Date:
July 26th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5651 05 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 1657)
---------------------------------------
Vector Time (GMT): 2007/204/22:48:27
915
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -389498
02 A = 6726398
65 meter
Y = -6651657
29 meter E =
0009717
Z = -932167
04 I = 51
33251
XDOT = 4799
185026 Wp = 93
48149
YDOT = -1102
568288 meter/sec RA = 273
07661 deg
ZDOT = 5914
739576 TA = 256
29715
MA = 256
40535
Ha = 189
752 n
mi
Hp = 178
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1277880
63 X = -310560
97
Y = -21823022
60 feet Y = -6655571
39 meter
Z = -3058290
81 Z = -933868
39
XDOT = 15745
357698 XDOT = 4782
424779
YDOT = -3617
350025 feet/sec YDOT = -1048
995625 meter/sec
ZDOT = 19405
313569 ZDOT = 5938
013086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21015091
73 X = 6405399
96
Y = -6016571
13 feet Y = -1833850
88 meter
Z = -3065489
91 Z = -934361
33
XDOT = 6520
199829 XDOT = 1987
356908
YDOT = 12929
701431 feet/sec YDOT = 3940
972996 meter/sec
ZDOT = 19493
261825 ZDOT = 5941
546204
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 07204
95212677
00020000 00000-0 20000-3 0 9001
2 25544 51
6343 273
8003 0009121 157
8157 202
3404 15
75894785 16588
Satellite: ISS
Catalog Number: 25544
Epoch time: 07204
95212677 = yrday
fracday
Element set: 900
Inclination: 51
6343 deg
RA of node: 273
8003 deg
Eccentricity:
0009121
Arg of perigee: 157
8157 deg
Mean anomaly: 202
3404 deg
Mean motion: 15
75894785 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1658
Checksum: 291
Coasting Arc #2 (Orbit 1673)
---------------------------------------
Vector Time (GMT): 2007/205/22:48:27
915
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4185973
73 A = 6714627
83 meter
Y = 488197
87 meter E =
0019597
Z = -5242442
99 I = 51
29348
XDOT = -523
575582 Wp = 114
01340
YDOT = -7667
395910 meter/sec RA = 267
91429 deg
ZDOT = -304
712755 TA = 153
12735
MA = 153
02571
Ha = 189
558 n
mi
Hp = 178
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13733509
63 X = -4165655
00
Y = 1601699
06 feet Y = 441502
38 meter
Z = -17199616
10 Z = -5262728
93
XDOT = -1717
767659 XDOT = -436
318485
YDOT = -25155
498394 feet/sec YDOT = -7672
762901 meter/sec
ZDOT = -999
713764 ZDOT = -307
045511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4775947
59 X = -1455708
82
Y = -12873233
34 feet Y = -3923761
52 meter
Z = -17276333
77 Z = -5265826
53
XDOT = 23101
467204 XDOT = 7041
327204
YDOT = -7254
310370 feet/sec YDOT = -2211
113801 meter/sec
ZDOT = -1009
421338 ZDOT = -307
671624
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 07205
96672694
00020000 00000-0 20000-3 0 9013
2 25544 51
6349 268
5740 0009068 161
4354 198
7143 15
75934828 16742
Satellite: ISS
Catalog Number: 25544
Epoch time: 07205
96672694 = yrday
fracday
Element set: 901
Inclination: 51
6349 deg
RA of node: 268
5740 deg
Eccentricity:
0009068
Arg of perigee: 161
4354 deg
Mean anomaly: 198
7143 deg
Mean motion: 15
75934828 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1674
Checksum: 327
Coasting Arc #3 (Orbit 1689)
---------------------------------------
Vector Time (GMT): 2007/206/22:48:27
915
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 527231
97 A = 6726690
49 meter
Y = 6682749
68 meter E =
0019984
Z = -401550
23 I = 51
33625
XDOT = -4838
483910 Wp = 150
44114
YDOT = 29
628855 meter/sec RA = 262
74190 deg
ZDOT = -6003
474448 TA = 33
95077
MA = 33
82304
Ha = 189
520 n
mi
Hp = 179
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1729763
68 X = 454415
94
Y = 21925031
75 feet Y = 6688238
