Date:
October 24th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5543 41 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
303/01:34:10
987 2
6 3
0 3
1
N/A 1
7 -0
9 191
6
000/00:06:21
973 0
4 -0
1 189
3
Coasting Arc #1 (Orbit 856)
---------------------------------------
Vector Time (GMT): 2008/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2372993
11 A = 6734904
96 meter
Y = -5943920
26 meter E =
0011120
Z = 2077382
59 I = 51
97990
XDOT = 3957
556662 Wp = 121
44038
YDOT = -3535
565185 meter/sec RA = 82
93779 deg
ZDOT = -5579
350266 TA = 35
48739
MA = 35
41347
Ha = 191
328 n
mi
Hp = 187
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7785410
48 X = -2316442
52
Y = -19501050
72 feet Y = -5970140
22 meter
Z = 6815559
66 Z = 2065991
90
XDOT = 12984
109782 XDOT = 4023
901545
YDOT = -11599
623310 feet/sec YDOT = -3490
938612 meter/sec
ZDOT = -18304
954942 ZDOT = -5559
963063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16646977
66 X = 5073998
79
Y = 12821411
16 feet Y = 3907966
12 meter
Z = 6770893
57 Z = 2063768
36
XDOT = -4445
448774 XDOT = -1354
972786
YDOT = 15427
103195 feet/sec YDOT = 4702
181054 meter/sec
ZDOT = -18230
125732 ZDOT = -5556
542323
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 08296
53586466
00020000 00000-0 20000-3 0 9007
2 25544 51
6396 83
4945 0003773 257
4344 102
6396 15
72394757 8571
Satellite: ISS
Catalog Number: 25544
Epoch time: 08296
53586466 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 83
4945 deg
Eccentricity:
0003773
Arg of perigee: 257
4344 deg
Mean anomaly: 102
6396 deg
Mean motion: 15
72394757 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 857
Checksum: 330
Coasting Arc #2 (Orbit 872)
---------------------------------------
Vector Time (GMT): 2008/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2875854
50 A = 6727303
47 meter
Y = 3923819
16 meter E =
0005505
Z = 4645349
06 I = 51
95098
XDOT = -3645
247089 Wp = 139
20489
YDOT = -6124
292139 meter/sec RA = 77
87729 deg
ZDOT = 2910
339578 TA = 282
07438
MA = 282
13606
Ha = 191
228 n
mi
Hp = 187
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9435218
19 X = -2942084
08
Y = 12873422
45 feet Y = 3891289
55 meter
Z = 15240646
53 Z = 4631216
99
XDOT = -11959
472078 XDOT = -3590
631410
YDOT = -20092
821977 feet/sec YDOT = -6164
749927 meter/sec
ZDOT = 9548
358196 ZDOT = 2892
763631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1387222
63 X = 422825
46
Y = -15952433
50 feet Y = -4862301
73 meter
Z = 15186215
24 Z = 4628758
41
XDOT = 19582
667178 XDOT = 5968
796956
YDOT = 10746
095151 feet/sec YDOT = 3275
409802 meter/sec
ZDOT = 9479
705249 ZDOT = 2889
414160
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 08297
55272438
00020000 00000-0 20000-3 0 9012
2 25544 51
6406 78
2845 0003818 261
5558 98
5172 15
72445766 8737
Satellite: ISS
Catalog Number: 25544
Epoch time: 08297
55272438 = yrday
fracday
Element set: 901
Inclination: 51
6406 deg
RA of node: 78
2845 deg
Eccentricity:
0003818
Arg of perigee: 261
5558 deg
Mean anomaly: 98
5172 deg
Mean motion: 15
72445766 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 873
Checksum: 321
Coasting Arc #3 (Orbit 887)
---------------------------------------
Vector Time (GMT): 2008/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3879351
