Date:
April 9th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6189 25 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 3913)
---------------------------------------
Vector Time (GMT): 2007/094/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4966436
60 A = 6711543
35 meter
Y = 1356064
17 meter E =
0020004
Z = 4284930
88 I = 51
89009
XDOT = 1207
635243 Wp = 57
44084
YDOT = -6757
218579 meter/sec RA = 123
97134 deg
ZDOT = 3536
901120 TA = 356
95281
MA = 356
96497
Ha = 188
389 n
mi
Hp = 172
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16294083
33 X = -5002046
83
Y = 4449029
42 feet Y = 1300327
82 meter
Z = 14058172
17 Z = 4260717
11
XDOT = 3962
057884 XDOT = 1265
923872
YDOT = -22169
352292 feet/sec YDOT = -6743
388027 meter/sec
ZDOT = 11604
006300 ZDOT = 3542
909821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16005102
70 X = -4878355
30
Y = 5628179
18 feet Y = 1715469
01 meter
Z = 13967229
71 Z = 4257211
62
XDOT = 2684
616480 XDOT = 818
271103
YDOT = -21227
140285 feet/sec YDOT = -6470
032359 meter/sec
ZDOT = 11625
686079 ZDOT = 3543
509117
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
53298785
00020000 00000-0 20000-3 0 9006
2 25544 51
6317 124
5423 0015713 28
3374 331
8643 15
78464849 39141
Satellite: ISS
Catalog Number: 25544
Epoch time: 07094
53298785 = yrday
fracday
Element set: 900
Inclination: 51
6317 deg
RA of node: 124
5423 deg
Eccentricity:
0015713
Arg of perigee: 28
3374 deg
Mean anomaly: 331
8643 deg
Mean motion: 15
78464849 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3914
Checksum: 309
Coasting Arc #2 (Orbit 3928)
---------------------------------------
Vector Time (GMT): 2007/095/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1835053
92 A = 6717962
57 meter
Y = 6207604
72 meter E =
0023150
Z = -1762005
28 I = 51
92831
XDOT = -5165
126410 Wp = 33
99089
YDOT = 83
554742 meter/sec RA = 118
77931 deg
ZDOT = 5728
190998 TA = 306
51996
MA = 306
73294
Ha = 188
237 n
mi
Hp = 172
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6020518
10 X = -1895772
25
Y = 20366157
22 feet Y = 6186744
57 meter
Z = -5780857
21 Z = -1771067
77
XDOT = -16945
952789 XDOT = -5193
503702
YDOT = 274
129730 feet/sec YDOT = 25
636932 meter/sec
ZDOT = 18793
277552 ZDOT = 5703
029579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4133158
86 X = -1259786
82
Y = 20822063
90 feet Y = 6346565
08 meter
Z = -5814117
38 Z = -1772142
98
XDOT = -15438
352607 XDOT = -4705
609875
YDOT = 2106
983808 feet/sec YDOT = 642
208665 meter/sec
ZDOT = 18698
587880 ZDOT = 5699
329586
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
48262544
00020000 00000-0 20000-3 0 9016
2 25544 51
6326 119
6324 0015691 31
8247 328
3864 15
78521124 39291
Satellite: ISS
Catalog Number: 25544
Epoch time: 07095
48262544 = yrday
fracday
Element set: 901
Inclination: 51
6326 deg
RA of node: 119
6324 deg
Eccentricity:
0015691
Arg of perigee: 31
8247 deg
Mean anomaly: 328
3864 deg
Mean motion: 15
78521124 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3929
Checksum: 299
Coasting Arc #3 (Orbit 3944)
---------------------------------------
Vector Time (GMT): 2007/096/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3931937
36 A = 6707292
64 meter
Y = 1349518
89 meter E =
0027583
Z = -5284834
06 I = 51
90511
XDOT = -2865
620837 Wp = 61
00213
YDOT = 7129
721764 meter/sec RA = 113
64755 deg
ZDOT = -299
511205 TA = 206
09143
MA = 206
23070
Ha = 188
327 n
mi
Hp = 172
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12900056
96 X = 3942227
69
Y = 4427555
43 feet Y = 1393545
49 meter
Z = -17338694
