Date:
October 4th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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
278/10:08:14
943 0
2 2
2 2
2
N/A -1
5 0
1 193
7
000/00:04:29
885 1
7 -0
1 186
8
Coasting Arc #1 (Orbit 541)
---------------------------------------
Vector Time (GMT): 2008/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628687
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1671396
18 A = 6725150
91 meter
Y = 3971866
83 meter E =
0016755
Z = -5177119
82 I = 51
59273
XDOT = -7427
886141 Wp = 119
26769
YDOT = -1592
947480 meter/sec RA = 185
08620 deg
ZDOT = 1170
742159 TA = 161
97008
MA = 161
91058
Ha = 193
707 n
mi
Hp = 185
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5483583
26 X = -1690535
93
Y = 13031059
17 feet Y = 3953069
06 meter
Z = -16985301
24 Z = -5185286
32
XDOT = -24369
705186 XDOT = -7415
208865
YDOT = -5226
205642 feet/sec YDOT = -1675
939454 meter/sec
ZDOT = 3841
017581 ZDOT = 1134
687545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2843597
49 X = 866728
51
Y = -13810567
00 feet Y = -4209460
82 meter
Z = -17016487
27 Z = -5186625
32
XDOT = 23931
703816 XDOT = 7294
383323
YDOT = 346
037795 feet/sec YDOT = 105
472320 meter/sec
ZDOT = 3701
332818 ZDOT = 1128
166243
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 08276
51400900
00020000 00000-0 20000-3 0 9001
2 25544 51
6417 186
0358 0005935 175
5068 184
6148 15
72380225 5429
Satellite: ISS
Catalog Number: 25544
Epoch time: 08276
51400900 = yrday
fracday
Element set: 900
Inclination: 51
6417 deg
RA of node: 186
0358 deg
Eccentricity:
0005935
Arg of perigee: 175
5068 deg
Mean anomaly: 184
6148 deg
Mean motion: 15
72380225 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 542
Checksum: 282
Coasting Arc #2 (Orbit 557)
---------------------------------------
Vector Time (GMT): 2008/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 628687
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6694191
59 A = 6736698
20 meter
Y = 412864
12 meter E =
0016234
Z = -525460
06 I = 51
66082
XDOT = -758
453557 Wp = 153
27081
YDOT = 4755
048767 meter/sec RA = 179
97687 deg
ZDOT = -6012
091501 TA = 32
44424
MA = 32
34454
Ha = 193
673 n
mi
Hp = 185
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21962570
85 X = 6691630
00
Y = 1354541
08 feet Y = 487708
10 meter
Z = -1723950
34 Z = -492945
21
XDOT = -2488
364689 XDOT = -782
362618
YDOT = 15600
553697 feet/sec YDOT = 4746
433454 meter/sec
ZDOT = -19724
709649 ZDOT = -6015
834355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21784315
31 X = -6639859
31
Y = 3170341
68 feet Y = 966320
14 meter
Z = -1598075
34 Z = -487093
36
XDOT = -636
156142 XDOT = -193
900392
YDOT = -14167
883759 feet/sec YDOT = -4318
370970 meter/sec
ZDOT = -19738
701028 ZDOT = -6016
356073
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 08277
53088143
00020000 00000-0 20000-3 0 9016
2 25544 51
6417 180
8263 0006048 179
8778 180
2387 15
72378512 5587
Satellite: ISS
Catalog Number: 25544
Epoch time: 08277
53088143 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 180
8263 deg
Eccentricity:
0006048
Arg of perigee: 179
8778 deg
Mean anomaly: 180
2387 deg
Mean motion: 15
72378512 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 558
Checksum: 315
Coasting Arc #3 (Orbit 572)
---------------------------------------
Vector Time (GMT): 2008/278/10:10:29
885
