Date:
March 11th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 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
077/02:55:34
987 -0
4 0
8 0
8
N/A -0
3 -0
0 185
9
000/00:05:09
975 0
7 -0
1 180
8
080/02:40:34
908 0
0 0
6 0
6
N/A -0
5 -0
0 186
4
000/00:05:09
817 0
3 -0
1 180
4
Coasting Arc #1 (Orbit 1294)
---------------------------------------
Vector Time (GMT): 2008/070/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4596839
70 A = 6721751
87 meter
Y = 3817031
67 meter E =
0002808
Z = -3081854
01 I = 51
73235
XDOT = -5373
866425 Wp = 94
96324
YDOT = -2511
677784 meter/sec RA = 164
30377 deg
ZDOT = 4908
303342 TA = 229
31408
MA = 229
33849
Ha = 186
228 n
mi
Hp = 180
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15081495
07 X = -4624209
61
Y = 12523069
78 feet Y = 3765473
89 meter
Z = -10111069
58 Z = -3104252
23
XDOT = -17630
795357 XDOT = -5369
224683
YDOT = -8240
412677 feet/sec YDOT = -2571
745060 meter/sec
ZDOT = 16103
357421 ZDOT = 4882
208618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19090859
27 X = -5818893
90
Y = 4252600
88 feet Y = 1296192
75 meter
Z = -10196419
80 Z = -3107868
75
XDOT = -11670
546401 XDOT = -3557
182543
YDOT = -14049
161739 feet/sec YDOT = -4282
184498 meter/sec
ZDOT = 16003
064003 ZDOT = 4877
733908
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 08070
46470412
00020000 00000-0 20000-3 0 9002
2 25544 51
6387 165
2886 0002066 230
7942 129
3039 15
76185394 12952
Satellite: ISS
Catalog Number: 25544
Epoch time: 08070
46470412 = yrday
fracday
Element set: 900
Inclination: 51
6387 deg
RA of node: 165
2886 deg
Eccentricity:
0002066
Arg of perigee: 230
7942 deg
Mean anomaly: 129
3039 deg
Mean motion: 15
76185394 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1295
Checksum: 296
Coasting Arc #2 (Orbit 1310)
---------------------------------------
Vector Time (GMT): 2008/071/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4201559
77 A = 6716333
31 meter
Y = 2358385
27 meter E =
0008973
Z = -4687552
28 I = 51
74195
XDOT = -5611
159007 Wp = 75
01166
YDOT = 4475
715308 meter/sec RA = 159
20455 deg
ZDOT = -2779
728602 TA = 167
61736
MA = 167
59530
Ha = 186
143 n
mi
Hp = 181
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13784644
90 X = 4197646
97
Y = 7737484
49 feet Y = 2405347
37 meter
Z = -15379108
53 Z = -4667150
72
XDOT = -18409
314329 XDOT = -5647
286683
YDOT = 14684
105340 feet/sec YDOT = 4412
765967 meter/sec
ZDOT = -9119
844495 ZDOT = -2807
075642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9014518
30 X = 2747625
18
Y = 13077874
49 feet Y = 3986136
14 meter
Z = -15300645
06 Z = -4663636
62
XDOT = -22006
808846 XDOT = -6707
675336
YDOT = 4385
539622 feet/sec YDOT = 1336
712477 meter/sec
ZDOT = -9224
088158 ZDOT = -2811
502071
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 08071
47909596
00020000 00000-0 20000-3 0 9015
2 25544 51
6386 160
0619 0002086 233
0607 127
0367 15
76242056 13111
Satellite: ISS
Catalog Number: 25544
Epoch time: 08071
47909596 = yrday
fracday
Element set: 901
Inclination: 51
6386 deg
RA of node: 160
0619 deg
Eccentricity:
0002086
Arg of perigee: 233
0607 deg
Mean anomaly: 127
0367 deg
Mean motion: 15
76242056 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1311
Checksum: 278
Coasting Arc #3 (Orbit 1326)
---------------------------------------
