Date:
November 3rd 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4036 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 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 3257)
---------------------------------------
Vector Time (GMT): 2007/306/09:03:21
019
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4371724
61 A = 6721416
09 meter
Y = -3611873
10 meter E =
0006320
Z = -3611662
04 I = 51
94146
XDOT = 1410
719943 Wp = 107
83792
YDOT = 6133
352038 meter/sec RA = 110
52659 deg
ZDOT = -4434
308145 TA = 115
18193
MA = 115
11637
Ha = 187
817 n
mi
Hp = 180
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14342928
51 X = 4429333
20
Y = -11849977
35 feet Y = -3562663
83 meter
Z = -11849284
90 Z = -3590284
09
XDOT = 4628
346271 XDOT = 1363
572337
YDOT = 20122
546056 feet/sec YDOT = 6148
863969 meter/sec
ZDOT = -14548
255070 ZDOT = -4427
569206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15132887
52 X = -4612504
12
Y = 10910936
55 feet Y = 3325653
46 meter
Z = -11768359
82 Z = -3586996
07
XDOT = -2627
170016 XDOT = -800
761421
YDOT = -19277
598875 feet/sec YDOT = -5875
812137 meter/sec
ZDOT = -14521
882076 ZDOT = -4426
269657
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 07306
40151928
00020000 00000-0 20000-3 0 9005
2 25544 51
6377 111
2061 0002792 166
7845 193
3393 15
75813177 32584
Satellite: ISS
Catalog Number: 25544
Epoch time: 07306
40151928 = yrday
fracday
Element set: 900
Inclination: 51
6377 deg
RA of node: 111
2061 deg
Eccentricity:
0002792
Arg of perigee: 166
7845 deg
Mean anomaly: 193
3393 deg
Mean motion: 15
75813177 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3258
Checksum: 291
Coasting Arc #2 (Orbit 3273)
---------------------------------------
Vector Time (GMT): 2007/307/09:03:21
019
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1218562
51 A = 6721747
68 meter
Y = -5652884
24 meter E =
0013096
Z = 3413166
58 I = 51
95280
XDOT = 4814
949598 Wp = 100
96124
YDOT = -3843
061246 meter/sec RA = 105
34659 deg
ZDOT = -4633
408426 TA = 38
83891
MA = 38
74487
Ha = 187
586 n
mi
Hp = 180
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3997908
51 X = -1171841
30
Y = -18546208
15 feet Y = -5666249
67 meter
Z = 11198053
09 Z = 3407360
22
XDOT = 15797
078733 XDOT = 4880
073979
YDOT = -12608
468656 feet/sec YDOT = -3788
853624 meter/sec
ZDOT = -15201
471214 ZDOT = -4609
858912
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3197318
28 X = 974542
61
Y = 18714476
16 feet Y = 5704172
33 meter
Z = 11175287
02 Z = 3406227
48
XDOT = -15084
853257 XDOT = -4597
863273
YDOT = 11625
895036 feet/sec YDOT = 3543
572807 meter/sec
ZDOT = -15112
303711 ZDOT = -4606
230171
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 07307
41616749
00020000 00000-0 20000-3 0 9015
2 25544 51
6382 105
9803 0002601 172
2165 187
9040 15
75889042 32740
Satellite: ISS
Catalog Number: 25544
Epoch time: 07307
41616749 = yrday
fracday
Element set: 901
Inclination: 51
6382 deg
RA of node: 105
9803 deg
Eccentricity:
0002601
Arg of perigee: 172
2165 deg
Mean anomaly: 187
9040 deg
Mean motion: 15
75889042 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3274
Checksum: 287
Coasting Arc #3 (Orbit 3289)
---------------------------------------
Vector Time (GMT): 2007/308/09:03:21
019
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4057735
58 A = 6718530
51 meter
Y = 3029773
89 meter E =
0010804
Z = 4410795
36 I = 51
94648
XDOT = -1427
939127 Wp = 123
13824
YDOT = -6794
897324 meter/sec RA = 100
26729 deg
ZDOT = 3342
143076 TA = 293
38325
MA = 293
49684
Ha = 187
673 n
mi
Hp = 180
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13312780