42 Z = -5265707
50
XDOT = -9401
643165 XDOT = -2943
678444
YDOT = 23391
475603 feet/sec YDOT = 7097
240342 meter/sec
ZDOT = -982
648310 ZDOT = -313
622249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13395642
14 X = 4082991
73
Y = 3011492
86 feet Y = 917903
02 meter
Z = -17266520
29 Z = -5262835
38
XDOT = -6619
266919 XDOT = -2017
552557
YDOT = 23285
834830 feet/sec YDOT = 7097
522456 meter/sec
ZDOT = -1034
798350 ZDOT = -315
406537
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
49554799
00020000 00000-0 20000-3 0 9025
2 25544 51
6329 114
3943 0015674 35
4196 324
8008 15
78520727 39454
Satellite: ISS
Catalog Number: 25544
Epoch time: 07096
49554799 = yrday
fracday
Element set: 902
Inclination: 51
6329 deg
RA of node: 114
3943 deg
Eccentricity:
0015674
Arg of perigee: 35
4196 deg
Mean anomaly: 324
8008 deg
Mean motion: 15
78520727 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3945
Checksum: 321
Coasting Arc #4 (Orbit 3960)
---------------------------------------
Vector Time (GMT): 2007/097/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3023347
02 A = 6718478
88 meter
Y = -5867374
91 meter E =
0016293
Z = -1283713
94 I = 51
95298
XDOT = 3776
281933 Wp = 72
54384
YDOT = 3220
470966 meter/sec RA = 108
50633 deg
ZDOT = -5881
887870 TA = 121
48580
MA = 121
32649
Ha = 188
342 n
mi
Hp = 172
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9919117
53 X = 3094968
27
Y = -19249917
70 feet Y = -5833165
69 meter
Z = -4211659
90 Z = -1268852
43
XDOT = 12389
376419 XDOT = 3768
562939
YDOT = 10565
849627 feet/sec YDOT = 3262
656340 meter/sec
ZDOT = -19297
532383 ZDOT = -5863
561237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7476660
29 X = 2278886
06
Y = -20334929
24 feet Y = -6198086
43 meter
Z = -4156501
76 Z = -1266901
74
XDOT = 12228
488313 XDOT = 3727
243238
YDOT = 8388
293904 feet/sec YDOT = 2556
751982 meter/sec
ZDOT = -19228
116098 ZDOT = -5860
729787
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 07097
50844549
00020000 00000-0 20000-3 0 9034
2 25544 51
6320 109
1558 0015749 39
6659 320
5655 15
78574566 39611
Satellite: ISS
Catalog Number: 25544
Epoch time: 07097
50844549 = yrday
fracday
Element set: 903
Inclination: 51
6320 deg
RA of node: 109
1558 deg
Eccentricity:
0015749
Arg of perigee: 39
6659 deg
Mean anomaly: 320
5655 deg
Mean motion: 15
78574566 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3961
Checksum: 327
Coasting Arc #5 (Orbit 3976)
---------------------------------------
Vector Time (GMT): 2007/098/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2660406
76 A = 6710073
46 meter
Y = -4164548
46 meter E =
0024060
Z = 4530732
95 I = 51
93256
XDOT = 3893
193492 Wp = 51
37015
YDOT = -5891
795752 meter/sec RA = 103
32144 deg
ZDOT = -3103
856145 TA = 69
49519
MA = 69
23711
Ha = 188
372 n
mi
Hp = 171
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8728368
63 X = -2635650
09
Y = -13663216
73 feet Y = -4194160
28 meter
Z = 14864609
41 Z = 4517868
66
XDOT = 12772
944526 XDOT = 3973
865128
YDOT = -19330
038558 feet/sec YDOT = -5847
808772 meter/sec
ZDOT = -10183
255068 ZDOT = -3084
747029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10651419
16 X = -3246552
56
Y = -12282870
17 feet Y = -3743818
83 meter
Z = 14815630
05 Z = 4515804
04
XDOT = 9076
934307 XDOT = 2766
649577
YDOT = -20170
591774 feet/sec YDOT = -6147
996373 meter/sec
ZDOT = -10112
097746 ZDOT = -3082
167393
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 07098
52131691
00020000 00000-0 20000-3 0 9045
2 25544 51
6315 103
9175 0015797 43
2071 317
0331 15
78640381 39772
Satellite: ISS