17 A = 6732844
49 meter
Y = 4625229
72 meter E =
0001549
Z = -2980102
04 I = 51
96299
XDOT = -2461
617466 Wp = 20
73751
YDOT = 5293
387687 meter/sec RA = 72
73073 deg
ZDOT = 5013
326406 TA = 305
06629
MA = 305
08082
Ha = 191
207 n
mi
Hp = 187
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12727530
09 X = 3841819
80
Y = 15174638
19 feet Y = 4668400
87 meter
Z = -9777237
68 Z = -2961347
26
XDOT = -8076
172790 XDOT = -2544
980247
YDOT = 17366
757502 feet/sec YDOT = 5265
394600 meter/sec
ZDOT = 16447
921281 ZDOT = 5001
164930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18935319
91 X = -5771485
51
Y = -5927663
69 feet Y = -1806751
89 meter
Z = -9704148
91 Z = -2957824
59
XDOT = -2874
568195 XDOT = -876
168386
YDOT = -17655
949353 feet/sec YDOT = -5381
533363 meter/sec
ZDOT = 16401
243001 ZDOT = 4999
098867
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 08298
50602182
00020000 00000-0 20000-3 0 9022
2 25544 51
6416 73
4007 0003677 266
2473 93
8269 15
72431634 8886
Satellite: ISS
Catalog Number: 25544
Epoch time: 08298
50602182 = yrday
fracday
Element set: 902
Inclination: 51
6416 deg
RA of node: 73
4007 deg
Eccentricity:
0003677
Arg of perigee: 266
2473 deg
Mean anomaly: 93
8269 deg
Mean motion: 15
72431634 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 888
Checksum: 300
Coasting Arc #4 (Orbit 903)
---------------------------------------
Vector Time (GMT): 2008/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1331604
89 A = 6729384
50 meter
Y = -5181356
86 meter E =
0004199
Z = -4086929
09 I = 51
94187
XDOT = 5046
665648 Wp = 52
85050
YDOT = 4339
658588 meter/sec RA = 67
67821 deg
ZDOT = -3857
681054 TA = 177
59291
MA = 177
59089
Ha = 191
139 n
mi
Hp = 187
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4368782
44 X = 1409298
66
Y = -16999202
31 feet Y = -5166031
91 meter
Z = -13408560
00 Z = -4080271
01
XDOT = 16557
301995 XDOT = 5016
504102
YDOT = 14237
725025 feet/sec YDOT = 4395
924466 meter/sec
ZDOT = -12656
433903 ZDOT = -3833
237354
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5672913
68 X = 1729104
09
Y = 16629993
91 feet Y = 5068822
14 meter
Z = -13383197
42 Z = -4079198
57
XDOT = -20512
422212 XDOT = -6252
186290
YDOT = -3110
985410 feet/sec YDOT = -948
228353 meter/sec
ZDOT = -12561
325909 ZDOT = -3828
692137
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 08299
52286035
00020000 00000-0 20000-3 0 9031
2 25544 51
6418 68
1908 0003740 270
9542 89
1192 15
72446935 9041
Satellite: ISS
Catalog Number: 25544
Epoch time: 08299
52286035 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 68
1908 deg
Eccentricity:
0003740
Arg of perigee: 270
9542 deg
Mean anomaly: 89
1192 deg
Mean motion: 15
72446935 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 904
Checksum: 304
Coasting Arc #5 (Orbit 919)
---------------------------------------
Vector Time (GMT): 2008/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4796169
14 A = 6730621
40 meter
Y = -2878732
30 meter E =
0008198
Z = 3737560
70 I = 51
93411
XDOT = 473
843402 Wp = 79
11845
YDOT = -6374
184431 meter/sec RA = 62
52436 deg
ZDOT = -4292
037893 TA = 55
99926
MA = 55
92141
Ha = 191
265 n
mi
Hp = 187
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15735463
05 X = -4781779
08
Y = -9444659
77 feet Y = -2932285
19 meter
