Date:
July 20th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6135 43 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
205/16:18:03
264 -11
0 11
8 11
8
N/A 1
7 -0
0 191
9
000/00:22:06
528 -4
0 -0
1 186
9
Coasting Arc #1 (Orbit 3315)
---------------------------------------
Vector Time (GMT): 2008/198/12:58:12
196
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -124583
05 A = 6720621
20 meter
Y = -5059059
72 meter E =
0013193
Z = 4408940
87 I = 51
39976
XDOT = 6448
911046 Wp = 63
49219
YDOT = 2687
421426 meter/sec RA = 224
52228 deg
ZDOT = 3264
224424 TA = 353
70447
MA = 353
72103
Ha = 191
130 n
mi
Hp = 180
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -408737
05 X = -89420
14
Y = -16597964
96 feet Y = -5060257
10 meter
Z = 14465029
11 Z = 4408420
12
XDOT = 21157
844638 XDOT = 6402
523772
YDOT = 8816
999428 feet/sec YDOT = 2759
276869 meter/sec
ZDOT = 10709
397716 ZDOT = 3295
440667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12677170
67 X = -3864001
62
Y = 10724761
26 feet Y = 3268907
23 meter
Z = 14462552
11 Z = 4408185
88
XDOT = -5463
966919 XDOT = -1665
417117
YDOT = -21070
640017 feet/sec YDOT = -6422
331077 meter/sec
ZDOT = 10830
000727 ZDOT = 3300
984222
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 08198
59386474
00020000 00000-0 20000-3 0 9001
2 25544 51
6381 225
1586 0009792 18
9078 341
2447 15
75079536 33161
Satellite: ISS
Catalog Number: 25544
Epoch time: 08198
59386474 = yrday
fracday
Element set: 900
Inclination: 51
6381 deg
RA of node: 225
1586 deg
Eccentricity:
0009792
Arg of perigee: 18
9078 deg
Mean anomaly: 341
2447 deg
Mean motion: 15
75079536 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3316
Checksum: 324
Coasting Arc #2 (Orbit 3330)
---------------------------------------
Vector Time (GMT): 2008/199/12:58:12
196
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5835757
08 A = 6726130
75 meter
Y = -2172615
08 meter E =
0014520
Z = -2530161
68 I = 51
44121
XDOT = -193
680574 Wp = 32
73040
YDOT = -5602
590918 meter/sec RA = 219
31774 deg
ZDOT = 5283
684037 TA = 298
49352
MA = 298
63967
Ha = 191
104 n
mi
Hp = 179
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19146184
65 X = -5798737
97
Y = -7128002
24 feet Y = -2237666
43 meter
Z = -8301055
39 Z = -2558421
79
XDOT = -635
434953 XDOT = -156
683865
YDOT = -18381
203798 feet/sec YDOT = -5604
550850 meter/sec
ZDOT = 17334
921381 ZDOT = 5282
832015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6654971
20 X = 2028435
22
Y = 19268412
72 feet Y = 5873012
20 meter
Z = -8410229
04 Z = -2563437
81
XDOT = -12306
612516 XDOT = -3751
055495
YDOT = 11778
242239 feet/sec YDOT = 3590
008234 meter/sec
ZDOT = 17331
110230 ZDOT = 5282
522398
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 08199
54554609
00020000 00000-0 20000-3 0 9015
2 25544 51
6385 220
2641 0009800 22
5396 337
6196 15
75116883 33311
Satellite: ISS
Catalog Number: 25544
Epoch time: 08199
54554609 = yrday
fracday
Element set: 901
Inclination: 51
6385 deg
RA of node: 220
2641 deg
Eccentricity:
0009800
Arg of perigee: 22
5396 deg
Mean anomaly: 337
6196 deg
Mean motion: 15
75116883 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3331
Checksum: 298
Coasting Arc #3 (Orbit 3346)
---------------------------------------
Vector Time (GMT): 2008/200/12:58:12
196
