Date:
August 1st 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 2421 88 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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 1761)
---------------------------------------
Vector Time (GMT): 2007/211/12:02:02
980
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4233205
46 A = 6714951
20 meter
Y = -912641
81 meter E =
0007225
Z = 5128276
44 I = 51
33623
XDOT = 3007
213866 Wp = 155
80989
YDOT = 6986
978748 meter/sec RA = 239
18911 deg
ZDOT = -1244
811478 TA = 306
09342
MA = 306
16030
Ha = 188
799 n
mi
Hp = 180
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13888469
35 X = 4218184
51
Y = -2994231
64 feet Y = -865388
28 meter
Z = 16825053
94 Z = 5148804
26
XDOT = 9866
187224 XDOT = 2934
907856
YDOT = 22923
158622 feet/sec YDOT = 7020
202961 meter/sec
ZDOT = -4084
027160 ZDOT = -1230
377638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10776375
57 X = -3284639
27
Y = -9116291
59 feet Y = -2778645
68 meter
Z = 16902674
39 Z = 5151935
15
XDOT = 11492
675286 XDOT = 3502
967427
YDOT = -21019
210940 feet/sec YDOT = -6406
655495 meter/sec
ZDOT = -4028
525577 ZDOT = -1227
894596
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 07211
54692747
00020000 00000-0 20000-3 0 9004
2 25544 51
6311 239
8336 0008912 182
4954 177
6167 15
75980904 17625
Satellite: ISS
Catalog Number: 25544
Epoch time: 07211
54692747 = yrday
fracday
Element set: 900
Inclination: 51
6311 deg
RA of node: 239
8336 deg
Eccentricity:
0008912
Arg of perigee: 182
4954 deg
Mean anomaly: 177
6167 deg
Mean motion: 15
75980904 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1762
Checksum: 311
Coasting Arc #2 (Orbit 1777)
---------------------------------------
Vector Time (GMT): 2007/212/12:02:02
980
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2609944
66 A = 6725320
59 meter
Y = -5950958
04 meter E =
0012148
Z = 1729689
29 I = 51
38693
XDOT = 5164
622860 Wp = 102
81020
YDOT = -604
043752 meter/sec RA = 234
04473 deg
ZDOT = 5678
617626 TA = 276
40973
MA = 276
54806
Ha = 188
779 n
mi
Hp = 180
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8562810
58 X = -2551608
51
Y = -19524140
56 feet Y = -5979817
88 meter
Z = 5674833
62 Z = 1717151
68
XDOT = 16944
300723 XDOT = 5143
408484
YDOT = -1981
770840 feet/sec YDOT = -546
409114 meter/sec
ZDOT = 18630
635257 ZDOT = 5703
655191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9926748
67 X = -3025673
00
Y = 18881692
00 feet Y = 5755139
72 meter
Z = 5626623
70 Z = 1714994
91
XDOT = -10658
781348 XDOT = -3248
796555
YDOT = -11219
354431 feet/sec YDOT = -3419
659231 meter/sec
ZDOT = 18725
375490 ZDOT = 5707
494449
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 07212
56148752
00020000 00000-0 20000-3 0 9010
2 25544 51
6311 234
6068 0008757 186
1953 173
9104 15
75963651 17784
Satellite: ISS
Catalog Number: 25544
Epoch time: 07212
56148752 = yrday
fracday
Element set: 901
Inclination: 51
6311 deg
RA of node: 234
6068 deg
Eccentricity:
0008757
Arg of perigee: 186
1953 deg
Mean anomaly: 173
9104 deg
Mean motion: 15
75963651 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1778
Checksum: 306
Coasting Arc #3 (Orbit 1792)
---------------------------------------
Vector Time (GMT): 2007/213/12:02:02
980
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4817488
99 A = 6716912
60 meter
Y = 182760
09 meter E =
0015223
Z = -4690164
18 I = 51
37746
XDOT = -2892
872416 Wp = 143
90283
YDOT = -6594
458866 meter/sec RA = 228
83772 deg
ZDOT = 2706
781467 TA = 152
90332
MA = 152
82378
Ha = 188
595 n
mi
Hp = 180
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15805410
