Date:
April 21st 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5597 23 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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
115/10:22:17
143 -3
1 3
3 3
3
N/A 0
0 0
0 189
2
000/00:00:34
285 1
1 -0
0 170
5
118/10:39:51
659 11
7 11
7 11
7
N/A 0
8 -0
0 189
0
000/00:02:03
319 0
9 -0
0 177
4
Coasting Arc #1 (Orbit 165)
---------------------------------------
Vector Time (GMT): 2007/110/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2846419
57 A = 6714544
10 meter
Y = -5428680
68 meter E =
0019547
Z = -2755088
13 I = 51
85479
XDOT = 5689
487675 Wp = 95
03270
YDOT = -375
019972 meter/sec RA = 41
65962 deg
ZDOT = -5172
057130 TA = 116
38562
MA = 116
18484
Ha = 187
952 n
mi
Hp = 170
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9338646
87 X = -2772119
82
Y = -17810632
14 feet Y = -5460095
33 meter
Z = -9039003
05 Z = -2768736
08
XDOT = 18666
298147 XDOT = 5718
383604
YDOT = -1230
380484 feet/sec YDOT = -311
235050 meter/sec
ZDOT = -16968
691372 ZDOT = -5144
347057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12901699
70 X = -3932438
07
Y = -15395821
71 feet Y = -4692646
46 meter
Z = -9091058
11 Z = -2770954
51
XDOT = 16934
162392 XDOT = 5161
532697
YDOT = -4295
993750 feet/sec YDOT = -1309
418895 meter/sec
ZDOT = -16864
380647 ZDOT = -5140
263221
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 07110
48449043
00020000 00000-0 20000-3 0 9004
2 25544 51
6340 42
0463 0015393 87
8918 272
4010 15
79028133 1660
Satellite: ISS
Catalog Number: 25544
Epoch time: 07110
48449043 = yrday
fracday
Element set: 900
Inclination: 51
6340 deg
RA of node: 42
0463 deg
Eccentricity:
0015393
Arg of perigee: 87
8918 deg
Mean anomaly: 272
4010 deg
Mean motion: 15
79028133 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 166
Checksum: 266
Coasting Arc #2 (Orbit 181)
---------------------------------------
Vector Time (GMT): 2007/111/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5704559
66 A = 6712818
84 meter
Y = -890108
55 meter E =
0027914
Z = 3400457
85 I = 51
82693
XDOT = -1857
443894 Wp = 90
56275
YDOT = -5894
023970 meter/sec RA = 36
45103 deg
ZDOT = -4626
749162 TA = 49
23112
MA = 48
98920
Ha = 187
965 n
mi
Hp = 170
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18715746
91 X = -5710701
30
Y = -2920303
65 feet Y = -953934
72 meter
Z = 11156357
76 Z = 3372729
89
XDOT = -6093
976030 XDOT = -1768
921924
YDOT = -19337
348983 feet/sec YDOT = -5914
299663 meter/sec
ZDOT = -15179
623234 ZDOT = -4635
558100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18943061
73 X = -5773845
21
Y = 1513055
81 feet Y = 461179
41 meter
Z = 11051821
05 Z = 3368595
06
XDOT = -10218
760987 XDOT = -3114
678349
YDOT = -16035
584339 feet/sec YDOT = -4887
646107 meter/sec
ZDOT = -15213
506340 ZDOT = -4637
076733
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 07111
49707639
00020000 00000-0 20000-3 0 9015
2 25544 51
6343 36
8070 0015325 91
7302 268
5619 15
79070134 1821
Satellite: ISS
Catalog Number: 25544
Epoch time: 07111
49707639 = yrday
fracday
Element set: 901
Inclination: 51
6343 deg
RA of node: 36
8070 deg
Eccentricity:
0015325
Arg of perigee: 91
7302 deg
Mean anomaly: 268
5619 deg
Mean motion: 15
79070134 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 182
Checksum: 278
Coasting Arc #3 (Orbit 197)
---------------------------------------
Vector Time (GMT): 2007/112/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 148783
17 A = 6707140
97 meter
Y = 4585669
46 meter E =
0021182
Z = 4876504
66 I = 51
78484
XDOT = -7046
502219 Wp = 103
57844
YDOT = -2198