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 153106
27 A = 6719068
51 meter
Y = 4724224
30 meter E =
0019819
Z = -4793508
30 I = 51
43930
XDOT = -6902
934807 Wp = 51
32927
YDOT = -2299
551074 meter/sec RA = 214
20058 deg
ZDOT = -2481
515226 TA = 194
26073
MA = 194
31675
Ha = 191
282 n
mi
Hp = 179
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 502317
17 X = 123553
40
Y = 15499423
55 feet Y = 4725771
96 meter
Z = -15726733
28 Z = -4792835
54
XDOT = -22647
423909 XDOT = -6864
653309
YDOT = -7544
458904 feet/sec YDOT = -2376
529206 meter/sec
ZDOT = -8141
454155 ZDOT = -2514
956421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11400033
40 X = 3474730
18
Y = -10517576
72 feet Y = -3205757
38 meter
Z = -15723689
48 Z = -4792580
55
XDOT = 8176
560265 XDOT = 2492
215569
YDOT = 21253
036730 feet/sec YDOT = 6477
925595 meter/sec
ZDOT = -8270
635739 ZDOT = -2520
889773
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 08200
56066516
00020000 00000-0 20000-3 0 9026
2 25544 51
6372 215
0413 0009819 25
7736 334
3915 15
75107002 33472
Satellite: ISS
Catalog Number: 25544
Epoch time: 08200
56066516 = yrday
fracday
Element set: 902
Inclination: 51
6372 deg
RA of node: 215
0413 deg
Eccentricity:
0009819
Arg of perigee: 25
7736 deg
Mean anomaly: 334
3915 deg
Mean motion: 15
75107002 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3347
Checksum: 270
Coasting Arc #4 (Orbit 3362)
---------------------------------------
Vector Time (GMT): 2008/201/12:58:12
196
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6221522
19 A = 6727457
83 meter
Y = 1820110
90 meter E =
0017992
Z = 1791160
97 I = 51
49279
XDOT = 118
603771 Wp = 80
72065
YDOT = 5216
912783 meter/sec RA = 209
00700 deg
ZDOT = -5662
088225 TA = 79
38104
MA = 79
17845
Ha = 191
326 n
mi
Hp = 179
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20411818
20 X = 6192006
07
Y = 5971492
45 feet Y = 1889518
25 meter
Z = 5876512
38 Z = 1821313
06
XDOT = 389
119985 XDOT = 87
763432
YDOT = 17115
855588 feet/sec YDOT = 5218
067431 meter/sec
ZDOT = -18576
404937 ZDOT = -5661
586242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9027772
45 X = -2751665
04
Y = -19220248
89 feet Y = -5858331
86 meter
Z = 5992979
13 Z = 1826660
04
XDOT = 11090
848923 XDOT = 3380
490752
YDOT = -11052
116108 feet/sec YDOT = -3368
684990 meter/sec
ZDOT = -18573
965373 ZDOT = -5661
344646
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 08201
57577492
00020000 00000-0 20000-3 0 9039
2 25544 51
6368 209
8187 0009990 28
9833 331
1883 15
75150508 33635
Satellite: ISS
Catalog Number: 25544
Epoch time: 08201
57577492 = yrday
fracday
Element set: 903
Inclination: 51
6368 deg
RA of node: 209
8187 deg
Eccentricity:
0009990
Arg of perigee: 28
9833 deg
Mean anomaly: 331
1883 deg
Mean motion: 15
75150508 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3363
Checksum: 316
Coasting Arc #5 (Orbit 3378)
---------------------------------------
Vector Time (GMT): 2008/202/12:58:12
196
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -33250
97 A = 6717789
31 meter
Y = -4414023
06 meter E =
0010900
Z = 5054545
88 I = 51
48576
XDOT = 7313
833912 Wp = 60
62998
YDOT = 1814
826250 meter/sec RA = 203
88261 deg
ZDOT = 1635
592900 TA = 13
65607
MA = 13
62661
Ha = 191
392 n
mi
Hp = 179
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -109091
