Date:
October 8th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9149 32 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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 604)
---------------------------------------
Vector Time (GMT): 2008/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2613882
52 A = 6726327
97 meter
Y = 3485940
15 meter E =
0012940
Z = -5135170
18 I = 51
71051
XDOT = -6901
796868 Wp = 95
45936
YDOT = 3070
194220 meter/sec RA = 164
63332 deg
ZDOT = -1433
254550 TA = 160
82593
MA = 160
77719
Ha = 193
337 n
mi
Hp = 186
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8575730
06 X = 2599654
00
Y = 11436811
52 feet Y = 3515090
53 meter
Z = -16847671
18 Z = -5122506
32
XDOT = -22643
690511 XDOT = -6928
652723
YDOT = 10072
815684 feet/sec YDOT = 2992
864183 meter/sec
ZDOT = -4702
278707 ZDOT = -1466
849205
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11300476
64 X = -3444385
28
Y = -8848982
94 feet Y = -2697170
00 meter
Z = -16798290
29 Z = -5120118
88
XDOT = 18657
218057 XDOT = 5686
720064
YDOT = -14679
987929 feet/sec YDOT = -4474
460321 meter/sec
ZDOT = -4832
018924 ZDOT = -1472
799368
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 08280
51841444
00020000 00000-0 20000-3 0 9008
2 25544 51
6423 165
5302 0003916 191
1489 168
9587 15
72069013 6056
Satellite: ISS
Catalog Number: 25544
Epoch time: 08280
51841444 = yrday
fracday
Element set: 900
Inclination: 51
6423 deg
RA of node: 165
5302 deg
Eccentricity:
0003916
Arg of perigee: 191
1489 deg
Mean anomaly: 168
9587 deg
Mean motion: 15
72069013 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 605
Checksum: 286
Coasting Arc #2 (Orbit 620)
---------------------------------------
Vector Time (GMT): 2008/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5391774
90 A = 6736217
74 meter
Y = -3572701
67 meter E =
0015291
Z = 1849907
61 I = 51
77161
XDOT = 4094
438844 Wp = 128
59842
YDOT = 3233
878573 meter/sec RA = 159
49098 deg
ZDOT = -5666
207000 TA = 30
91120
MA = 30
82128
Ha = 193
293 n
mi
Hp = 186
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17689550
20 X = 5422338
07
Y = -11721462
17 feet Y = -3512236
83 meter
Z = 6069250
70 Z = 1876175
43
XDOT = 13433
198306 XDOT = 4085
498518
YDOT = 10609
837838 feet/sec YDOT = 3279
614923 meter/sec
ZDOT = -18589
917980 ZDOT = -5646
337721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13809837
98 X = -4209238
62
Y = 16073608
55 feet Y = 4899235
89 meter
Z = 6170587
40 Z = 1880795
04
XDOT = -14739
055525 XDOT = -4492
464124
YDOT = -5529
089932 feet/sec YDOT = -1685
266611 meter/sec
ZDOT = -18512
660783 ZDOT = -5642
659007
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 08281
53550362
00020000 00000-0 20000-3 0 9018
2 25544 51
6422 160
3223 0004011 193
7684 166
3369 15
72045017 6218
Satellite: ISS
Catalog Number: 25544
Epoch time: 08281
53550362 = yrday
fracday
Element set: 901
Inclination: 51
6422 deg
RA of node: 160
3223 deg
Eccentricity:
0004011
Arg of perigee: 193
7684 deg
Mean anomaly: 166
3369 deg
Mean motion: 15
72045017 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 621
Checksum: 258
Coasting Arc #3 (Orbit 636)
---------------------------------------
Vector Time (GMT): 2008/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4384306
76 A = 6728179
26 meter
Y = -2000088
34 meter E =
0009301
Z = 4693582
61 I = 51
77193
XDOT = 5226
742699 Wp = 141
62090
YDOT = -4924
670633 meter/sec RA = 154
41727 deg
ZDOT = 2773
702008 TA = 281
02646
MA = 281
13106
Ha = 193
195 n
mi
Hp = 187
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14384208
52 X = -4384416