Vector Time (GMT): 2008/072/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5123793
12 A = 6724356
83 meter
Y = -3993288
52 meter E =
0013287
Z = 1709778
29 I = 51
79580
XDOT = 4224
296453 Wp = 122
58215
YDOT = 2956
856225 meter/sec RA = 154
02385 deg
ZDOT = -5728
255723 TA = 38
51837
MA = 38
42363
Ha = 186
055 n
mi
Hp = 180
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16810344
88 X = 5159760
08
Y = -13101340
28 feet Y = -3935790
19 meter
Z = 5609508
83 Z = 1734757
15
XDOT = 13859
240333 XDOT = 4218
745299
YDOT = 9700
971868 feet/sec YDOT = 3004
063522 meter/sec
ZDOT = -18793
489904 ZDOT = -5707
747660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20766550
48 X = 6329644
59
Y = -4680341
73 feet Y = -1426568
16 meter
Z = 5704750
99 Z = 1738808
10
XDOT = 8143
207381 XDOT = 2482
049610
YDOT = 13222
089724 feet/sec YDOT = 4030
092948 meter/sec
ZDOT = -18714
541677 ZDOT = -5704
192303
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 08072
49345744
00020000 00000-0 20000-3 0 9028
2 25544 51
6379 154
8353 0001899 235
2930 124
8056 15
76289555 13275
Satellite: ISS
Catalog Number: 25544
Epoch time: 08072
49345744 = yrday
fracday
Element set: 902
Inclination: 51
6379 deg
RA of node: 154
8353 deg
Eccentricity:
0001899
Arg of perigee: 235
2930 deg
Mean anomaly: 124
8056 deg
Mean motion: 15
76289555 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1327
Checksum: 315
Coasting Arc #4 (Orbit 1342)
---------------------------------------
Vector Time (GMT): 2008/073/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3147918
77 A = 6713734
34 meter
Y = -2871126
47 meter E =
0003347
Z = 5187803
36 I = 51
78689
XDOT = 6046
589649 Wp = 153
90566
YDOT = -4650
588729 meter/sec RA = 148
90637 deg
ZDOT = 1091
999518 TA = 285
68538
MA = 285
72230
Ha = 185
952 n
mi
Hp = 180
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10327817
50 X = -3140780
75
Y = -9419706
27 feet Y = -2906288
35 meter
Z = 17020352
24 Z = 5172528
18
XDOT = 19837
892550 XDOT = 6092
839141
YDOT = -15257
837037 feet/sec YDOT = -4582
713713 meter/sec
ZDOT = 3582
675583 ZDOT = 1121
486104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5624760
53 X = -1714427
01
Y = -12874698
35 feet Y = -3924208
06 meter
Z = 16961464
62 Z = 5169854
42
XDOT = 23401
284250 XDOT = 7132
711439
YDOT = -5341
670522 feet/sec YDOT = -1628
141175 meter/sec
ZDOT = 3695
130971 ZDOT = 1126
275920
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 08073
50778597
00020000 00000-0 20000-3 0 9038
2 25544 51
6384 149
6074 0001897 244
4094 115
6875 15
76383291 13431
Satellite: ISS
Catalog Number: 25544
Epoch time: 08073
50778597 = yrday
fracday
Element set: 903
Inclination: 51
6384 deg
RA of node: 149
6074 deg
Eccentricity:
0001897
Arg of perigee: 244
4094 deg
Mean anomaly: 115
6875 deg
Mean motion: 15
76383291 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1343
Checksum: 321
Coasting Arc #5 (Orbit 1357)
---------------------------------------
Vector Time (GMT): 2008/074/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5344702
44 A = 6725422
23 meter
Y = 4070552
95 meter E =
0010462
Z = -156428
62 I = 51
85048
XDOT = -2992
388411 Wp = 39
16770
YDOT = -3705
010457 meter/sec RA = 143
75489 deg
ZDOT = 6056
416000 TA = 319
13608
MA = 319
21447
Ha = 185
860 n
mi
Hp = 180
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17535113
00 X = -5389062