78 X = -4112740
58
Y = 9940203
07 feet Y = 2984090
50 meter
Z = 14471113
39 Z = 4390948
92
XDOT = -4684
839655 XDOT = -1368
087221
YDOT = -22292
970224 feet/sec YDOT = -6810
530658 meter/sec
ZDOT = 10965
036337 ZDOT = 3335
351503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13678043
30 X = 4169067
60
Y = -9545626
44 feet Y = -2909506
94 meter
Z = 14395938
30 Z = 4387881
99
XDOT = 3398
819634 XDOT = 1035
960224
YDOT = 21424
439585 feet/sec YDOT = 6530
169185 meter/sec
ZDOT = 10938
388876 ZDOT = 3334
020929
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 07308
43080288
00020000 00000-0 20000-3 0 9022
2 25544 51
6368 100
7540 0002628 173
9676 186
1520 15
75847401 32904
Satellite: ISS
Catalog Number: 25544
Epoch time: 07308
43080288 = yrday
fracday
Element set: 902
Inclination: 51
6368 deg
RA of node: 100
7540 deg
Eccentricity:
0002628
Arg of perigee: 173
9676 deg
Mean anomaly: 186
1520 deg
Mean motion: 15
75847401 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3290
Checksum: 288
Coasting Arc #4 (Orbit 3304)
---------------------------------------
Vector Time (GMT): 2007/309/09:03:21
019
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1305247
62 A = 6724364
20 meter
Y = 6159836
22 meter E =
0004336
Z = -2361510
28 I = 51
96981
XDOT = -4534
108502 Wp = 73
69839
YDOT = 3038
599178 meter/sec RA = 95
09395 deg
ZDOT = 5429
253336 TA = 259
82628
MA = 259
87519
Ha = 187
474 n
mi
Hp = 180
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4282308
45 X = 1247742
41
Y = 20209436
41 feet Y = 6174110
67 meter
Z = -7747737
13 Z = -2355309
04
XDOT = -14875
684062 XDOT = -4594
124462
YDOT = 9969
157407 feet/sec YDOT = 2987
560735 meter/sec
ZDOT = 17812
510945 ZDOT = 5407
080353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4084242
62 X = -1244877
15
Y = -20259682
15 feet Y = -6175151
12 meter
Z = -7723416
20 Z = -2354097
26
XDOT = 13616
396091 XDOT = 4150
277528
YDOT = -9491
719196 feet/sec YDOT = -2893
076011 meter/sec
ZDOT = 17728
478238 ZDOT = 5403
640167
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 07309
38200548
00020000 00000-0 20000-3 0 9031
2 25544 51
6361 95
8540 0002767 177
9475 182
1701 15
75896742 33052
Satellite: ISS
Catalog Number: 25544
Epoch time: 07309
38200548 = yrday
fracday
Element set: 903
Inclination: 51
6361 deg
RA of node: 95
8540 deg
Eccentricity:
0002767
Arg of perigee: 177
9475 deg
Mean anomaly: 182
1701 deg
Mean motion: 15
75896742 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3305
Checksum: 305
Coasting Arc #5 (Orbit 3320)
---------------------------------------
Vector Time (GMT): 2007/310/09:03:21
019
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3912611
24 A = 6715938
93 meter
Y = -2220447
25 meter E =
0012615
Z = -4997403
72 I = 51
94237
XDOT = 1567
781619 Wp = 87
29602
YDOT = 7262
111879 meter/sec RA = 90
00284 deg
ZDOT = -2002
972885 TA = 163
41985
MA = 163
37856
Ha = 187
429 n
mi
Hp = 180
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12836651
05 X = 3961426
91
Y = -7284931
92 feet Y = -2176421
34 meter
Z = -16395681
49 Z = -4978277
17
XDOT = 5143
640482 XDOT = 1496
189390
YDOT = 23825
826375 feet/sec YDOT = 7279
243383 meter/sec
ZDOT = -6571
433350 ZDOT = -1995
530409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12890297
86 X = -3928962
79
Y = 7352781
99 feet Y = 2241127
95 meter
Z = -16323144
09 Z = -4975294
32
XDOT = -4769
663877 XDOT = -1453
793550
YDOT = -22858
293421 feet/sec YDOT = -6967
207835 meter/sec
ZDOT = -6542
267999 ZDOT = -1994
083286
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 07310
39660670
00020000 00000-0 20000-3 0 9041
2 25544 51
6356 90
6281 0002730 179