39
Y = -6561969
64 feet Y = -2049116
72 meter
Z = 15398893
09 Z = 4672283
22
XDOT = 17148
105968 XDOT = 5267
948421
YDOT = -16157
055881 feet/sec YDOT = -4865
991731 meter/sec
ZDOT = 9100
072206 ZDOT = 2799
193959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15748804
32 X = 4800235
56
Y = 2116479
97 feet Y = 645103
10 meter
Z = 15316216
36 Z = 4668382
75
XDOT = -11564
545877 XDOT = -3524
873583
YDOT = 19247
137509 feet/sec YDOT = 5866
527513 meter/sec
ZDOT = 9198
277361 ZDOT = 2803
634940
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 08282
55257455
00020000 00000-0 20000-3 0 9029
2 25544 51
6424 155
1137 0003853 199
7128 160
3886 15
72083720 6376
Satellite: ISS
Catalog Number: 25544
Epoch time: 08282
55257455 = yrday
fracday
Element set: 902
Inclination: 51
6424 deg
RA of node: 155
1137 deg
Eccentricity:
0003853
Arg of perigee: 199
7128 deg
Mean anomaly: 160
3886 deg
Mean motion: 15
72083720 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 637
Checksum: 297
Coasting Arc #4 (Orbit 651)
---------------------------------------
Vector Time (GMT): 2008/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3616794
92 A = 6733702
06 meter
Y = 4853901
08 meter E =
0003069
Z = -2954231
34 I = 51
81661
XDOT = -5705
177672 Wp = 126
98660
YDOT = -1198
371189 meter/sec RA = 149
26161 deg
ZDOT = 5017
510046 TA = 199
09687
MA = 199
10837
Ha = 192
865 n
mi
Hp = 187
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11866125
06 X = -3656451
96
Y = 15924872
32 feet Y = 4813234
15 meter
Z = -9692360
03 Z = -2971898
39
XDOT = -18717
774513 XDOT = -5715
727645
YDOT = -3931
664005 feet/sec YDOT = -1262
228579 meter/sec
ZDOT = 16461
647131 ZDOT = 4989
768464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6402507
83 X = 1951484
39
Y = -18764145
61 feet Y = -5719311
58 meter
Z = -9760279
61 Z = -2974933
23
XDOT = 17747
589581 XDOT = 5409
465304
YDOT = -2448
045444 feet/sec YDOT = -746
164251 meter/sec
ZDOT = 16354
097780 ZDOT = 4984
729003
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 08283
50606349
00020000 00000-0 20000-3 0 9036
2 25544 51
6420 150
2306 0003886 207
1607 152
9353 15
72116615 6521
Satellite: ISS
Catalog Number: 25544
Epoch time: 08283
50606349 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 150
2306 deg
Eccentricity:
0003886
Arg of perigee: 207
1607 deg
Mean anomaly: 152
9353 deg
Mean motion: 15
72116615 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 652
Checksum: 269
Coasting Arc #5 (Orbit 667)
---------------------------------------
Vector Time (GMT): 2008/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5390095
76 A = 6730545
27 meter
Y = 22395
76 meter E =
0004810
Z = -4033853
85 I = 51
82976
XDOT = -2952
824218 Wp = 104
02883
YDOT = 5926
358938 meter/sec RA = 144
20268 deg
ZDOT = -3917
726539 TA = 125
62325
MA = 125
57844
Ha = 192
800 n
mi
Hp = 187
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17684041
22 X = 5409040
65
Y = 73476
91 feet Y = 82776
62 meter
Z = -13234428
64 Z = -4007622
49
XDOT = -9687
743496 XDOT = -2999
842464
YDOT = 19443
434837 feet/sec YDOT = 5893
075630 meter/sec
ZDOT = -12853
433528 ZDOT = -3932
186055
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16844915
75 X = -5134330
32
Y = 5626556
50 feet Y = 1714974
42 meter
Z = -13132840
12 Z = -4002889
67
XDOT = 3280
141808 XDOT = 999
787223
YDOT = -20271
334391 feet/sec YDOT = -6178
702722 meter/sec
ZDOT = -12908
826746 ZDOT = -3934
610392
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 08284
52310359
00020000 00000-0 20000-3 0 9043
2 25544 51
6414 145
0221 0003972 211
9899 148
1022 15
