Date:
July 29th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 2690 98 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 1715)
---------------------------------------
Vector Time (GMT): 2007/208/13:59:11
277
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4095696
27 A = 6714568
69 meter
Y = -928572
89 meter E =
0009435
Z = 5235593
51 I = 51
30243
XDOT = 1933
134913 Wp = 156
08589
YDOT = 7458
968440 meter/sec RA = 254
29243 deg
ZDOT = -197
739693 TA = 295
74912
MA = 295
84648
Ha = 189
247 n
mi
Hp = 179
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13437323
73 X = 4080342
12
Y = -3046498
97 feet Y = -882859
25 meter
Z = 17177144
08 Z = 5255452
66
XDOT = 6342
306146 XDOT = 1850
544523
YDOT = 24471
681232 feet/sec YDOT = 7480
124089 meter/sec
ZDOT = -648
752275 ZDOT = -188
547998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13322385
28 X = -4060663
03
Y = -3126067
76 feet Y = -952825
45 meter
Z = 17252213
03 Z = 5258474
53
XDOT = 4826
017195 XDOT = 1470
970041
YDOT = -23799
272928 feet/sec YDOT = -7254
018389 meter/sec
ZDOT = -613
087811 ZDOT = -186
869165
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 07208
63003017
00020000 00000-0 20000-3 0 9006
2 25544 51
6322 254
8574 0009105 171
0255 189
1073 15
75945050 17167
Satellite: ISS
Catalog Number: 25544
Epoch time: 07208
63003017 = yrday
fracday
Element set: 900
Inclination: 51
6322 deg
RA of node: 254
8574 deg
Eccentricity:
0009105
Arg of perigee: 171
0255 deg
Mean anomaly: 189
1073 deg
Mean motion: 15
75945050 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1716
Checksum: 265
Coasting Arc #2 (Orbit 1731)
---------------------------------------
Vector Time (GMT): 2007/209/13:59:11
277
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1747163
54 A = 6726280
77 meter
Y = -6441798
95 meter E =
0011724
Z = 828299
49 I = 51
35125
XDOT = 4871
328463 Wp = 95
12961
YDOT = -548
518726 meter/sec RA = 249
12975 deg
ZDOT = 5936
260556 TA = 273
94320
MA = 274
07722
Ha = 189
187 n
mi
Hp = 179
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5732163
84 X = -1679024
19
Y = -21134510
98 feet Y = -6460955
86 meter
Z = 2717518
02 Z = 819976
42
XDOT = 15982
048763 XDOT = 4848
263320
YDOT = -1799
602119 feet/sec YDOT = -494
174698 meter/sec
ZDOT = 19475
920458 ZDOT = 5959
868901
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3754465
44 X = -1144361
07
Y = 21577849
54 feet Y = 6576928
54 meter
Z = 2685248
46 Z = 818463
73
XDOT = -13565
115147 XDOT = -4134
647097
YDOT = -4825
277872 feet/sec YDOT = -1470
744695 meter/sec
ZDOT = 19565
235113 ZDOT = 5963
483662
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 07209
64460674
00020000 00000-0 20000-3 0 9015
2 25544 51
6321 249
6317 0009082 175
4582 184
6666 15
75972941 17323
Satellite: ISS
Catalog Number: 25544
Epoch time: 07209
64460674 = yrday
fracday
Element set: 901
Inclination: 51
6321 deg
RA of node: 249
6317 deg
Eccentricity:
0009082
Arg of perigee: 175
4582 deg
Mean anomaly: 184
6666 deg
Mean motion: 15
75972941 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1732
Checksum: 310
Coasting Arc #3 (Orbit 1746)
---------------------------------------
Vector Time (GMT): 2007/210/13:59:11
277
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4462244
79 A = 6715554
49 meter
Y = 45670
24 meter E =
0017885
Z = -5032952
82 I = 51
32557
XDOT = -2010
879524 Wp = 132
09413
YDOT = -7224
820512 meter/sec RA = 243
93456 deg
ZDOT = 1709
365972 TA = 154
48829
MA = 154
39991
Ha = 189
047 n
mi
Hp = 179
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14639910
74 X = -4437975
24
Y = 149836
75 feet Y = -4092