41 meter
Z = -1317422
02 Z = -399164
71
XDOT = -15874
291043 XDOT = -4809
292045
YDOT = 97
207530 feet/sec YDOT = -24
313569 meter/sec
ZDOT = -19696
438479 ZDOT = -6026
908722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20773993
59 X = -6331913
25
Y = 7222604
15 feet Y = 2201449
74 meter
Z = -1307623
70 Z = -398563
70
XDOT = -3551
933974 XDOT = -1082
629475
YDOT = -13712
274733 feet/sec YDOT = -4179
501339 meter/sec
ZDOT = -19785
131222 ZDOT = -6030
507996
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 07206
98131308
00020000 00000-0 20000-3 0 9029
2 25544 51
6349 263
3481 0009159 165
9169 194
2252 15
75908551 16905
Satellite: ISS
Catalog Number: 25544
Epoch time: 07206
98131308 = yrday
fracday
Element set: 902
Inclination: 51
6349 deg
RA of node: 263
3481 deg
Eccentricity:
0009159
Arg of perigee: 165
9169 deg
Mean anomaly: 194
2252 deg
Mean motion: 15
75908551 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1690
Checksum: 306
Coasting Arc #4 (Orbit 1705)
---------------------------------------
Vector Time (GMT): 2007/207/22:48:27
915
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4303153
00 A = 6714847
92 meter
Y = 420015
04 meter E =
0008083
Z = 5132383
13 I = 51
30206
XDOT = 687
366113 Wp = 143
36743
YDOT = 7583
827297 meter/sec RA = 257
55426 deg
ZDOT = -1202
376557 TA = 318
12926
MA = 318
19105
Ha = 189
085 n
mi
Hp = 179
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14117956
03 X = 4273204
61
Y = 1378002
09 feet Y = 467966
98 meter
Z = 16838527
33 Z = 5153214
94
XDOT = 2255
138167 XDOT = 608
352410
YDOT = 24881
323153 feet/sec YDOT = 7591
072231 meter/sec
ZDOT = -3944
804978 ZDOT = -1199
227986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2450463
58 X = 746901
30
Y = 13876143
86 feet Y = 4229448
65 meter
Z = 16917429
90 Z = 5156432
63
XDOT = -22336
356139 XDOT = -6808
121351
YDOT = 8716
661395 feet/sec YDOT = 2656
838393 meter/sec
ZDOT = -3932
008003 ZDOT = -1198
476039
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 07207
99588136
00020000 00000-0 20000-3 0 9037
2 25544 51
6346 258
1222 0008890 170
2329 189
9010 15
76008090 17066
Satellite: ISS
Catalog Number: 25544
Epoch time: 07207
99588136 = yrday
fracday
Element set: 903
Inclination: 51
6346 deg
RA of node: 258
1222 deg
Eccentricity:
0008890
Arg of perigee: 170
2329 deg
Mean anomaly: 189
9010 deg
Mean motion: 15
76008090 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1706
Checksum: 295
Coasting Arc #5 (Orbit 1721)
---------------------------------------
Vector Time (GMT): 2007/208/22:48:27
915
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -632917
75 A = 6725293
05 meter
Y = -6476478
71 meter E =
0013978
Z = 1693090
39 I = 51
34419
XDOT = 5091
423039 Wp = 100
86529
YDOT = 1000
801128 meter/sec RA = 252
40650 deg
ZDOT = 5689
273426 TA = 277
94537
MA = 278
10399
Ha = 189
124 n
mi
Hp = 179
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2076501
79 X = -568674
36
Y = -21248289
72 feet Y = -6483197
43 meter
Z = 5554758
50 Z = 1690170
69
XDOT = 16704
143830 XDOT = 5052
216530
YDOT = 3283
468268 feet/sec YDOT = 1057
516116 meter/sec
ZDOT = 18665
595229 ZDOT = 5713
912091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19758856
68 X = 6022499
52
Y = -8094462
83 feet Y = -2467192
27 meter
Z = 5542947
96 Z = 1689490
54
XDOT = 1009
045088 XDOT = 307
556943
YDOT = 15404
240996 feet/sec YDOT = 4695
212656 meter/sec
ZDOT = 18758
985989 ZDOT = 5717
738929
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
01043814
00020000 00000-0 20000-3 0 9042
2 25544 51
6343 252
8956 0008801 173
6803 186
4474 15
75986863 17220