0989 181
0181 15
75923937 33219
Satellite: ISS
Catalog Number: 25544
Epoch time: 07310
39660670 = yrday
fracday
Element set: 904
Inclination: 51
6356 deg
RA of node: 90
6281 deg
Eccentricity:
0002730
Arg of perigee: 179
0989 deg
Mean anomaly: 181
0181 deg
Mean motion: 15
75923937 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3321
Checksum: 292
Coasting Arc #6 (Orbit 3336)
---------------------------------------
Vector Time (GMT): 2007/311/09:03:21
019
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1452583
77 A = 6725983
05 meter
Y = -6464673
48 meter E =
0015076
Z = 1107701
60 I = 51
97632
XDOT = 4477
475272 Wp = 131
55273
YDOT = -2030
345990 meter/sec RA = 84
84774 deg
ZDOT = -5936
065517 TA = 36
36498
MA = 36
26265
Ha = 187
156 n
mi
Hp = 180
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4765694
77 X = -1385568
02
Y = -21209558
67 feet Y = -6480542
39 meter
Z = 3634191
60 Z = 1100807
54
XDOT = 14689
879500 XDOT = 4528
683301
YDOT = -6661
240124 feet/sec YDOT = -1979
990015 meter/sec
ZDOT = -19475
280568 ZDOT = -5914
188919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5261266
07 X = 1603633
90
Y = 21096721
37 feet Y = 6430280
67 meter
Z = 3607215
13 Z = 1099479
17
XDOT = -13107
600002 XDOT = -3995
196481
YDOT = 6608
238726 feet/sec YDOT = 2014
191164 meter/sec
ZDOT = -19392
250630 ZDOT = -5910
757992
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 07311
41118902
00020000 00000-0 20000-3 0 9052
2 25544 51
6363 85
4018 0002472 187
3856 172
7272 15
75995968 33373
Satellite: ISS
Catalog Number: 25544
Epoch time: 07311
41118902 = yrday
fracday
Element set: 905
Inclination: 51
6363 deg
RA of node: 85
4018 deg
Eccentricity:
0002472
Arg of perigee: 187
3856 deg
Mean anomaly: 172
7272 deg
Mean motion: 15
75995968 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3337
Checksum: 307
Coasting Arc #7 (Orbit 3352)
---------------------------------------
Vector Time (GMT): 2007/312/09:03:21
019
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3954307
32 A = 6714699
71 meter
Y = 1306252
77 meter E =
0004354
Z = 5265565
23 I = 51
93322
XDOT = -1770
874241 Wp = 147
48452
YDOT = -7481
808407 meter/sec RA = 79
73381 deg
ZDOT = 522
372604 TA = 297
55411
MA = 297
59833
Ha = 187
426 n
mi
Hp = 180
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12973449
20 X = -3994200
12
Y = 4285606
20 feet Y = 1261810
33 meter
Z = 17275476
48 Z = 5246257
71
XDOT = -5809
954859 XDOT = -1689
617586
YDOT = -24546
615507 feet/sec YDOT = -7501
157005 meter/sec
ZDOT = 1713
820880 ZDOT = 513
966684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12890332
57 X = 3928973
37
Y = -4800485
03 feet Y = -1463187
84 meter
Z = 17202138
30 Z = 5243211
75
XDOT = 6438
265286 XDOT = 1962
383259
YDOT = 23356
566227 feet/sec YDOT = 7119
081386 meter/sec
ZDOT = 1680
986635 ZDOT = 512
364726
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 07312
42575945
00020000 00000-0 20000-3 0 9069
2 25544 51
6358 80
1753 0002643 184
7311 175
3829 15
75926373 33531
Satellite: ISS
Catalog Number: 25544
Epoch time: 07312
42575945 = yrday
fracday
Element set: 906
Inclination: 51
6358 deg
RA of node: 80
1753 deg
Eccentricity:
0002643
Arg of perigee: 184
7311 deg
Mean anomaly: 175
3829 deg
Mean motion: 15
75926373 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3353
Checksum: 302
Coasting Arc #8 (Orbit 3368)
---------------------------------------
Vector Time (GMT): 2007/313/09:03:21
019
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1621032
75 A = 6726461
46 meter
Y = 6520314
37 meter E =
0010677
Z = 215300
07 I = 51
96791
XDOT = -4656
348675 Wp = 56
44453
YDOT = 950
