Date:
April 1st 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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 1578)
---------------------------------------
Vector Time (GMT): 2008/088/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4445463
93 A = 6716293
53 meter
Y = 2339990
51 meter E =
0008652
Z = -4466089
44 I = 51
93875
XDOT = -400
573698 Wp = 106
46990
YDOT = 6964
646822 meter/sec RA = 71
87590 deg
ZDOT = 3253
138112 TA = 195
98066
MA = 196
00797
Ha = 185
972 n
mi
Hp = 180
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14584855
43 X = 4440662
89
Y = 7677134
20 feet Y = 2389675
34 meter
Z = -14652524
42 Z = -4444505
03
XDOT = -1314
218170 XDOT = -494
226872
YDOT = 22849
891147 feet/sec YDOT = 6959
643761 meter/sec
ZDOT = 10673
025303 ZDOT = 3250
964584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13197135
49 X = 4022486
90
Y = 9995930
50 feet Y = 3046759
62 meter
Z = -14569483
77 Z = -4440778
65
XDOT = -4403
693967 XDOT = -1342
245921
YDOT = 21346
011565 feet/sec YDOT = 6506
264325 meter/sec
ZDOT = 10665
433970 ZDOT = 3250
824274
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 08088
46845422
00020000 00000-0 20000-3 0 9008
2 25544 51
6383 72
5135 0001120 323
7478 36
3611 15
76565376 15792
Satellite: ISS
Catalog Number: 25544
Epoch time: 08088
46845422 = yrday
fracday
Element set: 900
Inclination: 51
6383 deg
RA of node: 72
5135 deg
Eccentricity:
0001120
Arg of perigee: 323
7478 deg
Mean anomaly: 36
3611 deg
Mean motion: 15
76565376 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1579
Checksum: 292
Coasting Arc #2 (Orbit 1594)
---------------------------------------
Vector Time (GMT): 2008/089/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 591244
48 A = 6719262
47 meter
Y = -5676911
02 meter E =
0004970
Z = -3551151
20 I = 51
93824
XDOT = 5270
456177 Wp = 71
61660
YDOT = 3358
901985 meter/sec RA = 66
79051 deg
ZDOT = -4495
647016 TA = 150
52425
MA = 150
49622
Ha = 185
918 n
mi
Hp = 179
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1939778
46 X = 671931
46
Y = -18625036
14 feet Y = -5669848
26 meter
Z = -11650758
54 Z = -3548082
92
XDOT = 17291
522891 XDOT = 5254
343708
YDOT = 11020
019637 feet/sec YDOT = 3417
749118 meter/sec
ZDOT = -14749
498083 ZDOT = -4470
082339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4745714
92 X = 1446493
91
Y = -18121616
63 feet Y = -5523468
75 meter
Z = -11639591
36 Z = -3547747
45
XDOT = 14227
188728 XDOT = 4336
447124
YDOT = 13128
765895 feet/sec YDOT = 4001
647845 meter/sec
ZDOT = -14651
079716 ZDOT = -4465
649097
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 08089
48260520
00020000 00000-0 20000-3 0 9012
2 25544 51
6375 67
2843 0001060 328
6837 31
4259 15
76613813 15958
Satellite: ISS
Catalog Number: 25544
Epoch time: 08089
48260520 = yrday
fracday
Element set: 901
Inclination: 51
6375 deg
RA of node: 67
2843 deg
Eccentricity:
0001060
Arg of perigee: 328
6837 deg
Mean anomaly: 31
4259 deg
Mean motion: 15
76613813 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1595
Checksum: 292
Coasting Arc #3 (Orbit 1610)
---------------------------------------
Vector Time (GMT): 2008/090/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4760577
02 A = 6719996
11 meter
Y = -3434457
87 meter E =
0012230
Z = 3261235
63 I = 51
92832
XDOT = 1023
958744 Wp = 87
33719
YDOT = -5965
217010 meter/sec RA = 61
60444 deg
ZDOT = -4771
538497 TA = 54
57273
MA = 54
45860
Ha = 185
866 n