Vector Time (MET): N/A
Weight (LBS) : 628523
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6447898
76 A = 6736607
81 meter
Y = -846438
34 meter E =
0012782
Z = 1742390
14 I = 51
68211
XDOT = 2165
766200 Wp = 81
51698
YDOT = -4698
562201 meter/sec RA = 175
25478 deg
ZDOT = 5698
501217 TA = 297
74305
MA = 297
87263
Ha = 193
698 n
mi
Hp = 186
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21154523
51 X = -6446418
92
Y = -2777028
68 feet Y = -918534
17 meter
Z = 5716503
09 Z = 1711069
23
XDOT = 7105
532152 XDOT = 2190
462469
YDOT = -15415
230317 feet/sec YDOT = -4674
205192 meter/sec
ZDOT = 18695
870133 ZDOT = 5709
082772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19794824
13 X = 6033462
39
Y = 8047541
09 feet Y = 2452890
52 meter
Z = 5595192
66 Z = 1705414
72
XDOT = -10084
185879 XDOT = -3073
659856
YDOT = 11699
305533 feet/sec YDOT = 3565
948326 meter/sec
ZDOT = 18736
340197 ZDOT = 5710
836492
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 08278
48419981
00020000 00000-0 20000-3 0 9020
2 25544 51
6398 175
9419 0004102 181
5326 178
5824 15
72004750 5734
Satellite: ISS
Catalog Number: 25544
Epoch time: 08278
48419981 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 175
9419 deg
Eccentricity:
0004102
Arg of perigee: 181
5326 deg
Mean anomaly: 178
5824 deg
Mean motion: 15
72004750 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 573
Checksum: 306
Coasting Arc #4 (Orbit 587)
---------------------------------------
Vector Time (GMT): 2008/279/10:10:29
885
Vector Time (MET): N/A
Weight (LBS) : 628523
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -734904
03 A = 6726247
80 meter
Y = 4267762
34 meter E =
0015059
Z = -5159578
96 I = 51
67721
XDOT = -7570
687336 Wp = 115
73142
YDOT = 275
003911 meter/sec RA = 170
11030 deg
ZDOT = 1302
334060 TA = 166
76004
MA = 166
72047
Ha = 193
534 n
mi
Hp = 186
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2411102
45 X = -757507
47
Y = 14001844
94 feet Y = 4259417
81 meter
Z = -16927752
48 Z = -5163204
10
XDOT = -24838
213046 XDOT = -7579
526415
YDOT = 902
243802 feet/sec YDOT = 190
294699 meter/sec
ZDOT = 4272
749540 ZDOT = 1265
533543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5557804
94 X = 1694018
94
Y = -13058155
97 feet Y = -3980125
94 meter
Z = -16941347
28 Z = -5163722
65
XDOT = 23418
928506 XDOT = 7138
089409
YDOT = 4594
213890 feet/sec YDOT = 1400
316394 meter/sec
ZDOT = 4130
330740 ZDOT = 1258
924810
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 08279
43774151
00020000 00000-0 20000-3 0 9030
2 25544 51
6403 171
0591 0004079 185
5431 174
5687 15
72031922 5883
Satellite: ISS
Catalog Number: 25544
Epoch time: 08279
43774151 = yrday
fracday
Element set: 903
Inclination: 51
6403 deg
RA of node: 171
0591 deg
Eccentricity:
0004079
Arg of perigee: 185
5431 deg
Mean anomaly: 174
5687 deg
Mean motion: 15
72031922 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 588
Checksum: 295
Coasting Arc #5 (Orbit 603)
---------------------------------------
Vector Time (GMT): 2008/280/10:10:29
885
Vector Time (MET): N/A
Weight (LBS) : 628523
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6575819
65 A = 6737657
84 meter
Y = -1329991
50 meter E =
0014177
Z = -527645
75 I = 51
74470
XDOT = 490
191556 Wp = 152
24454
YDOT = 4780
416722 meter/sec RA = 165
01055 deg
ZDOT = -6017
273751 TA = 33
48581
MA = 33
39626
Ha = 193
