077
39
Y = -7262030
60 feet Y = -2262552
37 meter
Z = 15027271
81 Z = 4558988
53
XDOT = 1285
631480 XDOT = 485
674505
YDOT = -23207
543298 feet/sec YDOT = -7068
752909 meter/sec
ZDOT = -9957
926749 ZDOT = -3033
043925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15617967
22 X = 4760356
41
Y = 4341134
15 feet Y = 1323177
69 meter
Z = 14943838
74 Z = 4554882
05
XDOT = 3458
849340 XDOT = 1054
257279
YDOT = 21894
228500 feet/sec YDOT = 6673
360847 meter/sec
ZDOT = -9950
132964 ZDOT = -3032
800527
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 09073
09807979
00010596 00000-0 82463-4 0 9042
2 25544 51
6361 74
0642 0009727 121
9074 238
3036 15
71624881 30995
Satellite: ISS
Catalog Number: 25544
Epoch time: 09073
09807979 = yrday
fracday
Element set: 904
Inclination: 51
6361 deg
RA of node: 74
0642 deg
Eccentricity:
0009727
Arg of perigee: 121
9074 deg
Mean anomaly: 238
3036 deg
Mean motion: 15
71624881 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3099
Checksum: 327
Coasting Arc #6 (Orbit 3114)
---------------------------------------
Vector Time (GMT): 2009/074/01:20:10
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 875372
36 A = 6737094
90 meter
Y = 6384602
93 meter E =
0020959
Z = 1947258
68 I = 51
96044
XDOT = -5142
575201 Wp = 90
96824
YDOT = -1029
304820 meter/sec RA = 68
51804 deg
ZDOT = 5634
466134 TA = 290
57856
MA = 290
80329
Ha = 196
995 n
mi
Hp = 184
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2871956
58 X = 794454
18
Y = 20946860
00 feet Y = 6393939
54 meter
Z = 6388643
97 Z = 1951314
27
XDOT = -16871
965882 XDOT = -5158
054345
YDOT = -3376
984316 feet/sec YDOT = -1086
898271 meter/sec
ZDOT = 18485
781278 ZDOT = 5609
445983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7151256
15 X = -2179702
87
Y = -19891455
65 feet Y = -6062915
68 meter
Z = 6404949
48 Z = 1952228
60
XDOT = 15858
783898 XDOT = 4833
757332
YDOT = 274
374726 feet/sec YDOT = 83
629416 meter/sec
ZDOT = 18388
004907 ZDOT = 5604
663896
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 09074
11542077
00010596 00000-0 82463-4 0 9052
2 25544 51
6375 68
8574 0009774 126
2525 233
9542 15
71696048 31152
Satellite: ISS
Catalog Number: 25544
Epoch time: 09074
11542077 = yrday
fracday
Element set: 905
Inclination: 51
6375 deg
RA of node: 68
8574 deg
Eccentricity:
0009774
Arg of perigee: 126
2525 deg
Mean anomaly: 233
9542 deg
Mean motion: 15
71696048 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3115
Checksum: 324
Coasting Arc #7 (Orbit 3129)
---------------------------------------
Vector Time (GMT): 2009/075/01:20:10
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4326326
71 A = 6727336
44 meter
Y = -386785
89 meter E =
0023064
Z = -5157216
96 I = 51
91652
XDOT = 2344
288869 Wp = 112
44662
YDOT = 7173
207557 meter/sec RA = 63
39219 deg
ZDOT = 1425
064959 TA = 171
20909
MA = 171
16863
Ha = 196
948 n
mi
Hp = 184
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14193985
26 X = 4355383
07
Y = -1268982
58 feet Y = -338244
15 meter
Z = -16920003
15 Z = -5136129
10
XDOT = 7691
236446 XDOT = 2256
979932
YDOT = 23534
145529 feet/sec YDOT = 7198
934654 meter/sec
ZDOT = 4675
409972 ZDOT = 1436
241110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13635685
14 X = -4156156
83
Y = 4463915
27 feet Y = 1360601
38 meter
Z = -16837683
70 Z = -5132125
99
XDOT = -12455
486129 XDOT = -3796
432172
YDOT = -20201
007079 feet/sec YDOT = -6157
266958 meter/sec
ZDOT = 4719
567137 ZDOT = 1438
524063
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 09075
06916291
00010596 00000-0 82463-4 0 9061
2 25544 51
6384 63
9768 0009823 129
3501 230
8532 15
71709424 31301
Satellite: ISS
Catalog Number: 25544
Epoch time: 09075
06916291 = yrday
fracday
Element set: 906
Inclination: 51
6384 deg
RA of node: 63
9768 deg
Eccentricity:
0009823
Arg of perigee: 129
3501 deg
Mean anomaly: 230
8532 deg
Mean motion: 15
71709424 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3130
Checksum: 312
Coasting Arc #8 (Orbit 3145)
---------------------------------------
Vector Time (GMT): 2009/076/01:20:10
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3161149
66 A = 6738453
09 meter
Y = -5916676
62 meter E =
0020695
Z = -534249
43 I = 51
93982
XDOT = 4421
572792 Wp = 135
96571
YDOT = -1831
349682 meter/sec RA = 58
31026 deg
ZDOT = -6033
859263 TA = 49
82126
MA = 49
64025
Ha = 196
787 n
mi
Hp = 184
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10371225
92 X = -3092158
17
Y = -19411668
69 feet Y = -5951640
70 meter
Z = -1752786
84 Z = -549438
49
XDOT = 14506
472415 XDOT = 4471
033932
YDOT = -6008
365097 feet/sec YDOT = -1781
628701 meter/sec
ZDOT = -19796
126191 ZDOT = -6012
259141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14760032
14 X = 4498857
80
Y = 16318814
40 feet Y = 4973974
63 meter
Z = -1812517
02 Z = -552455
19
XDOT = -11536
576938 XDOT = -3516
348651
YDOT = 8299
191306 feet/sec YDOT = 2529
593510 meter/sec
ZDOT = -19711
904966 ZDOT = -6008
188634
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 09076
08646812
00010596 00000-0 82463-4 0 9074
2 25544 51
6381 58
7687 0009705 132
9750 227
2228 15
71751452 31462
Satellite: ISS
Catalog Number: 25544
Epoch time: 09076
08646812 = yrday
fracday
Element set: 907
Inclination: 51
6381 deg
RA of node: 58
7687 deg
Eccentricity:
0009705
Arg of perigee: 132
9750 deg
Mean anomaly: 227
2228 deg
Mean motion: 15
71751452 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3146
Checksum: 326
Coasting Arc #9 (Orbit 3161)
---------------------------------------
Vector Time (GMT): 2009/077/01:20:10
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3149906
10 A = 6726472
00 meter
Y = 2708483
17 meter E =
0011766
Z = 5282840
43 I = 51
88417
XDOT = -4767
577143 Wp = 129
51840
YDOT = -6047
321052 meter/sec RA = 53
20830 deg
ZDOT = 250
050050 TA = 318
07246
MA = 318
16249
Ha = 196
799 n
mi
Hp = 184
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10334337
61 X = -3205621
63
Y = 8886099
64 feet Y = 2672947
68 meter
Z = 17332153
65 Z = 5267402
89
XDOT = -15641
657294 XDOT = -4700
815344
YDOT = -19840
292165 feet/sec YDOT = -6100
261586 meter/sec
ZDOT = 820
374180 ZDOT = 227
051595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7774256
01 X = 2369593
23
Y = -11287246
43 feet Y = -3440352
71 meter
Z = 17272054
38 Z = 5264522
17
XDOT = 19431
139856 XDOT = 5922
611428
YDOT = 14539
553150 feet/sec YDOT = 4431
655800 meter/sec
ZDOT = 730
142971 ZDOT = 222
547577
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 09077
10375535
00010596 00000-0 82463-4 0 9080
2 25544 51
6392 53
5622 0009694 136
9907 223
2014 15
71768743 31629
Satellite: ISS
Catalog Number: 25544
Epoch time: 09077
10375535 = yrday
fracday
Element set: 908
Inclination: 51
6392 deg
RA of node: 53
5622 deg
Eccentricity:
0009694
Arg of perigee: 136
9907 deg
Mean anomaly: 223
2014 deg
Mean motion: 15
71768743 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3162
Checksum: 319
Coasting Arc #10 (Orbit 3176)
---------------------------------------
Vector Time (GMT): 2009/078/01:20:10
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4981020
66 A = 6738091
20 meter
Y = 4439841
64 meter E =
0012497
Z = -946518
54 I = 51
90568
XDOT = -2564
897497 Wp = 88
29620
YDOT = 4132
875226 meter/sec RA = 48
09700 deg
ZDOT = 5956
097166 TA = 261
42376
MA = 261
56538
Ha = 196
639 n
mi
Hp = 184
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16341931
31 X = 4935601
39
Y = 14566409
59 feet Y = 4495288
34 meter
Z = -3105375
79 Z = -922431
38
XDOT = -8415
018035 XDOT = -2639
854750
YDOT = 13559
301923 feet/sec YDOT = 4103
774072 meter/sec