282723 meter/sec RA = 31
33309 deg
ZDOT = 2269
112235 TA = 324
38942
MA = 324
53057
Ha = 187
728 n
mi
Hp = 170
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 488133
75 X = 73805
24
Y = 15044847
32 feet Y = 4586913
68 meter
Z = 15999031
04 Z = 4877045
65
XDOT = -23118
445602 XDOT = -7032
419963
YDOT = -7212
213658 feet/sec YDOT = -2277
002073 meter/sec
ZDOT = 7444
593947 ZDOT = 2234
914275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4125950
42 X = 1257589
69
Y = 14473407
66 feet Y = 4411494
65 meter
Z = 16001615
66 Z = 4877292
45
XDOT = -23170
031207 XDOT = -7062
225512
YDOT = -1530
192559 feet/sec YDOT = -466
402692 meter/sec
ZDOT = 7315
526508 ZDOT = 2229
772480
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 07112
50963597
00020000 00000-0 20000-3 0 9026
2 25544 51
6345 31
5677 0015164 96
2078 264
0816 15
79136869 1984
Satellite: ISS
Catalog Number: 25544
Epoch time: 07112
50963597 = yrday
fracday
Element set: 902
Inclination: 51
6345 deg
RA of node: 31
5677 deg
Eccentricity:
0015164
Arg of perigee: 96
2078 deg
Mean anomaly: 264
0816 deg
Mean motion: 15
79136869 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 198
Checksum: 312
Coasting Arc #4 (Orbit 212)
---------------------------------------
Vector Time (GMT): 2007/113/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6128056
03 A = 6717582
10 meter
Y = 2724665
69 meter E =
0023743
Z = -323607
88 I = 51
79442
XDOT = -1688
601051 Wp = 74
67910
YDOT = 4471
738315 meter/sec RA = 26
14752 deg
ZDOT = 6045
445855 TA = 281
80445
MA = 282
07068
Ha = 187
745 n
mi
Hp = 170
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20105170
71 X = 6098705
00
Y = 8939191
90 feet Y = 2793028
95 meter
Z = -1061705
65 Z = -293908
95
XDOT = -5540
029696 XDOT = -1767
846836
YDOT = 14671
057465 feet/sec YDOT = 4452
412010 meter/sec
ZDOT = 19834
139945 ZDOT = 6037
050399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21761310
33 X = 6632847
39
Y = 3286038
88 feet Y = 1001584
65 meter
Z = -949516
09 Z = -289412
50
XDOT = -1318
081162 XDOT = -401
751138
YDOT = 14057
236125 feet/sec YDOT = 4284
645571 meter/sec
ZDOT = 19803
049959 ZDOT = 6035
969627
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 07113
45889061
00020000 00000-0 20000-3 0 9035
2 25544 51
6343 26
6549 0015195 99
3079 260
9806 15
79127251 2131
Satellite: ISS
Catalog Number: 25544
Epoch time: 07113
45889061 = yrday
fracday
Element set: 903
Inclination: 51
6343 deg
RA of node: 26
6549 deg
Eccentricity:
0015195
Arg of perigee: 99
3079 deg
Mean anomaly: 260
9806 deg
Mean motion: 15
79127251 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 213
Checksum: 298
Coasting Arc #5 (Orbit 228)
---------------------------------------
Vector Time (GMT): 2007/114/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3117036
88 A = 6706328
57 meter
Y = -3103637
32 meter E =
0028787
Z = -5087759
45 I = 51
73101
XDOT = 6459
863551 Wp = 102
46309
YDOT = 3841
129537 meter/sec RA = 20
97005 deg
ZDOT = 1616
060243 TA = 183
05918
MA = 183
07683
Ha = 187
626 n
mi
Hp = 170
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10226498
96 X = 3176225
89
Y = -10182537
13 feet Y = -3068449
73 meter
Z = -16692124
19 Z = -5072473
28
XDOT = 21193
778056 XDOT = 6408
580868
YDOT = 12602
131026 feet/sec YDOT = 3913
080552 meter/sec
ZDOT = 5302
034919 ZDOT = 1647
317754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7032690
36 X = 2143564
02
Y = -12677271
60 feet Y = -3864032
38 meter
Z = -16634915
23 Z = -5070322
16
XDOT = 22932
576755 XDOT = 6989
849395
YDOT = 5616
220935 feet/sec YDOT = 1711
824141 meter/sec
ZDOT = 5420
