Date:
March 29th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5812 51 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
There are no maneuvers
Coasting Arc #1 (Orbit 3771)
---------------------------------------
Vector Time (GMT): 2007/085/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6644962
57 A = 6720793
31 meter
Y = 774787
11 meter E =
0024801
Z = 442821
09 I = 51
70752
XDOT = -153
711992 Wp = 18
83838
YDOT = -4808
774831 meter/sec RA = 170
35378 deg
ZDOT = 6037
117221 TA = 345
98887
MA = 346
05755
Ha = 187
678 n
mi
Hp = 175
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21801058
31 X = -6655283
61
Y = 2541952
45 feet Y = 700421
71 meter
Z = 1452825
11 Z = 410515
16
XDOT = -504
304437 XDOT = -129
255050
YDOT = -15776
820312 feet/sec YDOT = -4810
356944 meter/sec
ZDOT = 19806
815029 ZDOT = 6036
429930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21943741
05 X = -6688452
27
Y = 746960
94 feet Y = 227673
69 meter
Z = 1331406
99 Z = 405812
85
XDOT = 734
275856 XDOT = 223
807281
YDOT = -14174
166043 feet/sec YDOT = -4320
285810 meter/sec
ZDOT = 19803
553070 ZDOT = 6036
122976
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 07085
54172202
00020000 00000-0 20000-3 0 9002
2 25544 51
6340 171
0083 0015155 352
6057 7
4882 15
77991132 37729
Satellite: ISS
Catalog Number: 25544
Epoch time: 07085
54172202 = yrday
fracday
Element set: 900
Inclination: 51
6340 deg
RA of node: 171
0083 deg
Eccentricity:
0015155
Arg of perigee: 352
6057 deg
Mean anomaly: 7
4882 deg
Mean motion: 15
77991132 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3772
Checksum: 273
Coasting Arc #2 (Orbit 3786)
---------------------------------------
Vector Time (GMT): 2007/086/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1154992
13 A = 6709832
31 meter
Y = 4365584
67 meter E =
0016599
Z = -4969285
86 I = 51
69909
XDOT = -7425
855035 Wp = 44
98303
YDOT = 316
118069 meter/sec RA = 165
17234 deg
ZDOT = 2019
273209 TA = 244
44775
MA = 244
61945
Ha = 187
720 n
mi
Hp = 175
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3789344
25 X = -1179583
33
Y = 14322784
37 feet Y = 4352531
30 meter
Z = -16303431
29 Z = -4974956
55
XDOT = -24363
041453 XDOT = -7438
647134
YDOT = 1037
132771 feet/sec YDOT = 233
006523 meter/sec
ZDOT = 6624
912102 ZDOT = 1983
167844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4618239
25 X = -1407639
32
Y = 14053368
09 feet Y = 4283466
59 meter
Z = -16324149
75 Z = -4975600
84
XDOT = -23390
719026 XDOT = -7129
491159
YDOT = -208
401826 feet/sec YDOT = -63
520877 meter/sec
ZDOT = 6489
122546 ZDOT = 1977
884552
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 07086
49163528
00020000 00000-0 20000-3 0 9019
2 25544 51
6336 166
1012 0015159 356
3509 3
7543 15
78059523 37877
Satellite: ISS
Catalog Number: 25544
Epoch time: 07086
49163528 = yrday
fracday
Element set: 901
Inclination: 51
6336 deg
RA of node: 166
1012 deg
Eccentricity:
0015159
Arg of perigee: 356
3509 deg
Mean anomaly: 3
7543 deg
Mean motion: 15
78059523 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3787
Checksum: 298
Coasting Arc #3 (Orbit 3802)
---------------------------------------
Vector Time (GMT): 2007/087/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6018072
49 A = 6716830
06 meter
Y = 320347
41 meter E =
0014099
Z = -2986300
39 I = 51
74944
XDOT = -2751
092045 Wp = 17
85930
YDOT = 5176
542036 meter/sec RA = 160
05241 deg
ZDOT = -4981
798556 TA = 196
56944
MA = 196
61556
Ha = 187
855 n
mi
Hp = 175
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19744332
31 X = 6028549
73
Y = 1051008