490 n
mi
Hp = 186
902
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21574211
47 X = 6592766
35
Y = -4363489
16 feet Y = -1256362
13 meter
Z = -1731121
24 Z = -495658
79
XDOT = 1608
240013 XDOT = 465
930992
YDOT = 15683
781897 feet/sec YDOT = 4785
762669 meter/sec
ZDOT = -19741
711782 ZDOT = -6014
951303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22015141
81 X = -6710215
22
Y = -482829
72 feet Y = -147166
50 meter
Z = -1607428
24 Z = -489944
13
XDOT = 1729
603202 XDOT = 527
183056
YDOT = -14073
503475 feet/sec YDOT = -4289
603859 meter/sec
ZDOT = -19732
232941 ZDOT = -6014
384600
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 08280
45483664
00020000 00000-0 20000-3 0 9041
2 25544 51
6407 165
8510 0004163 189
5631 170
5453 15
72041024 6049
Satellite: ISS
Catalog Number: 25544
Epoch time: 08280
45483664 = yrday
fracday
Element set: 904
Inclination: 51
6407 deg
RA of node: 165
8510 deg
Eccentricity:
0004163
Arg of perigee: 189
5631 deg
Mean anomaly: 170
5453 deg
Mean motion: 15
72041024 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 604
Checksum: 272
Coasting Arc #6 (Orbit 619)
---------------------------------------
Vector Time (GMT): 2008/281/10:10:29
885
Vector Time (MET): N/A
Weight (LBS) : 628523
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1557631
39 A = 6725460
35 meter
Y = -3864038
70 meter E =
0004479
Z = 5278649
09 I = 51
73222
XDOT = 7196
763233 Wp = 163
61067
YDOT = -2733
867706 meter/sec RA = 159
89325 deg
ZDOT = 118
166985 TA = 285
24450
MA = 285
29401
Ha = 193
239 n
mi
Hp = 186
945
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5110339
21 X = -1539950
35
Y = -12677292
32 feet Y = -3881358
14 meter
Z = 17318402
51 Z = 5271125
00
XDOT = 23611
427931 XDOT = 7226
224861
YDOT = -8969
382236 feet/sec YDOT = -2653
224616 meter/sec
ZDOT = 387
686959 ZDOT = 153
200862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2530506
40 X = 771298
35
Y = 13470248
89 feet Y = 4105731
86 meter
Z = 17288878
08 Z = 5269650
04
XDOT = -23954
901046 XDOT = -7301
453839
YDOT = 3810
940736 feet/sec YDOT = 1161
574736 meter/sec
ZDOT = 523
047444 ZDOT = 159
424861
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 08281
47191248
00020000 00000-0 20000-3 0 9059
2 25544 51
6405 160
6429 0004107 195
7019 164
4017 15
72123363 6209
Satellite: ISS
Catalog Number: 25544
Epoch time: 08281
47191248 = yrday
fracday
Element set: 905
Inclination: 51
6405 deg
RA of node: 160
6429 deg
Eccentricity:
0004107
Arg of perigee: 195
7019 deg
Mean anomaly: 164
4017 deg
Mean motion: 15
72123363 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 620
Checksum: 270
Coasting Arc #7 (Orbit 634)
---------------------------------------
Vector Time (GMT): 2008/282/10:10:29
885
Vector Time (MET): N/A
Weight (LBS) : 628523
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5794683
82 A = 6737301
97 meter
Y = 3356109
42 meter E =
0006892
Z = -719561
91 I = 51
79972
XDOT = -2951
615040 Wp = 51
84198
YDOT = -3820
958450 meter/sec RA = 154
77255 deg
ZDOT = 5991
055596 TA = 300
34424
MA = 300
41238
Ha = 193
087 n
mi
Hp = 187
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19011429
85 X = -5828286
17
Y = 11010857
69 feet Y = 3291122
03 meter
Z = -2360767
41 Z = -747794
44
XDOT = -9683
776379 XDOT = -2937
772849
YDOT = -12535
952921 feet/sec YDOT = -3853
887608 meter/sec
ZDOT = 19655