231807 ZDOT = 1652
086655
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 07114
47140324
00020000 00000-0 20000-3 0 9041
2 25544 51
6351 21
4140 0015132 103
2003 257
0852 15
79167650 2295
Satellite: ISS
Catalog Number: 25544
Epoch time: 07114
47140324 = yrday
fracday
Element set: 904
Inclination: 51
6351 deg
RA of node: 21
4140 deg
Eccentricity:
0015132
Arg of perigee: 103
2003 deg
Mean anomaly: 257
0852 deg
Mean motion: 15
79167650 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 229
Checksum: 238
Coasting Arc #6 (Orbit 244)
---------------------------------------
Vector Time (GMT): 2007/115/10:22:34
285
Vector Time (MET): N/A
Weight (LBS) : 480125
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1524490
53 A = 6708815
90 meter
Y = 4393466
11 meter E =
0023660
Z = 4818653
32 I = 51
70745
XDOT = -7334
726327 Wp = 106
89530
YDOT = -118
192669 meter/sec RA = 15
96871 deg
ZDOT = 2411
833256 TA = 319
56690
MA = 319
74251
Ha = 189
155 n
mi
Hp = 170
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5001609
35 X = 1451840
77
Y = 14414258
88 feet Y = 4410107
52 meter
Z = 15809230
05 Z = 4825882
89
XDOT = -24064
062752 XDOT = -7344
575764
YDOT = -387
771223 feet/sec YDOT = -200
268804 meter/sec
ZDOT = 7912
838765 ZDOT = 2376
177328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6863667
86 X = 2092045
96
Y = 13594065
37 feet Y = 4143471
12 meter
Z = 15836987
10 Z = 4827113
67
XDOT = -22937
613221 XDOT = -6991
384510
YDOT = 2456
608671 feet/sec YDOT = 748
774323 meter/sec
ZDOT = 7778
516930 ZDOT = 2370
891960
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 07115
48391510
00020000 00000-0 20000-3 0 9059
2 25544 51
6348 16
1740 0017082 101
8406 258
4676 15
78623206 2455
Satellite: ISS
Catalog Number: 25544
Epoch time: 07115
48391510 = yrday
fracday
Element set: 905
Inclination: 51
6348 deg
RA of node: 16
1740 deg
Eccentricity:
0017082
Arg of perigee: 101
8406 deg
Mean anomaly: 258
4676 deg
Mean motion: 15
78623206 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 245
Checksum: 276
Coasting Arc #7 (Orbit 259)
---------------------------------------
Vector Time (GMT): 2007/116/10:22:34
285
Vector Time (MET): N/A
Weight (LBS) : 480125
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6645237
79 A = 6718904
10 meter
Y = 762255
89 meter E =
0023933
Z = -625605
53 I = 51
71347
XDOT = -6
626384 Wp = 80
12072
YDOT = 4824
424878 meter/sec RA = 10
77763 deg
ZDOT = 6005
496870 TA = 273
06562
MA = 273
33945
Ha = 189
174 n
mi
Hp = 170
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21801961
27 X = 6639259
33
Y = 2500839
54 feet Y = 836533
24 meter
Z = -2052511
59 Z = -593337
51
XDOT = -21
740104 XDOT = -89
746903
YDOT = 15828
165610 feet/sec YDOT = 4823
886013 meter/sec
ZDOT = 19703
073720 ZDOT = 6005
262791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21936513
19 X = 6686249
22
Y = -923919
28 feet Y = -281610
60 meter
Z = -1930875
29 Z = -588530
79
XDOT = 2265
591898 XDOT = 690
552410
YDOT = 14056
052080 feet/sec YDOT = 4284
284674 meter/sec
ZDOT = 19702
769444 ZDOT = 6005
404127
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 07116
43347366
00020000 00000-0 20000-3 0 9066
2 25544 51
6349 11
2634 0017047 104
9621 255
3433 15
78618492 2603
Satellite: ISS
Catalog Number: 25544
Epoch time: 07116
43347366 = yrday
fracday
Element set: 906
Inclination: 51
6349 deg
RA of node: 11
2634 deg
Eccentricity:
0017047
Arg of perigee: 104
9621 deg
Mean anomaly: 255
3433 deg
Mean motion: 15
78618492 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 260
Checksum: 281
Coasting Arc #8 (Orbit 275)