12 X = -8443
76
Y = -14481702
94 feet Y = -4414256
76 meter
Z = 16583155
78 Z = 5054444
10
XDOT = 23995
518083 XDOT = 7285
051406
YDOT = 5954
154363 feet/sec YDOT = 1896
452621 meter/sec
ZDOT = 5366
118438 ZDOT = 1671
053084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10543133
56 X = -3213547
11
Y = 9929818
75 feet Y = 3026608
76 meter
Z = 16582331
29 Z = 5054294
58
XDOT = -11067
761502 XDOT = -3373
453706
YDOT = -20926
813786 feet/sec YDOT = -6378
492842 meter/sec
ZDOT = 5503
072163 ZDOT = 1677
336395
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 08202
59087696
00020000 00000-0 20000-3 0 9045
2 25544 51
6364 204
5964 0009919 32
4795 327
6978 15
75133824 33798
Satellite: ISS
Catalog Number: 25544
Epoch time: 08202
59087696 = yrday
fracday
Element set: 904
Inclination: 51
6364 deg
RA of node: 204
5964 deg
Eccentricity:
0009919
Arg of perigee: 32
4795 deg
Mean anomaly: 327
6978 deg
Mean motion: 15
75133824 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3379
Checksum: 335
Coasting Arc #6 (Orbit 3393)
---------------------------------------
Vector Time (GMT): 2008/203/12:58:12
196
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6504245
65 A = 6728321
38 meter
Y = -1318521
44 meter E =
0019523
Z = -1054284
12 I = 51
54931
XDOT = 54
479348 Wp = 37
87398
YDOT = -4940
081336 meter/sec RA = 198
70615 deg
ZDOT = 5914
873598 TA = 310
56932
MA = 310
73910
Ha = 191
384 n
mi
Hp = 179
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21339388
62 X = -6483896
90
Y = -4325857
75 feet Y = -1391141
78 meter
Z = -3458937
41 Z = -1085831
88
XDOT = 178
738018 XDOT = 80
983201
YDOT = -16207
615933 feet/sec YDOT = -4939
324465 meter/sec
ZDOT = 19405
753274 ZDOT = 5915
202181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11525549
97 X = 3512987
63
Y = 18449570
06 feet Y = 5623428
95 meter
Z = -3580762
84 Z = -1091416
51
XDOT = -10464
987224 XDOT = -3189
728106
YDOT = 10259
280549 feet/sec YDOT = 3127
028711 meter/sec
ZDOT = 19406
531590 ZDOT = 5915
110829
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 08203
54252626
00020000 00000-0 20000-3 0 9059
2 25544 51
6366 199
7013 0009937 37
0948 323
0901 15
75172580 33946
Satellite: ISS
Catalog Number: 25544
Epoch time: 08203
54252626 = yrday
fracday
Element set: 905
Inclination: 51
6366 deg
RA of node: 199
7013 deg
Eccentricity:
0009937
Arg of perigee: 37
0948 deg
Mean anomaly: 323
0901 deg
Mean motion: 15
75172580 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3394
Checksum: 297
Coasting Arc #7 (Orbit 3409)
---------------------------------------
Vector Time (GMT): 2008/204/12:58:12
196
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -174903
80 A = 6717028
84 meter
Y = 4232757
00 meter E =
0022985
Z = -5231728
87 I = 51
53951
XDOT = -7552
750853 Wp = 66
75522
YDOT = -1224
909493 meter/sec RA = 193
57112 deg
ZDOT = -732
156375 TA = 196
22078
MA = 196
29448
Ha = 191
539 n
mi
Hp = 179
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -573831
37 X = -196807
72
Y = 13886998
03 feet Y = 4230679
04 meter
Z = -17164464
80 Z = -5232631
43
XDOT = -24779
366316 XDOT = -7534
935750
YDOT = -4018
731933 feet/sec YDOT = -1309
269027 meter/sec
ZDOT = -2402
087844 ZDOT = -768
803958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10246685
91 X = 3123189
87