70 meter
Z = -16512312
40 Z = -5054570
95
XDOT = -6597
373768 XDOT = -1938
244661
YDOT = -23703
479370 feet/sec YDOT = -7246
901411 meter/sec
ZDOT = 5608
156075 ZDOT = 1699
772777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13340484
22 X = 4066179
59
Y = 5802692
44 feet Y = 1768660
66 meter
Z = -16594159
80 Z = -5057899
91
XDOT = -3203
917675 XDOT = -976
554107
YDOT = 23371
404045 feet/sec YDOT = 7123
603953 meter/sec
ZDOT = 5570
970262 ZDOT = 1698
031736
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 07210
59576731
00020000 00000-0 20000-3 0 9024
2 25544 51
6314 244
7316 0008941 179
3776 180
7400 15
75936680 17470
Satellite: ISS
Catalog Number: 25544
Epoch time: 07210
59576731 = yrday
fracday
Element set: 902
Inclination: 51
6314 deg
RA of node: 244
7316 deg
Eccentricity:
0008941
Arg of perigee: 179
3776 deg
Mean anomaly: 180
7400 deg
Mean motion: 15
75936680 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1747
Checksum: 306
Coasting Arc #4 (Orbit 1762)
---------------------------------------
Vector Time (GMT): 2007/211/13:59:11
277
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1723008
20 A = 6724653
09 meter
Y = 6132612
20 meter E =
0014227
Z = -2131570
04 I = 51
36896
XDOT = -5381
110196 Wp = 164
73190
YDOT = -393
624597 meter/sec RA = 238
79587 deg
ZDOT = -5504
008887 TA = 39
23541
MA = 39
13238
Ha = 188
927 n
mi
Hp = 180
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5652914
04 X = 1664658
89
Y = 20120118
76 feet Y = 6151553
83 meter
Z = -6993340
02 Z = -2123340
93
XDOT = -17654
561012 XDOT = -5349
571878
YDOT = -1291
419283 feet/sec YDOT = -453
622258 meter/sec
ZDOT = -18057
771940 ZDOT = -5530
073116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2662669
85 X = 811581
77
Y = -20739576
25 feet Y = -6321422
84 meter
Z = -6961435
72 Z = -2121845
61
XDOT = 14124
896108 XDOT = 4305
268334
YDOT = 7883
692249 feet/sec YDOT = 2402
949397 meter/sec
ZDOT = -18156
515489 ZDOT = -5534
105921
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
61033132
00020000 00000-0 20000-3 0 9032
2 25544 51
6301 239
5045 0008932 182
6970 177
4147 15
75955881 17633
Satellite: ISS
Catalog Number: 25544
Epoch time: 07211
61033132 = yrday
fracday
Element set: 903
Inclination: 51
6301 deg
RA of node: 239
5045 deg
Eccentricity:
0008932
Arg of perigee: 182
6970 deg
Mean anomaly: 177
4147 deg
Mean motion: 15
75955881 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1763
Checksum: 287
Coasting Arc #5 (Orbit 1778)
---------------------------------------
Vector Time (GMT): 2007/212/13:59:11
277
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4948748
46 A = 6717629
78 meter
Y = 669504
78 meter E =
0008670
Z = 4484465
34 I = 51
36130
XDOT = 1907
923011 Wp = 127
32726
YDOT = 6787
160369 meter/sec RA = 233
58258 deg
ZDOT = -3119
804267 TA = 353
87012
MA = 353
88072
Ha = 188
576 n
mi
Hp = 180
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16236051
38 X = 4919109
95
Y = 2196537
99 feet Y = 724678
40 meter
Z = 14712812
80 Z = 4508433
86
XDOT = 6259
589932 XDOT = 1847
041268
YDOT = 22267
586512 feet/sec YDOT = 6808
155680 meter/sec
ZDOT = -10235
578303 ZDOT = -3110
683131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14136319
64 X = -4308750
23
Y = -8118932
69 feet Y = -2474650
69 meter
Z = 14803661
81 Z = 4512156
12
XDOT = 1943
513034 XDOT = 592
382773
YDOT = -21976
157304 feet/sec YDOT = -6698
332746 meter/sec
ZDOT = -10200
202256 ZDOT = -3109
021648
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
62488722
00020000 00000-0 20000-3 0 9044
2 25544 51
6296 234
2777 0008790 187
4425 172
6610 15
75988159 17793