Z = 12262338
26 Z = 3714295
42
XDOT = 1554
604336 XDOT = 565
935826
YDOT = -20912
678581 feet/sec YDOT = -6368
370941 meter/sec
ZDOT = -14081
489150 ZDOT = -4289
511884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18375704
15 X = 5600914
62
Y = -1161469
46 feet Y = -354015
89 meter
Z = 12171927
58 Z = 3710003
53
XDOT = 10405
421861 XDOT = 3171
572583
YDOT = 16825
233441 feet/sec YDOT = 5128
331153 meter/sec
ZDOT = -14072
235138 ZDOT = -4289
217270
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 08300
53968829
00020000 00000-0 20000-3 0 9044
2 25544 51
6423 62
9809 0003643 274
6234 85
4512 15
72449000 9209
Satellite: ISS
Catalog Number: 25544
Epoch time: 08300
53968829 = yrday
fracday
Element set: 904
Inclination: 51
6423 deg
RA of node: 62
9809 deg
Eccentricity:
0003643
Arg of perigee: 274
6234 deg
Mean anomaly: 85
4512 deg
Mean motion: 15
72449000 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 920
Checksum: 285
Coasting Arc #6 (Orbit 935)
---------------------------------------
Vector Time (GMT): 2008/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 547097
75 A = 6731409
77 meter
Y = 5788313
94 meter E =
0008886
Z = 3384123
65 I = 51
92420
XDOT = -5725
705058 Wp = 85
98476
YDOT = -2188
860672 meter/sec RA = 57
47184 deg
ZDOT = 4659
728212 TA = 313
73514
MA = 313
80868
Ha = 191
086 n
mi
Hp = 187
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1794940
12 X = 465891
27
Y = 18990531
30 feet Y = 5793977
98 meter
Z = 11102767
88 Z = 3386584
06
XDOT = -18785
121580 XDOT = -5723
440101
YDOT = -7181
301416 feet/sec YDOT = -2252
875978 meter/sec
ZDOT = 15287
822217 ZDOT = 4631
917497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12427898
29 X = -3788023
40
Y = -14463297
86 feet Y = -4408413
19 meter
Z = 11112781
05 Z = 3387175
66
XDOT = 18483
197237 XDOT = 5633
678518
YDOT = -4194
001942 feet/sec YDOT = -1278
331792 meter/sec
ZDOT = 15179
858142 ZDOT = 4626
820762
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 08301
55650206
00020000 00000-0 20000-3 0 9055
2 25544 51
6436 57
7709 0003722 279
5430 80
5311 15
72522204 9362
Satellite: ISS
Catalog Number: 25544
Epoch time: 08301
55650206 = yrday
fracday
Element set: 905
Inclination: 51
6436 deg
RA of node: 57
7709 deg
Eccentricity:
0003722
Arg of perigee: 279
5430 deg
Mean anomaly: 80
5311 deg
Mean motion: 15
72522204 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 936
Checksum: 269
Coasting Arc #7 (Orbit 950)
---------------------------------------
Vector Time (GMT): 2008/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5040348
65 A = 6728269
71 meter
Y = 926038
53 meter E =
0005169
Z = -4364975
53 I = 51
89678
XDOT = 1745
855800 Wp = 114
23857
YDOT = 6660
937126 meter/sec RA = 52
31846 deg
ZDOT = 3430
209886 TA = 190
27215
MA = 190
28272
Ha = 191
194 n
mi
Hp = 187
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16536576
93 X = 5050823
87
Y = 3038184
15 feet Y = 982461
11 meter
Z = -14320785
86 Z = -4340463
30
XDOT = 5727
873359 XDOT = 1654
578482
YDOT = 21853
468260 feet/sec YDOT = 6679
950000 meter/sec
ZDOT = 11253
969442 ZDOT = 3438
469685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15172696
31 X = -4624637
83
Y = 7429148
42 feet Y = 2264404
44 meter
Z = -14225712
20 Z = -4335997
08
XDOT = -16996
844902 XDOT = -5180
638326