mi
Hp = 179
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15618691
01 X = -4737660
98
Y = -11267906
39 feet Y = -3487565
19 meter
Z = 10699591
95 Z = 3238164
55
XDOT = 3359
444698 XDOT = 1113
765790
YDOT = -19570
921950 feet/sec YDOT = -5953
264439 meter/sec
ZDOT = -15654
653860 ZDOT = -4766
345916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14064465
73 X = -4286849
16
Y = -13228519
50 feet Y = -4032052
74 meter
Z = 10610728
84 Z = 3234150
15
XDOT = 5022
714809 XDOT = 1530
923474
YDOT = -17923
335100 feet/sec YDOT = -5463
032539 meter/sec
ZDOT = -15635
364047 ZDOT = -4765
658962
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 08090
49673095
00020000 00000-0 20000-3 0 9021
2 25544 51
6374 62
0556 0001264 330
1683 29
9409 15
76681516 16117
Satellite: ISS
Catalog Number: 25544
Epoch time: 08090
49673095 = yrday
fracday
Element set: 902
Inclination: 51
6374 deg
RA of node: 62
0556 deg
Eccentricity:
0001264
Arg of perigee: 330
1683 deg
Mean anomaly: 29
9409 deg
Mean motion: 15
76681516 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1611
Checksum: 290
Coasting Arc #4 (Orbit 1626)
---------------------------------------
Vector Time (GMT): 2008/091/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1280674
46 A = 6715056
97 meter
Y = 4670025
68 meter E =
0007076
Z = 4647697
21 I = 51
89696
XDOT = -5625
892717 Wp = 110
93227
YDOT = -4413
401320 meter/sec RA = 56
51506 deg
ZDOT = 2878
419539 TA = 310
70648
MA = 310
76793
Ha = 185
801 n
mi
Hp = 179
830
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4201687
87 X = -1355377
75
Y = 15321606
57 feet Y = 4655286
87 meter
Z = 15248350
44 Z = 4641294
18
XDOT = -18457
653272 XDOT = -5590
105993
YDOT = -14479
663122 feet/sec YDOT = -4476
113102 meter/sec
ZDOT = 9443
633659 ZDOT = 2851
176178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6009722
96 X = -1831763
56
Y = 14731686
26 feet Y = 4490217
97 meter
Z = 15224278
30 Z = 4640360
03
XDOT = -15662
195400 XDOT = -4773
837158
YDOT = -16060
509356 feet/sec YDOT = -4895
243252 meter/sec
ZDOT = 9338
660171 ZDOT = 2846
423620
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 08091
51083303
00020000 00000-0 20000-3 0 9033
2 25544 51
6373 56
8269 0001245 329
5344 30
5748 15
76714977 16272
Satellite: ISS
Catalog Number: 25544
Epoch time: 08091
51083303 = yrday
fracday
Element set: 903
Inclination: 51
6373 deg
RA of node: 56
8269 deg
Eccentricity:
0001245
Arg of perigee: 329
5344 deg
Mean anomaly: 30
5748 deg
Mean motion: 15
76714977 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1627
Checksum: 297
Coasting Arc #5 (Orbit 1641)
---------------------------------------
Vector Time (GMT): 2008/092/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5004823
14 A = 6723209
27 meter
Y = 4161235
12 meter E =
0008601
Z = -1669336
18 I = 51
90725
XDOT = -2006
177520 Wp = 30
90167
YDOT = 4713
266807 meter/sec RA = 51
34000 deg
ZDOT = 5754
495308 TA = 310
69726
MA = 310
77195
Ha = 185
845 n
mi
Hp = 179
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16420023
44 X = 4966028
87
Y = 13652346
19 feet Y = 4216984
93 meter
Z = -5476824
75 Z = -1645117
36
XDOT = -6581
947245 XDOT = -2086
686975
YDOT = 15463
473775 feet/sec YDOT = 4690
382673 meter/sec
ZDOT = 18879
577782 ZDOT = 5744
553623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15047706
14 X = 4586540
83
Y = 15184993
54 feet Y = 4628386
03 meter
Z = -5383479
06 Z = -1640884
42
XDOT = -7051
395213 XDOT = -2149