Satellite: ISS
Catalog Number: 25544
Epoch time: 07209
01043814 = yrday
fracday
Element set: 904
Inclination: 51
6343 deg
RA of node: 252
8956 deg
Eccentricity:
0008801
Arg of perigee: 173
6803 deg
Mean anomaly: 186
4474 deg
Mean motion: 15
75986863 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1722
Checksum: 304
Coasting Arc #6 (Orbit 1736)
---------------------------------------
Vector Time (GMT): 2007/209/22:48:27
915
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4631140
29 A = 6716719
97 meter
Y = -1306647
50 meter E =
0016614
Z = -4700909
84 I = 51
32523
XDOT = -696
072677 Wp = 138
52418
YDOT = -7178
215587 meter/sec RA = 247
19637 deg
ZDOT = 2674
097958 TA = 157
95515
MA = 157
88361
Ha = 188
919 n
mi
Hp = 179
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15194029
82 X = -4593349
28
Y = -4286901
25 feet Y = -1358223
50 meter
Z = -15422932
55 Z = -4723315
86
XDOT = -2283
703008 XDOT = -628
743087
YDOT = -23550
576074 feet/sec YDOT = -7185
623411 meter/sec
ZDOT = 8773
287263 ZDOT = 2670
878957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -481280
43 X = -146694
28
Y = -15696361
48 feet Y = -4784250
98 meter
Z = -15507917
93 Z = -4726813
39
XDOT = 20598
553766 XDOT = 6278
439188
YDOT = -9308
829125 feet/sec YDOT = -2837
331117 meter/sec
ZDOT = 8760
249993 ZDOT = 2670
124198
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
96156984
00020000 00000-0 20000-3 0 9050
2 25544 51
6339 247
9956 0008782 177
9473 182
1728 15
76021679 17375
Satellite: ISS
Catalog Number: 25544
Epoch time: 07209
96156984 = yrday
fracday
Element set: 905
Inclination: 51
6339 deg
RA of node: 247
9956 deg
Eccentricity:
0008782
Arg of perigee: 177
9473 deg
Mean anomaly: 182
1728 deg
Mean motion: 15
76021679 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1737
Checksum: 347
Coasting Arc #7 (Orbit 1752)
---------------------------------------
Vector Time (GMT): 2007/210/22:48:27
915
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 527760
27 A = 6722696
82 meter
Y = 6016786
29 meter E =
0011249
Z = -2941801
79 I = 51
35699
XDOT = -5543
124873 Wp = 160
36906
YDOT = -1944
054275 meter/sec RA = 242
06900 deg
ZDOT = -4986
507973 TA = 53
73060
MA = 53
62672
Ha = 188
811 n
mi
Hp = 180
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1731496
95 X = 474730
85
Y = 19740112
50 feet Y = 6022391
88 meter
Z = -9651580
67 Z = -2939366
03
XDOT = -18186
105227 XDOT = -5496
751227
YDOT = -6378
130825 feet/sec YDOT = -2005
780692 meter/sec
ZDOT = -16359
934295 ZDOT = -5013
323440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18141836
09 X = -5529631
64
Y = 7983469
61 feet Y = 2433361
54 meter
Z = -9641635
17 Z = -2938770
40
XDOT = 861
290235 XDOT = 262
521263
YDOT = -17860
320577 feet/sec YDOT = -5443
825712 meter/sec
ZDOT = -16461
702780 ZDOT = -5017
527007
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
97609676
00020000 00000-0 20000-3 0 9065
2 25544 51
6333 242
7692 0008846 182
6269 177
4850 15
76008756 17538
Satellite: ISS
Catalog Number: 25544
Epoch time: 07210
97609676 = yrday
fracday
Element set: 906
Inclination: 51
6333 deg
RA of node: 242
7692 deg
Eccentricity:
0008846
Arg of perigee: 182
6269 deg
Mean anomaly: 177
4850 deg
Mean motion: 15
76008756 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1753
Checksum: 325
Coasting Arc #8 (Orbit 1768)
---------------------------------------
Vector Time (GMT): 2007/211/22:48:27
915
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5060543
05 A = 6719391
84 meter
Y = 2016853
58 meter E =
0011812
Z = 3920197
89 I = 51
36154
XDOT = 478
086374 Wp = 123
28917
YDOT = 6576