Satellite: ISS
Catalog Number: 25544
Epoch time: 07212
62488722 = yrday
fracday
Element set: 904
Inclination: 51
6296 deg
RA of node: 234
2777 deg
Eccentricity:
0008790
Arg of perigee: 187
4425 deg
Mean anomaly: 172
6610 deg
Mean motion: 15
75988159 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1779
Checksum: 329
Coasting Arc #6 (Orbit 1794)
---------------------------------------
Vector Time (GMT): 2007/213/13:59:11
277
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1533293
03 A = 6721801
28 meter
Y = -5668601
19 meter E =
0013740
Z = 3270339
97 I = 51
39361
XDOT = 5996
399857 Wp = 126
98853
YDOT = 1104
425527 meter/sec RA = 228
46172 deg
ZDOT = 4704
003947 TA = 271
51908
MA = 271
67647
Ha = 188
540 n
mi
Hp = 180
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5030488
96 X = -1485678
34
Y = -18597772
94 feet Y = -5685481
29 meter
Z = 10729461
86 Z = 3263006
73
XDOT = 19673
227877 XDOT = 5960
753601
YDOT = 3623
443331 feet/sec YDOT = 1171
281081 meter/sec
ZDOT = 15433
083815 ZDOT = 4733
047355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1959627
24 X = -597294
38
Y = 19182104
59 feet Y = 5846705
48 meter
Z = 10700983
78 Z = 3261659
86
XDOT = -15562
486618 XDOT = -4743
445921
YDOT = -10300
724863 feet/sec YDOT = -3139
660938 meter/sec
ZDOT = 15543
212152 ZDOT = 4737
571064
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
63943584
00020000 00000-0 20000-3 0 9059
2 25544 51
6296 229
0512 0008866 191
8908 168
2048 15
76022843 17955
Satellite: ISS
Catalog Number: 25544
Epoch time: 07213
63943584 = yrday
fracday
Element set: 905
Inclination: 51
6296 deg
RA of node: 229
0512 deg
Eccentricity:
0008866
Arg of perigee: 191
8908 deg
Mean anomaly: 168
2048 deg
Mean motion: 15
76022843 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1795
Checksum: 316
Coasting Arc #7 (Orbit 1809)
---------------------------------------
Vector Time (GMT): 2007/214/13:59:11
277
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5524618
11 A = 6720671
06 meter
Y = -1203281
70 meter E =
0010061
Z = -3644313
04 I = 51
40978
XDOT = -1517
606455 Wp = 160
37017
YDOT = -6174
143179 meter/sec RA = 223
24125 deg
ZDOT = 4333
333750 TA = 155
75263
MA = 155
70525
Ha = 188
410 n
mi
Hp = 180
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18125387
50 X = -5493049
08
Y = -3947774
59 feet Y = -1264884
43 meter
Z = -11956407
62 Z = -3671074
61
XDOT = -4979
023803 XDOT = -1469
503726
YDOT = -20256
375259 feet/sec YDOT = -6190
845127 meter/sec
ZDOT = 14216
974244 ZDOT = 4326
077917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15591919
57 X = 4752417
09
Y = 9928195
62 feet Y = 3026114
02 meter
Z = -12057912
56 Z = -3675251
75
XDOT = -1506
860138 XDOT = -459
290970
YDOT = 19622
051540 feet/sec YDOT = 5980
801309 meter/sec
ZDOT = 14188
718234 ZDOT = 4324
721318
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
59057094
00020000 00000-0 20000-3 0 9068
2 25544 51
6296 224
1505 0008630 194
7852 165
3061 15
75979715 18101
Satellite: ISS
Catalog Number: 25544
Epoch time: 07214
59057094 = yrday
fracday
Element set: 906
Inclination: 51
6296 deg
RA of node: 224
1505 deg
Eccentricity:
0008630
Arg of perigee: 194
7852 deg
Mean anomaly: 165
3061 deg
Mean motion: 15
75979715 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1810
Checksum: 301
Coasting Arc #8 (Orbit 1825)
---------------------------------------
Vector Time (GMT): 2007/215/13:59:11
277
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1045631
07 A = 6718682
06 meter
Y = 5112366
32 meter E =
0007284
Z = -4233131
56 I = 51
42545
XDOT = -6636
999130 Wp = 136
35618
YDOT = -1590