Y = -9385008
98 feet Y = -2860550
74 meter
Z = -17167524
07 Z = -5232661
34
XDOT = 13789
203347 XDOT = 4202
949180
YDOT = 19746
291321 feet/sec YDOT = 6018
669595 meter/sec
ZDOT = -2543
587130 ZDOT = -775
285357
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 08204
55761052
00020000 00000-0 20000-3 0 9060
2 25544 51
6370 194
4782 0009987 39
8836 320
3060 15
75152786 34108
Satellite: ISS
Catalog Number: 25544
Epoch time: 08204
55761052 = yrday
fracday
Element set: 906
Inclination: 51
6370 deg
RA of node: 194
4782 deg
Eccentricity:
0009987
Arg of perigee: 39
8836 deg
Mean anomaly: 320
3060 deg
Mean motion: 15
75152786 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3410
Checksum: 300
Coasting Arc #8 (Orbit 3425)
---------------------------------------
Vector Time (GMT): 2008/205/12:58:12
196
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6674221
05 A = 6728755
69 meter
Y = 817390
13 meter E =
0016299
Z = 211910
75 I = 51
60887
XDOT = -380
497240 Wp = 94
56837
YDOT = 4772
271303 meter/sec RA = 188
41309 deg
ZDOT = -6028
470383 TA = 83
12836
MA = 82
94296
Ha = 191
562 n
mi
Hp = 179
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21897050
68 X = 6663555
40
Y = 2681726
15 feet Y = 891965
45 meter
Z = 695245
24 Z = 244307
98
XDOT = -1248
350525 XDOT = -404
548295
YDOT = 15657
058081 feet/sec YDOT = 4767
882307 meter/sec
ZDOT = -19778
446139 ZDOT = -6030
376911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13715631
51 X = -4180524
48
Y = -17273227
40 feet Y = -5264879
71 meter
Z = 820315
34 Z = 250032
12
XDOT = 10536
148926 XDOT = 3211
418193
YDOT = -9357
951090 feet/sec YDOT = -2852
303492 meter/sec
ZDOT = -19785
323195 ZDOT = -6030
566510
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 08205
57268495
00020000 00000-0 20000-3 0 9077
2 25544 51
6375 189
2557 0010072 42
8977 317
2971 15
75192884 34268
Satellite: ISS
Catalog Number: 25544
Epoch time: 08205
57268495 = yrday
fracday
Element set: 907
Inclination: 51
6375 deg
RA of node: 189
2557 deg
Eccentricity:
0010072
Arg of perigee: 42
8977 deg
Mean anomaly: 317
2971 deg
Mean motion: 15
75192884 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3426
Checksum: 327
Coasting Arc #9 (Orbit 3427)
---------------------------------------
Vector Time (GMT): 2008/205/16:29:06
528
Vector Time (MET): N/A
Weight (LBS) : 660953
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2643948
60 A = 6725645
11 meter
Y = 3648345
18 meter E =
0010269
Z = -5002278
91 I = 51
57902
XDOT = -7026
460503 Wp = 92
56918
YDOT = -2473
946276 meter/sec RA = 187
64733 deg
ZDOT = 1912
406180 TA = 195
91954
MA = 195
95184
Ha = 191
931 n
mi
Hp = 186
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8674372
06 X = -2660248
50
Y = 11969636
42 feet Y = 3618688
24 meter
Z = -16411676
22 Z = -5015162
45
XDOT = -23052
691940 XDOT = -7007
564270
YDOT = -8116
621642 feet/sec YDOT = -2552
414673 meter/sec
ZDOT = 6274
298490 ZDOT = 1878
317631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6761504
31 X = 2060906
51
Y = -13083465
47 feet Y = -3987840
27 meter
Z = -16461015
57 Z = -5017317
55
XDOT = 23064
385004 XDOT = 7030
024549
YDOT = 4203
373802 feet/sec YDOT = 1281
188335 meter/sec
ZDOT = 6142
536021 ZDOT = 1872
244979
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 08205
69958554