87
Y = 13354832
51 feet Y = 4010537
40 meter
Z = -513217
26 Z = -182500
69
XDOT = -9817
547280 XDOT = -2980
156719
YDOT = -12155
546118 feet/sec YDOT = -3738
404683 meter/sec
ZDOT = 19870
131232 ZDOT = 6041
908804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21385720
33 X = -6518367
56
Y = 5326418
24 feet Y = 1623492
28 meter
Z = -612670
96 Z = -186742
11
XDOT = -3920
540458 XDOT = -1194
980732
YDOT = -13533
530584 feet/sec YDOT = -4125
020122 meter/sec
ZDOT = 19814
083431 ZDOT = 6039
332630
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 08074
45869396
00020000 00000-0 20000-3 0 9042
2 25544 51
6383 144
7072 0001715 254
4714 105
6261 15
76370071 13589
Satellite: ISS
Catalog Number: 25544
Epoch time: 08074
45869396 = yrday
fracday
Element set: 904
Inclination: 51
6383 deg
RA of node: 144
7072 deg
Eccentricity:
0001715
Arg of perigee: 254
4714 deg
Mean anomaly: 105
6261 deg
Mean motion: 15
76370071 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1358
Checksum: 293
Coasting Arc #6 (Orbit 1373)
---------------------------------------
Vector Time (GMT): 2008/075/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2082620
82 A = 6713351
36 meter
Y = 3656613
57 meter E =
0013129
Z = -5242076
12 I = 51
83253
XDOT = -6126
383132 Wp = 98
13299
YDOT = 4592
799916 meter/sec RA = 138
61088 deg
ZDOT = 769
577401 TA = 179
17589
MA = 179
17372
Ha = 185
743 n
mi
Hp = 180
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6832745
48 X = 2067041
91
Y = 11996763
68 feet Y = 3679815
51 meter
Z = -17198412
45 Z = -5231996
74
XDOT = -20099
682193 XDOT = -6181
023623
YDOT = 15068
241193 feet/sec YDOT = 4523
985694 meter/sec
ZDOT = 2524
860239 ZDOT = 739
683133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1853243
19 X = 564868
52
Y = 13730138
13 feet Y = 4184946
10 meter
Z = -17159339
65 Z = -5230166
72
XDOT = -23328
835867 XDOT = -7110
629172
YDOT = 6162
523628 feet/sec YDOT = 1878
337202 meter/sec
ZDOT = 2410
801752 ZDOT = 734
812374
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 08075
47296543
00020000 00000-0 20000-3 0 9054
2 25544 51
6377 139
4799 0001742 259
3776 100
7192 15
76434364 13744
Satellite: ISS
Catalog Number: 25544
Epoch time: 08075
47296543 = yrday
fracday
Element set: 905
Inclination: 51
6377 deg
RA of node: 139
4799 deg
Eccentricity:
0001742
Arg of perigee: 259
3776 deg
Mean anomaly: 100
7192 deg
Mean motion: 15
76434364 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1374
Checksum: 320
Coasting Arc #7 (Orbit 1389)
---------------------------------------
Vector Time (GMT): 2008/076/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5288820
74 A = 6724173
72 meter
Y = -3865562
97 meter E =
0007774
Z = -1499650
18 I = 51
89017
XDOT = 1807
037706 Wp = 153
39925
YDOT = 4720
610999 meter/sec RA = 133
49294 deg
ZDOT = -5813
483749 TA = 43
07637
MA = 43
01556
Ha = 185
746 n
mi
Hp = 180
555
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17351774
10 X = 5338937
89
Y = -12682293
22 feet Y = -3806140
17 meter
Z = -4920112
14 Z = -1473835
76
XDOT = 5928
601399 XDOT = 1782
357129
YDOT = 15487
568893 feet/sec YDOT = 4740
680214 meter/sec
ZDOT = -19073
109414 ZDOT = -5804
765366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20803046
97 X = 6340768
72
Y = -5487947
69 feet Y = -1672726
46 meter
Z = -4821596
83 Z = -1469622
71
XDOT = -413