147675 meter/sec RA = 236
84675 deg
ZDOT = -3998
185237 TA = 8
31170
MA = 8
29216
Ha = 188
376 n
mi
Hp = 180
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16602831
54 X = 5018571
05
Y = 6616973
70 feet Y = 2073208
36 meter
Z = 12861541
62 Z = 3944679
65
XDOT = 1568
524849 XDOT = 423
937369
YDOT = 21575
287649 feet/sec YDOT = 6581
191537 meter/sec
ZDOT = -13117
405632 ZDOT = -3995
993628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -697897
20 X = -212719
07
Y = 17791898
12 feet Y = 5422970
55 meter
Z = 12954493
80 Z = 3948529
71
XDOT = -18481
681425 XDOT = -5633
216498
YDOT = 8824
698954 feet/sec YDOT = 2689
768241 meter/sec
ZDOT = -13108
304721 ZDOT = -3995
411279
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
99060743
00020000 00000-0 20000-3 0 9075
2 25544 51
6332 237
5420 0008594 186
3759 173
7298 15
76101634 17694
Satellite: ISS
Catalog Number: 25544
Epoch time: 07211
99060743 = yrday
fracday
Element set: 907
Inclination: 51
6332 deg
RA of node: 237
5420 deg
Eccentricity:
0008594
Arg of perigee: 186
3759 deg
Mean anomaly: 173
7298 deg
Mean motion: 15
76101634 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1769
Checksum: 311
Coasting Arc #9 (Orbit 1784)
---------------------------------------
Vector Time (GMT): 2007/212/22:48:27
915
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -229428
97 A = 6719468
25 meter
Y = -5414591
55 meter E =
0014128
Z = 3972423
56 I = 51
37700
XDOT = 6077
836529 Wp = 138
95613
YDOT = 2637
385943 meter/sec RA = 231
72667 deg
ZDOT = 3927
497678 TA = 270
21785
MA = 270
37974
Ha = 188
462 n
mi
Hp = 180
347
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -752719
73 X = -188162
04
Y = -17764407
99 feet Y = -5416926
70 meter
Z = 13032885
69 Z = 3971408
87
XDOT = 19940
408560 XDOT = 6028
814532
YDOT = 8652
841020 feet/sec YDOT = 2705
077363 meter/sec
ZDOT = 12885
491071 ZDOT = 3956
904257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16343571
65 X = 4981520
64
Y = -7010423
30 feet Y = -2136777
02 meter
Z = 13028373
58 Z = 3971048
27
XDOT = -1637
438775 XDOT = -499
091339
YDOT = 20449
195835 feet/sec YDOT = 6232
914891 meter/sec
ZDOT = 12997
179644 ZDOT = 3961
540356
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
00510651
00020000 00000-0 20000-3 0 9088
2 25544 51
6322 232
3141 0008575 189
8925 170
2072 15
76056107 17852
Satellite: ISS
Catalog Number: 25544
Epoch time: 07213
00510651 = yrday
fracday
Element set: 908
Inclination: 51
6322 deg
RA of node: 232
3141 deg
Eccentricity:
0008575
Arg of perigee: 189
8925 deg
Mean anomaly: 170
2072 deg
Mean motion: 15
76056107 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1785
Checksum: 272
Coasting Arc #10 (Orbit 1799)
---------------------------------------
Vector Time (GMT): 2007/213/22:48:27
915
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5540933
08 A = 6722569
64 meter
Y = -2528961
98 meter E =
0006769
Z = -2855555
64 I = 51
40643
XDOT = 46
177607 Wp = 163
04976
YDOT = -5806
572461 meter/sec RA = 226
50616 deg
ZDOT = 5049
490614 TA = 164
05415
MA = 164
03283
Ha = 188
263 n
mi
Hp = 180
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18178914
29 X = -5498370
52
Y = -8297119
37 feet Y = -2590685
70 meter
Z = -9368620
85 Z = -2882369
74
XDOT = 151
501334 XDOT = 86
575059
YDOT = -19050
434583 feet/sec YDOT = -5805
830445 meter/sec
ZDOT = 16566
570255 ZDOT = 5049
812786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1062442
07 X = 323832
34
Y = -19906462
88 feet Y = -6067489
89 meter
Z = -9470486
98 Z = -2886604
43
XDOT = 16289
899209 XDOT = 4965
161279
YDOT = -7017
558928 feet/sec YDOT = -2138
951961 meter/sec