265261
YDOT = 13643
687773 feet/sec YDOT = 4158
596033 meter/sec
ZDOT = 18841
934039 ZDOT = 5743
021495
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 08092
46153154
00020000 00000-0 20000-3 0 9041
2 25544 51
6371 51
9246 0001139 341
8745 18
2378 15
76740497 16420
Satellite: ISS
Catalog Number: 25544
Epoch time: 08092
46153154 = yrday
fracday
Element set: 904
Inclination: 51
6371 deg
RA of node: 51
9246 deg
Eccentricity:
0001139
Arg of perigee: 341
8745 deg
Mean anomaly: 18
2378 deg
Mean motion: 15
76740497 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1642
Checksum: 293
Coasting Arc #6 (Orbit 1657)
---------------------------------------
Vector Time (GMT): 2008/093/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2306400
14 A = 6712459
48 meter
Y = -3533554
90 meter E =
0014490
Z = -5232788
40 I = 51
85263
XDOT = 5757
338456 Wp = 78
51038
YDOT = 5032
344926 meter/sec RA = 46
22242 deg
ZDOT = -859
770691 TA = 183
31672
MA = 183
32634
Ha = 185
753 n
mi
Hp = 179
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7566929
61 X = 2371161
25
Y = -11593027
88 feet Y = -3507401
64 meter
Z = -17167940
95 Z = -5221426
47
XDOT = 18888
905694 XDOT = 5704
814675
YDOT = 16510
317998 feet/sec YDOT = 5096
433046 meter/sec
ZDOT = -2820
769984 ZDOT = -831
929636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8566616
45 X = 2611104
69
Y = -10943116
34 feet Y = -3335461
86 meter
Z = -17124724
91 Z = -5219616
15
XDOT = 16726
109167 XDOT = 5098
118074
YDOT = 17344
216051 feet/sec YDOT = 5286
517052 meter/sec
ZDOT = -2713
437304 ZDOT = -827
055690
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 08093
47558519
00020000 00000-0 20000-3 0 9058
2 25544 51
6378 46
6946 0001242 340
7012 19
4105 15
76765490 16583
Satellite: ISS
Catalog Number: 25544
Epoch time: 08093
47558519 = yrday
fracday
Element set: 905
Inclination: 51
6378 deg
RA of node: 46
6946 deg
Eccentricity:
0001242
Arg of perigee: 340
7012 deg
Mean anomaly: 19
4105 deg
Mean motion: 15
76765490 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1658
Checksum: 303
Coasting Arc #7 (Orbit 1673)
---------------------------------------
Vector Time (GMT): 2008/094/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4956426
30 A = 6724140
88 meter
Y = -4532465
89 meter E =
0010617
Z = -203917
51 I = 51
87209
XDOT = 3342
843574 Wp = 133
25494
YDOT = -3392
187411 meter/sec RA = 41
07625 deg
ZDOT = -6056
425810 TA = 48
95601
MA = 48
86429
Ha = 185
679 n
mi
Hp = 179
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16261241
13 X = -4904384
60
Y = -14870294
92 feet Y = -4587600
52 meter
Z = -669020
70 Z = -227868
96
XDOT = 10967
334561 XDOT = 3409
948005
YDOT = -11129
223791 feet/sec YDOT = -3354
431114 meter/sec
ZDOT = -19870
163420 ZDOT = -6040
023071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15291358
61 X = -4660806
10
Y = -15861774
17 feet Y = -4834668
77 meter
Z = -761377
15 Z = -232067
76
XDOT = 10600
284895 XDOT = 3230
966836
YDOT = -9296
414392 feet/sec YDOT = -2833
547107 meter/sec
ZDOT = -19807
595678 ZDOT = -6037
355163
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 08094
48961323
00020000 00000-0 20000-3 0 9062
2 25544 51
6385 41
4651 0001335 343
0753 17
0367 15
76820365 16743
Satellite: ISS
Catalog Number: 25544
Epoch time: 08094
48961323 = yrday
fracday
Element set: 906
Inclination: 51
6385 deg
RA of node: 41
4651 deg
Eccentricity:
0001335
Arg of perigee: 343
0753 deg