---------------------------------------
Vector Time (GMT): 2007/117/10:22:34
285
Vector Time (MET): N/A
Weight (LBS) : 480125
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1616365
25 A = 6707283
49 meter
Y = -3966649
53 meter E =
0031277
Z = -5188648
77 I = 51
64689
XDOT = 7436
944282 Wp = 103
80217
YDOT = 1598
703430 meter/sec RA = 5
60541 deg
ZDOT = 1092
742460 TA = 176
65509
MA = 176
63413
Ha = 189
040 n
mi
Hp = 170
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5303035
61 X = 1685806
36
Y = -13013942
02 feet Y = -3948186
20 meter
Z = -17023125
89 Z = -5180627
74
XDOT = 24399
423496 XDOT = 7413
206258
YDOT = 5245
089995 feet/sec YDOT = 1681
734792 meter/sec
ZDOT = 3585
113059 ZDOT = 1128
813561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3071004
48 X = 936042
17
Y = -13750103
98 feet Y = -4191031
69 meter
Z = -16993388
73 Z = -5179584
89
XDOT = 23915
771919 XDOT = 7289
527281
YDOT = 735
139406 feet/sec YDOT = 224
070491 meter/sec
ZDOT = 3721
171614 ZDOT = 1134
213108
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 07117
44631171
00020000 00000-0 20000-3 0 9079
2 25544 51
6358 6
0250 0016991 108
9028 251
3981 15
78663703 2767
Satellite: ISS
Catalog Number: 25544
Epoch time: 07117
44631171 = yrday
fracday
Element set: 907
Inclination: 51
6358 deg
RA of node: 6
0250 deg
Eccentricity:
0016991
Arg of perigee: 108
9028 deg
Mean anomaly: 251
3981 deg
Mean motion: 15
78663703 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 276
Checksum: 288
Coasting Arc #9 (Orbit 291)
---------------------------------------
Vector Time (GMT): 2007/118/10:22:34
285
Vector Time (MET): N/A
Weight (LBS) : 480125
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5923560
03 A = 6716133
38 meter
Y = -1993710
22 meter E =
0022023
Z = -2458915
54 I = 51
64896
XDOT = 3615
623604 Wp = 116
76253
YDOT = -4202
726574 meter/sec RA =
46575 deg
ZDOT = -5348
811488 TA = 91
06687
MA = 90
81455
Ha = 188
885 n
mi
Hp = 170
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19434252
06 X = -5888880
77
Y = -6541044
02 feet Y = -2059756
91 meter
Z = -8067308
19 Z = -2487608
14
XDOT = 11862
282164 XDOT = 3688
334127
YDOT = -13788
473013 feet/sec YDOT = -4161
888152 meter/sec
ZDOT = -17548
594121 ZDOT = -5331
070006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20277147
84 X = -6180474
66
Y = -2748347
45 feet Y = -837696
30 meter
Z = -8175618
21 Z = -2491928
43
XDOT = 8930
029794 XDOT = 2721
873081
YDOT = -14326
240316 feet/sec YDOT = -4366
638048 meter/sec
ZDOT = -17482
273387 ZDOT = -5328
596928
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 07118
45912613
00020000 00000-0 20000-3 0 9085
2 25544 51
6362
7867 0016901 113
0251 247
2699 15
78692668 2923
Satellite: ISS
Catalog Number: 25544
Epoch time: 07118
45912613 = yrday
fracday
Element set: 908
Inclination: 51
6362 deg
RA of node:
7867 deg
Eccentricity:
0016901
Arg of perigee: 113
0251 deg
Mean anomaly: 247
2699 deg
Mean motion: 15
78692668 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 292
Checksum: 300
Coasting Arc #10 (Orbit 291)
---------------------------------------
Vector Time (GMT): 2007/118/10:40:53
319
Vector Time (MET): N/A
Weight (LBS) : 479508
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1186780
67 A = 6713348
00 meter
Y = -4107205
79 meter E =
0022027
Z = -5194924
41 I = 51
61810
XDOT = 7568
623108 Wp = 109
84118
YDOT = 870
344212 meter/sec RA =
36956 deg
ZDOT = 1037
158279 TA = 170
08943
MA = 170
04592
Ha = 189
036 n
mi
Hp = 177
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3893637
37 X = 1257856
02
Y = -13475084
63 feet Y = -4093537
20 meter
