Date:
September 20th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 63 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 2031)
---------------------------------------
Vector Time (GMT): 2009/259/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6519495
92 A = 6731523
01 meter
Y = 1477790
81 meter E =
0021734
Z = 722326
32 I = 51
55287
XDOT = -421
517405 Wp = 113
88589
YDOT = 4844
783258 meter/sec RA = 197
69285 deg
ZDOT = -5974
990479 TA = 58
23005
MA = 58
01849
Ha = 193
208 n
mi
Hp = 180
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21389422
30 X = 6498977
56
Y = 4848395
05 feet Y = 1550580
98 meter
Z = 2369837
02 Z = 753947
84
XDOT = -1382
931120 XDOT = -446
636085
YDOT = 15894
958197 feet/sec YDOT = 4839
928751 meter/sec
ZDOT = -19602
987136 ZDOT = -5977
099536
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9915888
85 X = -3022362
92
Y = -19546951
72 feet Y = -5957910
88 meter
Z = 2494448
90 Z = 760308
03
XDOT = 11617
831060 XDOT = 3541
114907
YDOT = -8448
822755 feet/sec YDOT = -2575
201176 meter/sec
ZDOT = -19610
966778 ZDOT = -5977
422674
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 09259
40827893
00020000 00000-0 20000-3 0 9005
2 25544 51
6365 198
5461 0009185 93
5953 266
6261 15
74144048 20323
Satellite: ISS
Catalog Number: 25544
Epoch time: 09259
40827893 = yrday
fracday
Element set: 900
Inclination: 51
6365 deg
RA of node: 198
5461 deg
Eccentricity:
0009185
Arg of perigee: 93
5953 deg
Mean anomaly: 266
6261 deg
Mean motion: 15
74144048 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2032
Checksum: 310
Coasting Arc #2 (Orbit 2047)
---------------------------------------
Vector Time (GMT): 2009/260/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 57311
32 A = 6719909
90 meter
Y = -4228689
14 meter E =
0012123
Z = 5212485
85 I = 51
54248
XDOT = 7597
422664 Wp = 103
73771
YDOT = 1063
009720 meter/sec RA = 192
56417 deg
ZDOT = 774
510389 TA = 338
86724
MA = 338
91728
Ha = 193
172 n
mi
Hp = 180
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 188029
28 X = 79271
79
Y = -13873652
02 feet Y = -4227924
98 meter
Z = 17101331
53 Z = 5212817
99
XDOT = 24925
927374 XDOT = 7581
208832
YDOT = 3487
564698 feet/sec YDOT = 1147
877987 meter/sec
ZDOT = 2541
044582 ZDOT = 811
379021
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10581191
19 X = -3225147
08
Y = 8973130
71 feet Y = 2735010
24 meter
Z = 17102351
70 Z = 5212796
80
XDOT = -12932
330654 XDOT = -3941
774383
YDOT = -20396
975668 feet/sec YDOT = -6216
998184 meter/sec
ZDOT = 2686
300528 ZDOT = 818
784401
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 09260
42402123
00020000 00000-0 20000-3 0 9015
2 25544 51
6364 193
3287 0009061 97
6102 262
6090 15
74141648 20481
Satellite: ISS
Catalog Number: 25544
Epoch time: 09260
42402123 = yrday
fracday
Element set: 901
Inclination: 51
6364 deg
RA of node: 193
3287 deg
Eccentricity:
0009061
Arg of perigee: 97
6102 deg
Mean anomaly: 262
6090 deg
Mean motion: 15
74141648 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2048
Checksum: 268
Coasting Arc #3 (Orbit 2062)
---------------------------------------
Vector Time (GMT): 2009/261/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6689425
92 A = 6731458
82 meter
Y = -374769
86 meter E =
0017172
Z = -619923
26 I = 51
61157
XDOT = -272
315274 Wp = 68
69098
YDOT = -4823
853094 meter/sec RA = 187
41047 deg
ZDOT = 5993
526230 TA = 284
55862
MA = 284
74902
Ha = 193
115 n
mi
Hp = 180
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21946935
43 X = -6681726
52
Y = -1229559
91 feet Y = -449531
97 meter
Z = -2033868
95 Z = -652401
78
XDOT = -893
422814 XDOT = -247
469384
YDOT = -15826
289679 feet/sec YDOT = -4826
758749 meter/sec
ZDOT = 19663
799968 ZDOT = 5992
