Date:
July 10th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 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 3204)
---------------------------------------
Vector Time (GMT): 2008/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3523784
24 A = 6718648
49 meter
Y = -2911201
73 meter E =
0006519
Z = 4919625
50 I = 51
30101
XDOT = 2789
875670 Wp = 30
26263
YDOT = 6877
170536 meter/sec RA = 260
86643 deg
ZDOT = 2075
644204 TA = 39
57223
MA = 39
52465
Ha = 190
080 n
mi
Hp = 181
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11560971
93 X = 3532177
37
Y = -9551186
78 feet Y = -2871750
39 meter
Z = 16140503
62 Z = 4936763
99
XDOT = 9153
135401 XDOT = 2702
683670
YDOT = 22562
895458 feet/sec YDOT = 6907
880774 meter/sec
ZDOT = 6809
856313 ZDOT = 2088
986331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12493345
25 X = -3807971
63
Y = -8165163
30 feet Y = -2488741
77 meter
Z = 16206280
59 Z = 4939674
33
XDOT = 18304
786720 XDOT = 5579
298992
YDOT = -14416
570036 feet/sec YDOT = -4394
170547 meter/sec
ZDOT = 6861
882585 ZDOT = 2091
501812
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 08191
55117999
00020000 00000-0 20000-3 0 9004
2 25544 51
6396 261
3770 0009221 348
7281 11
3674 15
75014161 32058
Satellite: ISS
Catalog Number: 25544
Epoch time: 08191
55117999 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 261
3770 deg
Eccentricity:
0009221
Arg of perigee: 348
7281 deg
Mean anomaly: 11
3674 deg
Mean motion: 15
75014161 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3205
Checksum: 284
Coasting Arc #2 (Orbit 3219)
---------------------------------------
Vector Time (GMT): 2008/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2746730
41 A = 6728425
57 meter
Y = -5948939
42 meter E =
0016505
Z = -1485938
80 I = 51
33890
XDOT = 3936
573230 Wp = 13
62600
YDOT = -3252
551303 meter/sec RA = 255
66944 deg
ZDOT = 5773
659323 TA = 329
92097
MA = 330
01566
Ha = 190
411 n
mi
Hp = 181
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9011582
72 X = -2672785
89
Y = -19517517
78 feet Y = -5979241
30 meter
Z = -4875127
29 Z = -1499103
50
XDOT = 12915
266502 XDOT = 3944
603901
YDOT = -10671
100075 feet/sec YDOT = -3208
486096 meter/sec
ZDOT = 18942
451848 ZDOT = 5792
802239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15778318
66 X = -4809231
53
Y = 14583700
33 feet Y = 4445111
86 meter
Z = -4926391
59 Z = -1501564
16
XDOT = -13047
624347 XDOT = -3976
915901
YDOT = -7724
388245 feet/sec YDOT = -2354
393537 meter/sec
ZDOT = 19015
922800 ZDOT = 5796
053269
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 08192
50291724
00020000 00000-0 20000-3 0 9010
2 25544 51
6390 256
4824 0009481 352
8317 7
2710 15
74973309 32200
Satellite: ISS
Catalog Number: 25544
Epoch time: 08192
50291724 = yrday
fracday
Element set: 901
Inclination: 51
6390 deg
RA of node: 256
4824 deg
Eccentricity:
0009481
Arg of perigee: 352
8317 deg
Mean anomaly: 7
2710 deg
Mean motion: 15
74973309 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3220
Checksum: 282
Coasting Arc #3 (Orbit 3235)
---------------------------------------
Vector Time (GMT): 2008/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3386219
50 A = 6717807
07 meter
Y = 2740957
14 meter E =
0017915
Z = -5127516
43 I = 51
31159
XDOT = -3480
029544 Wp = 48
76854
YDOT = -6735
362218 meter/sec RA = 250
52873 deg
ZDOT = -1293
521415 TA = 208
73867
MA = 208
83749
Ha = 190
502 n
mi
Hp = 181
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11109644
03 X = -3391709
14
Y = 8992641
55 feet Y = 2703060
51 meter
Z = -16822560
