Date:
August 20th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 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 3833)
---------------------------------------
Vector Time (GMT): 2008/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4430621
09 A = 6740171
33 meter
Y = 4938900
24 meter E =
0017768
Z = -1137145
27 I = 51
92812
XDOT = -2914
676197 Wp = 32
88686
YDOT = 3964
978016 meter/sec RA = 55
82029 deg
ZDOT = 5921
986048 TA = 314
72243
MA = 314
86696
Ha = 197
171 n
mi
Hp = 186
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14536158
42 X = 4380588
19
Y = 16203740
94 feet Y = 4988166
23 meter
Z = -3730791
56 Z = -1115743
22
XDOT = -9562
585947 XDOT = -2987
564127
YDOT = 13008
458059 feet/sec YDOT = 3931
976988 meter/sec
ZDOT = 19429
088083 ZDOT = 5907
649643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3184317
79 X = -970580
06
Y = -21548431
39 feet Y = -6567961
89 meter
Z = -3647622
91 Z = -1111795
46
XDOT = 13678
098865 XDOT = 4169
084534
YDOT = -5268
184068 feet/sec YDOT = -1605
742504 meter/sec
ZDOT = 19374
027661 ZDOT = 5905
203631
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 08231
50214911
00020000 00000-0 20000-3 0 9006
2 25544 51
6385 56
4260 0008331 27
6831 332
4772 15
71006828 38349
Satellite: ISS
Catalog Number: 25544
Epoch time: 08231
50214911 = yrday
fracday
Element set: 900
Inclination: 51
6385 deg
RA of node: 56
4260 deg
Eccentricity:
0008331
Arg of perigee: 27
6831 deg
Mean anomaly: 332
4772 deg
Mean motion: 15
71006828 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3834
Checksum: 267
Coasting Arc #2 (Orbit 3849)
---------------------------------------
Vector Time (GMT): 2008/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1318521
02 A = 6730335
34 meter
Y = -4451712
76 meter E =
0019406
Z = -4890202
62 I = 51
87786
XDOT = 5902
297093 Wp = 56
51433
YDOT = 4322
793438 meter/sec RA = 50
75470 deg
ZDOT = -2339
957290 TA = 190
68226
MA = 190
72354
Ha = 197
200 n
mi
Hp = 186
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4325856
36 X = 1391958
30
Y = -14605356
83 feet Y = -4436557
82 meter
Z = -16043971
85 Z = -4883618
81
XDOT = 19364
491775 XDOT = 5864
887245
YDOT = 14182
393170 feet/sec YDOT = 4388
587093 meter/sec
ZDOT = -7677
025230 ZDOT = -2311
375160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11580943
25 X = -3529871
50
Y = 9935514
88 feet Y = 3028344
94 meter
Z = -16018920
43 Z = -4882566
95
XDOT = -8006
520256 XDOT = -2440
387374
YDOT = -21551
549504 feet/sec YDOT = -6568
912289 meter/sec
ZDOT = -7566
162666 ZDOT = -2306
166381
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 08232
51991005
00020000 00000-0 20000-3 0 9015
2 25544 51
6385 51
2220 0008415 32
6115 327
5565 15
71037413 38509
Satellite: ISS
Catalog Number: 25544
Epoch time: 08232
51991005 = yrday
fracday
Element set: 901
Inclination: 51
6385 deg
RA of node: 51
2220 deg
Eccentricity:
0008415
Arg of perigee: 32
6115 deg
Mean anomaly: 327
5565 deg
Mean motion: 15
71037413 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3850
Checksum: 256
Coasting Arc #3 (Orbit 3865)
---------------------------------------
Vector Time (GMT): 2008/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5567478
99 A = 6737030
57 meter
Y = -2445547
66 meter E =
0018639
Z = 2890943
88 I = 51
88126
XDOT = -104
142728 Wp = 74
90411
YDOT = -5791
346299 meter/sec RA = 45
61590 deg
ZDOT = -5067
897443 TA = 72
01985
MA = 71
81678
Ha = 197
224 n
mi
Hp = 186
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18266007
19 X = -5553762
34
Y = -8023450
32 feet Y = -2507729