264167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13658290
76 X = 4163047
02
Y = 17207386
23 feet Y = 5244811
32 meter
Z = -2161797
40 Z = -658915
85
XDOT = -9900
916172 XDOT = -3017
799249
YDOT = 10274
713044 feet/sec YDOT = 3131
732536 meter/sec
ZDOT = 19658
499036 ZDOT = 5991
910506
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 09261
37626899
00020000 00000-0 20000-3 0 9029
2 25544 51
6366 188
4375 0009203 101
7566 258
4630 15
74183547 20639
Satellite: ISS
Catalog Number: 25544
Epoch time: 09261
37626899 = yrday
fracday
Element set: 902
Inclination: 51
6366 deg
RA of node: 188
4375 deg
Eccentricity:
0009203
Arg of perigee: 101
7566 deg
Mean anomaly: 258
4630 deg
Mean motion: 15
74183547 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2063
Checksum: 310
Coasting Arc #4 (Orbit 2078)
---------------------------------------
Vector Time (GMT): 2009/262/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 497555
48 A = 6719769
80 meter
Y = 4186222
93 meter E =
0023535
Z = -5252971
50 I = 51
60245
XDOT = -7658
941494 Wp = 92
88258
YDOT = 167
200293 meter/sec RA = 182
28226 deg
ZDOT = -595
651219 TA = 171
46096
MA = 171
42084
Ha = 193
086 n
mi
Hp = 180
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1632399
86 X = 476225
61
Y = 13734327
19 feet Y = 4191667
09 meter
Z = -17234158
46 Z = -5250606
59
XDOT = -25127
760808 XDOT = -7657
348337
YDOT = 548
557391 feet/sec YDOT = 81
562347 meter/sec
ZDOT = -1954
236284 ZDOT = -632
854772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8930254
73 X = 2721941
64
Y = -10577232
29 feet Y = -3223940
40 meter
Z = -17224557
99 Z = -5250045
27
XDOT = 16643
814654 XDOT = 5073
034707
YDOT = 17454
729488 feet/sec YDOT = 5320
201548 meter/sec
ZDOT = -2100
742152 ZDOT = -640
306208
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 09262
39198935
00020000 00000-0 20000-3 0 9038
2 25544 51
6374 183
2190 0009029 104
7814 255
4351 15
74167364 20794
Satellite: ISS
Catalog Number: 25544
Epoch time: 09262
39198935 = yrday
fracday
Element set: 903
Inclination: 51
6374 deg
RA of node: 183
2190 deg
Eccentricity:
0009029
Arg of perigee: 104
7814 deg
Mean anomaly: 255
4351 deg
Mean motion: 15
74167364 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2079
Checksum: 304
Coasting Arc #5 (Orbit 2094)
---------------------------------------
Vector Time (GMT): 2009/263/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6676251
73 A = 6731523
93 meter
Y = -668334
49 meter E =
0021624
Z = 422369
17 I = 51
67271
XDOT = 867
606598 Wp = 121
63114
YDOT = 4724
760191 meter/sec RA = 177
13579 deg
ZDOT = -6024
103032 TA = 53
77539
MA = 53
57568
Ha = 192
997 n
mi
Hp = 180
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21903713
01 X = 6681177
14
Y = -2192698
47 feet Y = -593649
14 meter
Z = 1385725
62 Z = 454814
82
XDOT = 2846
478341 XDOT = 843
973398
YDOT = 15501
181729 feet/sec YDOT = 4734
329601 meter/sec
ZDOT = -19764
117560 ZDOT = -6019
945975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16692362
67 X = -5087832
14
Y = -14337895
70 feet Y = -4370190
61 meter
Z = 1513466
64 Z = 461304
63
XDOT = 8132
770161 XDOT = 2478
868345
YDOT = -11620
505753 feet/sec YDOT = -3541
930154 meter/sec
ZDOT = -19747
423907 ZDOT = -6019
014807
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 09263
40769805
00020000 00000-0 20000-3 0 9042
2 25544 51
6377 178
0012 0008949 108
1629 252
0510 15
74199633 20956
Satellite: ISS
Catalog Number: 25544
Epoch time: 09263
40769805 = yrday
fracday
Element set: 904
Inclination: 51
6377 deg
RA of node: 178
0012 deg
Eccentricity:
0008949
Arg of perigee: 108
1629 deg
Mean anomaly: 252
0510 deg
Mean motion: 15
74199633 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2095
Checksum: 300