595986 meter/sec RA = 74
60234 deg
ZDOT = 6061
986941 TA = 305
88587
MA = 305
98495
Ha = 187
129 n
mi
Hp = 180
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5318348
91 X = 1546955
20
Y = 21392107
50 feet Y = 6538027
48 meter
Z = 706365
07 Z = 222995
60
XDOT = -15276
734499 XDOT = -4696
081335
YDOT = 3118
753236 feet/sec YDOT = 898
303688 meter/sec
ZDOT = 19888
408598 ZDOT = 6039
269158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6521545
16 X = -1987766
96
Y = -21055480
26 feet Y = -6417710
38 meter
Z = 736376
11 Z = 224447
44
XDOT = 13651
004914 XDOT = 4160
826298
YDOT = -3512
722925 feet/sec YDOT = -1070
677947 meter/sec
ZDOT = 19802
046851 ZDOT = 6035
663880
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 07313
44030810
00020000 00000-0 20000-3 0 9070
2 25544 51
6365 74
9488 0002743 189
5297 170
5816 15
76005356 33692
Satellite: ISS
Catalog Number: 25544
Epoch time: 07313
44030810 = yrday
fracday
Element set: 907
Inclination: 51
6365 deg
RA of node: 74
9488 deg
Eccentricity:
0002743
Arg of perigee: 189
5297 deg
Mean anomaly: 170
5816 deg
Mean motion: 15
76005356 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3369
Checksum: 304
Coasting Arc #9 (Orbit 3383)
---------------------------------------
Vector Time (GMT): 2007/314/09:03:21
019
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4231168
97 A = 6714698
41 meter
Y = -351962
63 meter E =
0014632
Z = -5214502
03 I = 51
92023
XDOT = 1896
961071 Wp = 108
55922
YDOT = 7383
330964 meter/sec RA = 69
46234 deg
ZDOT = 1038
695118 TA = 171
32934
MA = 171
30403
Ha = 187
065 n
mi
Hp = 180
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13881787
94 X = 4260122
15
Y = -1154733
05 feet Y = -304485
13 meter
Z = -17107946
29 Z = -5193876
01
XDOT = 6223
625560 XDOT = 1809
212599
YDOT = 24223
526785 feet/sec YDOT = 7404
053173 meter/sec
ZDOT = 3407
792382 ZDOT = 1047
698127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13854168
98 X = -4222750
70
Y = 2185910
76 feet Y = 666265
60 meter
Z = -17029476
43 Z = -5190584
42
XDOT = -7820
495739 XDOT = -2383
687101
YDOT = -22687
708169 feet/sec YDOT = -6915
213450 meter/sec
ZDOT = 3442
862739 ZDOT = 1049
384563
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 07314
39143400
00020000 00000-0 20000-3 0 9086
2 25544 51
6373 70
0500 0002700 190
4747 169
6361 15
76026920 33848
Satellite: ISS
Catalog Number: 25544
Epoch time: 07314
39143400 = yrday
fracday
Element set: 908
Inclination: 51
6373 deg
RA of node: 70
0500 deg
Eccentricity:
0002700
Arg of perigee: 190
4747 deg
Mean anomaly: 169
6361 deg
Mean motion: 15
76026920 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3384
Checksum: 266
Coasting Arc #10 (Orbit 3399)
---------------------------------------
Vector Time (GMT): 2007/315/09:03:21
019
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1650785
12 A = 6725150
57 meter
Y = -6317120
04 meter E =
0009711
Z = -1591386
37 I = 51
94485
XDOT = 5084
478114 Wp = 154
29603
YDOT = 123
670800 meter/sec RA = 64
35540 deg
ZDOT = -5786
790767 TA = 43
20539
MA = 43
12925
Ha = 186
872 n
mi
Hp = 180
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5415961
69 X = -1572292
53
Y = -20725459
45 feet Y = -6335141
06 meter
Z = -5221083
90 Z = -1599215
95
XDOT = 16681
358643 XDOT = 5110
829389
YDOT = 405
744096 feet/sec YDOT = 180
676086 meter/sec
ZDOT = -18985
534012 ZDOT = -5762
025568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7253056
49 X = 2210731
62
Y = 20148232
97 feet Y = 6141181
41 meter
Z = -5251562
34 Z = -1600676
20
XDOT = -15285
929013 XDOT = -4659
151163
YDOT = 597
141509 feet/sec YDOT = 182
008732 meter/sec
ZDOT = -18891
