Date:
July 22nd 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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 1120)
---------------------------------------
Vector Time (GMT): 2009/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4900436
76 A = 6732337
81 meter
Y = 4599614
81 meter E =
0008286
Z = 289528
92 I = 51
89357
XDOT = -3063
533187 Wp = 24
75357
YDOT = -3648
160790 meter/sec RA = 134
87752 deg
ZDOT = 6050
111717 TA = 338
38188
MA = 338
41684
Ha = 188
214 n
mi
Hp = 186
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16077548
41 X = -4952912
68
Y = 15090599
77 feet Y = 4544521
79 meter
Z = 949898
03 Z = 265596
34
XDOT = -10050
961900 XDOT = -3051
901071
YDOT = -11969
031463 feet/sec YDOT = -3682
355115 meter/sec
ZDOT = 19849
447890 ZDOT = 6035
256845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20828959
99 X = 6348667
00
Y = 7248282
04 feet Y = 2209276
37 meter
Z = 856097
98 Z = 260938
66
XDOT = -5359
110414 XDOT = -1633
456854
YDOT = 13039
184495 feet/sec YDOT = 3974
343434 meter/sec
ZDOT = 19790
870319 ZDOT = 6032
257273
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 09201
56299492
00010596 00000-0 82463-4 0 9008
2 25544 51
6381 135
5004 0006095 260
6257 99
4217 15
73933536 11214
Satellite: ISS
Catalog Number: 25544
Epoch time: 09201
56299492 = yrday
fracday
Element set: 900
Inclination: 51
6381 deg
RA of node: 135
5004 deg
Eccentricity:
0006095
Arg of perigee: 260
6257 deg
Mean anomaly: 99
4217 deg
Mean motion: 15
73933536 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1121
Checksum: 302
Coasting Arc #2 (Orbit 1135)
---------------------------------------
Vector Time (GMT): 2009/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2949707
14 A = 6720265
15 meter
Y = 2937716
21 meter E =
0009011
Z = -5283195
43 I = 51
87434
XDOT = -5114
955500 Wp = 97
95727
YDOT = 5738
656312 meter/sec RA = 129
75431 deg
ZDOT = 334
462141 TA = 175
21456
MA = 175
20594
Ha = 188
043 n
mi
Hp = 186
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9677516
88 X = 2942302
15
Y = 9638176
53 feet Y = 2970661
05 meter
Z = -17333318
35 Z = -5268883
53
XDOT = -16781
350065 XDOT = -5180
370703
YDOT = 18827
612573 feet/sec YDOT = 5681
092074 meter/sec
ZDOT = 1097
316737 ZDOT = 309
456279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3776267
54 X = 1151006
35
Y = -13200039
14 feet Y = -4023371
93 meter
Z = -17276905
83 Z = -5266000
90
XDOT = 23605
908193 XDOT = 7195
080817
YDOT = 5442
005950 feet/sec YDOT = 1658
723414 meter/sec
ZDOT = 999
346677 ZDOT = 304
600867
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 09202
51537098
00010596 00000-0 82463-4 0 9012
2 25544 51
6392 130
6099 0006094 264
5447 95
5021 15
73952286 11368
Satellite: ISS
Catalog Number: 25544
Epoch time: 09202
51537098 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 130
6099 deg
Eccentricity:
0006094
Arg of perigee: 264
5447 deg
Mean anomaly: 95
5021 deg
Mean motion: 15
73952286 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1136
Checksum: 310
Coasting Arc #3 (Orbit 1151)
---------------------------------------
Vector Time (GMT): 2009/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4011093
44 A = 6732271
95 meter
Y = -5391276
52 meter E =
0008978
Z = -300257
98 I = 51
93375
XDOT = 3653
088747 Wp = 168
30801
YDOT = 3052
807329 meter/sec RA = 124
64375 deg
ZDOT = -6053
558129 TA = 14
94231
MA = 14
91580
Ha = 187
995 n
mi
Hp = 186
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13159755
38 X = 4072540
07
Y = -17687915
10 feet Y = -5346078
52 meter
Z = -985098
35 Z = -280624
06
XDOT = 11985
199302 XDOT = 3648
086603
YDOT = 10015
772076 feet/sec YDOT = 3093
631180 meter/sec
ZDOT = -19860
755015 ZDOT = -6035