ZDOT = 19541
001201 ZDOT = 5943
454847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19742392
66 X = -6017481
28
Y = -9489686
33 feet Y = -2892456
39 meter
Z = -3011005
03 Z = -917754
33
XDOT = 3765
554035 XDOT = 1147
740870
YDOT = -13945
859883 feet/sec YDOT = -4250
698092 meter/sec
ZDOT = 19491
911196 ZDOT = 5941
134532
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 09078
05744383
00010596 00000-0 82463-4 0 9097
2 25544 51
6401 48
6810 0009764 140
5863 219
6011 15
71792115 31776
Satellite: ISS
Catalog Number: 25544
Epoch time: 09078
05744383 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 48
6810 deg
Eccentricity:
0009764
Arg of perigee: 140
5863 deg
Mean anomaly: 219
6011 deg
Mean motion: 15
71792115 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3177
Checksum: 313
Coasting Arc #11 (Orbit 3192)
---------------------------------------
Vector Time (GMT): 2009/079/01:20:10
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1207127
90 A = 6727397
82 meter
Y = -4297173
33 meter E =
0019161
Z = -5048011
35 I = 51
84949
XDOT = 6338
846906 Wp = 104
11703
YDOT = 3934
205484 meter/sec RA = 43
01890 deg
ZDOT = -1843
610163 TA = 148
17890
MA = 148
06298
Ha = 196
496 n
mi
Hp = 184
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3960393
37 X = 1279611
93
Y = -14098337
68 feet Y = -4283269
39 meter
Z = -16561717
02 Z = -5041971
00
XDOT = 20796
741816 XDOT = 6303
338668
YDOT = 12907
498308 feet/sec YDOT = 4004
891571 meter/sec
ZDOT = -6048
589775 ZDOT = -1812
902773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 241792
48 X = 73698
35
Y = 14668352
66 feet Y = 4470913
89 meter
Z = -16538418
26 Z = -5040909
88
XDOT = -22624
674800 XDOT = -6896
000879
YDOT = -6272
812063 feet/sec YDOT = -1911
953117 meter/sec
ZDOT = -5928
398661 ZDOT = -1806
975912
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 09079
07469245
00010596 00000-0 82463-4 0 9103
2 25544 51
6403 43
4741 0009677 144
7705 215
4098 15
71820460 31930
Satellite: ISS
Catalog Number: 25544
Epoch time: 09079
07469245 = yrday
fracday
Element set: 910
Inclination: 51
6403 deg
RA of node: 43
4741 deg
Eccentricity:
0009677
Arg of perigee: 144
7705 deg
Mean anomaly: 215
4098 deg
Mean motion: 15
71820460 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3193
Checksum: 313
Coasting Arc #12 (Orbit 3208)
---------------------------------------
Vector Time (GMT): 2009/080/01:20:10
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5887170
59 A = 6736187
98 meter
Y = -2330460
24 meter E =
0022422
Z = 2260688
00 I = 51
85680
XDOT = 33
678781 Wp = 124
42077
YDOT = -5422
876808 meter/sec RA = 37
88008 deg
ZDOT = -5476
685593 TA = 30
26705
MA = 30
13773
Ha = 196
496 n
mi
Hp = 184
693
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19314864
14 X = -5871655
31
Y = -7645866
92 feet Y = -2396207
16 meter
Z = 7416955
37 Z = 2232126
30
XDOT = 110
494689 XDOT = 120
920183
YDOT = -17791
590576 feet/sec YDOT = -5422
012635 meter/sec
ZDOT = -17968
128586 ZDOT = -5476
309845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20772231
49 X = 6331376
16
Y = 1296988
99 feet Y = 395322
24 meter
Z = 7305251
75 Z = 2226640
73
XDOT = 5382
801691 XDOT = 1640
677955
YDOT = 15474
295767 feet/sec YDOT = 4716
565350 meter/sec
ZDOT = -17967
027326 ZDOT = -5476
349929
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 09080
09192188
00010596 00000-0 82463-4 0 9117
2 25544 51
6405 38
2666 0009809 148
6106 211
5644 15
71838584 32093
Satellite: ISS
Catalog Number: 25544
Epoch time: 09080
09192188 = yrday
fracday
Element set: 911
Inclination: 51
6405 deg
RA of node: 38
2666 deg
Eccentricity:
0009809
Arg of perigee: 148
6106 deg
Mean anomaly: 211
5644 deg
Mean motion: 15
71838584 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3209
Checksum: 320