Catalog Number: 25544
Epoch time: 07098
52131691 = yrday
fracday
Element set: 904
Inclination: 51
6315 deg
RA of node: 103
9175 deg
Eccentricity:
0015797
Arg of perigee: 43
2071 deg
Mean anomaly: 317
0331 deg
Mean motion: 15
78640381 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3977
Checksum: 289
Coasting Arc #6 (Orbit 3992)
---------------------------------------
Vector Time (GMT): 2007/099/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3657803
69 A = 6712407
54 meter
Y = 4046675
12 meter E =
0024361
Z = 3885433
44 I = 51
94561
XDOT = -2368
494422 Wp = 68
50219
YDOT = -6096
474066 meter/sec RA = 98
22097 deg
ZDOT = 4108
117683 TA = 338
95600
MA = 339
05606
Ha = 188
456 n
mi
Hp = 171
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12000668
27 X = -3721657
13
Y = 13276493
18 feet Y = 4005414
41 meter
Z = 12747485
05 Z = 3867508
76
XDOT = -7770
650990 XDOT = -2320
103293
YDOT = -20001
555336 feet/sec YDOT = -6122
689417 meter/sec
ZDOT = 13478
076389 ZDOT = 4096
728913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9819807
22 X = -2993077
24
Y = 15018494
00 feet Y = 4577636
97 meter
Z = 12680532
69 Z = 3865026
36
XDOT = -9815
145718 XDOT = -2991
656415
YDOT = -17793
002258 feet/sec YDOT = -5423
307088 meter/sec
ZDOT = 13434
398381 ZDOT = 4094
804627
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 07099
53416410
00020000 00000-0 20000-3 0 9053
2 25544 51
6313 98
6796 0015795 47
0523 313
1965 15
78654962 39939
Satellite: ISS
Catalog Number: 25544
Epoch time: 07099
53416410 = yrday
fracday
Element set: 905
Inclination: 51
6313 deg
RA of node: 98
6796 deg
Eccentricity:
0015795
Arg of perigee: 47
0523 deg
Mean anomaly: 313
1965 deg
Mean motion: 15
78654962 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3993
Checksum: 324
Coasting Arc #7 (Orbit 4007)
---------------------------------------
Vector Time (GMT): 2007/100/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1469714
66 A = 6716519
80 meter
Y = 6136376
70 meter E =
0021694
Z = -2290124
47 I = 51
96333
XDOT = -4454
570283 Wp = 49
10481
YDOT = 3093
455822 meter/sec RA = 93
02603 deg
ZDOT = 5477
392514 TA = 285
22686
MA = 285
46663
Ha = 188
367 n
mi
Hp = 171
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4821898
50 X = 1412112
58
Y = 20132469
50 feet Y = 6152489
85 meter
Z = -7513531
72 Z = -2283124
41
XDOT = -14614
731901 XDOT = -4515
438845
YDOT = 10149
133274 feet/sec YDOT = 3043
301895 meter/sec
ZDOT = 17970
447881 ZDOT = 5455
604430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8314136
13 X = 2534148
69
Y = 18969700
76 feet Y = 5781964
79 meter
Z = -7486373
32 Z = -2281846
59
XDOT = -11326
682578 XDOT = -3452
372850
YDOT = 11962
696375 feet/sec YDOT = 3646
229855 meter/sec
ZDOT = 17888
816372 ZDOT = 5452
511230
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 07100
48368365
00020000 00000-0 20000-3 0 9066
2 25544 51
6317 93
7694 0015830 50
9833 309
2740 15
78709666 40080
Satellite: ISS
Catalog Number: 25544
Epoch time: 07100
48368365 = yrday
fracday
Element set: 906
Inclination: 51
6317 deg
RA of node: 93
7694 deg
Eccentricity:
0015830
Arg of perigee: 50
9833 deg
Mean anomaly: 309
2740 deg
Mean motion: 15
78709666 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4008
Checksum: 308
Coasting Arc #8 (Orbit 4023)
---------------------------------------
Vector Time (GMT): 2007/101/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4065981
93 A = 6706947
88 meter
Y = -1118765
79 meter E =
0029464
Z = -5239991
16 I = 51
93036
XDOT = 957
738471 Wp = 68
33298
YDOT = 7577
645573 meter/sec RA = 87