Mean anomaly: 17
0367 deg
Mean motion: 15
76820365 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1674
Checksum: 287
Coasting Arc #8 (Orbit 1689)
---------------------------------------
Vector Time (GMT): 2008/095/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3560065
59 A = 6712587
29 meter
Y = 2421344
48 meter E =
0004970
Z = 5147944
07 I = 51
81095
XDOT = -5484
431606 Wp = 39
84047
YDOT = -5252
907873 meter/sec RA = 35
92060 deg
ZDOT = -1317
611180 TA = 62
74696
MA = 62
69635
Ha = 185
767 n
mi
Hp = 179
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11680005
21 X = -3611884
67
Y = 7944043
58 feet Y = 2381244
53 meter
Z = 16889580
29 Z = 5130523
16
XDOT = -17993
542015 XDOT = -5418
884429
YDOT = -17233
949713 feet/sec YDOT = -5313
871550 meter/sec
ZDOT = -4322
871325 ZDOT = -1344
094889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12125830
80 X = -3695953
23
Y = 7398577
84 feet Y = 2255086
52 meter
Z = 16823006
44 Z = 5127652
36
XDOT = -16624
352180 XDOT = -5067
102545
YDOT = -17151
424121 feet/sec YDOT = -5227
754072 meter/sec
ZDOT = -4425
011723 ZDOT = -1348
743573
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 08095
50361630
00020000 00000-0 20000-3 0 9072
2 25544 51
6390 36
2361 0001319 345
0527 15
0598 15
76850563 16907
Satellite: ISS
Catalog Number: 25544
Epoch time: 08095
50361630 = yrday
fracday
Element set: 907
Inclination: 51
6390 deg
RA of node: 36
2361 deg
Eccentricity:
0001319
Arg of perigee: 345
0527 deg
Mean anomaly: 15
0598 deg
Mean motion: 15
76850563 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1690
Checksum: 281
Coasting Arc #9 (Orbit 1705)
---------------------------------------
Vector Time (GMT): 2008/096/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4476088
62 A = 6722015
52 meter
Y = 4559485
33 meter E =
0014286
Z = 2064974
29 I = 51
81949
XDOT = -4841
019526 Wp = 64
27517
YDOT = 2217
158294 meter/sec RA = 30
80582 deg
ZDOT = 5574
419673 TA = 318
75535
MA = 318
86319
Ha = 185
556 n
mi
Hp = 179
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14685330
13 X = 4414739
72
Y = 14958941
36 feet Y = 4609196
67 meter
Z = 6774850
03 Z = 2086569
88
XDOT = -15882
609994 XDOT = -4892
532081
YDOT = 7274
141384 feet/sec YDOT = 2162
735720 meter/sec
ZDOT = 18288
778454 ZDOT = 5550
776494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14215492
23 X = 4332882
03
Y = 15369218
06 feet Y = 4684537
67 meter
Z = 6858159
90 Z = 2090367
14
XDOT = -15065
768623 XDOT = -4592
046276
YDOT = 5780
135659 feet/sec YDOT = 1761
785349 meter/sec
ZDOT = 18198
316732 ZDOT = 5546
846940
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 08096
51759262
00020000 00000-0 20000-3 0 9087
2 25544 51
6396 31
0065 0001268 345
4640 14
6488 15
76908727 17067
Satellite: ISS
Catalog Number: 25544
Epoch time: 08096
51759262 = yrday
fracday
Element set: 908
Inclination: 51
6396 deg
RA of node: 31
0065 deg
Eccentricity:
0001268
Arg of perigee: 345
4640 deg
Mean anomaly: 14
6488 deg
Mean motion: 15
76908727 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1706
Checksum: 306
Coasting Arc #10 (Orbit 1720)
---------------------------------------
Vector Time (GMT): 2008/097/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4864289
00 A = 6715572
09 meter
Y = -1501009
81 meter E =
0008423
Z = -4388097
50 I = 51
77241
XDOT = 4622
446836 Wp = 102
52996
YDOT = 5155
224034 meter/sec RA = 25
61633 deg
ZDOT = 3364
256678 TA = 201
25412
MA = 201
28914