Coasting Arc #13 (Orbit 3224)
---------------------------------------
Vector Time (GMT): 2009/081/01:20:10
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1196709
74 A = 6729564
80 meter
Y = 4918149
09 meter E =
0017686
Z = 4430111
02 I = 51
81222
XDOT = -6832
444850 Wp = 132
24111
YDOT = -1322
897350 meter/sec RA = 32
81781 deg
ZDOT = 3294
294338 TA = 284
68097
MA = 284
87695
Ha = 196
180 n
mi
Hp = 184
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3926213
05 X = 1120104
86
Y = 16135659
74 feet Y = 4931103
34 meter
Z = 14534484
96 Z = 4435738
19
XDOT = -22416
157645 XDOT = -6833
147052
YDOT = -4340
214403 feet/sec YDOT = -1399
305460 meter/sec
ZDOT = 10808
052291 ZDOT = 3261
101166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8877748
66 X = -2705937
79
Y = -14011111
73 feet Y = -4270586
86 meter
Z = 14556793
73 Z = 4436910
73
XDOT = 21646
824772 XDOT = 6597
952191
YDOT = -2553
650308 feet/sec YDOT = -778
352614 meter/sec
ZDOT = 10678
328811 ZDOT = 3254
754621
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 09081
10912893
00010596 00000-0 82463-4 0 9124
2 25544 51
6413 33
0592 0009726 152
6534 207
5142 15
71917672 32253
Satellite: ISS
Catalog Number: 25544
Epoch time: 09081
10912893 = yrday
fracday
Element set: 912
Inclination: 51
6413 deg
RA of node: 33
0592 deg
Eccentricity:
0009726
Arg of perigee: 152
6534 deg
Mean anomaly: 207
5142 deg
Mean motion: 15
71917672 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3225
Checksum: 297
Coasting Arc #14 (Orbit 3239)
---------------------------------------
Vector Time (GMT): 2009/082/01:20:10
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5805612
75 A = 6733179
37 meter
Y = -1647
15 meter E =
0012378
Z = -3426724
21 I = 51
79863
XDOT = 2719
212646 Wp = 134
69951
YDOT = 5517
705999 meter/sec RA = 27
66152 deg
ZDOT = 4605
914987 TA = 184
99766
MA = 185
01003
Ha = 196
092 n
mi
Hp = 185
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19047285
92 X = 5821845
87
Y = -5404
04 feet Y = 63365
09 meter
Z = -11242533
49 Z = -3398481
49
XDOT = 8921
301332 XDOT = 2634
936230
YDOT = 18102
709969 feet/sec YDOT = 5547
642964 meter/sec
ZDOT = 15111
269643 ZDOT = 4618
919612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17963023
02 X = -5475129
42
Y = 6526625
12 feet Y = 1989315
34 meter
Z = -11132235
08 Z = -3393105
25
XDOT = -14004
799771 XDOT = -4268
662970
YDOT = -12692
164827 feet/sec YDOT = -3868
571839 meter/sec
ZDOT = 15162
430848 ZDOT = 4621
508923
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 09082
06274486
00010596 00000-0 82463-4 0 9130
2 25544 51
6414 28
1777 0009566 156
2287 203
9319 15
71898376 32403
Satellite: ISS
Catalog Number: 25544
Epoch time: 09082
06274486 = yrday
fracday
Element set: 913
Inclination: 51
6414 deg
RA of node: 28
1777 deg
Eccentricity:
0009566
Arg of perigee: 156
2287 deg
Mean anomaly: 203
9319 deg
Mean motion: 15
71898376 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3240
Checksum: 333
Coasting Arc #15 (Orbit 3255)
---------------------------------------
Vector Time (GMT): 2009/083/01:20:10
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3487371
22 A = 6732417
89 meter
Y = -4508768
82 meter E =
0012028
Z = -3582405
09 I = 51
77020
XDOT = 6153
414592 Wp = 133
13397
YDOT = -1236
520850 meter/sec RA = 22
60309 deg
ZDOT = -4451
299496 TA = 89
50658
MA = 89
36876
Ha = 195
953 n
mi
Hp = 184
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11441506
63 X = -3419291
73
Y = -14792548
62 feet Y = -4547386
33 meter
Z = -11753297
55 Z = -3599180
77
XDOT = 20188
368083 XDOT = 6188
407622
YDOT = -4056
826936 feet/sec YDOT = -1167
514547 meter/sec
ZDOT = -14604
000972 ZDOT = -4421
321414
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15908464
02 X = 4848899
83
Y = 9751760
65 feet Y = 2972336
64 meter