47 Z = -5143979
62
XDOT = -11417
419764 XDOT = -3398
171328
YDOT = -22097
645072 feet/sec YDOT = -6773
820031 meter/sec
ZDOT = -4243
836664 ZDOT = -1310
229481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12090414
25 X = 3685158
26
Y = 7482213
61 feet Y = 2280578
71 meter
Z = -16885754
23 Z = -5146777
89
XDOT = -16633
742970 XDOT = -5069
964857
YDOT = 17089
922051 feet/sec YDOT = 5209
008241 meter/sec
ZDOT = -4308
831085 ZDOT = -1313
331715
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 08193
51809229
00020000 00000-0 20000-3 0 9028
2 25544 51
6387 251
2607 0009375 357
0949 3
0159 15
75009458 32362
Satellite: ISS
Catalog Number: 25544
Epoch time: 08193
51809229 = yrday
fracday
Element set: 902
Inclination: 51
6387 deg
RA of node: 251
2607 deg
Eccentricity:
0009375
Arg of perigee: 357
0949 deg
Mean anomaly: 3
0159 deg
Mean motion: 15
75009458 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3236
Checksum: 302
Coasting Arc #4 (Orbit 3251)
---------------------------------------
Vector Time (GMT): 2008/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3327390
50 A = 6728859
01 meter
Y = 5799324
13 meter E =
0011172
Z = 756586
65 I = 51
36103
XDOT = -3855
836539 Wp = 82
47067
YDOT = 2998
300447 meter/sec RA = 245
34477 deg
ZDOT = -5948
283067 TA = 89
25270
MA = 89
12469
Ha = 190
635 n
mi
Hp = 181
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10916635
49 X = 3258618
88
Y = 19026653
96 feet Y = 5836148
28 meter
Z = 2482239
66 Z = 772584
96
XDOT = -12650
382347 XDOT = -3860
181791
YDOT = 9836
943724 feet/sec YDOT = 2955
158908 meter/sec
ZDOT = -19515
364392 ZDOT = -5967
024786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14149776
22 X = 4312851
79
Y = -16752843
49 feet Y = -5106266
69 meter
Z = 2544419
97 Z = 775539
21
XDOT = 12310
800146 XDOT = 3752
331885
YDOT = 7385
850643 feet/sec YDOT = 2251
207276 meter/sec
ZDOT = -19587
319685 ZDOT = -5970
215040
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 08194
53325490
00020000 00000-0 20000-3 0 9035
2 25544 51
6392 246
0390 0009588 1
7130 358
4065 15
75073976 32527
Satellite: ISS
Catalog Number: 25544
Epoch time: 08194
53325490 = yrday
fracday
Element set: 903
Inclination: 51
6392 deg
RA of node: 246
0390 deg
Eccentricity:
0009588
Arg of perigee: 1
7130 deg
Mean anomaly: 358
4065 deg
Mean motion: 15
75073976 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3252
Checksum: 294
Coasting Arc #5 (Orbit 3267)
---------------------------------------
Vector Time (GMT): 2008/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3383735
80 A = 6717094
04 meter
Y = -2509547
29 meter E =
0009189
Z = 5228298
63 I = 51
33418
XDOT = 4131
902846 Wp = 22
03613
YDOT = 6489
637280 meter/sec RA = 240
19194 deg
ZDOT = 448
980124 TA = 63
73192
MA = 63
63753
Ha = 190
613 n
mi
Hp = 180
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11101495
39 X = 3386148
40
Y = -8233422
87 feet Y = -2471695
83 meter
Z = 17153210
72 Z = 5244742
21
XDOT = 13556
111698 XDOT = 4056
846541
YDOT = 21291
460892 feet/sec YDOT = 6535
422848 meter/sec
ZDOT = 1473
031902 ZDOT = 468
871670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11628174
31 X = -3544267
53
Y = -7324455
26 feet Y = -2232493
96 meter
Z = 17216358
72 Z = 5247546
14
XDOT = 14492
523960 XDOT = 4417
321303
YDOT = -19426
705517 feet/sec YDOT = -5921
259842 meter/sec
ZDOT = 1550
286979 ZDOT = 472
527471
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 08195
54840655
00020000 00000-0 20000-3 0 9043
2 25544 51
6385 240
8176 0009523 5
6254 354
5015 15
75078550 32684
Satellite: ISS