694211 ZDOT = 5976
750201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20713444
00 X = 6313457
73
Y = -7286993
92 feet Y = -2221075
75 meter
Z = -2469743
37 Z = -752777
78
XDOT = 6763
540559 XDOT = 2061
527163
YDOT = 12628
134919 feet/sec YDOT = 3849
055523 meter/sec
ZDOT = 19599
913669 ZDOT = 5974
053686
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 08282
42540833
00020000 00000-0 20000-3 0 9064
2 25544 51
6411 155
7598 0004023 198
9276 161
1737 15
72112336 6352
Satellite: ISS
Catalog Number: 25544
Epoch time: 08282
42540833 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 155
7598 deg
Eccentricity:
0004023
Arg of perigee: 198
9276 deg
Mean anomaly: 161
1737 deg
Mean motion: 15
72112336 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 635
Checksum: 288
Coasting Arc #8 (Orbit 650)
---------------------------------------
Vector Time (GMT): 2008/283/10:10:29
885
Vector Time (MET): N/A
Weight (LBS) : 628523
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3467354
38 A = 6726112
86 meter
Y = 2649374
47 meter E =
0012024
Z = -5128539
30 I = 51
78898
XDOT = -5842
069015 Wp = 94
54062
YDOT = 4773
192854 meter/sec RA = 149
68182 deg
ZDOT = -1487
871877 TA = 161
22523
MA = 161
18084
Ha = 192
929 n
mi
Hp = 187
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11375834
59 X = 3462384
69
Y = 8692173
46 feet Y = 2688120
46 meter
Z = -16825916
35 Z = -5111706
91
XDOT = -19166
893093 XDOT = -5887
781553
YDOT = 15660
081543 feet/sec YDOT = 4707
607819 meter/sec
ZDOT = -4881
469412 ZDOT = -1516
364111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9838288
50 X = -2998710
33
Y = -10505706
04 feet Y = -3202139
20 meter
Z = -16760464
58 Z = -5108589
61
XDOT = 20743
570277 XDOT = 6322
640220
YDOT = -11483
320152 feet/sec YDOT = -3500
115982 meter/sec
ZDOT = -4991
316217 ZDOT = -1521
353183
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 08283
44245227
00020000 00000-0 20000-3 0 9077
2 25544 51
6417 150
5513 0003966 203
2167 156
8817 15
72161072 6511
Satellite: ISS
Catalog Number: 25544
Epoch time: 08283
44245227 = yrday
fracday
Element set: 907
Inclination: 51
6417 deg
RA of node: 150
5513 deg
Eccentricity:
0003966
Arg of perigee: 203
2167 deg
Mean anomaly: 156
8817 deg
Mean motion: 15
72161072 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 651
Checksum: 280
Coasting Arc #9 (Orbit 666)
---------------------------------------
Vector Time (GMT): 2008/284/10:10:29
885
Vector Time (MET): N/A
Weight (LBS) : 628523
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4275148
53 A = 6735932
11 meter
Y = -4846691
37 meter E =
0014458
Z = 1868558
28 I = 51
84638
XDOT = 4801
765161 Wp = 129
63103
YDOT = 2043
920172 meter/sec RA = 144
54358 deg
ZDOT = -5664
770407 TA = 29
68508
MA = 29
60311
Ha = 192
864 n
mi
Hp = 187
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14026077
85 X = 4319950
07
Y = -15901218
39 feet Y = -4798633
58 meter
Z = 6130440
55 Z = 1889436
25
XDOT = 15753
822706 XDOT = 4806
071536
YDOT = 6705
774844 feet/sec YDOT = 2097
640039 meter/sec
ZDOT = -18585
204748 ZDOT = -5641
432863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16245189
01 X = -4951533
61
Y = 13589764
60 feet Y = 4142160
25 meter
Z = 6210800
25 Z = 1893051
92
XDOT = -13665
521032 XDOT = -4165
250811
YDOT = -7853
979851 feet/sec YDOT = -2393
893058 meter/sec
ZDOT = -18494
617391 ZDOT = -5637