72133408 6680
Satellite: ISS
Catalog Number: 25544
Epoch time: 08284
52310359 = yrday
fracday
Element set: 904
Inclination: 51
6414 deg
RA of node: 145
0221 deg
Eccentricity:
0003972
Arg of perigee: 211
9899 deg
Mean anomaly: 148
1022 deg
Mean motion: 15
72133408 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 668
Checksum: 275
Coasting Arc #6 (Orbit 683)
---------------------------------------
Vector Time (GMT): 2008/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1489678
03 A = 6730769
64 meter
Y = -5304477
22 meter E =
0008896
Z = 3857505
04 I = 51
85491
XDOT = 6375
635841 Wp = 98
50711
YDOT = -1226
432314 meter/sec RA = 139
04422 deg
ZDOT = -4141
805342 TA = 34
66755
MA = 34
60960
Ha = 192
452 n
mi
Hp = 187
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4887395
12 X = 1530143
54
Y = -17403140
49 feet Y = -5287592
23 meter
Z = 12655856
43 Z = 3864840
69
XDOT = 20917
440423 XDOT = 6408
996551
YDOT = -4023
728065 feet/sec YDOT = -1154
950063 meter/sec
ZDOT = -13588
600205 ZDOT = -4110
750984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1331313
20 X = 405784
26
Y = 18007701
37 feet Y = 5488747
38 meter
Z = 12683726
92 Z = 3865999
97
XDOT = -17097
973556 XDOT = -5211
462340
YDOT = 10766
220299 feet/sec YDOT = 3281
543947 meter/sec
ZDOT = -13468
454121 ZDOT = -4105
184816
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 08285
54012629
00020000 00000-0 20000-3 0 9056
2 25544 51
6417 139
8133 0003856 217
6986 142
3907 15
72215780 6847
Satellite: ISS
Catalog Number: 25544
Epoch time: 08285
54012629 = yrday
fracday
Element set: 905
Inclination: 51
6417 deg
RA of node: 139
8133 deg
Eccentricity:
0003856
Arg of perigee: 217
6986 deg
Mean anomaly: 142
3907 deg
Mean motion: 15
72215780 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 684
Checksum: 305
Coasting Arc #7 (Orbit 699)
---------------------------------------
Vector Time (GMT): 2008/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5533821
05 A = 6733052
57 meter
Y = 2158529
53 meter E =
0010577
Z = 3163841
42 I = 51
88203
XDOT = 459
316625 Wp = 100
98241
YDOT = -5957
908772 meter/sec RA = 133
98817 deg
ZDOT = 4852
566345 TA = 295
71184
MA = 295
82101
Ha = 192
425 n
mi
Hp = 187
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18155580
88 X = -5572916
43
Y = 7081789
80 feet Y = 2096428
83 meter
Z = 10380057
15 Z = 3136862
49
XDOT = 1506
944309 XDOT = 502
331484
YDOT = -19546
944791 feet/sec YDOT = -5952
531488 meter/sec
ZDOT = 15920
493257 ZDOT = 4854
902759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14540561
34 X = 4431963
10
Y = -13057671
21 feet Y = -3979978
18 meter
Z = 10275784
57 Z = 3132059
14
XDOT = 4625
845166 XDOT = 1409
957607
YDOT = 17727
196572 feet/sec YDOT = 5403
249515 meter/sec
ZDOT = 15928
938965 ZDOT = 4855
140597
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 08286
55713467
00020000 00000-0 20000-3 0 9067
2 25544 51
6402 134
6037 0003938 221
5544 138
5319 15
72201018 7004
Satellite: ISS
Catalog Number: 25544
Epoch time: 08286
55713467 = yrday
fracday
Element set: 906
Inclination: 51
6402 deg
RA of node: 134
6037 deg
Eccentricity:
0003938
Arg of perigee: 221
5544 deg
Mean anomaly: 138
5319 deg
Mean motion: 15
72201018 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 700
Checksum: 273
Coasting Arc #8 (Orbit 714)
---------------------------------------
Vector Time (GMT): 2008/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 644914
51 A = 6728218
14 meter
Y = 4909391
09 meter E =
0009352
Z = -4564378
59 I = 51
88435
XDOT = -6031
609869 Wp = 133
11122
YDOT = 3649
930280 meter/sec RA = 128
83507 deg