Coasting Arc #6 (Orbit 2110)
---------------------------------------
Vector Time (GMT): 2009/264/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1026251
13 A = 6719502
26 meter
Y = -4050926
79 meter E =
0011496
Z = 5253100
88 I = 51
66238
XDOT = 7573
360545 Wp = 111
92402
YDOT = -1386
679180 meter/sec RA = 172
00988 deg
ZDOT = 405
278890 TA = 334
20469
MA = 334
26197
Ha = 192
927 n
mi
Hp = 180
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3366965
67 X = -1006395
70
Y = -13290442
22 feet Y = -4062291
54 meter
Z = 17234582
95 Z = 5248163
80
XDOT = 24846
983414 XDOT = 7586
334956
YDOT = -4549
472374 feet/sec YDOT = -1301
916831 meter/sec
ZDOT = 1329
655150 ZDOT = 442
102443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7027067
55 X = -2141850
19
Y = 11801351
21 feet Y = 3597051
85 meter
Z = 17214865
46 Z = 5247090
99
XDOT = -19820
906755 XDOT = -6041
412379
YDOT = -13976
898904 feet/sec YDOT = -4260
158786 meter/sec
ZDOT = 1474
600765 ZDOT = 449
458313
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 09264
42339490
00020000 00000-0 20000-3 0 9059
2 25544 51
6377 172
7844 0008832 112
1225 248
0877 15
74230146 21113
Satellite: ISS
Catalog Number: 25544
Epoch time: 09264
42339490 = yrday
fracday
Element set: 905
Inclination: 51
6377 deg
RA of node: 172
7844 deg
Eccentricity:
0008832
Arg of perigee: 112
1225 deg
Mean anomaly: 248
0877 deg
Mean motion: 15
74230146 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2111
Checksum: 284
Coasting Arc #7 (Orbit 2125)
---------------------------------------
Vector Time (GMT): 2009/265/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6495142
99 A = 6731449
52 meter
Y = 1736818
99 meter E =
0016535
Z = -273783
66 I = 51
73171
XDOT = -1458
120484 Wp = 73
99216
YDOT = -4549
405565 meter/sec RA = 166
87006 deg
ZDOT = 6036
221852 TA = 283
03725
MA = 283
22179
Ha = 192
838 n
mi
Hp = 180
414
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21309524
24 X = -6512751
65
Y = 5698225
03 feet Y = 1664088
01 meter
Z = -898240
36 Z = -305380
42
XDOT = -4783
859856 XDOT = -1436
463212
YDOT = -14925
871277 feet/sec YDOT = -4565
589730 meter/sec
ZDOT = 19803
877468 ZDOT = 6029
191028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19206303
08 X = 5854081
18
Y = 10837188
92 feet Y = 3303175
18 meter
Z = -1022587
88 Z = -311684
79
XDOT = -6154
283729 XDOT = -1875
825681
YDOT = 12690
170812 feet/sec YDOT = 3867
964064 meter/sec
ZDOT = 19775
882451 ZDOT = 6027
688971
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 09265
37560068
00020000 00000-0 20000-3 0 9062
2 25544 51
6372 167
8924 0008877 115
7872 244
4208 15
74238375 21264
Satellite: ISS
Catalog Number: 25544
Epoch time: 09265
37560068 = yrday
fracday
Element set: 906
Inclination: 51
6372 deg
RA of node: 167
8924 deg
Eccentricity:
0008877
Arg of perigee: 115
7872 deg
Mean anomaly: 244
4208 deg
Mean motion: 15
74238375 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2126
Checksum: 318
Coasting Arc #8 (Orbit 2141)
---------------------------------------
Vector Time (GMT): 2009/266/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1488928
11 A = 6719432
38 meter
Y = 3900222
64 meter E =
0022976
Z = -5284459
48 I = 51
72054
XDOT = -7251
528026 Wp = 100
05721
YDOT = 2537
522391 meter/sec RA = 161
74298 deg
ZDOT = -174
900156 TA = 168
30811
MA = 168
25466
Ha = 192
767 n
mi
Hp = 180
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4884934
75 X = 1470875
81
Y = 12796006
04 feet Y = 3916771
61 meter
Z = -17337465
50 Z = -5277270
14
XDOT = -23791
102449 XDOT = -7278
514441
YDOT = 8325
204695 feet/sec YDOT = 2456
280642 meter/sec
ZDOT = -573
819411 ZDOT = -210
194217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5174175
69 X = 1577088