823577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21882762
74 X = -6669866
08
Y = -2707722
54 feet Y = -825313
83 meter
Z = -908215
18 Z = -276823
99
XDOT = 2532
113264 XDOT = 771
788123
YDOT = -13872
995621 feet/sec YDOT = -4228
489065 meter/sec
ZDOT = -19790
874621 ZDOT = -6032
258585
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 09203
53122854
00010596 00000-0 82463-4 0 9026
2 25544 51
6400 125
3936 0006101 267
9550 92
0915 15
73954804 11520
Satellite: ISS
Catalog Number: 25544
Epoch time: 09203
53122854 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 125
3936 deg
Eccentricity:
0006101
Arg of perigee: 267
9550 deg
Mean anomaly: 92
0915 deg
Mean motion: 15
73954804 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1152
Checksum: 286
Coasting Arc #4 (Orbit 1167)
---------------------------------------
Vector Time (GMT): 2009/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3409471
35 A = 6720071
61 meter
Y = -2381322
99 meter E =
0003910
Z = 5281938
01 I = 51
90899
XDOT = 4027
946552 Wp = 284
07551
YDOT = -6551
373551 meter/sec RA = 119
52293 deg
ZDOT = -352
900473 TA = 169
26764
MA = 169
25929
Ha = 187
924 n
mi
Hp = 186
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11185929
63 X = -3408247
66
Y = -7812739
46 feet Y = -2419443
41 meter
Z = 17329192
95 Z = 5265377
92
XDOT = 13215
047744 XDOT = 4102
620050
YDOT = -21494
007714 feet/sec YDOT = -6505
913135 meter/sec
ZDOT = -1157
809952 ZDOT = -333
152497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -980984
01 X = -299003
93
Y = 13691537
99 feet Y = 4173180
78 meter
Z = 17263959
73 Z = 5262054
93
XDOT = -24232
672391 XDOT = -7386
118545
YDOT = -370
809025 feet/sec YDOT = -113
022591 meter/sec
ZDOT = -1080
536702 ZDOT = -329
347587
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 09204
54707305
00010596 00000-0 82463-4 0 9039
2 25544 51
6398 120
1773 0006248 272
6388 87
4060 15
74021240 11688
Satellite: ISS
Catalog Number: 25544
Epoch time: 09204
54707305 = yrday
fracday
Element set: 903
Inclination: 51
6398 deg
RA of node: 120
1773 deg
Eccentricity:
0006248
Arg of perigee: 272
6388 deg
Mean anomaly: 87
4060 deg
Mean motion: 15
74021240 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1168
Checksum: 297
Coasting Arc #5 (Orbit 1183)
---------------------------------------
Vector Time (GMT): 2009/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3004033
17 A = 6732161
10 meter
Y = 6009018
78 meter E =
0009916
Z = 321799
17 I = 51
96320
XDOT = -4119
014439 Wp = 20
50162
YDOT = -2385
936862 meter/sec RA = 114
41384 deg
ZDOT = 6054
902860 TA = 342
98110
MA = 343
01434
Ha = 188
041 n
mi
Hp = 186
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9855751
86 X = -3072566
98
Y = 19714628
54 feet Y = 5975042
70 meter
Z = 1055771
56 Z = 307039
89
XDOT = -13513
826900 XDOT = -4121
441349
YDOT = -7827
876843 feet/sec YDOT = -2432
012140 meter/sec
ZDOT = 19865
166862 ZDOT = 6034
887029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21959639
70 X = 6693298
18
Y = -1922275
62 feet Y = -585909
61 meter
Z = 998076
77 Z = 304213
80
XDOT = 328
368726 XDOT = 100
086788
YDOT = 14108
710324 feet/sec YDOT = 4300
334907 meter/sec
ZDOT = 19786
343086 ZDOT = 6030
877373
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 09205
56290963
00010596 00000-0 82463-4 0 9040
2 25544 51
6399 114
9599 0006161 277
3256 82
7207 15
73992391 11848
Satellite: ISS
Catalog Number: 25544
Epoch time: 09205
56290963 = yrday
fracday
Element set: 904
Inclination: 51
6399 deg
RA of node: 114
9599 deg
Eccentricity:
0006161
Arg of perigee: 277
3256 deg
Mean anomaly: 82
7207 deg
Mean motion: 15
73992391 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1184