90304 deg
ZDOT = -867
960297 TA = 193
38187
MA = 193
46018
Ha = 188
342 n
mi
Hp = 171
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13339835
73 X = 4103644
78
Y = -3670491
43 feet Y = -1073087
09 meter
Z = -17191572
06 Z = -5220147
22
XDOT = 3142
186586 XDOT = 877
149344
YDOT = 24861
041905 feet/sec YDOT = 7587
904949 meter/sec
ZDOT = -2847
638770 ZDOT = -863
503326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12480576
14 X = 3804079
61
Y = -6182031
37 feet Y = -1884283
16 meter
Z = -17116996
87 Z = -5217260
65
XDOT = 7422
484988 XDOT = 2262
373424
YDOT = 22881
854471 feet/sec YDOT = 6974
389243 meter/sec
ZDOT = -2829
868597 ZDOT = -862
543948
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 07101
49647925
00020000 00000-0 20000-3 0 9071
2 25544 51
6309 88
5299 0015734 54
4864 305
7767 15
78719371 40242
Satellite: ISS
Catalog Number: 25544
Epoch time: 07101
49647925 = yrday
fracday
Element set: 907
Inclination: 51
6309 deg
RA of node: 88
5299 deg
Eccentricity:
0015734
Arg of perigee: 54
4864 deg
Mean anomaly: 305
7767 deg
Mean motion: 15
78719371 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4024
Checksum: 325
Coasting Arc #9 (Orbit 4039)
---------------------------------------
Vector Time (GMT): 2007/102/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -168098
59 A = 6718263
67 meter
Y = -6663137
23 meter E =
0019854
Z = -861354
58 I = 51
96663
XDOT = 4801
099552 Wp = 88
80074
YDOT = 637
522320 meter/sec RA = 82
75306 deg
ZDOT = -5985
915549 TA = 100
56393
MA = 100
34021
Ha = 188
318 n
mi
Hp = 171
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -551504
56 X = -89393
65
Y = -21860686
46 feet Y = -6664576
96 meter
Z = -2825966
46 Z = -861979
94
XDOT = 15751
638949 XDOT = 4822
692220
YDOT = 2091
608663 feet/sec YDOT = 691
331560 meter/sec
ZDOT = -19638
830540 ZDOT = -5962
539475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5090227
95 X = -1551501
48
Y = -21266525
92 feet Y = -6482037
10 meter
Z = -2829189
08 Z = -862336
83
XDOT = 14397
122387 XDOT = 4388
242904
YDOT = -896
221633 feet/sec YDOT = -273
168354 meter/sec
ZDOT = -19550
721844 ZDOT = -5959
060018
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 07102
50924765
00020000 00000-0 20000-3 0 9085
2 25544 51
6306 83
2903 0015823 58
1298 302
1405 15
78784161 40401
Satellite: ISS
Catalog Number: 25544
Epoch time: 07102
50924765 = yrday
fracday
Element set: 908
Inclination: 51
6306 deg
RA of node: 83
2903 deg
Eccentricity:
0015823
Arg of perigee: 58
1298 deg
Mean anomaly: 302
1405 deg
Mean motion: 15
78784161 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4040
Checksum: 278
Coasting Arc #10 (Orbit 4055)
---------------------------------------
Vector Time (GMT): 2007/103/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4250908
54 A = 6708850
30 meter
Y = -2160293
23 meter E =
0023449
Z = 4706482
11 I = 51
92970
XDOT = 606
610624 Wp = 61
59795
YDOT = -7192
966824 meter/sec RA = 77
57276 deg
ZDOT = -2732
568923 TA = 55
23710
MA = 55
01657
Ha = 188
333 n
mi
Hp = 171
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13946550
33 X = -4249299
05
Y = -7087576
21 feet Y = -2207820
11 meter
Z = 15441214
26 Z = 4685835
25
XDOT = 1990
192337 XDOT = 700
272613
YDOT = -23598
972519 feet/sec YDOT = -7185
659768 meter/sec
ZDOT = -8965
121137 ZDOT = -2729
394265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15269905
92 X = -4654267
32
Y = -3738141
28 feet Y = -1139385
46 meter
Z = 15363182
40 Z = 4682698
00
XDOT = -3610
724847 XDOT = -1100
548933
YDOT = -22337
016202 feet/sec YDOT = -6808
322539 meter/sec