75
Y = -12720781
63 feet Y = -3877294
24 meter
Z = -17308890
45 Z = -5275749
81
XDOT = 22071
705737 XDOT = 6727
455909
YDOT = 9926
974481 feet/sec YDOT = 3025
741822 meter/sec
ZDOT = -712
694563 ZDOT = -217
229303
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 09266
39127527
00020000 00000-0 20000-3 0 9075
2 25544 51
6377 162
6738 0008756 119
4356 240
7682 15
74243462 21425
Satellite: ISS
Catalog Number: 25544
Epoch time: 09266
39127527 = yrday
fracday
Element set: 907
Inclination: 51
6377 deg
RA of node: 162
6738 deg
Eccentricity:
0008756
Arg of perigee: 119
4356 deg
Mean anomaly: 240
7682 deg
Mean motion: 15
74243462 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2142
Checksum: 312
Coasting Arc #9 (Orbit 2157)
---------------------------------------
Vector Time (GMT): 2009/267/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6159646
72 A = 6731447
96 meter
Y = -2691897
23 meter E =
0021096
Z = 32495
97 I = 51
78973
XDOT = 1946
859115 Wp = 129
93748
YDOT = 4350
827068 meter/sec RA = 156
61168 deg
ZDOT = -6054
487934 TA = 49
71002
MA = 49
52582
Ha = 192
740 n
mi
Hp = 180
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20208814
71 X = 6189132
32
Y = -8831683
83 feet Y = -2622851
57 meter
Z = 106614
06 Z = 62491
55
XDOT = 6387
333055 XDOT = 1927
474675
YDOT = 14274
367020 feet/sec YDOT = 4372
489492 meter/sec
ZDOT = -19863
805557 ZDOT = -6045
077150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20873198
37 X = -6362150
86
Y = -7117958
49 feet Y = -2169553
75 meter
Z = 224621
46 Z = 68464
62
XDOT = 4313
432050 XDOT = 1314
734089
YDOT = -13400
547647 feet/sec YDOT = -4084
486923 meter/sec
ZDOT = -19826
450148 ZDOT = -6043
102005
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 09267
40693853
00020000 00000-0 20000-3 0 9089
2 25544 51
6382 157
4557 0008789 123
3028 236
8978 15
74258025 21580
Satellite: ISS
Catalog Number: 25544
Epoch time: 09267
40693853 = yrday
fracday
Element set: 908
Inclination: 51
6382 deg
RA of node: 157
4557 deg
Eccentricity:
0008789
Arg of perigee: 123
3028 deg
Mean anomaly: 236
8978 deg
Mean motion: 15
74258025 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2158
Checksum: 331
Coasting Arc #10 (Orbit 2173)
---------------------------------------
Vector Time (GMT): 2009/268/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1918900
68 A = 6719177
28 meter
Y = -3684185
35 meter E =
0010568
Z = 5273370
84 I = 51
77590
XDOT = 6799
448870 Wp = 119
54757
YDOT = -3632
559651 meter/sec RA = 151
48511 deg
ZDOT = -68
644065 TA = 331
07258
MA = 331
13112
Ha = 192
597 n
mi
Hp = 180
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6295605
89 X = -1903178
16
Y = -12087222
27 feet Y = -3705555
64 meter
Z = 17301085
45 Z = 5264086
99
XDOT = 22307
903118 XDOT = 6839
896890
YDOT = -11917
846625 feet/sec YDOT = -3556
298057 meter/sec
ZDOT = -225
210187 ZDOT = -35
513761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3207190
44 X = -977551
65
Y = 13293683
11 feet Y = 4051914
61 meter
Z = 17264271
56 Z = 5262149
97
XDOT = -23640
883836 XDOT = -7205
741393
YDOT = -5601
683868 feet/sec YDOT = -1707
393243 meter/sec
ZDOT = -94
894963 ZDOT = -28
923985
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 09268
42258830
00020000 00000-0 20000-3 0 9095
2 25544 51
6382 152
2382 0008609 127
3724 232
8224 15
74320594 21746
Satellite: ISS
Catalog Number: 25544
Epoch time: 09268
42258830 = yrday
fracday
Element set: 909
Inclination: 51
6382 deg
RA of node: 152
2382 deg
Eccentricity:
0008609
Arg of perigee: 127
3724 deg
Mean anomaly: 232
8224 deg
Mean motion: 15
74320594 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2174
Checksum: 293
Coasting Arc #11 (Orbit 2189)
---------------------------------------