56 feet Y = 387703
32 meter
Z = -9797573
46 Z = -2957039
61
XDOT = -9025
892536 XDOT = -2784
572109
YDOT = 16983
405629 feet/sec YDOT = 5145
590376 meter/sec
ZDOT = -16344
483452 ZDOT = -4995
244698
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19726158
09 X = 6012532
99
Y = 1991988
94 feet Y = 607158
23 meter
Z = -9687434
65 Z = -2952730
08
XDOT = -9587
464680 XDOT = -2922
259235
YDOT = 15100
729403 feet/sec YDOT = 4602
702322 meter/sec
ZDOT = -16394
342192 ZDOT = -4996
995500
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 07087
50485680
00020000 00000-0 20000-3 0 9029
2 25544 51
6330 160
8656 0015152
1985 359
9183 15
78065906 38038
Satellite: ISS
Catalog Number: 25544
Epoch time: 07087
50485680 = yrday
fracday
Element set: 902
Inclination: 51
6330 deg
RA of node: 160
8656 deg
Eccentricity:
0015152
Arg of perigee:
1985 deg
Mean anomaly: 359
9183 deg
Mean motion: 15
78065906 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3803
Checksum: 299
Coasting Arc #4 (Orbit 3818)
---------------------------------------
Vector Time (GMT): 2007/088/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3486868
48 A = 6715294
60 meter
Y = -4612620
93 meter E =
0020598
Z = 3418653
38 I = 51
77228
XDOT = 6068
051105 Wp = 41
29240
YDOT = 1154
214897 meter/sec RA = 154
84373 deg
ZDOT = -4600
952992 TA = 98
32681
MA = 98
09321
Ha = 187
938 n
mi
Hp = 174
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11439857
23 X = 3521581
36
Y = -15133270
78 feet Y = -4573434
51 meter
Z = 11216054
39 Z = 3435676
95
XDOT = 19908
304150 XDOT = 6077
043800
YDOT = 3786
794283 feet/sec YDOT = 1222
121231 meter/sec
ZDOT = -15094
990132 ZDOT = -4571
453054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11831914
32 X = 3606367
48
Y = -14780587
86 feet Y = -4505123
18 meter
Z = 11279455
66 Z = 3437978
09
XDOT = 18789
922814 XDOT = 5727
168474
YDOT = 3530
036892 feet/sec YDOT = 1075
955245 meter/sec
ZDOT = -14983
825263 ZDOT = -4567
069940
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 07088
51805575
00020000 00000-0 20000-3 0 9031
2 25544 51
6337 155
6298 0015369 4
0305 356
0982 15
78131370 38199
Satellite: ISS
Catalog Number: 25544
Epoch time: 07088
51805575 = yrday
fracday
Element set: 903
Inclination: 51
6337 deg
RA of node: 155
6298 deg
Eccentricity:
0015369
Arg of perigee: 4
0305 deg
Mean anomaly: 356
0982 deg
Mean motion: 15
78131370 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3819
Checksum: 302
Coasting Arc #5 (Orbit 3834)
---------------------------------------
Vector Time (GMT): 2007/089/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4372770
03 A = 6710556
95 meter
Y = -1783736
30 meter E =
0014381
Z = 4755396
42 I = 51
78151
XDOT = 4982
797303 Wp = 37
16247
YDOT = -5284
616748 meter/sec RA = 149
73266 deg
ZDOT = 2606
819583 TA = 27
41005
MA = 27
33426
Ha = 188
127 n
mi
Hp = 174
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14346358
36 X = -4375599
64
Y = -5852153
20 feet Y = -1832650
50 meter
Z = 15601694
28 Z = 4734147
01
XDOT = 16347
760182 XDOT = 5028
857002
YDOT = -17337
981457 feet/sec YDOT = -5228
638579 meter/sec
ZDOT = 8552
557687 ZDOT = 2631
138032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14354556
82 X = -4375268
92
Y = -6042260
01 feet Y = -1841680
85 meter
Z = 15521480
35 Z = 4730947
21
XDOT = 16086
636668 XDOT = 4903
206857
YDOT = -16074
708191 feet/sec YDOT = -4899
571057 meter/sec
ZDOT = 8643
316136 ZDOT = 2634
482758
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 07089
53123383
00020000 00000-0 20000-3 0 9045
2 25544 51
6334 150
3940 0015303 7
8647 352
2756 15
78156170 38350