159381
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 08284
45948055
00020000 00000-0 20000-3 0 9089
2 25544 51
6415 145
3429 0004049 206
3144 153
7813 15
72137957 6673
Satellite: ISS
Catalog Number: 25544
Epoch time: 08284
45948055 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 145
3429 deg
Eccentricity:
0004049
Arg of perigee: 206
3144 deg
Mean anomaly: 153
7813 deg
Mean motion: 15
72137957 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 667
Checksum: 304
Coasting Arc #10 (Orbit 682)
---------------------------------------
Vector Time (GMT): 2008/285/10:10:29
885
Vector Time (MET): N/A
Weight (LBS) : 628523
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4738928
87 A = 6727849
23 meter
Y = -812218
71 meter E =
0008523
Z = 4704886
63 I = 51
84289
XDOT = 3796
817064 Wp = 144
76835
YDOT = -6100
572767 meter/sec RA = 139
47434 deg
ZDOT = 2761
841214 TA = 278
03698
MA = 278
13368
Ha = 192
734 n
mi
Hp = 187
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15547666
90 X = -4752350
08
Y = -2664759
55 feet Y = -865286
83 meter
Z = 15435979
76 Z = 4681832
09
XDOT = 12456
748899 XDOT = 3851
335773
YDOT = -20015
002518 feet/sec YDOT = -6057
809525 meter/sec
ZDOT = 9061
158839 ZDOT = 2780
419272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15133116
62 X = 4612573
95
Y = 4750866
15 feet Y = 1448064
00 meter
Z = 15346609
16 Z = 4677646
47
XDOT = -14646
277484 XDOT = -4464
185377
YDOT = 17053
888271 feet/sec YDOT = 5198
025145 meter/sec
ZDOT = 9132
488766 ZDOT = 2783
582576
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 08285
47648949
00020000 00000-0 20000-3 0 9092
2 25544 51
6417 140
1340 0003916 212
5208 147
5714 15
72186207 6833
Satellite: ISS
Catalog Number: 25544
Epoch time: 08285
47648949 = yrday
fracday
Element set: 909
Inclination: 51
6417 deg
RA of node: 140
1340 deg
Eccentricity:
0003916
Arg of perigee: 212
5208 deg
Mean anomaly: 147
5714 deg
Mean motion: 15
72186207 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 683
Checksum: 297
Coasting Arc #11 (Orbit 697)
---------------------------------------
Vector Time (GMT): 2008/286/10:10:29
885
Vector Time (MET): N/A
Weight (LBS) : 628523
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2289673
85 A = 6733523
23 meter
Y = 5621321
25 meter E =
0002098
Z = -2918285
73 I = 51
88361
XDOT = -5795
267752 Wp = 126
92768
YDOT = 261
389899 meter/sec RA = 134
32306 deg
ZDOT = 5051
693656 TA = 199
65351
MA = 199
66160
Ha = 192
397 n
mi
Hp = 187
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7512053
31 X = -2338185
45
Y = 18442655
04 feet Y = 5595445
30 meter
Z = -9574428
24 Z = -2929527
49
XDOT = -19013
345642 XDOT = -5822
300571
YDOT = 857
578408 feet/sec YDOT = 196
433165 meter/sec
ZDOT = 16573
798085 ZDOT = 5023
474084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9579719
25 X = 2919898
43
Y = -17434642
75 feet Y = -5314079
11 meter
Z = -9617398
67 Z = -2931383
11
XDOT = 17804
510217 XDOT = 5426
814714
YDOT = 702
946803 feet/sec YDOT = 214
258185 meter/sec
ZDOT = 16464
528509 ZDOT = 5018
388290
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 08286
42991948
00020000 00000-0 20000-3 0 9100
2 25544 51
6414 135
2504 0003950 219
4869 140
6006 15
72218129 6987
Satellite: ISS
Catalog Number: 25544
Epoch time: 08286
42991948 = yrday
fracday
Element set: 910
Inclination: 51
6414 deg
RA of node: 135