ZDOT = 16567
064209 ZDOT = 5049
641171
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
95618290
00020000 00000-0 20000-3 0 9091
2 25544 51
6316 227
4128 0008703 194
3239 165
7680 15
76102160 18000
Satellite: ISS
Catalog Number: 25544
Epoch time: 07213
95618290 = yrday
fracday
Element set: 909
Inclination: 51
6316 deg
RA of node: 227
4128 deg
Eccentricity:
0008703
Arg of perigee: 194
3239 deg
Mean anomaly: 165
7680 deg
Mean motion: 15
76102160 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1800
Checksum: 283
Coasting Arc #11 (Orbit 1815)
---------------------------------------
Vector Time (GMT): 2007/214/22:48:27
915
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -388444
48 A = 6716249
94 meter
Y = 4724412
58 meter E =
0009534
Z = -4763112
04 I = 51
40505
XDOT = -6577
513901 Wp = 119
34879
YDOT = -3093
128994 meter/sec RA = 221
38102 deg
ZDOT = -2539
995917 TA = 125
72940
MA = 125
64067
Ha = 188
072 n
mi
Hp = 180
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1274424
16 X = -418106
65
Y = 15500041
27 feet Y = 4719903
11 meter
Z = -15627008
01 Z = -4765070
95
XDOT = -21579
770015 XDOT = -6530
098535
YDOT = -10148
061005 feet/sec YDOT = -3166
417250 meter/sec
ZDOT = -8333
319938 ZDOT = -2571
834029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14772187
17 X = -4502562
65
Y = 4841962
56 feet Y = 1475830
19 meter
Z = -15633831
92 Z = -4765191
97
XDOT = 1477
589835 XDOT = 450
369382
YDOT = -22700
395366 feet/sec YDOT = -6919
080508 meter/sec
ZDOT = -8454
291448 ZDOT = -2576
868033
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
97065135
00020000 00000-0 20000-3 0 9100
2 25544 51
6307 222
1851 0008694 198
0526 162
0331 15
76121361 18168
Satellite: ISS
Catalog Number: 25544
Epoch time: 07214
97065135 = yrday
fracday
Element set: 910
Inclination: 51
6307 deg
RA of node: 222
1851 deg
Eccentricity:
0008694
Arg of perigee: 198
0526 deg
Mean anomaly: 162
0331 deg
Mean motion: 15
76121361 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1816
Checksum: 270
Coasting Arc #12 (Orbit 1831)
---------------------------------------
Vector Time (GMT): 2007/215/22:48:27
915
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5904947
70 A = 6724903
32 meter
Y = 2799789
50 meter E =
0017120
Z = 1538812
94 I = 51
45844
XDOT = -884
778738 Wp = 147
51031
YDOT = 5043
607158 meter/sec RA = 216
17924 deg
ZDOT = -5766
062990 TA = 15
44978
MA = 15
39758
Ha = 187
744 n
mi
Hp = 180
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19373188
00 X = 5865725
95
Y = 9185661
09 feet Y = 2865602
58 meter
Z = 5048598
88 Z = 1567403
83
XDOT = -2902
817382 XDOT = -913
101046
YDOT = 16547
267579 feet/sec YDOT = 5033
554956 meter/sec
ZDOT = -18917
529494 ZDOT = -5770
429790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -705773
45 X = -215119
75
Y = 21403034
36 feet Y = 6523644
87 meter
Z = 5157241
27 Z = 1571927
14
XDOT = -14728
529586 XDOT = -4489
255818
YDOT = 4088
346270 feet/sec YDOT = 1246
127943 meter/sec
ZDOT = -18933
431441 ZDOT = -5770
909903
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
98510400
00020000 00000-0 20000-3 0 9113
2 25544 51
6317 216
9580 0008567 202
4523 157
6268 15
76182676 18328
Satellite: ISS
Catalog Number: 25544
Epoch time: 07215
98510400 = yrday
fracday
Element set: 911
Inclination: 51
6317 deg
RA of node: 216
9580 deg
Eccentricity:
0008567
Arg of perigee: 202
4523 deg
Mean anomaly: 157
6268 deg
Mean motion: 15
76182676 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1832
Checksum: 293
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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