Satellite: ISS
Catalog Number: 25544
Epoch time: 07089
53123383 = yrday
fracday
Element set: 904
Inclination: 51
6334 deg
RA of node: 150
3940 deg
Eccentricity:
0015303
Arg of perigee: 7
8647 deg
Mean anomaly: 352
2756 deg
Mean motion: 15
78156170 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3835
Checksum: 287
Coasting Arc #6 (Orbit 3849)
---------------------------------------
Vector Time (GMT): 2007/090/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4933299
50 A = 6720051
65 meter
Y = 4439557
45 meter E =
0024863
Z = -960750
33 I = 51
83677
XDOT = -3857
690315 Wp = 22
19737
YDOT = -3010
825480 meter/sec RA = 144
54785 deg
ZDOT = 5968
016221 TA = 327
30378
MA = 327
45745
Ha = 188
276 n
mi
Hp = 174
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16185365
81 X = -4977909
50
Y = 14565477
21 feet Y = 4384141
02 meter
Z = -3152068
02 Z = -984824
88
XDOT = -12656
464289 XDOT = -3852
727462
YDOT = -9878
036351 feet/sec YDOT = -3053
936057 meter/sec
ZDOT = 19580
105712 ZDOT = 5949
288018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16109085
07 X = -4910049
13
Y = 14630151
36 feet Y = 4459270
13 meter
Z = -3242032
55 Z = -988171
52
XDOT = -11737
953667 XDOT = -3577
728278
YDOT = -8652
327433 feet/sec YDOT = -2637
229402 meter/sec
ZDOT = 19509
202096 ZDOT = 5946
404799
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 07090
48106993
00020000 00000-0 20000-3 0 9050
2 25544 51
6327 145
4858 0015619 11
5906 348
5616 15
78121141 38505
Satellite: ISS
Catalog Number: 25544
Epoch time: 07090
48106993 = yrday
fracday
Element set: 905
Inclination: 51
6327 deg
RA of node: 145
4858 deg
Eccentricity:
0015619
Arg of perigee: 11
5906 deg
Mean anomaly: 348
5616 deg
Mean motion: 15
78121141 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3850
Checksum: 297
Coasting Arc #7 (Orbit 3865)
---------------------------------------
Vector Time (GMT): 2007/091/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2268533
18 A = 6708295
60 meter
Y = 3507740
89 meter E =
0023684
Z = -5264255
87 I = 51
81979
XDOT = -6083
924479 Wp = 54
12985
YDOT = 4682
753024 meter/sec RA = 139
39872 deg
ZDOT = 513
696695 TA = 220
65359
MA = 220
83064
Ha = 188
326 n
mi
Hp = 174
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7442694
16 X = 2254713
27
Y = 11508336
24 feet Y = 3533031
15 meter
Z = -17271180
68 Z = -5253269
24
XDOT = -19960
382149 XDOT = -6138
330968
YDOT = 15363
362939 feet/sec YDOT = 4614
415017 meter/sec
ZDOT = 1685
356612 ZDOT = 484
008486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7781140
94 X = 2371691
76
Y = 11346052
17 feet Y = 3458276
70 meter
Z = -17229339
14 Z = -5251502
57
XDOT = -18811
806538 XDOT = -5733
838633
YDOT = 15215
956453 feet/sec YDOT = 4637
823527 meter/sec
ZDOT = 1574
296557 ZDOT = 479
845590
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 07091
49420707
00020000 00000-0 20000-3 0 9065
2 25544 51
6322 140
2495 0015512 15
6850 344
4792 15
78178517 38661
Satellite: ISS
Catalog Number: 25544
Epoch time: 07091
49420707 = yrday
fracday
Element set: 906
Inclination: 51
6322 deg
RA of node: 140
2495 deg
Eccentricity:
0015512
Arg of perigee: 15
6850 deg
Mean anomaly: 344
4792 deg
Mean motion: 15
78178517 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3866
Checksum: 298
Coasting Arc #8 (Orbit 3881)
---------------------------------------
Vector Time (GMT): 2007/092/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5438599
55 A = 6718646
44 meter
Y = -3499179
42 meter E =
0013357
Z = -1850481
04 I = 51
87665
XDOT = 1312
457512 Wp = 48
27207
YDOT = 5029
900238 meter/sec RA = 134