Vector Time (GMT): 2009/269/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5670916
83 A = 6731316
85 meter
Y = 3618470
42 meter E =
0015953
Z = 164107
31 I = 51
84228
XDOT = -2424
455912 Wp = 79
45444
YDOT = -4096
313878 meter/sec RA = 146
36075 deg
ZDOT = 6049
685934 TA = 282
32291
MA = 282
50147
Ha = 192
515 n
mi
Hp = 180
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18605370
19 X = -5711754
93
Y = 11871622
10 feet Y = 3554826
55 meter
Z = 538409
81 Z = 136458
59
XDOT = -7954
251681 XDOT = -2407
858474
YDOT = -13439
349995 feet/sec YDOT = -4123
332669 meter/sec
ZDOT = 19848
050963 ZDOT = 6037
948246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21861599
56 X = 6663415
54
Y = 3044821
40 feet Y = 928061
56 meter
Z = 429678
91 Z = 130966
13
XDOT = -2360
344687 XDOT = -719
433060
YDOT = 13867
448686 feet/sec YDOT = 4226
798359 meter/sec
ZDOT = 19801
539355 ZDOT = 6035
509195
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 09269
43822921
00020000 00000-0 20000-3 0 9107
2 25544 51
6381 147
0195 0008632 130
6173 229
5742 15
74301210 21900
Satellite: ISS
Catalog Number: 25544
Epoch time: 09269
43822921 = yrday
fracday
Element set: 910
Inclination: 51
6381 deg
RA of node: 147
0195 deg
Eccentricity:
0008632
Arg of perigee: 130
6173 deg
Mean anomaly: 229
5742 deg
Mean motion: 15
74301210 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2190
Checksum: 269
Coasting Arc #12 (Orbit 2204)
---------------------------------------
Vector Time (GMT): 2009/270/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2294338
64 A = 6719216
50 meter
Y = 3485880
71 meter E =
0022187
Z = -5284575
85 I = 51
82686
XDOT = -6154
617506 Wp = 107
75450
YDOT = 4589
795549 meter/sec RA = 141
23193 deg
ZDOT = 350
091340 TA = 165
59894
MA = 165
53560
Ha = 192
420 n
mi
Hp = 180
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7527357
74 X = 2280859
99
Y = 11436616
49 feet Y = 3511461
85 meter
Z = -17337847
27 Z = -5273462
75
XDOT = -20192
314652 XDOT = -6207
184653
YDOT = 15058
384347 feet/sec YDOT = 4520
677084 meter/sec
ZDOT = 1148
593635 ZDOT = 320
064310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1383481
48 X = 421685
16
Y = -13677266
10 feet Y = -4168830
71 meter
Z = -17293832
15 Z = -5271160
04
XDOT = 24167
169672 XDOT = 7366
153316
YDOT = 1118
998817 feet/sec YDOT = 341
070839 meter/sec
ZDOT = 1030
537202 ZDOT = 314
107739
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 09270
39038031
00020000 00000-0 20000-3 0 9116
2 25544 51
6391 142
1269 0008616 134
2079 225
9794 15
74325219 22055
Satellite: ISS
Catalog Number: 25544
Epoch time: 09270
39038031 = yrday
fracday
Element set: 911
Inclination: 51
6391 deg
RA of node: 142
1269 deg
Eccentricity:
0008616
Arg of perigee: 134
2079 deg
Mean anomaly: 225
9794 deg
Mean motion: 15
74325219 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2205
Checksum: 283
Coasting Arc #13 (Orbit 2220)
---------------------------------------
Vector Time (GMT): 2009/271/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5071033
08 A = 6731197
57 meter
Y = -4389463
30 meter E =
0019999
Z = -448133
25 I = 51
89017
XDOT = 2822
677035 Wp = 138
61558
YDOT = 3860
806179 meter/sec RA = 136
11647 deg
ZDOT = -6042
172146 TA = 46
24491
MA = 46
07955
Ha = 192
406 n
mi
Hp = 180
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16637247
65 X = 5121916
88
Y = -14401126
31 feet Y = -4332471
53 meter
Z = -1470253
43 Z = -423374
35
XDOT = 9260
751426 XDOT = 2808
646883
YDOT = 12666
686940 feet/sec YDOT = 3892
292325 meter/sec
ZDOT = -19823
399428 ZDOT = -6028
493790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21991779
34 X = -6703094
34
Y = 910372
73 feet Y = 277481
61 meter
Z = -1372937
16 Z = -418471
25
XDOT = 612
024169 XDOT = 186