358609 meter/sec RA = 218
12479 deg
ZDOT = -3568
926861 TA = 97
33427
MA = 97
25149
Ha = 188
220 n
mi
Hp = 180
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3430548
14 X = 1008949
73
Y = 16772855
37 feet Y = 5123854
22 meter
Z = -13888226
91 Z = -4228140
83
XDOT = -21774
931528 XDOT = -6601
385183
YDOT = -5217
711973 feet/sec YDOT = -1664
378003 meter/sec
ZDOT = -11709
077628 ZDOT = -3601
082674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2193867
84 X = 668690
92
Y = -16994907
09 feet Y = -5180047
68 meter
Z = -13868679
15 Z = -4227173
41
XDOT = 17552
522094 XDOT = 5350
008734
YDOT = 11896
901649 feet/sec YDOT = 3626
175623 meter/sec
ZDOT = -11831
067002 ZDOT = -3606
109222
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
60510708
00020000 00000-0 20000-3 0 9078
2 25544 51
6300 218
9231 0008612 198
8340 161
2506 15
76005789 18269
Satellite: ISS
Catalog Number: 25544
Epoch time: 07215
60510708 = yrday
fracday
Element set: 907
Inclination: 51
6300 deg
RA of node: 218
9231 deg
Eccentricity:
0008612
Arg of perigee: 198
8340 deg
Mean anomaly: 161
2506 deg
Mean motion: 15
76005789 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1826
Checksum: 279
Coasting Arc #9 (Orbit 1841)
---------------------------------------
Vector Time (GMT): 2007/216/13:59:11
277
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6033057
31 A = 6723537
39 meter
Y = 1499515
82 meter E =
0014867
Z = 2535509
09 I = 51
46584
XDOT = 841
730946 Wp = 138
00703
YDOT = 5554
915166 meter/sec RA = 212
91291 deg
ZDOT = -5281
165177 TA = 13
12519
MA = 13
08654
Ha = 187
897 n
mi
Hp = 181
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19793495
13 X = 6003524
13
Y = 4919671
34 feet Y = 1566815
60 meter
Z = 8318599
37 Z = 2564745
90
XDOT = 2761
584470 XDOT = 805
207338
YDOT = 18224
787291 feet/sec YDOT = 5564
123948 meter/sec
ZDOT = -17326
657406 ZDOT = -5277
164481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17225047
80 X = -5250194
57
Y = -10836304
61 feet Y = -3302905
65 meter
Z = 8429527
95 Z = 2569320
12
XDOT = 2181
344544 XDOT = 664
873817
YDOT = -16950
751364 feet/sec YDOT = -5166
589016 meter/sec
ZDOT = -17310
802106 ZDOT = -5276
332482
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
61963555
00020000 00000-0 20000-3 0 9083
2 25544 51
6301 213
6967 0008522 203
7153 156
3619 15
76027463 18427
Satellite: ISS
Catalog Number: 25544
Epoch time: 07216
61963555 = yrday
fracday
Element set: 908
Inclination: 51
6301 deg
RA of node: 213
6967 deg
Eccentricity:
0008522
Arg of perigee: 203
7153 deg
Mean anomaly: 156
3619 deg
Mean motion: 15
76027463 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1842
Checksum: 292
Coasting Arc #10 (Orbit 1857)
---------------------------------------
Vector Time (GMT): 2007/217/13:59:11
277
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -355235
86 A = 6715899
05 meter
Y = -4590776
94 meter E =
0011195
Z = 4891503
38 I = 51
46570
XDOT = 7160
265942 Wp = 172
92032
YDOT = 1797
278883 meter/sec RA = 207
79010 deg
ZDOT = 2195
308394 TA = 255
64774
MA = 255
77205
Ha = 187
810 n
mi
Hp = 181
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1165471
97 X = -327636
70
Y = -15061604
12 feet Y = -4594595
45 meter
Z = 16048239
42 Z = 4889844
32
XDOT = 23491
686162 XDOT = 7128
971950
YDOT = 5896
584261 feet/sec YDOT = 1877
173862 meter/sec
ZDOT = 7202
455360 ZDOT = 2230
017023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3254175
54 X = -991872
70
Y = 14759431
81 feet Y = 4498674
82 meter
Z = 16041376
07 Z = 4889411
43
XDOT = -19582
514308 XDOT = -5968
750361
YDOT = -12329
681263 feet/sec YDOT = -3758
086849 meter/sec