65 meter
Z = 9484724
03 Z = 2863930
53
XDOT = -341
675616 XDOT = -14
756374
YDOT = -19000
479985 feet/sec YDOT = -5792
011217 meter/sec
ZDOT = -16626
960114 ZDOT = -5068
186112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11411226
60 X = 3478141
87
Y = 16424994
51 feet Y = 5006338
33 meter
Z = 9380097
37 Z = 2859053
68
XDOT = -8536
588669 XDOT = -2601
952226
YDOT = 15487
313862 feet/sec YDOT = 4720
533265 meter/sec
ZDOT = -16628
587419 ZDOT = -5068
393445
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 08233
53765933
00020000 00000-0 20000-3 0 9028
2 25544 51
6388 46
0171 0008324 34
8676 325
3030 15
71057178 38664
Satellite: ISS
Catalog Number: 25544
Epoch time: 08233
53765933 = yrday
fracday
Element set: 902
Inclination: 51
6388 deg
RA of node: 46
0171 deg
Eccentricity:
0008324
Arg of perigee: 34
8676 deg
Mean anomaly: 325
3030 deg
Mean motion: 15
71057178 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3866
Checksum: 294
Coasting Arc #4 (Orbit 3881)
---------------------------------------
Vector Time (GMT): 2008/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1581468
51 A = 6734136
32 meter
Y = 5303099
89 meter E =
0017227
Z = 3819198
71 I = 51
85062
XDOT = -6369
968022 Wp = 73
85267
YDOT = -1123
728274 meter/sec RA = 40
56748 deg
ZDOT = 4187
225975 TA = 332
39084
MA = 332
48222
Ha = 197
208 n
mi
Hp = 186
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5188544
99 X = 1503497
86
Y = 17398621
69 feet Y = 5320348
86 meter
Z = 12530179
51 Z = 3826692
06
XDOT = -20898
845217 XDOT = -6377
269692
YDOT = -3686
772552 feet/sec YDOT = -1195
001712 meter/sec
ZDOT = 13737
618027 ZDOT = 4156
262910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4444225
02 X = 1354599
78
Y = -17582480
90 feet Y = -5359140
18 meter
Z = 12559604
44 Z = 3828167
43
XDOT = 14903
482013 XDOT = 4542
581318
YDOT = 13519
919275 feet/sec YDOT = 4120
871395 meter/sec
ZDOT = 13617
845699 ZDOT = 4150
719369
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 08234
55540000
00020000 00000-0 20000-3 0 9038
2 25544 51
6388 40
8128 0008276 39
9556 320
2213 15
71080775 38821
Satellite: ISS
Catalog Number: 25544
Epoch time: 08234
55540000 = yrday
fracday
Element set: 903
Inclination: 51
6388 deg
RA of node: 40
8128 deg
Eccentricity:
0008276
Arg of perigee: 39
9556 deg
Mean anomaly: 320
2213 deg
Mean motion: 15
71080775 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3882
Checksum: 281
Coasting Arc #5 (Orbit 3896)
---------------------------------------
Vector Time (GMT): 2008/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5170377
53 A = 6732633
75 meter
Y = -468534
62 meter E =
0014158
Z = -4296625
65 I = 51
82343
XDOT = 3463
989076 Wp = 77
28736
YDOT = 5878
915736 meter/sec RA = 35
41815 deg
ZDOT = 3540
138287 TA = 228
51306
MA = 228
63468
Ha = 197
379 n
mi
Hp = 185
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16963180
88 X = 5196104
78
Y = -1537187
08 feet Y = -410572
57 meter
Z = -14096540
83 Z = -4271445
39
XDOT = 11364
793558 XDOT = 3380
795239
YDOT = 19287
781286 feet/sec YDOT = 5917
186843 meter/sec
ZDOT = 11614
626926 ZDOT = 3556
764409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15580103
16 X = -4748815
44
Y = -7078563
47 feet Y = -2157546
15 meter
Z = -13999258
47 Z = -4266973
98
XDOT = -817
605696 XDOT = -249
206216
YDOT = -21215
111827 feet/sec YDOT = -6466
366085 meter/sec
ZDOT = 11679
392821 ZDOT = 3559
878932
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 08235
50952342
00020000 00000-0 20000-3 0 9041
2 25544 51
6400 35
9343 0008403 44