Catalog Number: 25544
Epoch time: 08195
54840655 = yrday
fracday
Element set: 904
Inclination: 51
6385 deg
RA of node: 240
8176 deg
Eccentricity:
0009523
Arg of perigee: 5
6254 deg
Mean anomaly: 354
5015 deg
Mean motion: 15
75078550 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3268
Checksum: 299
Coasting Arc #6 (Orbit 3282)
---------------------------------------
Vector Time (GMT): 2008/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3869673
85 A = 6729220
21 meter
Y = -5490207
95 meter E =
0020963
Z = -29576
58 I = 51
39027
XDOT = 3922
061347 Wp = 29
42888
YDOT = -2787
056246 meter/sec RA = 235
02407 deg
ZDOT = 6024
962987 TA = 330
24826
MA = 330
36730
Ha = 190
937 n
mi
Hp = 180
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12695780
36 X = -3807850
20
Y = -18012493
29 feet Y = -5533135
19 meter
Z = -97036
02 Z = -48226
20
XDOT = 12867
655339 XDOT = 3923
667130
YDOT = -9143
885323 feet/sec YDOT = -2743
189638 meter/sec
ZDOT = 19766
938935 ZDOT = 6044
019656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11953846
04 X = -3643532
27
Y = 18512672
15 feet Y = 5642662
47 meter
Z = -169423
21 Z = -51640
19
XDOT = -11902
045433 XDOT = -3627
743448
YDOT = -7534
984438 feet/sec YDOT = -2296
663257 meter/sec
ZDOT = 19840
139418 ZDOT = 6047
274495
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 08196
50010173
00020000 00000-0 20000-3 0 9055
2 25544 51
6384 235
9223 0009808 9
6268 350
5082 15
75040987 32836
Satellite: ISS
Catalog Number: 25544
Epoch time: 08196
50010173 = yrday
fracday
Element set: 905
Inclination: 51
6384 deg
RA of node: 235
9223 deg
Eccentricity:
0009808
Arg of perigee: 9
6268 deg
Mean anomaly: 350
5082 deg
Mean motion: 15
75040987 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3283
Checksum: 293
Coasting Arc #7 (Orbit 3298)
---------------------------------------
Vector Time (GMT): 2008/197/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3496668
72 A = 6717070
97 meter
Y = 2354510
68 meter E =
0019224
Z = -5243907
49 I = 51
36806
XDOT = -4694
904506 Wp = 63
65021
YDOT = -6077
277295 meter/sec RA = 229
85851 deg
ZDOT = 411
461021 TA = 210
22148
MA = 210
33250
Ha = 190
937 n
mi
Hp = 180
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11472010
23 X = -3497263
62
Y = 7724772
57 feet Y = 2315406
59 meter
Z = -17204420
89 Z = -5260895
16
XDOT = -15403
230005 XDOT = -4628
597276
YDOT = -19938
573804 feet/sec YDOT = -6129
407745 meter/sec
ZDOT = 1349
937733 ZDOT = 388
813276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11549282
23 X = 3520221
22
Y = 7459426
65 feet Y = 2273633
24 meter
Z = -17269692
01 Z = -5263802
13
XDOT = -11803
873281 XDOT = -3597
820576
YDOT = 21125
220396 feet/sec YDOT = 6438
967177 meter/sec
ZDOT = 1262
072353 ZDOT = 384
679653
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 08197
51523144
00020000 00000-0 20000-3 0 9065
2 25544 51
6389 230
7004 0009643 13
3597 346
7820 15
75081720 32999
Satellite: ISS
Catalog Number: 25544
Epoch time: 08197
51523144 = yrday
fracday
Element set: 906
Inclination: 51
6389 deg
RA of node: 230
7004 deg
Eccentricity:
0009643
Arg of perigee: 13
3597 deg
Mean anomaly: 346
7820 deg
Mean motion: 15
75081720 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3299
Checksum: 296
Coasting Arc #8 (Orbit 3314)
---------------------------------------
Vector Time (GMT): 2008/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4303793
68 A = 6728740
18 meter
Y = 5117754
73 meter E =
0009768
Z = -764294
86 I = 51
42691
XDOT = -4129
076141 Wp = 83
72554
YDOT = 2592
910967 meter/sec RA = 224
70766 deg