ZDOT = -8954
102431 ZDOT = -2729
210421
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 07103
52198823
00020000 00000-0 20000-3 0 9097
2 25544 51
6301 78
0511 0015652 61
6142 298
6599 15
78828277 40567
Satellite: ISS
Catalog Number: 25544
Epoch time: 07103
52198823 = yrday
fracday
Element set: 909
Inclination: 51
6301 deg
RA of node: 78
0511 deg
Eccentricity:
0015652
Arg of perigee: 61
6142 deg
Mean anomaly: 298
6599 deg
Mean motion: 15
78828277 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4056
Checksum: 306
Coasting Arc #11 (Orbit 4071)
---------------------------------------
Vector Time (GMT): 2007/104/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1294146
82 A = 6712380
95 meter
Y = 5449755
16 meter E =
0026470
Z = 3672105
93 I = 51
93522
XDOT = -4876
352283 Wp = 78
42920
YDOT = -4108
201209 meter/sec RA = 72
46862 deg
ZDOT = 4357
445479 TA = 325
70757
MA = 325
87819
Ha = 188
150 n
mi
Hp = 170
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4245888
53 X = -1372829
02
Y = 17879774
15 feet Y = 5434843
55 meter
Z = 12047591
63 Z = 3665627
55
XDOT = -15998
531113 XDOT = -4851
219050
YDOT = -13478
350424 feet/sec YDOT = -4162
590547 meter/sec
ZDOT = 14296
080968 ZDOT = 4333
817432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 149637
41 X = 45609
48
Y = 18391892
44 feet Y = 5605848
82 meter
Z = 12023903
62 Z = 3664885
82
XDOT = -17524
457003 XDOT = -5341
454494
YDOT = -9190
171507 feet/sec YDOT = -2801
164275 meter/sec
ZDOT = 14206
569624 ZDOT = 4330
162421
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 07104
53470054
00020000 00000-0 20000-3 0 9100
2 25544 51
6305 72
8124 0015504 65
8725 294
4060 15
78899835 40725
Satellite: ISS
Catalog Number: 25544
Epoch time: 07104
53470054 = yrday
fracday
Element set: 910
Inclination: 51
6305 deg
RA of node: 72
8124 deg
Eccentricity:
0015504
Arg of perigee: 65
8725 deg
Mean anomaly: 294
4060 deg
Mean motion: 15
78899835 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4072
Checksum: 287
Coasting Arc #12 (Orbit 4086)
---------------------------------------
Vector Time (GMT): 2007/105/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4090522
45 A = 6715602
50 meter
Y = 4705804
15 meter E =
0020825
Z = -2495721
13 I = 51
93608
XDOT = -2466
761546 Wp = 63
86999
YDOT = 4960
376244 meter/sec RA = 67
26801 deg
ZDOT = 5353
121667 TA = 267
96682
MA = 268
20531
Ha = 188
249 n
mi
Hp = 170
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13420349
26 X = 4049721
29
Y = 15438990
00 feet Y = 4751318
37 meter
Z = -8188061
45 Z = -2475948
66
XDOT = -8093
049693 XDOT = -2548
050512
YDOT = 16274
200274 feet/sec YDOT = 4932
337368 meter/sec
ZDOT = 17562
735127 ZDOT = 5340
940297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17005593
50 X = 5183304
90
Y = 11423730
92 feet Y = 3481953
18 meter
Z = -8112995
64 Z = -2472841
07
XDOT = -2862
390864 XDOT = -872
456735
YDOT = 16600
268665 feet/sec YDOT = 5059
761889 meter/sec
ZDOT = 17517
504751 ZDOT = 5339
335448
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 07105
48409519
00020000 00000-0 20000-3 0 9114
2 25544 51
6305 67
9000 0015711 69
2489 291
0358 15
78893120 40878
Satellite: ISS
Catalog Number: 25544
Epoch time: 07105
48409519 = yrday
fracday
Element set: 911
Inclination: 51
6305 deg
RA of node: 67
9000 deg
Eccentricity:
0015711
Arg of perigee: 69
2489 deg
Mean anomaly: 291
0358 deg
Mean motion: 15
78893120 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4087
Checksum: 294
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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