ZDOT = 3071
281944 TA = 167
40688
MA = 167
38350
Ha = 192
263 n
mi
Hp = 187
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2115861
26 X = 612142
42
Y = 16106926
15 feet Y = 4916419
26 meter
Z = -14974995
39 Z = -4561325
56
XDOT = -19788
746290 XDOT = -6086
895775
YDOT = 11974
836876 feet/sec YDOT = 3582
172484 meter/sec
ZDOT = 10076
384331 ZDOT = 3041
845091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7992248
65 X = -2436037
39
Y = -14156364
38 feet Y = -4314859
86 meter
Z = -14962678
07 Z = -4560624
28
XDOT = 12991
322441 XDOT = 3959
755080
YDOT = -17872
728236 feet/sec YDOT = -5447
607566 meter/sec
ZDOT = 9962
736006 ZDOT = 3036
641935
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 08287
51056415
00020000 00000-0 20000-3 0 9078
2 25544 51
6389 129
7191 0003941 224
0450 136
0399 15
72226679 7159
Satellite: ISS
Catalog Number: 25544
Epoch time: 08287
51056415 = yrday
fracday
Element set: 907
Inclination: 51
6389 deg
RA of node: 129
7191 deg
Eccentricity:
0003941
Arg of perigee: 224
0450 deg
Mean anomaly: 136
0399 deg
Mean motion: 15
72226679 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 715
Checksum: 299
Coasting Arc #9 (Orbit 730)
---------------------------------------
Vector Time (GMT): 2008/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4833071
26 A = 6735164
06 meter
Y = -4142164
43 meter E =
0007344
Z = -2188803
59 I = 51
92450
XDOT = 1828
148789 Wp = 170
75697
YDOT = 5044
589673 meter/sec RA = 123
77391 deg
ZDOT = -5519
460644 TA = 33
64183
MA = 33
59523
Ha = 192
187 n
mi
Hp = 187
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15856533
02 X = 4889663
53
Y = -13589778
32 feet Y = -4087801
97 meter
Z = -7181114
14 Z = -2165186
08
XDOT = 5997
863482 XDOT = 1798
416819
YDOT = 16550
491052 feet/sec YDOT = 5064
866446 meter/sec
ZDOT = -18108
466680 ZDOT = -5510
651830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9437977
62 X = -2876695
58
Y = 18663760
21 feet Y = 5688714
11 meter
Z = -7090045
66 Z = -2161045
92
XDOT = -10643
527888 XDOT = -3244
147300
YDOT = -12236
066446 feet/sec YDOT = -3729
553053 meter/sec
ZDOT = -18073
848927 ZDOT = -5508
909153
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 08288
52753943
00020000 00000-0 20000-3 0 9081
2 25544 51
6383 124
5104 0003936 228
9535 131
1288 15
72239704 7315
Satellite: ISS
Catalog Number: 25544
Epoch time: 08288
52753943 = yrday
fracday
Element set: 908
Inclination: 51
6383 deg
RA of node: 124
5104 deg
Eccentricity:
0003936
Arg of perigee: 228
9535 deg
Mean anomaly: 131
1288 deg
Mean motion: 15
72239704 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 731
Checksum: 298
Coasting Arc #10 (Orbit 746)
---------------------------------------
Vector Time (GMT): 2008/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2449055
27 A = 6726222
36 meter
Y = -3736766
11 meter E =
0001628
Z = 5026979
17 I = 51
90960
XDOT = 4809
096709 Wp = 62
35763
YDOT = -5705
168011 meter/sec RA = 118
63553 deg
ZDOT = -1896
781706 TA = 45
89112
MA = 45
87772
Ha = 192
090 n
mi
Hp = 187
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8034958
25 X = -2431509
09
Y = -12259731
34 feet Y = -3764054
53 meter
Z = 16492713
80 Z = 5015124
06
XDOT = 15777
876343 XDOT = 4881
749921
YDOT = -18717
742819 feet/sec YDOT = -5650
983776 meter/sec
ZDOT = -6223
037092 ZDOT = -1873
241606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12362522
06 X = 3768096
72
Y = 7972083
77 feet Y = 2429891
13 meter
Z = 16446431
34 Z = 5012872
27
XDOT = -6401
243271 XDOT = -1951
098949
YDOT = 22585
925601 feet/sec YDOT = 6884
190123 meter/sec
ZDOT = -6132
408111 ZDOT = -1869