635874 XDOT = -126
076214
YDOT = 15105
537247 feet/sec YDOT = 4604
167753 meter/sec
ZDOT = -19039
124872 ZDOT = -5803
125261
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 08076
48720736
00020000 00000-0 20000-3 0 9063
2 25544 51
6373 134
2521 0001595 262
7342 97
3641 15
76484485 13906
Satellite: ISS
Catalog Number: 25544
Epoch time: 08076
48720736 = yrday
fracday
Element set: 906
Inclination: 51
6373 deg
RA of node: 134
2521 deg
Eccentricity:
0001595
Arg of perigee: 262
7342 deg
Mean anomaly: 97
3641 deg
Mean motion: 15
76484485 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1390
Checksum: 301
Coasting Arc #8 (Orbit 1400)
---------------------------------------
Vector Time (GMT): 2008/077/02:58:09
975
Vector Time (MET): N/A
Weight (LBS) : 567143
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5006354
98 A = 6724656
05 meter
Y = 4258193
06 meter E =
0013101
Z = 1390078
01 I = 51
90119
XDOT = -2201
702014 Wp = 53
63503
YDOT = -4508
210828 meter/sec RA = 130
07128 deg
ZDOT = 5850
212231 TA = 321
61002
MA = 321
70318
Ha = 185
936 n
mi
Hp = 180
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16425049
13 X = -5060351
28
Y = 13970449
67 feet Y = 4201907
28 meter
Z = 4560623
39 Z = 1365626
32
XDOT = -7223
431804 XDOT = -2179
545568
YDOT = -14790
717941 feet/sec YDOT = -4532
707423 meter/sec
ZDOT = 19193
609682 ZDOT = 5839
570559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4045883
81 X = 1233185
39
Y = -21199726
07 feet Y = -6461676
51 meter
Z = 4467373
67 Z = 1361655
49
XDOT = 13443
130290 XDOT = 4097
466112
YDOT = 6622
851561 feet/sec YDOT = 2018
645156 meter/sec
ZDOT = 19152
273564 ZDOT = 5837
612982
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 08077
18448600
00020000 00000-0 20000-3 0 9079
2 25544 51
6349 130
6555 0001833 296
9875 63
1102 15
76365468 14016
Satellite: ISS
Catalog Number: 25544
Epoch time: 08077
18448600 = yrday
fracday
Element set: 907
Inclination: 51
6349 deg
RA of node: 130
6555 deg
Eccentricity:
0001833
Arg of perigee: 296
9875 deg
Mean anomaly: 63
1102 deg
Mean motion: 15
76365468 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1401
Checksum: 297
Coasting Arc #9 (Orbit 1415)
---------------------------------------
Vector Time (GMT): 2008/078/02:58:09
975
Vector Time (MET): N/A
Weight (LBS) : 567143
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1535903
52 A = 6715203
89 meter
Y = 4417795
88 meter E =
0010336
Z = -4828072
35 I = 51
88738
XDOT = -5610
892678 Wp = 105
59419
YDOT = 4651
697915 meter/sec RA = 124
90233 deg
ZDOT = 2473
114474 TA = 188
50136
MA = 188
51889
Ha = 185
916 n
mi
Hp = 180
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5039053
53 X = 1509842
31
Y = 14494080
98 feet Y = 4434825
22 meter
Z = -15840132
37 Z = -4820674
66
XDOT = -18408
440544 XDOT = -5674
505374
YDOT = 15261
476098 feet/sec YDOT = 4588
598186 meter/sec
ZDOT = 8113
892631 ZDOT = 2445
702513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13223986
89 X = -4030671
21
Y = -7842896
11 feet Y = -2390514
74 meter
Z = -15811242
48 Z = -4819266
71
XDOT = 3819
930249 XDOT = 1164
314740
YDOT = -22576
738856 feet/sec YDOT = -6881
390003 meter/sec
ZDOT = 8009
331977 ZDOT = 2441
244386
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 08078
13538502
00020000 00000-0 20000-3 0 9087
2 25544 51
6346 125
7537 0001670 301
3260 58
7741 15