26641 deg
ZDOT = -5671
428732 TA = 152
19663
MA = 152
12517
Ha = 188
366 n
mi
Hp = 173
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17843174
38 X = 5486313
00
Y = -11480247
44 feet Y = -3438095
33 meter
Z = -6071132
03 Z = -1823944
07
XDOT = 4305
962966 XDOT = 1283
665757
YDOT = 16502
297368 feet/sec YDOT = 5044
415419 meter/sec
ZDOT = -18607
049645 ZDOT = -5665
123148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17422687
15 X = 5310435
04
Y = -12158193
91 feet Y = -3705817
50 meter
Z = -5971757
77 Z = -1820191
77
XDOT = 4153
404937 XDOT = 1265
957825
YDOT = 15050
498924 feet/sec YDOT = 4587
392072 meter/sec
ZDOT = -18582
611668 ZDOT = -5663
980036
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 07092
50732210
00020000 00000-0 20000-3 0 9074
2 25544 51
6325 135
0126 0015664 20
2363 339
9420 15
78253078 38827
Satellite: ISS
Catalog Number: 25544
Epoch time: 07092
50732210 = yrday
fracday
Element set: 907
Inclination: 51
6325 deg
RA of node: 135
0126 deg
Eccentricity:
0015664
Arg of perigee: 20
2363 deg
Mean anomaly: 339
9420 deg
Mean motion: 15
78253078 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3882
Checksum: 273
Coasting Arc #9 (Orbit 3897)
---------------------------------------
Vector Time (GMT): 2007/093/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -100528
43 A = 6712026
89 meter
Y = -5182504
09 meter E =
0023410
Z = 4261425
14 I = 51
87313
XDOT = 6102
406107 Wp = 42
32385
YDOT = -3074
655262 meter/sec RA = 129
07276 deg
ZDOT = -3567
020612 TA = 83
84346
MA = 83
57680
Ha = 188
380 n
mi
Hp = 173
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -329817
70 X = -63270
84
Y = -17002966
18 feet Y = -5183419
64 meter
Z = 13981053
60 Z = 4261027
63
XDOT = 20021
017413 XDOT = 6153
661870
YDOT = -10087
451647 feet/sec YDOT = -3006
128407 meter/sec
ZDOT = -11702
823530 ZDOT = -3537
250191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1352152
48 X = -412136
08
Y = -16954155
39 feet Y = -5167626
56 meter
Z = 13978833
90 Z = 4260748
57
XDOT = 18257
840178 XDOT = 5564
989686
YDOT = -11089
585350 feet/sec YDOT = -3380
105615 meter/sec
ZDOT = -11591
214289 ZDOT = -3533
002115
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 07093
52041416
00020000 00000-0 20000-3 0 9089
2 25544 51
6317 129
7759 0015673 23
6710 336
5173 15
78303499 38981
Satellite: ISS
Catalog Number: 25544
Epoch time: 07093
52041416 = yrday
fracday
Element set: 908
Inclination: 51
6317 deg
RA of node: 129
7759 deg
Eccentricity:
0015673
Arg of perigee: 23
6710 deg
Mean anomaly: 336
5173 deg
Mean motion: 15
78303499 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3898
Checksum: 312
Coasting Arc #10 (Orbit 3913)
---------------------------------------
Vector Time (GMT): 2007/094/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5012158
31 A = 6712575
53 meter
Y = 1642620
20 meter E =
0020926
Z = 4129334
43 I = 51
89149
XDOT = 925
569560 Wp = 57
62537
YDOT = -6672
470553 meter/sec RA = 123
97143 deg
ZDOT = 3774
955676 TA = 353
95151
MA = 353
97674
Ha = 188
653 n
mi
Hp = 173
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16444088
93 X = -5050213
58
Y = 5389173
89 feet Y = 1586358
89 meter
Z = 13547685
13 Z = 4104892
58
XDOT = 3036
645537 XDOT = 981
775050
YDOT = -21891
307588 feet/sec YDOT = -6661
805852 meter/sec
ZDOT = 12385
025185 ZDOT = 3779
589024
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16083476
60 X = -4902243
67
Y = 6576543
16 feet Y = 2004530
36 meter
Z = 13455923
93 Z = 4101365
61
XDOT = 1846
714409 XDOT = 562
878552
YDOT = -20876
485487 feet/sec YDOT = -6363
152777 meter/sec