Checksum: 338
Coasting Arc #6 (Orbit 1198)
---------------------------------------
Vector Time (GMT): 2009/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3760932
01 A = 6720047
08 meter
Y = 1781045
16 meter E =
0008912
Z = -5284163
55 I = 51
93447
XDOT = -2829
272093 Wp = 87
71456
YDOT = 7144
856355 meter/sec RA = 109
29349 deg
ZDOT = 395
418398 TA = 186
02245
MA = 186
03317
Ha = 188
139 n
mi
Hp = 186
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12339015
78 X = 3766405
63
Y = 5843324
01 feet Y = 1823133
05 meter
Z = -17336494
59 Z = -5265879
83
XDOT = -9282
388757 XDOT = -2910
877659
YDOT = 23441
129772 feet/sec YDOT = 7112
761470 meter/sec
ZDOT = 1297
304454 ZDOT = 381
476260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1771006
54 X = -539802
79
Y = -13629011
51 feet Y = -4154122
71 meter
Z = -17264511
92 Z = -5262223
23
XDOT = 23762
315583 XDOT = 7242
753790
YDOT = -4658
356212 feet/sec YDOT = -1419
866973 meter/sec
ZDOT = 1242
879663 ZDOT = 378
829721
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 09206
51524387
00010596 00000-0 82463-4 0 9057
2 25544 51
6404 110
0691 0006167 280
7544 79
2925 15
74034382 11991
Satellite: ISS
Catalog Number: 25544
Epoch time: 09206
51524387 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 110
0691 deg
Eccentricity:
0006167
Arg of perigee: 280
7544 deg
Mean anomaly: 79
2925 deg
Mean motion: 15
74034382 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1199
Checksum: 308
Coasting Arc #7 (Orbit 1214)
---------------------------------------
Vector Time (GMT): 2009/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1930125
74 A = 6732088
32 meter
Y = -6433577
64 meter E =
0007257
Z = -376690
75 I = 51
98344
XDOT = 4452
478434 Wp = 166
85119
YDOT = 1688
348691 meter/sec RA = 104
18693 deg
ZDOT = -6051
125579 TA = 17
22441
MA = 17
19979
Ha = 188
253 n
mi
Hp = 186
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6332433
52 X = 2003753
52
Y = -21107538
20 feet Y = -6411582
15 meter
Z = -1235862
04 Z = -367135
87
XDOT = 14607
868878 XDOT = 4462
663046
YDOT = 5539
201741 feet/sec YDOT = 1738
196236 meter/sec
ZDOT = -19852
774208 ZDOT = -6029
470844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21094829
74 X = -6429704
10
Y = 6381744
05 feet Y = 1945155
59 meter
Z = -1198640
58 Z = -365345
65
XDOT = -3055
271827 XDOT = -931
246853
YDOT = -13793
232679 feet/sec YDOT = -4204
177321 meter/sec
ZDOT = -19767
541825 ZDOT = -6025
146748
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 09207
53105759
00010596 00000-0 82463-4 0 9069
2 25544 51
6404 104
8519 0006217 283
4904 76
5566 15
74010144 12157
Satellite: ISS
Catalog Number: 25544
Epoch time: 09207
53105759 = yrday
fracday
Element set: 906
Inclination: 51
6404 deg
RA of node: 104
8519 deg
Eccentricity:
0006217
Arg of perigee: 283
4904 deg
Mean anomaly: 76
5566 deg
Mean motion: 15
74010144 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1215
Checksum: 296
Coasting Arc #8 (Orbit 1230)
---------------------------------------
Vector Time (GMT): 2009/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3997537
71 A = 6719911
86 meter
Y = -1164104
58 meter E =
0004590
Z = 5277839
64 I = 51
94928
XDOT = 1570
517171 Wp = 309
75962
YDOT = -7522
452566 meter/sec RA = 99
06606 deg
ZDOT = -467
042977 TA = 144
67388
MA = 144
64345
Ha = 188
479 n
mi
Hp = 185
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13115281
22 X = -4009861
98
Y = -3819240
75 feet Y = -1208876
67 meter
Z = 17315746
84 Z = 5258389
73
XDOT = 5152
615390 XDOT = 1656
786589
YDOT = -24679
962488 feet/sec YDOT = -7504
407733 meter/sec
ZDOT = -1532
293233 ZDOT = -459
204442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4346163
22 X = 1324710