00020000 00000-0 20000-3 0 9083
2 25544 51
6400 188
6045 0003796 317
7378 42
3492 15
72462572 34283
Satellite: ISS
Catalog Number: 25544
Epoch time: 08205
69958554 = yrday
fracday
Element set: 908
Inclination: 51
6400 deg
RA of node: 188
6045 deg
Eccentricity:
0003796
Arg of perigee: 317
7378 deg
Mean anomaly: 42
3492 deg
Mean motion: 15
72462572 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3428
Checksum: 318
Coasting Arc #10 (Orbit 3443)
---------------------------------------
Vector Time (GMT): 2008/206/16:29:06
528
Vector Time (MET): N/A
Weight (LBS) : 660953
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6503680
56 A = 6735965
57 meter
Y = 1251715
57 meter E =
0005560
Z = -1214738
07 I = 51
64318
XDOT = -1972
121100 Wp = 144
11490
YDOT = 4564
586973 meter/sec RA = 182
54842 deg
ZDOT = -5873
101025 TA = 49
18552
MA = 49
13731
Ha = 192
032 n
mi
Hp = 186
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21337534
64 X = 6495101
26
Y = 4106678
37 feet Y = 1324395
58 meter
Z = -3985361
11 Z = -1183164
03
XDOT = -6470
213584 XDOT = -1994
486101
YDOT = 14975
679044 feet/sec YDOT = 4542
408995 meter/sec
ZDOT = -19268
704151 ZDOT = -5882
735523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21742750
07 X = -6627190
22
Y = -604272
61 feet Y = -184182
29 meter
Z = -3863414
16 Z = -1177568
64
XDOT = 3814
752920 XDOT = 1162
736690
YDOT = -14220
437900 feet/sec YDOT = -4334
389472 meter/sec
ZDOT = -19305
420017 ZDOT = -5884
292021
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 08206
71640862
00020000 00000-0 20000-3 0 9098
2 25544 51
6404 183
3944 0003760 320
5110 39
5778 15
72457947 34447
Satellite: ISS
Catalog Number: 25544
Epoch time: 08206
71640862 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 183
3944 deg
Eccentricity:
0003760
Arg of perigee: 320
5110 deg
Mean anomaly: 39
5778 deg
Mean motion: 15
72457947 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3444
Checksum: 297
Coasting Arc #11 (Orbit 3459)
---------------------------------------
Vector Time (GMT): 2008/207/16:29:06
528
Vector Time (MET): N/A
Weight (LBS) : 660953
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 752425
35 A = 6724513
83 meter
Y = -4171137
30 meter E =
0004779
Z = 5220716
44 I = 51
63423
XDOT = 7646
148201 Wp = 6
25592
YDOT = 320
316087 meter/sec RA = 177
40621 deg
ZDOT = -841
329497 TA = 91
78308
MA = 91
72834
Ha = 191
981 n
mi
Hp = 186
821
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2468587
09 X = 773650
46
Y = -13684833
67 feet Y = -4162605
09 meter
Z = 17128334
79 Z = 5224422
87
XDOT = 25085
788060 XDOT = 7646
085120
YDOT = 1050
905798 feet/sec YDOT = 405
819438 meter/sec
ZDOT = -2760
267379 ZDOT = -804
184644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 108692
74 X = 33129
55
Y = 13888155
99 feet Y = 4233109
95 meter
Z = 17142221
46 Z = 5224949
10
XDOT = -23873
218152 XDOT = -7276
556893
YDOT = 3436
069216 feet/sec YDOT = 1047
313897 meter/sec
ZDOT = -2616
908319 ZDOT = -797
633656
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 08207
73322202
00020000 00000-0 20000-3 0 9108
2 25544 51
6400 178
1844 0003925 324
1468 35
9430 15
72526535 34606
Satellite: ISS
Catalog Number: 25544
Epoch time: 08207
73322202 = yrday
fracday
Element set: 910
Inclination: 51
6400 deg
RA of node: 178
1844 deg
Eccentricity:
0003925