253311 ZDOT = -5758
054009
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 07315
40595044
00020000 00000-0 20000-3 0 9095
2 25544 51
6375 64
8235 0002475 196
1210 163
9876 15
76078811 34006
Satellite: ISS
Catalog Number: 25544
Epoch time: 07315
40595044 = yrday
fracday
Element set: 909
Inclination: 51
6375 deg
RA of node: 64
8235 deg
Eccentricity:
0002475
Arg of perigee: 196
1210 deg
Mean anomaly: 163
9876 deg
Mean motion: 15
76078811 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3400
Checksum: 293
Coasting Arc #11 (Orbit 3415)
---------------------------------------
Vector Time (GMT): 2007/316/09:03:21
019
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4679428
07 A = 6716480
42 meter
Y = -521134
93 meter E =
0005781
Z = 4785456
55 I = 51
90156
XDOT = -1847
185731 Wp = 78
49281
YDOT = -7028
197910 meter/sec RA = 59
18932 deg
ZDOT = -2567
904880 TA = 36
57512
MA = 36
53567
Ha = 187
058 n
mi
Hp = 180
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15352454
29 X = -4696500
42
Y = -1709760
26 feet Y = -573558
83 meter
Z = 15700316
77 Z = 4762681
72
XDOT = -6060
320639 XDOT = -1755
983297
YDOT = -23058
392093 feet/sec YDOT = -7048
344013 meter/sec
ZDOT = -8424
884778 ZDOT = -2576
657873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15535020
18 X = 4735074
15
Y = 28122
50 feet Y = 8571
74 meter
Z = 15613565
79 Z = 4759014
85
XDOT = 8475
790272 XDOT = 2583
420875
YDOT = 21139
070000 feet/sec YDOT = 6443
188536 meter/sec
ZDOT = -8458
945248 ZDOT = -2578
286512
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 07316
42045244
00020000 00000-0 20000-3 0 9102
2 25544 51
6376 59
5975 0002617 197
1555 162
9521 15
76043295 34161
Satellite: ISS
Catalog Number: 25544
Epoch time: 07316
42045244 = yrday
fracday
Element set: 910
Inclination: 51
6376 deg
RA of node: 59
5975 deg
Eccentricity:
0002617
Arg of perigee: 197
1555 deg
Mean anomaly: 162
9521 deg
Mean motion: 15
76043295 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3416
Checksum: 295
Coasting Arc #12 (Orbit 3431)
---------------------------------------
Vector Time (GMT): 2007/317/09:03:21
019
Vector Time (MET): N/A
Weight (LBS) : 540904
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1503353
65 A = 6722558
22 meter
Y = 5892934
08 meter E =
0012280
Z = 2854583
33 I = 51
90827
XDOT = -5682
114771 Wp = 91
58307
YDOT = -1030
605280 meter/sec RA = 54
10061 deg
ZDOT = 5100
960981 TA = 301
09230
MA = 301
21274
Ha = 186
686 n
mi
Hp = 180
836
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4932262
63 X = 1423478
84
Y = 19333773
23 feet Y = 5909298
54 meter
Z = 9365430
86 Z = 2861693
38
XDOT = -18642
108829 XDOT = -5694
948238
YDOT = -3381
250918 feet/sec YDOT = -1094
218177 meter/sec
ZDOT = 16735
436289 ZDOT = 5073
325299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7264323
94 X = -2214165
94
Y = -18569661
86 feet Y = -5660032
94 meter
Z = 9393112
00 Z = 2863020
54
XDOT = 17658
048988 XDOT = 5382
173332
YDOT = 1535
857925 feet/sec YDOT = 468
129496 meter/sec
ZDOT = 16630
122879 ZDOT = 5068
861454
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 07317
43493380
00020000 00000-0 20000-3 0 9113
2 25544 51
6388 54
3715 0002647 203
3099 156
7945 15
76129580 34326
Satellite: ISS
Catalog Number: 25544
Epoch time: 07317
43493380 = yrday
fracday
Element set: 911
Inclination: 51
6388 deg
RA of node: 54
3715 deg
Eccentricity:
0002647
Arg of perigee: 203
3099 deg
Mean anomaly: 156
7945 deg
Mean motion: 15
76129580 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3432
Checksum: 301
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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