YDOT = -13107
909821 feet/sec YDOT = -3995
290913 meter/sec
ZDOT = 11286
518599 ZDOT = 3440
130869
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 08302
50975781
00020000 00000-0 20000-3 0 9060
2 25544 51
6439 52
8878 0003762 285
4497 74
6250 15
72508398 9512
Satellite: ISS
Catalog Number: 25544
Epoch time: 08302
50975781 = yrday
fracday
Element set: 906
Inclination: 51
6439 deg
RA of node: 52
8878 deg
Eccentricity:
0003762
Arg of perigee: 285
4497 deg
Mean anomaly: 74
6250 deg
Mean motion: 15
72508398 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 951
Checksum: 324
Coasting Arc #8 (Orbit 959)
---------------------------------------
Vector Time (GMT): 2008/303/01:37:21
973
Vector Time (MET): N/A
Weight (LBS) : 642049
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3866903
93 A = 6726311
07 meter
Y = -1777557
69 meter E =
0008472
Z = -5216004
87 I = 51
87491
XDOT = 4302
058745 Wp = 92
85629
YDOT = 6289
385848 meter/sec RA = 49
43646 deg
ZDOT = 1047
033207 TA = 187
10253
MA = 187
11454
Ha = 191
580 n
mi
Hp = 189
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12686692
69 X = 3911832
72
Y = -5831882
19 feet Y = -1734064
56 meter
Z = -17112876
86 Z = -5197109
68
XDOT = 14114
365961 XDOT = 4226
323602
YDOT = 20634
468006 feet/sec YDOT = 6337
070505 meter/sec
ZDOT = 3435
148317 ZDOT = 1067
749293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1011924
04 X = 308434
45
Y = -14015533
49 feet Y = -4271934
61 meter
Z = -17039788
92 Z = -5193727
66
XDOT = 23843
787835 XDOT = 7267
586532
YDOT = -2548
905747 feet/sec YDOT = -776
906472 meter/sec
ZDOT = 3515
936111 ZDOT = 1071
657327
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 08303
08170698
00020000 00000-0 20000-3 0 9079
2 25544 51
6444 49
9582 0006050 285
4361 74
6133 15
71955861 9600
Satellite: ISS
Catalog Number: 25544
Epoch time: 08303
08170698 = yrday
fracday
Element set: 907
Inclination: 51
6444 deg
RA of node: 49
9582 deg
Eccentricity:
0006050
Arg of perigee: 285
4361 deg
Mean anomaly: 74
6133 deg
Mean motion: 15
71955861 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 960
Checksum: 301
Coasting Arc #9 (Orbit 975)
---------------------------------------
Vector Time (GMT): 2008/304/01:37:21
973
Vector Time (MET): N/A
Weight (LBS) : 642049
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4665929
39 A = 6738017
84 meter
Y = -4847928
20 meter E =
0006962
Z = -262051
75 I = 51
89451
XDOT = 3586
634335 Wp = 161
58988
YDOT = -3127
720933 meter/sec RA = 44
34562 deg
ZDOT = -6048
735907 TA = 21
24497
MA = 21
21607
Ha = 191
708 n
mi
Hp = 189
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15308167
27 X = -4610099
24
Y = -15905276
25 feet Y = -4899793
15 meter
Z = -859749
83 Z = -284584
04
XDOT = 11767
173015 XDOT = 3650
727094
YDOT = -10261
551619 feet/sec YDOT = -3087
254670 meter/sec
ZDOT = -19844
934077 ZDOT = -6031
155814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21192148
13 X = -6459366
75
Y = 6168643
06 feet Y = 1880202
40 meter
Z = -947453
54 Z = -288783
84
XDOT = -3122
411606 XDOT = -951
711058
YDOT = -13741
725683 feet/sec YDOT = -4188
477988 meter/sec
ZDOT = -19777
044221 ZDOT = -6028
043079
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 08304
09886288
00020000 00000-0 20000-3 0 9081
2 25544 51
6447 44
7510 0006060 288