Arg of perigee: 324
1468 deg
Mean anomaly: 35
9430 deg
Mean motion: 15
72526535 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3460
Checksum: 266
Coasting Arc #12 (Orbit 3475)
---------------------------------------
Vector Time (GMT): 2008/208/16:29:06
528
Vector Time (MET): N/A
Weight (LBS) : 660953
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6686385
49 A = 6736455
90 meter
Y = 706443
85 meter E =
0013998
Z = 248974
56 I = 51
70347
XDOT = -274
302810 Wp = 31
75519
YDOT = -4773
840387 meter/sec RA = 172
29323 deg
ZDOT = 6037
460244 TA = 330
94735
MA = 331
02518
Ha = 192
193 n
mi
Hp = 186
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21936960
28 X = -6694997
59
Y = 2317729
16 feet Y = 631624
66 meter
Z = 816845
67 Z = 216471
27
XDOT = -899
943604 XDOT = -250
229466
YDOT = -15662
205995 feet/sec YDOT = -4776
773956 meter/sec
ZDOT = 19807
940433 ZDOT = 6036
185555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21066115
62 X = 6420952
04
Y = -6558197
35 feet Y = -1998938
55 meter
Z = 691485
38 Z = 210764
74
XDOT = 3574
146712 XDOT = 1089
399918
YDOT = 13626
496903 feet/sec YDOT = 4153
356256 meter/sec
ZDOT = 19802
550427 ZDOT = 6035
817370
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 08208
75003056
00020000 00000-0 20000-3 0 9115
2 25544 51
6403 172
9739 0003938 329
4408 30
6525 15
72494576 34763
Satellite: ISS
Catalog Number: 25544
Epoch time: 08208
75003056 = yrday
fracday
Element set: 911
Inclination: 51
6403 deg
RA of node: 172
9739 deg
Eccentricity:
0003938
Arg of perigee: 329
4408 deg
Mean anomaly: 30
6525 deg
Mean motion: 15
72494576 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3476
Checksum: 300
Coasting Arc #13 (Orbit 3490)
---------------------------------------
Vector Time (GMT): 2008/209/16:29:06
528
Vector Time (MET): N/A
Weight (LBS) : 660953
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1203981
86 A = 6724322
21 meter
Y = 4002745
13 meter E =
0013801
Z = -5278811
91 I = 51
69202
XDOT = -7445
943372 Wp = 73
03773
YDOT = 1900
766488 meter/sec RA = 167
17330 deg
ZDOT = -253
568795 TA = 194
53370
MA = 194
57342
Ha = 192
242 n
mi
Hp = 186
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3950071
73 X = 1184776
49
Y = 13132365
91 feet Y = 4016102
16 meter
Z = -17318936
71 Z = -5273009
02
XDOT = -24428
948071 XDOT = -7465
412858
YDOT = 6236
110524 feet/sec YDOT = 1817
392854 meter/sec
ZDOT = -831
918619 ZDOT = -289
788105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6742685
54 X = -2055170
55
Y = -11974434
54 feet Y = -3649807
65 meter
Z = -17296149
25 Z = -5271866
29
XDOT = 21671
779940 XDOT = 6605
558526
YDOT = -10783
738698 feet/sec YDOT = -3286
883555 meter/sec
ZDOT = -971
520187 ZDOT = -296
119353
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 08209
70327917
00020000 00000-0 20000-3 0 9127
2 25544 51
6405 168
0893 0003952 332
7894 27
3061 15
72531554 34917
Satellite: ISS
Catalog Number: 25544
Epoch time: 08209
70327917 = yrday
fracday
Element set: 912
Inclination: 51
6405 deg
RA of node: 168
0893 deg
Eccentricity:
0003952
Arg of perigee: 332
7894 deg
Mean anomaly: 27
3061 deg
Mean motion: 15
72531554 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3491
Checksum: 296
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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