76413130 14161
Satellite: ISS
Catalog Number: 25544
Epoch time: 08078
13538502 = yrday
fracday
Element set: 908
Inclination: 51
6346 deg
RA of node: 125
7537 deg
Eccentricity:
0001670
Arg of perigee: 301
3260 deg
Mean anomaly: 58
7741 deg
Mean motion: 15
76413130 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1416
Checksum: 270
Coasting Arc #10 (Orbit 1431)
---------------------------------------
Vector Time (GMT): 2008/079/02:58:09
975
Vector Time (MET): N/A
Weight (LBS) : 567143
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4764822
28 A = 6721560
23 meter
Y = -3756158
58 meter E =
0002997
Z = -2893804
47 I = 51
92502
XDOT = 1357
758037 Wp = 108
17523
YDOT = 5628
909437 meter/sec RA = 119
81061 deg
ZDOT = -5075
874245 TA = 104
97679
MA = 104
94361
Ha = 185
902 n
mi
Hp = 180
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15632619
02 X = 4820527
42
Y = -12323354
93 feet Y = -3702564
40 meter
Z = -9494109
16 Z = -2870521
76
XDOT = 4454
586737 XDOT = 1319
371025
YDOT = 18467
550647 feet/sec YDOT = 5643
877597 meter/sec
ZDOT = -16653
130725 ZDOT = -5069
372097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3812704
29 X = -1162112
27
Y = 19580247
98 feet Y = 5968059
59 meter
Z = -9405271
81 Z = -2866726
85
XDOT = -14088
162469 XDOT = -4294
071921
YDOT = -10721
984640 feet/sec YDOT = -3268
060918 meter/sec
ZDOT = -16627
529839 ZDOT = -5068
071095
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 08079
14964761
00020000 00000-0 20000-3 0 9090
2 25544 51
6347 120
5261 0001701 310
8657 49
2360 15
76474540 14321
Satellite: ISS
Catalog Number: 25544
Epoch time: 08079
14964761 = yrday
fracday
Element set: 909
Inclination: 51
6347 deg
RA of node: 120
5261 deg
Eccentricity:
0001701
Arg of perigee: 310
8657 deg
Mean anomaly: 49
2360 deg
Mean motion: 15
76474540 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1432
Checksum: 283
Coasting Arc #11 (Orbit 1447)
---------------------------------------
Vector Time (GMT): 2008/080/02:43:09
817
Vector Time (MET): N/A
Weight (LBS) : 567060
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4416365
07 A = 6714405
10 meter
Y = 121903
90 meter E =
0003940
Z = 5053502
91 I = 51
91240
XDOT = 1824
773626 Wp = 115
52982
YDOT = -7276
374318 meter/sec RA = 114
71984 deg
ZDOT = 1767
510776 TA = 317
51441
MA = 317
54490
Ha = 186
380 n
mi
Hp = 180
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14489386
70 X = -4441948
65
Y = 399947
19 feet Y = 72375
05 meter
Z = 16579733
95 Z = 5031986
36
XDOT = 5986
790112 XDOT = 1897
417424
YDOT = -23872
619152 feet/sec YDOT = -7255
562305 meter/sec
ZDOT = 5798
919870 ZDOT = 1776
552588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11237088
15 X = 3425064
47
Y = -9303704
05 feet Y = -2835768
99 meter
Z = 16497236
23 Z = 5028357
60
XDOT = 9347
842457 XDOT = 2849
222381
YDOT = 21648
867852 feet/sec YDOT = 6598
574921 meter/sec
ZDOT = 5832
733019 ZDOT = 1777
817024
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 08080
16388571
00020000 00000-0 20000-3 0 9105
2 25544 51
6340 115
2971 0001640 329
7779 30
3290 15
76367860 14485
Satellite: ISS
Catalog Number: 25544
Epoch time: 08080
16388571 = yrday
fracday
Element set: 910
Inclination: 51
6340 deg
RA of node: 115
2971 deg
Eccentricity:
0001640
Arg of perigee: 329
7779 deg
Mean anomaly: 30
3290 deg
Mean motion: 15