157992
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 08289
54449772
00020000 00000-0 20000-3 0 9097
2 25544 51
6380 119
3000 0003980 232
5863 127
4937 15
72258977 7472
Satellite: ISS
Catalog Number: 25544
Epoch time: 08289
54449772 = yrday
fracday
Element set: 909
Inclination: 51
6380 deg
RA of node: 119
3000 deg
Eccentricity:
0003980
Arg of perigee: 232
5863 deg
Mean anomaly: 127
4937 deg
Mean motion: 15
72258977 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 747
Checksum: 321
Coasting Arc #11 (Orbit 762)
---------------------------------------
Vector Time (GMT): 2008/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3432377
39 A = 6736520
64 meter
Y = 5682002
74 meter E =
0009861
Z = 1118625
28 I = 51
95663
XDOT = -3598
533357 Wp = 57
44037
YDOT = -3346
604281 meter/sec RA = 113
55810 deg
ZDOT = 5924
791636 TA = 314
74039
MA = 314
82061
Ha = 191
855 n
mi
Hp = 187
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11261080
67 X = -3501093
62
Y = 18641741
27 feet Y = 5643235
72 meter
Z = 3670030
44 Z = 1101783
24
XDOT = -11806
211800 XDOT = -3589
626169
YDOT = -10979
672838 feet/sec YDOT = -3386
795278 meter/sec
ZDOT = 19438
292769 ZDOT = 5907
331054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2489814
01 X = 758895
31
Y = -21647124
92 feet Y = -6598043
67 meter
Z = 3605327
74 Z = 1098903
89
XDOT = 13829
676003 XDOT = 4215
285246
YDOT = 4834
828213 feet/sec YDOT = 1473
655639 meter/sec
ZDOT = 19370
338499 ZDOT = 5904
079175
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 08290
56143899
00020000 00000-0 20000-3 0 9104
2 25544 51
6372 114
0892 0003940 236
2452 123
8335 15
72293609 7636
Satellite: ISS
Catalog Number: 25544
Epoch time: 08290
56143899 = yrday
fracday
Element set: 910
Inclination: 51
6372 deg
RA of node: 114
0892 deg
Eccentricity:
0003940
Arg of perigee: 236
2452 deg
Mean anomaly: 123
8335 deg
Mean motion: 15
72293609 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 763
Checksum: 292
Coasting Arc #12 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2008/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628516
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3678156
34 A = 6725025
16 meter
Y = 2013490
22 meter E =
0011951
Z = -5267780
84 I = 51
92881
XDOT = -2915
321555 Wp = 106
32622
YDOT = 7084
048925 meter/sec RA = 108
43991 deg
ZDOT = 670
100223 TA = 170
04088
MA = 170
01718
Ha = 191
758 n
mi
Hp = 187
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12067442
06 X = 3680958
52
Y = 6605939
05 feet Y = 2054637
25 meter
Z = -17282745
55 Z = -5249904
96
XDOT = -9564
703265 XDOT = -2997
575189
YDOT = 23241
630331 feet/sec YDOT = 7050
988201 meter/sec
ZDOT = 2198
491545 ZDOT = 655
737466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13826369
05 X = -4214277
29
Y = -698888
64 feet Y = -213021
26 meter
Z = -17213307
52 Z = -5246616
13
XDOT = -1459
244140 XDOT = -444
777614
YDOT = -24089
821390 feet/sec YDOT = -7342
577560 meter/sec
ZDOT = 2143
506087 ZDOT = 653
340655
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 08291
51480588
00020000 00000-0 20000-3 0 9110
2 25544 51
6372 109
2046 0003855 238
3461 121
7325 15
72324647 7780
Satellite: ISS
Catalog Number: 25544
Epoch time: 08291
51480588 = yrday
fracday
Element set: 911
Inclination: 51
6372 deg
RA of node: 109
2046 deg
Eccentricity:
0003855
Arg of perigee: 238
3461 deg
Mean anomaly: 121
7325 deg
Mean motion: 15
72324647 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 778
Checksum: 292
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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