2504 deg
Eccentricity:
0003950
Arg of perigee: 219
4869 deg
Mean anomaly: 140
6006 deg
Mean motion: 15
72218129 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 698
Checksum: 299
Coasting Arc #12 (Orbit 713)
---------------------------------------
Vector Time (GMT): 2008/287/10:10:29
885
Vector Time (MET): N/A
Weight (LBS) : 628523
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5192561
35 A = 6730063
99 meter
Y = -1287249
26 meter E =
0004163
Z = -4086571
89 I = 51
89078
XDOT = -1416
202689 Wp = 96
86095
YDOT = 6507
050150 meter/sec RA = 129
26723 deg
ZDOT = -3852
991134 TA = 133
62708
MA = 133
59254
Ha = 192
304 n
mi
Hp = 187
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17035962
43 X = 5226421
94
Y = -4223258
73 feet Y = -1228994
08 meter
Z = -13407388
10 Z = -4061263
49
XDOT = -4646
334281 XDOT = -1470
142757
YDOT = 21348
589730 feet/sec YDOT = 6490
911417 meter/sec
ZDOT = -12641
047026 ZDOT = -3860
002802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17451136
43 X = -5319106
38
Y = 2476531
38 feet Y = 754846
76 meter
Z = -13309493
45 Z = -4056733
60
XDOT = 6883
403441 XDOT = 2098
061369
YDOT = -19506
091563 feet/sec YDOT = -5945
456708 meter/sec
ZDOT = -12667
551201 ZDOT = -3861
069606
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 08287
44689494
00020000 00000-0 20000-3 0 9114
2 25544 51
6406 130
0411 0004061 224
9145 135
1689 15
72235966 7143
Satellite: ISS
Catalog Number: 25544
Epoch time: 08287
44689494 = yrday
fracday
Element set: 911
Inclination: 51
6406 deg
RA of node: 130
0411 deg
Eccentricity:
0004061
Arg of perigee: 224
9145 deg
Mean anomaly: 135
1689 deg
Mean motion: 15
72235966 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 714
Checksum: 289
Coasting Arc #13 (Orbit 729)
---------------------------------------
Vector Time (GMT): 2008/288/10:10:29
885
Vector Time (MET): N/A
Weight (LBS) : 628523
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 183177
45 A = 6730756
31 meter
Y = -5558175
63 meter E =
0008492
Z = 3783531
40 I = 51
91158
XDOT = 5837
534733 Wp = 96
95148
YDOT = -2696
612705 meter/sec RA = 124
11199 deg
ZDOT = -4237
003697 TA = 37
43057
MA = 37
37145
Ha = 191
996 n
mi
Hp = 187
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 600975
90 X = 226936
02
Y = -18235484
36 feet Y = -5555882
29 meter
Z = 12413160
77 Z = 3784528
01
XDOT = 19152
016842 XDOT = 5887
838019
YDOT = -8847
154543 feet/sec YDOT = -2631
053074 meter/sec
ZDOT = -13900
930763 ZDOT = -4208
521754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2054065
75 X = -626079
24
Y = 18127125
64 feet Y = 5525147
90 meter
Z = 12416470
99 Z = 3784540
36
XDOT = -18582
492821 XDOT = -5663
943812
YDOT = 7356
485787 feet/sec YDOT = 2242
256868 meter/sec
ZDOT = -13790
878587 ZDOT = -4203
459793
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 08288
46385207
00020000 00000-0 20000-3 0 9123
2 25544 51
6406 124
8317 0003911 230
4383 129
6434 15
72315614 7301
Satellite: ISS
Catalog Number: 25544
Epoch time: 08288
46385207 = yrday
fracday
Element set: 912
Inclination: 51
6406 deg
RA of node: 124
8317 deg
Eccentricity:
0003911
Arg of perigee: 230
4383 deg
Mean anomaly: 129
6434 deg
Mean motion: 15
72315614 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 730
Checksum: 276
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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