ZDOT = 12401
540455 ZDOT = 3779
989531
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 07094
53348666
00020000 00000-0 20000-3 0 9099
2 25544 51
6312 124
5387 0015761 28
4915 331
7109 15
78303501 39143
Satellite: ISS
Catalog Number: 25544
Epoch time: 07094
53348666 = yrday
fracday
Element set: 909
Inclination: 51
6312 deg
RA of node: 124
5387 deg
Eccentricity:
0015761
Arg of perigee: 28
4915 deg
Mean anomaly: 331
7109 deg
Mean motion: 15
78303501 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3914
Checksum: 294
Coasting Arc #11 (Orbit 3928)
---------------------------------------
Vector Time (GMT): 2007/095/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1566332
63 A = 6717919
22 meter
Y = 6192985
28 meter E =
0022237
Z = -2053316
18 I = 51
92619
XDOT = -5280
474941 Wp = 34
70263
YDOT = 504
843535 meter/sec RA = 118
77762 deg
ZDOT = 5598
011282 TA = 302
42197
MA = 302
63687
Ha = 188
495 n
mi
Hp = 172
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5138886
59 X = -1625492
31
Y = 20318193
18 feet Y = 6175138
83 meter
Z = -6736601
65 Z = -2061069
43
XDOT = -17324
392852 XDOT = -5312
922175
YDOT = 1656
310809 feet/sec YDOT = 445
613073 meter/sec
ZDOT = 18366
178746 ZDOT = 5572
279593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3254118
80 X = -991855
41
Y = 20694571
29 feet Y = 6307705
33 meter
Z = -6764936
14 Z = -2061952
54
XDOT = -15697
930590 XDOT = -4784
729244
YDOT = 3453
277549 feet/sec YDOT = 1052
558997 meter/sec
ZDOT = 18269
400327 ZDOT = 5568
513220
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 07095
48322075
00020000 00000-0 20000-3 0 9102
2 25544 51
6322 119
6295 0015724 32
0353 328
1765 15
78364207 39297
Satellite: ISS
Catalog Number: 25544
Epoch time: 07095
48322075 = yrday
fracday
Element set: 910
Inclination: 51
6322 deg
RA of node: 119
6295 deg
Eccentricity:
0015724
Arg of perigee: 32
0353 deg
Mean anomaly: 328
1765 deg
Mean motion: 15
78364207 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3929
Checksum: 291
Coasting Arc #12 (Orbit 3944)
---------------------------------------
Vector Time (GMT): 2007/096/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4095838
08 A = 6707907
56 meter
Y = 916121
59 meter E =
0027787
Z = -5254497
01 I = 51
90506
XDOT = -2548
389996 Wp = 59
28397
YDOT = 7218
959370 meter/sec RA = 113
65283 deg
ZDOT = -716
739583 TA = 203
84907
MA = 203
97806
Ha = 188
593 n
mi
Hp = 172
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13437788
96 X = 4110815
16
Y = 3005648
27 feet Y = 962007
22 meter
Z = -17239163
43 Z = -5234562
83
XDOT = -8360
859566 XDOT = -2625
442204
YDOT = 23684
249901 feet/sec YDOT = 7190
031017 meter/sec
ZDOT = -2351
507817 ZDOT = -729
307060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13777563
68 X = 4199401
41
Y = 1540265
73 feet Y = 469473
00 meter
Z = -17164007
99 Z = -5231589
63
XDOT = -5652
845494 XDOT = -1722
987307
YDOT = 23436
897970 feet/sec YDOT = 7143
566501 meter/sec
ZDOT = -2397
835856 ZDOT = -730
860369
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 07096
49624869
00020000 00000-0 20000-3 0 9111
2 25544 51
6324 114
3921 0015709 35
5740 324
6470 15
78355910 39451
Satellite: ISS
Catalog Number: 25544
Epoch time: 07096
49624869 = yrday
fracday
Element set: 911
Inclination: 51
6324 deg
RA of node: 114
3921 deg
Eccentricity:
0015709
Arg of perigee: 35
5740 deg
Mean anomaly: 324
6470 deg
Mean motion: 15
78355910 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3945
Checksum: 304
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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