55
Y = 13051925
71 feet Y = 3978226
95 meter
Z = 17239210
85 Z = 5254511
47
XDOT = -22305
215064 XDOT = -6798
629552
YDOT = 9422
444033 feet/sec YDOT = 2871
960941 meter/sec
ZDOT = -1501
867888 ZDOT = -457
769332
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 09208
54685775
00010596 00000-0 82463-4 0 9073
2 25544 51
6404 99
6344 0006369 288
5232 71
5239 15
74089102 12312
Satellite: ISS
Catalog Number: 25544
Epoch time: 09208
54685775 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 99
6344 deg
Eccentricity:
0006369
Arg of perigee: 288
5232 deg
Mean anomaly: 71
5239 deg
Mean motion: 15
74089102 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1231
Checksum: 325
Coasting Arc #9 (Orbit 1246)
---------------------------------------
Vector Time (GMT): 2009/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -808104
06 A = 6731873
84 meter
Y = 6660878
18 meter E =
0011647
Z = 442820
22 I = 51
99321
XDOT = -4670
824628 Wp = 20
23129
YDOT = -971
185429 meter/sec RA = 93
96103 deg
ZDOT = 6048
491862 TA = 344
56292
MA = 344
59841
Ha = 188
690 n
mi
Hp = 185
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2651260
03 X = -884678
20
Y = 21853274
88 feet Y = 6651413
30 meter
Z = 1452822
25 Z = 438709
03
XDOT = -15324
227783 XDOT = -4688
999840
YDOT = -3186
303900 feet/sec YDOT = -1023
519453 meter/sec
ZDOT = 19844
133404 ZDOT = 6025
756888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19331825
21 X = 5892340
32
Y = -10531907
29 feet Y = -3210125
34 meter
Z = 1436996
21 Z = 437996
44
XDOT = 5609
133092 XDOT = 1709
663766
YDOT = 13007
601929 feet/sec YDOT = 3964
717068 meter/sec
ZDOT = 19754
689171 ZDOT = 6021
229259
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 09209
56264936
00010596 00000-0 82463-4 0 9089
2 25544 51
6406 94
4167 0006400 293
0424 67
0064 15
74078650 12479
Satellite: ISS
Catalog Number: 25544
Epoch time: 09209
56264936 = yrday
fracday
Element set: 908
Inclination: 51
6406 deg
RA of node: 94
4167 deg
Eccentricity:
0006400
Arg of perigee: 293
0424 deg
Mean anomaly: 67
0064 deg
Mean motion: 15
74078650 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1247
Checksum: 308
Coasting Arc #10 (Orbit 1261)
---------------------------------------
Vector Time (GMT): 2009/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4139238
70 A = 6719886
40 meter
Y = 534244
31 meter E =
0009248
Z = -5274305
28 I = 51
95398
XDOT = -281
651057 Wp = 78
82383
YDOT = 7669
441074 meter/sec RA = 88
83907 deg
ZDOT = 558
386183 TA = 196
44818
MA = 196
47821
Ha = 188
874 n
mi
Hp = 185
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13580179
46 X = 4158578
55
Y = 1752770
06 feet Y = 580640
36 meter
Z = -17304151
19 Z = -5254149
93
XDOT = -924
052025 XDOT = -370
103651
YDOT = 25162
208247 feet/sec YDOT = 7665
796867 meter/sec
ZDOT = 1831
975665 ZDOT = 556
803837
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6730097
60 X = -2051333
75
Y = -12038969
10 feet Y = -3669477
78 meter
Z = -17224869
66 Z = -5250140
27
XDOT = 19903
411885 XDOT = 6066
559943
YDOT = -13727
153143 feet/sec YDOT = -4184
036278 meter/sec
ZDOT = 1826
131608 ZDOT = 556
604914
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 09210
51494309
00010596 00000-0 82463-4 0 9096
2 25544 51
6407 89
5254 0006474 296
7642 63
2858 15
74109826 12621
Satellite: ISS
Catalog Number: 25544
Epoch time: 09210
51494309 = yrday
fracday
Element set: 909
Inclination: 51
6407 deg
RA of node: 89
5254 deg
Eccentricity:
0006474
Arg of perigee: 296
7642 deg
Mean anomaly: 63
2858 deg
Mean motion: 15
74109826 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1262
Checksum: 327
Coasting Arc #11 (Orbit 1277)
---------------------------------------