06 X = -4796391
09
Y = 599606
58 feet Y = 129006
44 meter
Z = -15387677
74 Z = -4713515
81
XDOT = -9491
051232 XDOT = -2832
065986
YDOT = -21635
363733 feet/sec YDOT = -6626
468761 meter/sec
ZDOT = 8880
516623 ZDOT = 2692
875501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10459949
13 X = 3188192
50
Y = 11748669
88 feet Y = 3580994
58 meter
Z = -15476090
01 Z = -4717112
23
XDOT = -9771
196629 XDOT = -2978
260732
YDOT = 20359
827382 feet/sec YDOT = 6205
675386 meter/sec
ZDOT = 8827
032454 ZDOT = 2690
479492
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 07213
51262995
00020000 00000-0 20000-3 0 9023
2 25544 51
6318 229
7066 0008771 190
7465 169
3513 15
75966632 17931
Satellite: ISS
Catalog Number: 25544
Epoch time: 07213
51262995 = yrday
fracday
Element set: 902
Inclination: 51
6318 deg
RA of node: 229
7066 deg
Eccentricity:
0008771
Arg of perigee: 190
7465 deg
Mean anomaly: 169
3513 deg
Mean motion: 15
75966632 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1793
Checksum: 316
Coasting Arc #4 (Orbit 1808)
---------------------------------------
Vector Time (GMT): 2007/214/12:02:02
980
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2381231
55 A = 6722754
44 meter
Y = 5541611
58 meter E =
0010455
Z = -2957901
16 I = 51
41623
XDOT = -5879
326732 Wp = 169
00508
YDOT = -124
649758 meter/sec RA = 223
71406 deg
ZDOT = -4979
620314 TA = 45
27727
MA = 45
19219
Ha = 188
484 n
mi
Hp = 180
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7812439
48 X = 2333456
19
Y = 18181140
36 feet Y = 5567972
85 meter
Z = -9704400
14 Z = -2946449
13
XDOT = -19289
129698 XDOT = -5853
306187
YDOT = -408
955899 feet/sec YDOT = -190
250010 meter/sec
ZDOT = -16337
336987 ZDOT = -5008
118455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8722317
16 X = 2658562
27
Y = -17786585
57 feet Y = -5421351
28 meter
Z = -9660332
03 Z = -2944469
20
XDOT = 10854
398175 XDOT = 3308
420564
YDOT = 14231
443264 feet/sec YDOT = 4337
743907 meter/sec
ZDOT = -16445
282799 ZDOT = -5012
522197
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 07214
52717676
00020000 00000-0 20000-3 0 9037
2 25544 51
6309 224
4793 0008800 194
3248 165
7668 15
75983456 18094
Satellite: ISS
Catalog Number: 25544
Epoch time: 07214
52717676 = yrday
fracday
Element set: 903
Inclination: 51
6309 deg
RA of node: 224
4793 deg
Eccentricity:
0008800
Arg of perigee: 194
3248 deg
Mean anomaly: 165
7668 deg
Mean motion: 15
75983456 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1809
Checksum: 323
Coasting Arc #5 (Orbit 1824)
---------------------------------------
Vector Time (GMT): 2007/215/12:02:02
980
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5437384
88 A = 6719587
41 meter
Y = 327156
94 meter E =
0010106
Z = 3922971
47 I = 51
42757
XDOT = 2523
064855 Wp = 127
32427
YDOT = 6086
372650 meter/sec RA = 218
49694 deg
ZDOT = -4003
636981 TA = 4
30261
MA = 4
29393
Ha = 188
095 n
mi
Hp = 180
850
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17839189
23 X = 5414265
53
Y = 1073349
55 feet Y = 387831
42 meter
Z = 12870641
29 Z = 3949329
89
XDOT = 8277
771833 XDOT = 2474
267379
YDOT = 19968
414207 feet/sec YDOT = 6114
314299 meter/sec
ZDOT = -13135
291932 ZDOT = -3991
498336
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10960266
41 X = -3340689
20
Y = -14024282
50 feet Y = -4274601
31 meter
Z = 12970513
47 Z = 3953412
51
XDOT = 8410
856833 XDOT = 2563
629163
YDOT = -18681
357145 feet/sec YDOT = -5694
077658 meter/sec
ZDOT = -13088
549119 ZDOT = -3989
389771
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 07215
54171647
00020000 00000-0 20000-3 0 9043
2 25544 51
6305 219
2525 0008641 198