ZDOT = 7334
156293 ZDOT = 2235
450838
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
63415604
00020000 00000-0 20000-3 0 9094
2 25544 51
6306 208
4706 0008611 208
3445 151
7252 15
76062043 18581
Satellite: ISS
Catalog Number: 25544
Epoch time: 07217
63415604 = yrday
fracday
Element set: 909
Inclination: 51
6306 deg
RA of node: 208
4706 deg
Eccentricity:
0008611
Arg of perigee: 208
3445 deg
Mean anomaly: 151
7252 deg
Mean motion: 15
76062043 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1858
Checksum: 277
Coasting Arc #11 (Orbit 1872)
---------------------------------------
Vector Time (GMT): 2007/218/13:59:11
277
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6413721
49 A = 6725625
04 meter
Y = -1592895
29 meter E =
0001062
Z = -1250656
02 I = 51
52431
XDOT = 100
469884 Wp = 96
01845
YDOT = -4997
814156 meter/sec RA = 202
59793 deg
ZDOT = 5854
354589 TA = 250
24138
MA = 250
25283
Ha = 187
663 n
mi
Hp = 181
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21042393
34 X = -6389357
38
Y = -5226034
41 feet Y = -1664480
77 meter
Z = -4103202
18 Z = -1281754
79
XDOT = 329
625603 XDOT = 127
909402
YDOT = -16397
028070 feet/sec YDOT = -4996
537845 meter/sec
ZDOT = 19207
200096 ZDOT = 5854
908790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18723966
47 X = 5707064
98
Y = 10886893
49 feet Y = 3318325
14 meter
Z = -4221214
41 Z = -1286626
15
XDOT = -3997
386095 XDOT = -1218
403282
YDOT = 14317
687498 feet/sec YDOT = 4364
031149 meter/sec
ZDOT = 19208
671181 ZDOT = 5854
802976
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
58526386
00020000 00000-0 20000-3 0 9101
2 25544 51
6302 203
5701 0008499 211
2076 148
8585 15
76048301 18739
Satellite: ISS
Catalog Number: 25544
Epoch time: 07218
58526386 = yrday
fracday
Element set: 910
Inclination: 51
6302 deg
RA of node: 203
5701 deg
Eccentricity:
0008499
Arg of perigee: 211
2076 deg
Mean anomaly: 148
8585 deg
Mean motion: 15
76048301 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1873
Checksum: 292
Coasting Arc #12 (Orbit 1888)
---------------------------------------
Vector Time (GMT): 2007/219/13:59:11
277
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -578084
35 A = 6714407
73 meter
Y = 4178470
31 meter E =
0011241
Z = -5231796
64 I = 51
51410
XDOT = -7453
719774 Wp = 119
79188
YDOT = -1816
000013 meter/sec RA = 197
45556 deg
ZDOT = -633
293402 TA = 144
21284
MA = 144
13746
Ha = 187
431 n
mi
Hp = 181
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1896602
21 X = -599350
70
Y = 13708892
08 feet Y = 4171887
60 meter
Z = -17164687
15 Z = -5234656
08
XDOT = -24454
461200 XDOT = -7429
782612
YDOT = -5958
005293 feet/sec YDOT = -1899
217783 meter/sec
ZDOT = -2077
734259 ZDOT = -669
445435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5337735
01 X = 1626941
63
Y = -12754817
84 feet Y = -3887668
48 meter
Z = -17174996
76 Z = -5234939
01
XDOT = 21089
298791 XDOT = 6428
018271
YDOT = 11779
406223 feet/sec YDOT = 3590
363017 meter/sec
ZDOT = -2214
933991 ZDOT = -675
111881
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
59977057
00020000 00000-0 20000-3 0 9119
2 25544 51
6308 198
3430 0008482 216
0003 144
0591 15
76052097 18899
Satellite: ISS
Catalog Number: 25544
Epoch time: 07219
59977057 = yrday
fracday
Element set: 911
Inclination: 51
6308 deg
RA of node: 198
3430 deg
Eccentricity:
0008482
Arg of perigee: 216
0003 deg
Mean anomaly: 144
0591 deg
Mean motion: 15
76052097 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1889
Checksum: 300
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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