Vector Time (GMT): 2009/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -308720
26 A = 6731851
84 meter
Y = -6699438
24 meter E =
0005468
Z = -542568
11 I = 51
99232
XDOT = 4773
484935 Wp = 163
03476
YDOT = 267
094696 meter/sec RA = 83
73668 deg
ZDOT = -6034
348237 TA = 22
83927
MA = 22
81495
Ha = 188
966 n
mi
Hp = 185
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1012861
76 X = -231147
37
Y = -21979784
26 feet Y = -6702456
74 meter
Z = -1780079
11 Z = -543880
20
XDOT = 15661
039812 XDOT = 4799
457054
YDOT = 876
294936 feet/sec YDOT = 320
620506 meter/sec
ZDOT = -19797
730435 ZDOT = -6011
095667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16829538
62 X = -5129643
37
Y = 14173351
66 feet Y = 4320037
58 meter
Z = -1785558
54 Z = -544238
24
XDOT = -7873
441203 XDOT = -2399
824879
YDOT = -11823
231109 feet/sec YDOT = -3603
720842 meter/sec
ZDOT = -19706
278454 ZDOT = -6006
473673
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 09211
53071379
00010596 00000-0 82463-4 0 9109
2 25544 51
6409 84
3086 0006449 299
0821 60
9696 15
74067850 12787
Satellite: ISS
Catalog Number: 25544
Epoch time: 09211
53071379 = yrday
fracday
Element set: 910
Inclination: 51
6409 deg
RA of node: 84
3086 deg
Eccentricity:
0006449
Arg of perigee: 299
0821 deg
Mean anomaly: 60
9696 deg
Mean motion: 15
74067850 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1278
Checksum: 326
Coasting Arc #12 (Orbit 1293)
---------------------------------------
Vector Time (GMT): 2009/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4185833
86 A = 6719860
80 meter
Y = 67411
20 meter E =
0005783
Z = 5259358
13 I = 51
94812
XDOT = -986
472639 Wp = 331
32371
YDOT = -7605
111743 meter/sec RA = 78
61192 deg
ZDOT = -682
986098 TA = 125
17166
MA = 125
11748
Ha = 189
208 n
mi
Hp = 185
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13733050
72 X = -4211825
35
Y = 221165
36 feet Y = 20456
78 meter
Z = 17255111
97 Z = 5238960
40
XDOT = -3236
458789 XDOT = -898
039869
YDOT = -24951
154014 feet/sec YDOT = -7615
648520 meter/sec
ZDOT = -2240
768037 ZDOT = -687
564486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8780479
06 X = 2676290
02
Y = 10691612
16 feet Y = 3258803
38 meter
Z = 17174897
45 Z = 5234908
74
XDOT = -16747
920058 XDOT = -5104
766034
YDOT = 17407
892306 feet/sec YDOT = 5305
925575 meter/sec
ZDOT = -2259
125770 ZDOT = -688
581535
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 09212
54647117
00010596 00000-0 82463-4 0 9111
2 25544 51
6410 79
0908 0006592 304
3179 55
7360 15
74137927 12949
Satellite: ISS
Catalog Number: 25544
Epoch time: 09212
54647117 = yrday
fracday
Element set: 911
Inclination: 51
6410 deg
RA of node: 79
0908 deg
Eccentricity:
0006592
Arg of perigee: 304
3179 deg
Mean anomaly: 55
7360 deg
Mean motion: 15
74137927 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1294
Checksum: 310
Coasting Arc #13 (Orbit 1309)
---------------------------------------
Vector Time (GMT): 2009/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1404958
72 A = 6731534
74 meter
Y = 6542014
99 meter E =
0013374
Z = 652030
48 I = 51
97991
XDOT = -4785
800818 Wp = 22
90535
YDOT = 424
560001 meter/sec RA = 73
50979 deg
ZDOT = 6023
486098 TA = 344
16638
MA = 344
20815
Ha = 189
290 n
mi
Hp = 185
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4609444
62 X = 1328532
96
Y = 21463303
77 feet Y = 6557298
66 meter
Z = 2139207
62 Z = 658670
89
XDOT = -15701
446252 XDOT = -4819
453277
YDOT = 1392
913390 feet/sec YDOT = 370
853437 meter/sec
ZDOT = 19762
093497 ZDOT = 6000
155271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13648770
62 X = 4160145
28
Y = -17190629
69 feet Y = -5239703
93 meter
Z = 2165619
79 Z = 660080
91
XDOT = 9874