5283 71
5221 15
71937315 9760
Satellite: ISS
Catalog Number: 25544
Epoch time: 08304
09886288 = yrday
fracday
Element set: 908
Inclination: 51
6447 deg
RA of node: 44
7510 deg
Eccentricity:
0006060
Arg of perigee: 288
5283 deg
Mean anomaly: 71
5221 deg
Mean motion: 15
71937315 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 976
Checksum: 303
Coasting Arc #10 (Orbit 991)
---------------------------------------
Vector Time (GMT): 2008/305/01:37:21
973
Vector Time (MET): N/A
Weight (LBS) : 642049
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2233497
83 A = 6725847
57 meter
Y = 3528902
58 meter E =
0003556
Z = 5274744
96 I = 51
83253
XDOT = -6168
904516 Wp = 296
72313
YDOT = -4578
994896 meter/sec RA = 39
24248 deg
ZDOT = 453
117533 TA = 148
99260
MA = 148
97161
Ha = 191
937 n
mi
Hp = 189
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7327748
80 X = -2298417
17
Y = 11577764
36 feet Y = 3503563
16 meter
Z = 17305593
71 Z = 5263736
71
XDOT = -20239
188046 XDOT = -6119
444193
YDOT = -15022
949135 feet/sec YDOT = -4647
702619 meter/sec
ZDOT = 1486
606080 ZDOT = 423
268031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7010535
96 X = 2136811
36
Y = 11834630
25 feet Y = 3607195
30 meter
Z = 17263198
32 Z = 5261822
85
XDOT = -21651
536616 XDOT = -6599
388360
YDOT = 10835
198976 feet/sec YDOT = 3302
568648 meter/sec
ZDOT = 1370
570128 ZDOT = 417
749775
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 08305
11600571
00020000 00000-0 20000-3 0 9095
2 25544 51
6449 39
5435 0006168 293
7134 66
3380 15
72005493 9922
Satellite: ISS
Catalog Number: 25544
Epoch time: 08305
11600571 = yrday
fracday
Element set: 909
Inclination: 51
6449 deg
RA of node: 39
5435 deg
Eccentricity:
0006168
Arg of perigee: 293
7134 deg
Mean anomaly: 66
3380 deg
Mean motion: 15
72005493 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 992
Checksum: 289
Coasting Arc #11 (Orbit 1006)
---------------------------------------
Vector Time (GMT): 2008/306/01:37:21
973
Vector Time (MET): N/A
Weight (LBS) : 642049
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5922694
79 A = 6737395
63 meter
Y = 3021120
56 meter E =
0010634
Z = -1045691
99 I = 51
84823
XDOT = -1358
037403 Wp = 2
80977
YDOT = 4712
401948 meter/sec RA = 34
12284 deg
ZDOT = 5935
784264 TA = 345
79512
MA = 345
82500
Ha = 192
131 n
mi
Hp = 188
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19431413
36 X = 5893551
87
Y = 9911812
86 feet Y = 3087188
66 meter
Z = -3430747
98 Z = -1016989
34
XDOT = -4455
503290 XDOT = -1439
467123
YDOT = 15460
636311 feet/sec YDOT = 4696
760008 meter/sec
ZDOT = 19474
357820 ZDOT = 5928
989151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17364870
60 X = 5292812
56
Y = -13230176
17 feet Y = -4032557
70 meter
Z = -3319276
81 Z = -1011715
57
XDOT = 10987
154086 XDOT = 3348
884565
YDOT = 9552
509094 feet/sec YDOT = 2911
604772 meter/sec
ZDOT = 19448
374025 ZDOT = 5927
864403
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 08306
06956906
00020000 00000-0 20000-3 0 9108
2 25544 51
6453 34
6614 0006211 298
0904 61
9630 15
72011793 10071
Satellite: ISS
Catalog Number: 25544
Epoch time: 08306
06956906 = yrday
fracday
Element set: 910
Inclination: 51
6453 deg
RA of node: 34
6614 deg
Eccentricity:
0006211
Arg of perigee: 298
0904 deg
Mean anomaly: 61