76367860 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1448
Checksum: 292
Coasting Arc #12 (Orbit 1462)
---------------------------------------
Vector Time (GMT): 2008/081/02:43:09
817
Vector Time (MET): N/A
Weight (LBS) : 567060
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1676912
28 A = 6724978
16 meter
Y = 6463680
26 meter E =
0011159
Z = -746858
97 I = 51
96018
XDOT = -4791
923857 Wp = 32
75922
YDOT = -554
783244 meter/sec RA = 109
56419 deg
ZDOT = 6008
453674 TA = 319
12756
MA = 319
21118
Ha = 186
167 n
mi
Hp = 180
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5501680
72 X = -1745437
45
Y = 21206300
08 feet Y = 6444544
85 meter
Z = -2450324
71 Z = -755172
49
XDOT = -15721
534965 XDOT = -4814
551769
YDOT = -1820
155001 feet/sec YDOT = -608
495143 meter/sec
ZDOT = 19712
774522 ZDOT = 5985
119814
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9093971
36 X = -2771842
47
Y = -19927916
57 feet Y = -6074028
97 meter
Z = -2481445
38 Z = -756344
55
XDOT = 11991
365751 XDOT = 3654
968281
YDOT = -7895
281744 feet/sec YDOT = -2406
481875 meter/sec
ZDOT = 19623
226614 ZDOT = 5981
159472
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 08081
11476439
00020000 00000-0 20000-3 0 9113
2 25544 51
6343 110
3953 0001442 332
0727 28
0359 15
76443952 14638
Satellite: ISS
Catalog Number: 25544
Epoch time: 08081
11476439 = yrday
fracday
Element set: 911
Inclination: 51
6343 deg
RA of node: 110
3953 deg
Eccentricity:
0001442
Arg of perigee: 332
0727 deg
Mean anomaly: 28
0359 deg
Mean motion: 15
76443952 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1463
Checksum: 273
Coasting Arc #13 (Orbit 1478)
---------------------------------------
Vector Time (GMT): 2008/082/02:43:09
817
Vector Time (MET): N/A
Weight (LBS) : 567060
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3983429
56 A = 6712999
57 meter
Y = 1152007
24 meter E =
0014673
Z = -5291628
30 I = 51
92890
XDOT = -2002
431916 Wp = 85
85779
YDOT = 7428
463325 meter/sec RA = 104
43802 deg
ZDOT = 111
112722 TA = 185
18565
MA = 185
20087
Ha = 186
171 n
mi
Hp = 180
196
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13068994
63 X = 3995957
27
Y = 3779551
32 feet Y = 1196621
71 meter
Z = -17360985
25 Z = -5272246
57
XDOT = -6569
658516 XDOT = -2085
889085
YDOT = 24371
598834 feet/sec YDOT = 7405
604366 meter/sec
ZDOT = 364
543051 ZDOT = 101
181439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12513954
52 X = -3814253
34
Y = 5573552
17 feet Y = 1698818
70 meter
Z = -17286523
54 Z = -5268932
38
XDOT = -10234
523402 XDOT = -3119
482733
YDOT = -21977
009463 feet/sec YDOT = -6698
592484 meter/sec
ZDOT = 327
324424 ZDOT = 99
768485
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 08082
12900656
00020000 00000-0 20000-3 0 9129
2 25544 51
6345 105
1673 0001358 341
4238 18
6876 15
76497131 14792
Satellite: ISS
Catalog Number: 25544
Epoch time: 08082
12900656 = yrday
fracday
Element set: 912
Inclination: 51
6345 deg
RA of node: 105
1673 deg
Eccentricity:
0001358
Arg of perigee: 341
4238 deg
Mean anomaly: 18
6876 deg
Mean motion: 15
76497131 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1479
Checksum: 293
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 may contain past, current and future orbital data 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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