Z = -17043715
24 Z = -5188986
30
XDOT = 24831
440644 XDOT = 7553
289911
YDOT = 2855
460012 feet/sec YDOT = 954
895075 meter/sec
ZDOT = 3402
750260 ZDOT = 1073
889664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 238815
46 X = 72790
95
Y = -14050852
25 feet Y = -4282699
77 meter
Z = -17021840
83 Z = -5188257
08
XDOT = 23647
120937 XDOT = 7207
642462
YDOT = -3903
113152 feet/sec YDOT = -1189
668889 meter/sec
ZDOT = 3541
204003 ZDOT = 1079
358980
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 07118
45912791
00020000 00000-0 20000-3 0 9093
2 25544 51
6363
7872 0008431 131
0694 229
1200 15
76511723 2927
Satellite: ISS
Catalog Number: 25544
Epoch time: 07118
45912791 = yrday
fracday
Element set: 909
Inclination: 51
6363 deg
RA of node:
7872 deg
Eccentricity:
0008431
Arg of perigee: 131
0694 deg
Mean anomaly: 229
1200 deg
Mean motion: 15
76511723 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 292
Checksum: 272
Coasting Arc #11 (Orbit 307)
---------------------------------------
Vector Time (GMT): 2007/119/10:40:53
319
Vector Time (MET): N/A
Weight (LBS) : 479508
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6430790
52 A = 6723663
74 meter
Y = -853282
44 meter E =
0015821
Z = -1747836
93 I = 51
62448
XDOT = 2163
460591 Wp = 138
41023
YDOT = -4710
609498 meter/sec RA = 355
23889 deg
ZDOT = -5701
243128 TA = 60
97060
MA = 60
81217
Ha = 188
906 n
mi
Hp = 177
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21098394
09 X = -6412280
26
Y = -2799483
07 feet Y = -925091
65 meter
Z = -5734373
12 Z = -1779033
12
XDOT = 7097
967817 XDOT = 2243
670457
YDOT = -15454
755571 feet/sec YDOT = -4685
968011 meter/sec
ZDOT = -18704
865907 ZDOT = -5690
538064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20993615
36 X = -6398853
96
Y = 3299228
82 feet Y = 1005604
94 meter
Z = -5851972
09 Z = -1783681
09
XDOT = 2756
588471 XDOT = 840
208166
YDOT = -15332
871519 feet/sec YDOT = -4673
459239 meter/sec
ZDOT = -18665
108533 ZDOT = -5689
125081
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 07119
47333448
00020000 00000-0 20000-3 0 9104
2 25544 51
6364 355
5586 0008398 136
1267 224
0566 15
76506516 3086
Satellite: ISS
Catalog Number: 25544
Epoch time: 07119
47333448 = yrday
fracday
Element set: 910
Inclination: 51
6364 deg
RA of node: 355
5586 deg
Eccentricity:
0008398
Arg of perigee: 136
1267 deg
Mean anomaly: 224
0566 deg
Mean motion: 15
76506516 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 308
Checksum: 302
Coasting Arc #12 (Orbit 323)
---------------------------------------
Vector Time (GMT): 2007/120/10:40:53
319
Vector Time (MET): N/A
Weight (LBS) : 479508
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2535472
74 A = 6715532
03 meter
Y = 4159392
34 meter E =
0013119
Z = 4610490
70 I = 51
56896
XDOT = -7065
758321 Wp = 100
81025
YDOT = -1092
335660 meter/sec RA = 350
04233 deg
ZDOT = -2895
745791 TA = 17
84684
MA = 17
80081
Ha = 188
741 n
mi
Hp = 177
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8318480
11 X = -2604192
52
Y = 13646300
33 feet Y = 4130654
98 meter
Z = 15126281
82 Z = 4598006
29
XDOT = -23181
621789 XDOT = -7038
951282
YDOT = -3583
778413 feet/sec YDOT = -1171
199014 meter/sec
ZDOT = -9500
478317 ZDOT = -2930
006699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3914006
27 X = -1192989
11
Y = 15540416
29 feet Y = 4736718
89 meter
Z = 15079756
03 Z = 4596309
64
XDOT = -22003
082959 XDOT = -6706
539686
YDOT = 3816
893388 feet/sec YDOT = 1163
389105 meter/sec
ZDOT = -9629
644264 ZDOT = -2935
115572
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 07120
48751986