522493 XDOT = 3009
754456
YDOT = 10329
860332 feet/sec YDOT = 3148
541429 meter/sec
ZDOT = 19670
354202 ZDOT = 5995
523961
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 09213
56221849
00010596 00000-0 82463-4 0 9125
2 25544 51
6403 73
8728 0006669 307
9320 52
1240 15
74160985 13102
Satellite: ISS
Catalog Number: 25544
Epoch time: 09213
56221849 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 73
8728 deg
Eccentricity:
0006669
Arg of perigee: 307
9320 deg
Mean anomaly: 52
1240 deg
Mean motion: 15
74160985 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1310
Checksum: 297
Coasting Arc #14 (Orbit 1324)
---------------------------------------
Vector Time (GMT): 2009/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4155512
86 A = 6719835
06 meter
Y = -667852
55 meter E =
0010013
Z = -5246356
94 I = 51
92989
XDOT = 2210
042009 Wp = 73
39789
YDOT = 7324
523379 meter/sec RA = 68
38117 deg
ZDOT = 822
202418 TA = 204
37912
MA = 204
42651
Ha = 189
491 n
mi
Hp = 185
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13633572
38 X = 4188157
50
Y = -2191117
30 feet Y = -621199
99 meter
Z = -17212457
16 Z = -5226090
57
XDOT = 7250
793992 XDOT = 2123
979634
YDOT = 24030
588513 feet/sec YDOT = 7348
756061 meter/sec
ZDOT = 2697
514496 ZDOT = 832
730508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10577470
95 X = -3224013
15
Y = -9029345
09 feet Y = -2752144
38 meter
Z = -17132775
84 Z = -5222070
07
XDOT = 12934
825674 XDOT = 3942
534865
YDOT = -20324
642524 feet/sec YDOT = -6194
951041 meter/sec
ZDOT = 2739
248740 ZDOT = 834
923016
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 09214
51447280
00010596 00000-0 82463-4 0 9131
2 25544 51
6393 68
9806 0006715 311
9280 48
1310 15
74172695 13254
Satellite: ISS
Catalog Number: 25544
Epoch time: 09214
51447280 = yrday
fracday
Element set: 913
Inclination: 51
6393 deg
RA of node: 68
9806 deg
Eccentricity:
0006715
Arg of perigee: 311
9280 deg
Mean anomaly: 48
1310 deg
Mean motion: 15
74172695 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1325
Checksum: 305
Coasting Arc #15 (Orbit 1340)
---------------------------------------
Vector Time (GMT): 2009/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672678
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2434326
62 A = 6731450
62 meter
Y = -6222920
37 meter E =
0003740
Z = -796783
17 I = 51
95667
XDOT = 4708
595940 Wp = 151
10825
YDOT = -1076
450429 meter/sec RA = 63
28133 deg
ZDOT = -5993
345757 TA = 37
53859
MA = 37
51248
Ha = 189
584 n
mi
Hp = 185
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7986635
88 X = -2360689
38
Y = -20416405
41 feet Y = -6249730
62 meter
Z = -2614118
00 Z = -808430
75
XDOT = 15448
149410 XDOT = 4749
397075
YDOT = -3531
661512 feet/sec YDOT = -1023
567331 meter/sec
ZDOT = -19663
207864 ZDOT = -5970
372849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10031488
93 X = -3057597
83
Y = 19486972
83 feet Y = 5939629
32 meter
Z = -2660205
92 Z = -810830
76
XDOT = -11525
505730 XDOT = -3512
974146
YDOT = -8598
507264 feet/sec YDOT = -2620
825014 meter/sec
ZDOT = -19572
894085 ZDOT = -5965
818117
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 09215
53020012
00010596 00000-0 82463-4 0 9145
2 25544 51
6392 63
7637 0006720 315
1025 44
9594 15
74153124 13419
Satellite: ISS
Catalog Number: 25544
Epoch time: 09215
53020012 = yrday
fracday
Element set: 914
Inclination: 51
6392 deg
RA of node: 63
7637 deg
Eccentricity:
0006720
Arg of perigee: 315
1025 deg
Mean anomaly: 44
9594 deg
Mean motion: 15
74153124 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1341
Checksum: 274
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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