6564 161
4284 15
76027726 18251
Satellite: ISS
Catalog Number: 25544
Epoch time: 07215
54171647 = yrday
fracday
Element set: 904
Inclination: 51
6305 deg
RA of node: 219
2525 deg
Eccentricity:
0008641
Arg of perigee: 198
6564 deg
Mean anomaly: 161
4284 deg
Mean motion: 15
76027726 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1825
Checksum: 296
Coasting Arc #6 (Orbit 1840)
---------------------------------------
Vector Time (GMT): 2007/216/12:02:02
980
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1940678
13 A = 6719614
77 meter
Y = -5065080
89 meter E =
0012552
Z = 3967531
54 I = 51
45034
XDOT = 6589
013946 Wp = 143
82426
YDOT = 577
839340 meter/sec RA = 213
38350 deg
ZDOT = 3944
321789 TA = 265
19190
MA = 265
33524
Ha = 188
090 n
mi
Hp = 181
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6367054
24 X = -1903168
87
Y = -16617719
47 feet Y = -5086573
13 meter
Z = 13016835
75 Z = 3958194
61
XDOT = 21617
499824 XDOT = 6562
902040
YDOT = 1895
798358 feet/sec YDOT = 651
375199 meter/sec
ZDOT = 12940
688285 ZDOT = 3976
267676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7914792
00 X = -2412428
60
Y = 15968096
15 feet Y = 4867075
71 meter
Z = 12980830
72 Z = 3956557
20
XDOT = -11978
520560 XDOT = -3651
053067
YDOT = -16599
150412 feet/sec YDOT = -5059
421046 meter/sec
ZDOT = 13061
760791 ZDOT = 3981
224689
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 07216
55625072
00020000 00000-0 20000-3 0 9052
2 25544 51
6301 214
0258 0008653 203
0355 157
0422 15
76022629 18415
Satellite: ISS
Catalog Number: 25544
Epoch time: 07216
55625072 = yrday
fracday
Element set: 905
Inclination: 51
6301 deg
RA of node: 214
0258 deg
Eccentricity:
0008653
Arg of perigee: 203
0355 deg
Mean anomaly: 157
0422 deg
Mean motion: 15
76022629 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1841
Checksum: 259
Coasting Arc #7 (Orbit 1855)
---------------------------------------
Vector Time (GMT): 2007/217/12:02:02
980
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6040949
83 A = 6722717
10 meter
Y = -625307
26 meter E =
0005855
Z = -2890844
17 I = 51
48582
XDOT = -1838
038321 Wp = 176
01793
YDOT = -5526
318636 meter/sec RA = 208
17023 deg
ZDOT = 5031
156119 TA = 150
66395
MA = 150
63107
Ha = 187
915 n
mi
Hp = 181
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19819389
21 X = -6019465
41
Y = -2051533
02 feet Y = -692740
22 meter
Z = -9484396
87 Z = -2920138
90
XDOT = -6030
309453 XDOT = -1800
545993
YDOT = -18130
966652 feet/sec YDOT = -5546
663371 meter/sec
ZDOT = 16506
417713 ZDOT = 5022
317593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12100399
80 X = 3688201
86
Y = 15763203
45 feet Y = 4804624
41 meter
Z = -9595441
74 Z = -2924690
64
XDOT = -7806
374904 XDOT = -2379
383071
YDOT = 16029
647610 feet/sec YDOT = 4885
836592 meter/sec
ZDOT = 16472
240982 ZDOT = 5020
739051
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 07217
50737058
00020000 00000-0 20000-3 0 9067
2 25544 51
6300 209
1260 0008521 206
0868 153
9868 15
76016406 18569
Satellite: ISS
Catalog Number: 25544
Epoch time: 07217
50737058 = yrday
fracday
Element set: 906
Inclination: 51
6300 deg
RA of node: 209
1260 deg
Eccentricity:
0008521
Arg of perigee: 206
0868 deg
Mean anomaly: 153
9868 deg
Mean motion: 15
76016406 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1856
Checksum: 288
Coasting Arc #8 (Orbit 1871)
---------------------------------------
Vector Time (GMT): 2007/218/12:02:02
980
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1202721
17 A = 6716663
14 meter
Y = 4609670
99 meter E =
0007468
Z = -4738756
27 I = 51
49063
XDOT = -7198
368292 Wp = 120