4519 315
7315 15
71075336 38977
Satellite: ISS
Catalog Number: 25544
Epoch time: 08235
50952342 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 35
9343 deg
Eccentricity:
0008403
Arg of perigee: 44
4519 deg
Mean anomaly: 315
7315 deg
Mean motion: 15
71075336 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3897
Checksum: 280
Coasting Arc #6 (Orbit 3912)
---------------------------------------
Vector Time (GMT): 2008/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4324392
78 A = 6738048
98 meter
Y = -4631882
14 meter E =
0010489
Z = -2302573
02 I = 51
81781
XDOT = 5040
644629 Wp = 80
26477
YDOT = -2009
166176 meter/sec RA = 30
36213 deg
ZDOT = -5444
255925 TA = 125
48716
MA = 125
38924
Ha = 197
352 n
mi
Hp = 185
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14187640
36 X = -4261091
42
Y = -15196463
72 feet Y = -4679885
96 meter
Z = -7554373
43 Z = -2323427
41
XDOT = 16537
547997 XDOT = 5089
184092
YDOT = -6591
752545 feet/sec YDOT = -1952
527163 meter/sec
ZDOT = -17861
732036 ZDOT = -5419
650591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5143185
64 X = 1567642
98
Y = 20113154
35 feet Y = 6130489
45 meter
Z = -7635369
67 Z = -2327260
68
XDOT = -16297
865004 XDOT = -4967
589253
YDOT = -2553
374003 feet/sec YDOT = -778
268396 meter/sec
ZDOT = -17766
800469 ZDOT = -5415
320783
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 08236
52724315
00020000 00000-0 20000-3 0 9052
2 25544 51
6401 30
7301 0008539 47
4003 312
7877 15
71115408 39130
Satellite: ISS
Catalog Number: 25544
Epoch time: 08236
52724315 = yrday
fracday
Element set: 905
Inclination: 51
6401 deg
RA of node: 30
7301 deg
Eccentricity:
0008539
Arg of perigee: 47
4003 deg
Mean anomaly: 312
7877 deg
Mean motion: 15
71115408 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3913
Checksum: 264
Coasting Arc #7 (Orbit 3928)
---------------------------------------
Vector Time (GMT): 2008/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3334517
37 A = 6729368
04 meter
Y = 2862081
38 meter E =
0013566
Z = 5089167
56 I = 51
76194
XDOT = -6175
867313 Wp = 52
63535
YDOT = -4312
255461 meter/sec RA = 25
22550 deg
ZDOT = -1610
390009 TA = 52
86369
MA = 52
73984
Ha = 197
591 n
mi
Hp = 185
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10940017
61 X = -3390996
02
Y = 9390030
77 feet Y = 2824476
78 meter
Z = 16696743
95 Z = 5072831
48
XDOT = -20262
031868 XDOT = -6119
365002
YDOT = -14147
819754 feet/sec YDOT = -4381
001541 meter/sec
ZDOT = -5283
431788 ZDOT = -1640
255373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14130900
74 X = 4307098
54
Y = -3204823
43 feet Y = -976830
18 meter
Z = 16633841
20 Z = 5069994
80
XDOT = 11134
561702 XDOT = 3393
814407
YDOT = 20883
854327 feet/sec YDOT = 6365
398799 meter/sec
ZDOT = -5399
228272 ZDOT = -1645
684777
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 08237
54495477
00020000 00000-0 20000-3 0 9060
2 25544 51
6399 25
5259 0008515 52
2588 307
9344 15
71067673 39298
Satellite: ISS
Catalog Number: 25544
Epoch time: 08237
54495477 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 25
5259 deg
Eccentricity:
0008515
Arg of perigee: 52
2588 deg
Mean anomaly: 307
9344 deg
Mean motion: 15
71067673 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3929
Checksum: 330
Coasting Arc #8 (Orbit 3944)
---------------------------------------
Vector Time (GMT): 2008/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6168951
93 A = 6740241
77 meter
Y = 2650805
72 meter E =
0021529
Z = 463034
80 I = 51
77366
XDOT = -2278
769554 Wp = 51
94980
YDOT = 4219