544967
YDOT = -14146
025842 feet/sec YDOT = -4311
708677 meter/sec
ZDOT = -19769
247056 ZDOT = -6025
666503
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 09271
40599748
00020000 00000-0 20000-3 0 9127
2 25544 51
6395 136
9085 0008640 138
5755 221
6065 15
74319545 22218
Satellite: ISS
Catalog Number: 25544
Epoch time: 09271
40599748 = yrday
fracday
Element set: 912
Inclination: 51
6395 deg
RA of node: 136
9085 deg
Eccentricity:
0008640
Arg of perigee: 138
5755 deg
Mean anomaly: 221
6065 deg
Mean motion: 15
74319545 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2221
Checksum: 307
Coasting Arc #14 (Orbit 2236)
---------------------------------------
Vector Time (GMT): 2009/272/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2643821
64 A = 6719070
12 meter
Y = -3241494
01 meter E =
0009467
Z = 5251122
37 I = 51
87062
XDOT = 5410
187865 Wp = 125
38924
YDOT = -5452
846526 meter/sec RA = 130
98610 deg
ZDOT = -646
671433 TA = 330
70627
MA = 330
75932
Ha = 192
211 n
mi
Hp = 180
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8673955
51 X = -2632887
26
Y = -10634822
88 feet Y = -3270997
34 meter
Z = 17228091
77 Z = 5238305
41
XDOT = 17749
960187 XDOT = 5473
901859
YDOT = -17889
916424 feet/sec YDOT = -5391
990413 meter/sec
ZDOT = -2121
625436 ZDOT = -620
233612
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 485029
81 X = 147837
08
Y = 13778490
98 feet Y = 4199684
05 meter
Z = 17177370
00 Z = 5235662
37
XDOT = -23978
077333 XDOT = -7308
517971
YDOT = 3340
849264 feet/sec YDOT = 1018
290856 meter/sec
ZDOT = -2017
748323 ZDOT = -615
009689
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 09272
42160048
00020000 00000-0 20000-3 0 9138
2 25544 51
6393 131
6904 0008416 142
6216 217
5534 15
74401610 22374
Satellite: ISS
Catalog Number: 25544
Epoch time: 09272
42160048 = yrday
fracday
Element set: 913
Inclination: 51
6393 deg
RA of node: 131
6904 deg
Eccentricity:
0008416
Arg of perigee: 142
6216 deg
Mean anomaly: 217
5534 deg
Mean motion: 15
74401610 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2237
Checksum: 264
Coasting Arc #15 (Orbit 2252)
---------------------------------------
Vector Time (GMT): 2009/273/09:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 711041
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4349136
24 A = 6730926
79 meter
Y = 5087361
40 meter E =
0015350
Z = 692581
57 I = 51
92925
XDOT = -3215
851992 Wp = 85
36254
YDOT = -3582
249026 meter/sec RA = 125
87776 deg
ZDOT = 6006
963716 TA = 282
15010
MA = 282
32202
Ha = 192
096 n
mi
Hp = 181
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14268819
67 X = -4409065
20
Y = 16690818
25 feet Y = 5038391
77 meter
Z = 2272249
26 Z = 671307
44
XDOT = -10550
695513 XDOT = -3204
736509
YDOT = -11752
785518 feet/sec YDOT = -3618
147971 meter/sec
ZDOT = 19707
886207 ZDOT = 5991
368322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21410669
91 X = 6525972
19
Y = -4913101
13 feet Y = -1497513
23 meter
Z = 2188697
51 Z = 667115
00
XDOT = 1218
134667 XDOT = 371
287446
YDOT = 14230
736872 feet/sec YDOT = 4337
528599 meter/sec
ZDOT = 19646
188906 ZDOT = 5988
158379
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 09273
43719492
00020000 00000-0 20000-3 0 9144
2 25544 51
6396 126
4716 0008395 145
6818 214
4890 15
74373318 22539
Satellite: ISS
Catalog Number: 25544
Epoch time: 09273
43719492 = yrday
fracday
Element set: 914
Inclination: 51
6396 deg
RA of node: 126
4716 deg
Eccentricity:
0008395
Arg of perigee: 145
6818 deg
Mean anomaly: 214
4890 deg
Mean motion: 15
74373318 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2253
Checksum: 315
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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