11910
YDOT = -802
475020 meter/sec RA = 203
05201 deg
ZDOT = -2614
346157 TA = 124
20254
MA = 124
13174
Ha = 187
736 n
mi
Hp = 181
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3945935
60 X = 1174105
72
Y = 15123592
49 feet Y = 4622960
99 meter
Z = -15547100
63 Z = -4732982
49
XDOT = -23616
693870 XDOT = -7176
159914
YDOT = -2632
792059 feet/sec YDOT = -882
846781 meter/sec
ZDOT = -8577
251172 ZDOT = -2649
261879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7978413
48 X = 2431820
43
Y = -13466106
00 feet Y = -4104469
11 meter
Z = -15524648
24 Z = -4731912
78
XDOT = 13634
058545 XDOT = 4155
661044
YDOT = 18093
413596 feet/sec YDOT = 5514
872464 meter/sec
ZDOT = -8709
622700 ZDOT = -2654
692999
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 07218
52189205
00020000 00000-0 20000-3 0 9076
2 25544 51
6294 203
8983 0008520 210
4266 149
6405 15
76023861 18724
Satellite: ISS
Catalog Number: 25544
Epoch time: 07218
52189205 = yrday
fracday
Element set: 907
Inclination: 51
6294 deg
RA of node: 203
8983 deg
Eccentricity:
0008520
Arg of perigee: 210
4266 deg
Mean anomaly: 149
6405 deg
Mean motion: 15
76023861 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1872
Checksum: 292
Coasting Arc #9 (Orbit 1887)
---------------------------------------
Vector Time (GMT): 2007/219/12:02:02
980
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6472581
18 A = 6725102
27 meter
Y = 718864
86 meter E =
0015200
Z = 1637606
62 I = 51
54657
XDOT = 890
675944 Wp = 149
40902
YDOT = 5073
380770 meter/sec RA = 197
85615 deg
ZDOT = -5737
098445 TA = 12
44682
MA = 12
40932
Ha = 187
380 n
mi
Hp = 181
738
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21235502
56 X = 6456106
52
Y = 2358480
52 feet Y = 791152
59 meter
Z = 5372725
12 Z = 1669010
30
XDOT = 2922
165169 XDOT = 861
748069
YDOT = 16644
950032 feet/sec YDOT = 5083
179788 meter/sec
ZDOT = -18822
501459 ZDOT = -5732
841193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13444798
03 X = -4097974
44
Y = -16566615
89 feet Y = -5049504
52 meter
Z = 5491795
57 Z = 1673899
29
XDOT = 8321
574324 XDOT = 2536
415854
YDOT = -12998
517704 feet/sec YDOT = -3961
948196 meter/sec
ZDOT = -18805
735306 ZDOT = -5731
988121
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 07219
53640591
00020000 00000-0 20000-3 0 9089
2 25544 51
6292 198
6716 0008406 215
5679 144
4926 15
76061359 18886
Satellite: ISS
Catalog Number: 25544
Epoch time: 07219
53640591 = yrday
fracday
Element set: 908
Inclination: 51
6292 deg
RA of node: 198
6716 deg
Eccentricity:
0008406
Arg of perigee: 215
5679 deg
Mean anomaly: 144
4926 deg
Mean motion: 15
76061359 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1888
Checksum: 327
Coasting Arc #10 (Orbit 1903)
---------------------------------------
Vector Time (GMT): 2007/220/12:02:02
980
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -302996
44 A = 6714700
75 meter
Y = -4278243
72 meter E =
0008983
Z = 5169717
06 I = 51
53887
XDOT = 7578
723753 Wp = 194
19785
YDOT = 810
161353 meter/sec RA = 192
72344 deg
ZDOT = 1106
481642 TA = 245
18327
MA = 245
27673
Ha = 187
321 n
mi
Hp = 181
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -994082
81 X = -280247
23
Y = -14036232
68 feet Y = -4281505
50 meter
Z = 16961013
99 Z = 5168299
80
XDOT = 24864
579241 XDOT = 7563
726116
YDOT = 2658
009687 feet/sec YDOT = 894
826901 meter/sec
ZDOT = 3630
189113 ZDOT = 1143
262355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8892165
21 X = -2710331
96
Y = 10914841
69 feet Y = 3326843
75 meter
Z = 16955106
98 Z = 5167916
61
XDOT = -15360
087875 XDOT = -4681
754784
YDOT = -18411
047259 feet/sec YDOT = -5611