Z = -11819116
24 Z = -3602466
63
XDOT = -16773
108445 XDOT = -5112
443454
YDOT = 9873
225868 feet/sec YDOT = 3009
359245 meter/sec
ZDOT = -14487
012780 ZDOT = -4415
641495
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 09083
07991451
00010596 00000-0 82463-4 0 9141
2 25544 51
6417 22
9700 0009699 160
1269 200
0273 15
71937582 32562
Satellite: ISS
Catalog Number: 25544
Epoch time: 09083
07991451 = yrday
fracday
Element set: 914
Inclination: 51
6417 deg
RA of node: 22
9700 deg
Eccentricity:
0009699
Arg of perigee: 160
1269 deg
Mean anomaly: 200
0273 deg
Mean motion: 15
71937582 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3256
Checksum: 313
Coasting Arc #16 (Orbit 3271)
---------------------------------------
Vector Time (GMT): 2009/084/01:20:10
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4726883
04 A = 6729964
33 meter
Y = 2073663
49 meter E =
0013635
Z = 4304298
81 I = 51
73459
XDOT = -5170
548959 Wp = 116
39830
YDOT = -4517
561407 meter/sec RA = 17
44139 deg
ZDOT = -3499
225139 TA = 8
94661
MA = 8
92233
Ha = 195
921 n
mi
Hp = 185
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15508146
44 X = -4770629
15
Y = 6803357
92 feet Y = 2020560
60 meter
Z = 14121715
27 Z = 4281229
28
XDOT = -16963
743304 XDOT = -5102
650047
YDOT = -14821
395693 feet/sec YDOT = -4575
002233 meter/sec
ZDOT = -11480
397439 ZDOT = -3524
178096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11922113
40 X = 3633860
16
Y = -12131934
59 feet Y = -3697813
66 meter
Z = 14031767
61 Z = 4276882
77
XDOT = 20324
241592 XDOT = 6194
828837
YDOT = 6571
746884 feet/sec YDOT = 2003
068450 meter/sec
ZDOT = -11578
146279 ZDOT = -3529
018986
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 09084
09706383
00010596 00000-0 82463-4 0 9153
2 25544 51
6420 17
7626 0009590 163
0982 197
0501 15
71982195 32726
Satellite: ISS
Catalog Number: 25544
Epoch time: 09084
09706383 = yrday
fracday
Element set: 915
Inclination: 51
6420 deg
RA of node: 17
7626 deg
Eccentricity:
0009590
Arg of perigee: 163
0982 deg
Mean anomaly: 197
0501 deg
Mean motion: 15
71982195 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3272
Checksum: 319
Coasting Arc #17 (Orbit 3287)
---------------------------------------
Vector Time (GMT): 2009/085/01:20:10
000
Vector Time (MET): N/A
Weight (LBS) : 638785
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5377446
83 A = 6735056
37 meter
Y = 3194454
91 meter E =
0016639
Z = 2493978
03 I = 51
72391
XDOT = -4456
722562 Wp = 110
79157
YDOT = 3321
066435 meter/sec RA = 12
37368 deg
ZDOT = 5321
340821 TA = 277
35950
MA = 277
54857
Ha = 195
633 n
mi
Hp = 185
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17642542
10 X = 5329210
95
Y = 10480495
10 feet Y = 3254319
23 meter
Z = 8182342
62 Z = 2519984
12
XDOT = -14621
793182 XDOT = -4519
378140
YDOT = 10895
887253 feet/sec YDOT = 3270
879026 meter/sec
ZDOT = 17458
467259 ZDOT = 5299
537528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20286851
44 X = -6183432
32
Y = -2804998
07 feet Y = -854963
41 meter
Z = 8284107
96 Z = 2524996
11
XDOT = 9115
399357 XDOT = 2778
373724
YDOT = -14288
145241 feet/sec YDOT = -4355
026669 meter/sec
ZDOT = 17373
552511 ZDOT = 5295
458805
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 09085
11419180
00010596 00000-0 82463-4 0 9164
2 25544 51
6421 12
5549 0009609 167
5361 192
6040 15
72020423 32889
Satellite: ISS
Catalog Number: 25544
Epoch time: 09085
11419180 = yrday
fracday
Element set: 916
Inclination: 51
6421 deg
RA of node: 12
5549 deg
Eccentricity:
0009609
Arg of perigee: 167
5361 deg
Mean anomaly: 192
6040 deg
Mean motion: 15
72020423 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 3288
Checksum: 293
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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