00020000 00000-0 20000-3 0 9119
2 25544 51
6361 350
3302 0008163 138
9604 221
2176 15
76603722 3248
Satellite: ISS
Catalog Number: 25544
Epoch time: 07120
48751986 = yrday
fracday
Element set: 911
Inclination: 51
6361 deg
RA of node: 350
3302 deg
Eccentricity:
0008163
Arg of perigee: 138
9604 deg
Mean anomaly: 221
2176 deg
Mean motion: 15
76603722 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 324
Checksum: 269
Coasting Arc #13 (Orbit 339)
---------------------------------------
Vector Time (GMT): 2007/121/10:40:53
319
Vector Time (MET): N/A
Weight (LBS) : 479508
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5779420
71 A = 6720184
50 meter
Y = 1105142
56 meter E =
0018782
Z = 3237367
80 I = 51
55658
XDOT = -3609
640216 Wp = 108
34411
YDOT = 4877
572758 meter/sec RA = 344
92866 deg
ZDOT = 4750
687793 TA = 289
64139
MA = 289
84400
Ha = 188
618 n
mi
Hp = 177
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18961354
05 X = 5750906
45
Y = 3625795
81 feet Y = 1169611
76 meter
Z = 10621285
45 Z = 3265375
55
XDOT = -11842
651626 XDOT = -3686
992095
YDOT = 16002
535295 feet/sec YDOT = 4836
775109 meter/sec
ZDOT = 15586
246041 ZDOT = 4732
964065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19076748
92 X = 5814593
07
Y = -2549968
36 feet Y = -777230
36 meter
Z = 10726898
87 Z = 3269558
78
XDOT = -6430
488291 XDOT = -1960
012831
YDOT = 17566
583632 feet/sec YDOT = 5354
294691 meter/sec
ZDOT = 15520
070450 ZDOT = 4730
517473
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 07121
50168843
00020000 00000-0 20000-3 0 9128
2 25544 51
6361 345
1011 0008165 142
5173 217
6562 15
76582309 3404
Satellite: ISS
Catalog Number: 25544
Epoch time: 07121
50168843 = yrday
fracday
Element set: 912
Inclination: 51
6361 deg
RA of node: 345
1011 deg
Eccentricity:
0008165
Arg of perigee: 142
5173 deg
Mean anomaly: 217
6562 deg
Mean motion: 15
76582309 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 340
Checksum: 264
Coasting Arc #14 (Orbit 354)
---------------------------------------
Vector Time (GMT): 2007/122/10:40:53
319
Vector Time (MET): N/A
Weight (LBS) : 479508
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3696313
32 A = 6719322
90 meter
Y = -4365705
04 meter E =
0011968
Z = -3540254
53 I = 51
52625
XDOT = 6078
092233 Wp = 126
96383
YDOT = 1532
061674 meter/sec RA = 339
71420 deg
ZDOT = 4460
024791 TA = 190
79936
MA = 190
82508
Ha = 188
458 n
mi
Hp = 177
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12127012
22 X = 3762054
83
Y = -14323179
26 feet Y = -4324003
04 meter
Z = -11615008
31 Z = -3522137
98
XDOT = 19941
247482 XDOT = 6038
842305
YDOT = 5026
449062 feet/sec YDOT = 1599
810631 meter/sec
ZDOT = 14632
627266 ZDOT = 4489
457524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6724154
17 X = 2049522
19
Y = -17566222
10 feet Y = -5354184
49 meter
Z = -11547289
69 Z = -3519613
90
XDOT = 19118
495668 XDOT = 5827
317480
YDOT = -2366
387516 feet/sec YDOT = -721
274915 meter/sec
ZDOT = 14743
656031 ZDOT = 4493
866358
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 07122
45245152
00020000 00000-0 20000-3 0 9133
2 25544 51
6358 340
1987 0007998 147
3467 212
8193 15
76624538 3553
Satellite: ISS
Catalog Number: 25544
Epoch time: 07122
45245152 = yrday
fracday
Element set: 913
Inclination: 51
6358 deg
RA of node: 340
1987 deg
Eccentricity:
0007998
Arg of perigee: 147
3467 deg
Mean anomaly: 212
8193 deg
Mean motion: 15
76624538 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 355
Checksum: 308
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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