687204 meter/sec
ZDOT = 3769
661977 ZDOT = 1148
992970
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 07220
55091387
00020000 00000-0 20000-3 0 9097
2 25544 51
6290 193
4449 0008451 219
7855 140
2690 15
76053034 19044
Satellite: ISS
Catalog Number: 25544
Epoch time: 07220
55091387 = yrday
fracday
Element set: 909
Inclination: 51
6290 deg
RA of node: 193
4449 deg
Eccentricity:
0008451
Arg of perigee: 219
7855 deg
Mean anomaly: 140
2690 deg
Mean motion: 15
76053034 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1904
Checksum: 293
Coasting Arc #11 (Orbit 1918)
---------------------------------------
Vector Time (GMT): 2007/221/12:02:02
980
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6685573
59 A = 6726195
78 meter
Y = -674168
33 meter E =
0003171
Z = -265824
98 I = 51
60641
XDOT = 244
695319 Wp = 43
89956
YDOT = -4785
365251 meter/sec RA = 187
55460 deg
ZDOT = 6027
195363 TA = 313
20948
MA = 313
23596
Ha = 187
132 n
mi
Hp = 182
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21934296
55 X = -6676246
75
Y = -2211838
34 feet Y = -748877
99 meter
Z = -872129
20 Z = -298280
38
XDOT = 802
806165 XDOT = 268
909269
YDOT = -15700
017229 feet/sec YDOT = -4782
494330 meter/sec
ZDOT = 19774
263002 ZDOT = 6028
442263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14638757
00 X = 4461893
13
Y = 16476727
46 feet Y = 5022106
53 meter
Z = -995212
94 Z = -303340
90
XDOT = -9938
826226 XDOT = -3029
354234
YDOT = 10016
975026 feet/sec YDOT = 3053
173988 meter/sec
ZDOT = 19778
386477 ZDOT = 6028
452198
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 07221
50200799
00020000 00000-0 20000-3 0 9104
2 25544 51
6288 188
5445 0008466 222
3718 137
6793 15
76087283 19199
Satellite: ISS
Catalog Number: 25544
Epoch time: 07221
50200799 = yrday
fracday
Element set: 910
Inclination: 51
6288 deg
RA of node: 188
5445 deg
Eccentricity:
0008466
Arg of perigee: 222
3718 deg
Mean anomaly: 137
6793 deg
Mean motion: 15
76087283 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1919
Checksum: 315
Coasting Arc #12 (Orbit 1934)
---------------------------------------
Vector Time (GMT): 2007/222/12:02:02
980
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -748575
02 A = 6714287
29 meter
Y = 4131784
16 meter E =
0010942
Z = -5247158
75 I = 51
59568
XDOT = -7646
283946 Wp = 127
61184
YDOT = -726
950816 meter/sec RA = 182
39843 deg
ZDOT = 512
582225 TA = 147
29646
MA = 147
22867
Ha = 186
889 n
mi
Hp = 182
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2455954
78 X = -769232
41
Y = 13555722
32 feet Y = 4123298
27 meter
Z = -17215087
77 Z = -5250844
96
XDOT = -25086
233420 XDOT = -7640
076768
YDOT = -2385
009239 feet/sec YDOT = -812
421220 meter/sec
ZDOT = 1681
700214 ZDOT = 475
452377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10769616
86 X = 3282579
22
Y = -8563961
49 feet Y = -2610295
46 meter
Z = -17228536
93 Z = -5251258
06
XDOT = 16546
854696 XDOT = 5043
481311
YDOT = 17670
180736 feet/sec YDOT = 5385
871088 meter/sec
ZDOT = 1540
875062 ZDOT = 469
658719
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 07222
51650188
00020000 00000-0 20000-3 0 9118
2 25544 51
6297 183
3169 0008400 227
6682 132
3771 15
76068428 19357
Satellite: ISS
Catalog Number: 25544
Epoch time: 07222
51650188 = yrday
fracday
Element set: 911
Inclination: 51
6297 deg
RA of node: 183
3169 deg
Eccentricity:
0008400
Arg of perigee: 227
6682 deg
Mean anomaly: 132
3771 deg
Mean motion: 15
76068428 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1935
Checksum: 297
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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