9630 deg
Mean motion: 15
72011793 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1007
Checksum: 271
Coasting Arc #12 (Orbit 1022)
---------------------------------------
Vector Time (GMT): 2008/307/01:37:21
973
Vector Time (MET): N/A
Weight (LBS) : 642049
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 63102
72 A = 6726853
36 meter
Y = -4485899
37 meter E =
0010005
Z = -5020603
23 I = 51
78783
XDOT = 7108
898180 Wp = 48
31207
YDOT = 2233
892589 meter/sec RA = 29
04043 deg
ZDOT = -1902
541217 TA = 203
31367
MA = 203
35907
Ha = 192
250 n
mi
Hp = 188
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 207029
92 X = 137649
90
Y = -14717517
62 feet Y = -4484776
62 meter
Z = -16471795
37 Z = -5020115
84
XDOT = 23323
156758 XDOT = 7092
632517
YDOT = 7329
043928 feet/sec YDOT = 2313
297558 meter/sec
ZDOT = -6241
933128 ZDOT = -1868
044672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13244162
48 X = -4036820
72
Y = -6425859
99 feet Y = -1958602
12 meter
Z = -16470237
17 Z = -5020128
29
XDOT = 15953
269251 XDOT = 4862
556468
YDOT = -17190
779851 feet/sec YDOT = -5239
749699 meter/sec
ZDOT = -6108
063168 ZDOT = -1861
737654
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 08307
08669160
00020000 00000-0 20000-3 0 9115
2 25544 51
6450 29
4539 0006321 302
7989 57
2564 15
72036759 10235
Satellite: ISS
Catalog Number: 25544
Epoch time: 08307
08669160 = yrday
fracday
Element set: 911
Inclination: 51
6450 deg
RA of node: 29
4539 deg
Eccentricity:
0006321
Arg of perigee: 302
7989 deg
Mean anomaly: 57
2564 deg
Mean motion: 15
72036759 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1023
Checksum: 292
Coasting Arc #13 (Orbit 1038)
---------------------------------------
Vector Time (GMT): 2008/308/01:37:21
973
Vector Time (MET): N/A
Weight (LBS) : 642049
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6288126
97 A = 6735682
15 meter
Y = -846439
41 meter E =
0008348
Z = 2252699
55 I = 51
79094
XDOT = -1256
595610 Wp = 94
66413
YDOT = -5265
988910 meter/sec RA = 23
89582 deg
ZDOT = -5469
650873 TA = 60
13409
MA = 60
05117
Ha = 192
451 n
mi
Hp = 188
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20630337
83 X = -6289138
05
Y = -2777032
20 feet Y = -916762
67 meter
Z = 7390746
57 Z = 2222148
63
XDOT = -4122
689009 XDOT = -1171
045895
YDOT = -17276
866501 feet/sec YDOT = -5279
562230 meter/sec
ZDOT = -17945
048796 ZDOT = -5475
548061
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10859036
61 X = -3309834
36
Y = 17808461
83 feet Y = 5428019
17 meter
Z = 7272268
74 Z = 2216587
51
XDOT = -16135
680601 XDOT = -4918
155447
YDOT = -2478
829010 feet/sec YDOT = -755
547082 meter/sec
ZDOT = -17968
290987 ZDOT = -5476
735093
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 08308
10380486
00020000 00000-0 20000-3 0 9121
2 25544 51
6450 24
2464 0006213 307
0359 53
0235 15
72022779 10397
Satellite: ISS
Catalog Number: 25544
Epoch time: 08308
10380486 = yrday
fracday
Element set: 912
Inclination: 51
6450 deg
RA of node: 24
2464 deg
Eccentricity:
0006213
Arg of perigee: 307
0359 deg
Mean anomaly: 53
0235 deg
Mean motion: 15
72022779 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1039
Checksum: 260
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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