ZDOT = -5952
895011 TA = 104
62624
MA = 104
51792
Ha = 191
047 n
mi
Hp = 180
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14120058
00 X = 4249959
02
Y = 16790533
90 feet Y = 5165581
36 meter
Z = -2507529
06 Z = -743517
09
XDOT = -13546
837734 XDOT = -4128
845889
YDOT = 8506
925745 feet/sec YDOT = 2546
739677 meter/sec
ZDOT = -19530
495442 ZDOT = -5972
952764
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9609097
00 X = 2928852
76
Y = -19732231
34 feet Y = -6014384
11 meter
Z = -2426946
59 Z = -739733
32
XDOT = 11788
485052 XDOT = 3593
130244
YDOT = 8125
603460 feet/sec YDOT = 2476
683935 meter/sec
ZDOT = -19607
586992 ZDOT = -5976
392515
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
53034922
00020000 00000-0 20000-3 0 9070
2 25544 51
6381 225
4782 0009719 17
9297 342
2208 15
75122395 33150
Satellite: ISS
Catalog Number: 25544
Epoch time: 08198
53034922 = yrday
fracday
Element set: 907
Inclination: 51
6381 deg
RA of node: 225
4782 deg
Eccentricity:
0009719
Arg of perigee: 17
9297 deg
Mean anomaly: 342
2208 deg
Mean motion: 15
75122395 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3315
Checksum: 302
Coasting Arc #9 (Orbit 3330)
---------------------------------------
Vector Time (GMT): 2008/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3737926
88 A = 6717378
30 meter
Y = -2212826
91 meter E =
0013521
Z = 5119982
54 I = 51
40951
XDOT = 5132
491240 Wp = 31
87815
YDOT = 5596
318354 meter/sec RA = 219
52917 deg
ZDOT = -1315
462448 TA = 70
80902
MA = 70
66274
Ha = 191
019 n
mi
Hp = 179
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12263539
62 X = 3737521
72
Y = -7259930
82 feet Y = -2171030
45 meter
Z = 16797842
97 Z = 5138139
71
XDOT = 16838
882021 XDOT = 5075
921034
YDOT = 18360
624522 feet/sec YDOT = 5653
396750 meter/sec
ZDOT = -4315
821681 ZDOT = -1290
665619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11712117
65 X = -3569853
46
Y = -7973535
39 feet Y = -2430333
59 meter
Z = 16867648
37 Z = 5141259
22
XDOT = 8960
239332 XDOT = 2731
080948
YDOT = -22177
166625 feet/sec YDOT = -6759
600387 meter/sec
ZDOT = -4219
681733 ZDOT = -1286
158992
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
54545525
00020000 00000-0 20000-3 0 9089
2 25544 51
6370 220
2560 0009788 21
8858 338
2722 15
75148689 33316
Satellite: ISS
Catalog Number: 25544
Epoch time: 08199
54545525 = yrday
fracday
Element set: 908
Inclination: 51
6370 deg
RA of node: 220
2560 deg
Eccentricity:
0009788
Arg of perigee: 21
8858 deg
Mean anomaly: 338
2722 deg
Mean motion: 15
75148689 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3331
Checksum: 317
Coasting Arc #10 (Orbit 3346)
---------------------------------------
Vector Time (GMT): 2008/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4620876
27 A = 6727950
30 meter
Y = -4629121
78 meter E =
0022767
Z = 1518603
46 I = 51
46857
XDOT = 4444
031913 Wp = 47
11006
YDOT = -2529
297618 meter/sec RA = 214
39640 deg
ZDOT = 5773
407714 TA = 329
69457
MA = 329
82603
Ha = 191
218 n
mi
Hp = 179
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15160355
20 X = -4576146
21
Y = -15187407
41 feet Y = -4680545
22 meter
Z = 4982294
82 Z = 1496263
57
XDOT = 14580
157194 XDOT = 4443
939012
YDOT = -8298
220532 feet/sec YDOT = -2479
603363 meter/sec
ZDOT = 18941
626358 ZDOT = 5794
995766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7021913
73 X = -2140279
31
Y = 20298812
55 feet Y = 6187078
07 meter
Z = 4895703
42 Z = 1492210
40
XDOT = -12308
304707 XDOT = -3751
571275
YDOT = -8877
661034 feet/sec YDOT = -2705
911083 meter/sec