852002 meter/sec RA = 20
13947 deg
ZDOT = 6025
939380 TA = 313
07445
MA = 313
25446
Ha = 197
408 n
mi
Hp = 185
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20239343
59 X = 6136602
38
Y = 8696869
16 feet Y = 2719609
58 meter
Z = 1519143
04 Z = 492924
99
XDOT = -7476
278065 XDOT = -2355
059990
YDOT = 13844
658800 feet/sec YDOT = 4193
942494 meter/sec
ZDOT = 19770
142324 ZDOT = 6014
684183
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14185849
80 X = -4323847
02
Y = -16842301
67 feet Y = -5133533
55 meter
Z = 1634899
96 Z = 498317
51
XDOT = 11761
771126 XDOT = 3584
987839
YDOT = -7939
708599 feet/sec YDOT = -2420
023181 meter/sec
ZDOT = 19726
987387 ZDOT = 6012
785756
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 08238
56265202
00020000 00000-0 20000-3 0 9075
2 25544 51
6413 20
3222 0008448 55
8284 304
3678 15
71137131 39451
Satellite: ISS
Catalog Number: 25544
Epoch time: 08238
56265202 = yrday
fracday
Element set: 907
Inclination: 51
6413 deg
RA of node: 20
3222 deg
Eccentricity:
0008448
Arg of perigee: 55
8284 deg
Mean anomaly: 304
3678 deg
Mean motion: 15
71137131 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3945
Checksum: 278
Coasting Arc #9 (Orbit 3959)
---------------------------------------
Vector Time (GMT): 2008/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 516358
10 A = 6728304
75 meter
Y = -4172085
11 meter E =
0022816
Z = -5272696
17 I = 51
70599
XDOT = 7495
531259 Wp = 75
87090
YDOT = 1588
522923 meter/sec RA = 15
03336 deg
ZDOT = -519
318957 TA = 189
16540
MA = 189
20712
Ha = 197
429 n
mi
Hp = 185
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1694088
26 X = 588586
14
Y = -13687943
27 feet Y = -4165906
71 meter
Z = -17298871
94 Z = -5270012
56
XDOT = 24591
637990 XDOT = 7479
733785
YDOT = 5211
689380 feet/sec YDOT = 1672
253972 meter/sec
ZDOT = -1703
802353 ZDOT = -482
944375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7540564
42 X = -2298364
03
Y = 11563582
03 feet Y = 3524579
80 meter
Z = -17288844
82 Z = -5269639
90
XDOT = -19078
730922 XDOT = -5815
197185
YDOT = -14795
674303 feet/sec YDOT = -4509
721528 meter/sec
ZDOT = -1563
062751 ZDOT = -476
421526
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 08239
51673533
00020000 00000-0 20000-3 0 9082
2 25544 51
6415 15
4443 0008538 58
6841 301
5155 15
71156530 39603
Satellite: ISS
Catalog Number: 25544
Epoch time: 08239
51673533 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 15
4443 deg
Eccentricity:
0008538
Arg of perigee: 58
6841 deg
Mean anomaly: 301
5155 deg
Mean motion: 15
71156530 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3960
Checksum: 287
Coasting Arc #10 (Orbit 3975)
---------------------------------------
Vector Time (GMT): 2008/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6597242
11 A = 6739547
58 meter
Y = -70844
33 meter E =
0019737
Z = 1349493
41 I = 51
71504
XDOT = -1156
062307 Wp = 98
70255
YDOT = -4879
999485 meter/sec RA = 9
90635 deg
ZDOT = -5838
337802 TA = 66
50621
MA = 66
29890
Ha = 197
454 n
mi
Hp = 185
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21644495
11 X = -6602515
08
Y = -232428
89 feet Y = -144648
03 meter
Z = 4427471
83 Z = 1317431
74
XDOT = -3792
855339 XDOT = -1073
046340
YDOT = -16010
496999 feet/sec YDOT = -4892
462820 meter/sec
ZDOT = -19154
651580 ZDOT = -5843
752427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19596303
37 X = 5972953
27
Y = 9252311
19 feet Y = 2820104
45 meter
Z = 4303525
39 Z = 1311714
54
XDOT = -2658
078393 XDOT = -810
182294
YDOT = 14658
168115 feet/sec YDOT = 4467