ZDOT = 19024
637800 ZDOT = 5798
709602
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
56055035
00020000 00000-0 20000-3 0 9097
2 25544 51
6371 215
0342 0009867 25
3862 334
7785 15
75150721 33476
Satellite: ISS
Catalog Number: 25544
Epoch time: 08200
56055035 = yrday
fracday
Element set: 909
Inclination: 51
6371 deg
RA of node: 215
0342 deg
Eccentricity:
0009867
Arg of perigee: 25
3862 deg
Mean anomaly: 334
7785 deg
Mean motion: 15
75150721 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3347
Checksum: 285
Coasting Arc #11 (Orbit 3361)
---------------------------------------
Vector Time (GMT): 2008/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4032377
42 A = 6718355
16 meter
Y = 2222194
67 meter E =
0017621
Z = -4905441
09 I = 51
46145
XDOT = -5407
106132 Wp = 73
18821
YDOT = -5015
886846 meter/sec RA = 209
20750 deg
ZDOT = 2183
998810 TA = 218
03399
MA = 218
15853
Ha = 191
237 n
mi
Hp = 179
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13229584
72 X = -4033097
42
Y = 7290664
94 feet Y = 2177098
98 meter
Z = -16093966
84 Z = -4925031
41
XDOT = -17739
849515 XDOT = -5361
225071
YDOT = -16456
321673 feet/sec YDOT = -5076
095982 meter/sec
ZDOT = 7165
350426 ZDOT = 2157
842371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12445775
47 X = 3793472
36
Y = 8417102
30 feet Y = 2565532
78 meter
Z = -16169308
51 Z = -4928405
23
XDOT = -6016
778608 XDOT = -1833
914120
YDOT = 22394
601754 feet/sec YDOT = 6825
874615 meter/sec
ZDOT = 7063
986423 ZDOT = 2153
103062
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
51219030
00020000 00000-0 20000-3 0 9102
2 25544 51
6372 210
1382 0009831 28
4017 331
7681 15
75148941 33624
Satellite: ISS
Catalog Number: 25544
Epoch time: 08201
51219030 = yrday
fracday
Element set: 910
Inclination: 51
6372 deg
RA of node: 210
1382 deg
Eccentricity:
0009831
Arg of perigee: 28
4017 deg
Mean anomaly: 331
7681 deg
Mean motion: 15
75148941 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3362
Checksum: 258
Coasting Arc #12 (Orbit 3377)
---------------------------------------
Vector Time (GMT): 2008/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4777237
24 A = 6726558
53 meter
Y = 4144331
36 meter E =
0010251
Z = -2306263
95 I = 51
51441
XDOT = -4826
413727 Wp = 67
19565
YDOT = 2558
297318 meter/sec RA = 204
08919 deg
ZDOT = -5415
473215 TA = 138
75989
MA = 138
68241
Ha = 191
330 n
mi
Hp = 179
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15673350
53 X = 4741742
80
Y = 13596887
67 feet Y = 4197554
98 meter
Z = -7566482
78 Z = -2283142
34
XDOT = -15834
690704 XDOT = -4828
355454
YDOT = 8393
363903 feet/sec YDOT = 2504
315356 meter/sec
ZDOT = -17767
300574 ZDOT = -5438
923880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4666859
65 X = 1422458
82
Y = -20250862
09 feet Y = -6172462
76 meter
Z = -7476893
65 Z = -2278957
19
XDOT = 13300
638500 XDOT = 4054
034615
YDOT = 9639
783417 feet/sec YDOT = 2938
205985 meter/sec
ZDOT = -17857
503340 ZDOT = -5442
967018
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
52726204
00020000 00000-0 20000-3 0 9111
2 25544 51
6361 204
9149 0009856 32
8368 327
3406 15
75179460 33782
Satellite: ISS
Catalog Number: 25544
Epoch time: 08202
52726204 = yrday
fracday
Element set: 911
Inclination: 51
6361 deg
RA of node: 204
9149 deg
Eccentricity:
0009856
Arg of perigee: 32
8368 deg
Mean anomaly: 327
3406 deg
Mean motion: 15
75179460 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3378
Checksum: 295
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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