809641 meter/sec
ZDOT = -19175
990396 ZDOT = -5844
841873
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 08240
53441332
00020000 00000-0 20000-3 0 9097
2 25544 51
6414 10
2387 0008460 62
2461 297
9557 15
71154360 39765
Satellite: ISS
Catalog Number: 25544
Epoch time: 08240
53441332 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 10
2387 deg
Eccentricity:
0008460
Arg of perigee: 62
2461 deg
Mean anomaly: 297
9557 deg
Mean motion: 15
71154360 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3976
Checksum: 284
Coasting Arc #11 (Orbit 3991)
---------------------------------------
Vector Time (GMT): 2008/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2516763
80 A = 6730152
38 meter
Y = 4004113
42 meter E =
0013880
Z = 4776407
19 I = 51
65649
XDOT = -7128
576748 Wp = 90
01803
YDOT = 1425
712260 meter/sec RA = 4
82822 deg
ZDOT = 2554
602651 TA = 334
94297
MA = 335
01027
Ha = 197
314 n
mi
Hp = 185
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8257099
08 X = 2448599
63
Y = 13136855
04 feet Y = 4031876
12 meter
Z = 15670627
25 Z = 4788467
88
XDOT = -23387
718990 XDOT = -7156
399042
YDOT = 4677
533660 feet/sec YDOT = 1345
840811 meter/sec
ZDOT = 8381
242293 ZDOT = 2519
905132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2205056
73 X = -672101
29
Y = -15310791
19 feet Y = -4666729
15 meter
Z = 15717588
93 Z = 4790721
11
XDOT = 22224
813303 XDOT = 6774
123095
YDOT = 5286
918594 feet/sec YDOT = 1611
452787 meter/sec
ZDOT = 8247
230161 ZDOT = 2513
755753
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 08241
55207910
00020000 00000-0 20000-3 0 9104
2 25544 51
6427 5
0347 0008402 65
5185 294
6853 15
71209258 39920
Satellite: ISS
Catalog Number: 25544
Epoch time: 08241
55207910 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 5
0347 deg
Eccentricity:
0008402
Arg of perigee: 65
5185 deg
Mean anomaly: 294
6853 deg
Mean motion: 15
71209258 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3992
Checksum: 286
Coasting Arc #12 (Orbit 4006)
---------------------------------------
Vector Time (GMT): 2008/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5499688
74 A = 6736324
05 meter
Y = -2435204
76 meter E =
0013044
Z = -3037899
93 I = 51
64785
XDOT = 4435
212371 Wp = 68
44678
YDOT = 3882
404634 meter/sec RA = 359
67200 deg
ZDOT = 4938
797476 TA = 256
46126
MA = 256
60661
Ha = 197
522 n
mi
Hp = 185
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18043598
22 X = 5541268
14
Y = -7989516
94 feet Y = -2373471
64 meter
Z = -9966863
28 Z = -3011081
91
XDOT = 14551
221689 XDOT = 4367
477726
YDOT = 12737
548013 feet/sec YDOT = 3931
623087 meter/sec
ZDOT = 16203
403792 ZDOT = 4960
178751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19781398
41 X = -6029370
24
Y = 389624
05 feet Y = 118757
41 meter
Z = -9863399
58 Z = -3006364
19
XDOT = -8397
852675 XDOT = -2559
665495
YDOT = -15886
252335 feet/sec YDOT = -4842
129712 meter/sec
ZDOT = 16286
389935 ZDOT = 4964
091652
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 08242
50613323
00020000 00000-0 20000-3 0 9110
2 25544 51
6431
1566 0008520 67
9804 292
2262 15
71169131 40070
Satellite: ISS
Catalog Number: 25544
Epoch time: 08242
50613323 = yrday
fracday
Element set: 911
Inclination: 51
6431 deg
RA of node:
1566 deg
Eccentricity:
0008520
Arg of perigee: 67
9804 deg
Mean anomaly: 292
2262 deg
Mean motion: 15
71169131 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4007
Checksum: 252
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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