Ha = 185
587 n
mi
Hp = 179
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15958953
42 X = 4902028
88
Y = -4924572
87 feet Y = -1446403
85 meter
Z = -14396645
33 Z = -4364374
68
XDOT = 15165
507992 XDOT = 4548
113589
YDOT = 16913
464677 feet/sec YDOT = 5206
499497 meter/sec
ZDOT = 11037
587525 ZDOT = 3386
531906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16094719
05 X = 4905670
37
Y = -4744149
36 feet Y = -1446016
73 meter
Z = -14305805
62 Z = -4360409
55
XDOT = 14565
804572 XDOT = 4439
657234
YDOT = 15908
285342 feet/sec YDOT = 4848
845372 meter/sec
ZDOT = 11123
556505 ZDOT = 3390
460023
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 08097
46817332
00020000 00000-0 20000-3 0 9096
2 25544 51
6400 26
1039 0001374 347
3511 12
7619 15
76926545 17215
Satellite: ISS
Catalog Number: 25544
Epoch time: 08097
46817332 = yrday
fracday
Element set: 909
Inclination: 51
6400 deg
RA of node: 26
1039 deg
Eccentricity:
0001374
Arg of perigee: 347
3511 deg
Mean anomaly: 12
7619 deg
Mean motion: 15
76926545 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1721
Checksum: 283
Coasting Arc #11 (Orbit 1736)
---------------------------------------
Vector Time (GMT): 2008/098/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3444101
79 A = 6717609
95 meter
Y = -4416629
15 meter E =
0006263
Z = -3716355
36 I = 51
75400
XDOT = 6261
424818 Wp = 63
72839
YDOT = -1271
266583 meter/sec RA = 20
51760 deg
ZDOT = -4294
750085 TA = 161
02092
MA = 160
99757
Ha = 185
506 n
mi
Hp = 179
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11299546
56 X = -3376404
69
Y = -14490253
13 feet Y = -4454764
71 meter
Z = -12192766
93 Z = -3732922
47
XDOT = 20542
732343 XDOT = 6296
038428
YDOT = -4170
822122 feet/sec YDOT = -1201
054393 meter/sec
ZDOT = -14090
387419 ZDOT = -4264
247441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11316509
30 X = -3449272
04
Y = -14422872
96 feet Y = -4396091
68 meter
Z = -12256757
58 Z = -3735859
71
XDOT = 19545
389469 XDOT = 5957
434710
YDOT = -3468
730556 feet/sec YDOT = -1057
269074 meter/sec
ZDOT = -13973
519351 ZDOT = -4259
128698
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 08098
48210073
00020000 00000-0 20000-3 0 9100
2 25544 51
6408 20
8742 0001395 352
1752 7
9391 15
76985414 17379
Satellite: ISS
Catalog Number: 25544
Epoch time: 08098
48210073 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 20
8742 deg
Eccentricity:
0001395
Arg of perigee: 352
1752 deg
Mean anomaly: 7
9391 deg
Mean motion: 15
76985414 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1737
Checksum: 291
Coasting Arc #12 (Orbit 1752)
---------------------------------------
Vector Time (GMT): 2008/099/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 590825
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5974417
58 A = 6719856
90 meter
Y = 786413
04 meter E =
0013098
Z = 2962349
64 I = 51
73399
XDOT = -3141
311049 Wp = 91
36104
YDOT = -4951
431823 meter/sec RA = 15
31694 deg
ZDOT = -5002
286168 TA = 54
45172
MA = 54
32967
Ha = 185
532 n
mi
Hp = 179
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19601107
53 X = -5997158
13
Y = 2580095
27 feet Y = 719476
56 meter
Z = 9718994
87 Z = 2933270
19
XDOT = -10306
138613 XDOT = -3061
409289
YDOT = -16244
855062 feet/sec YDOT = -4986
113040 meter/sec
ZDOT = -16411
700025 ZDOT = -5017
352791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19590908
49 X = -5971308
91
Y = 3034920
23 feet Y = 925043
69 meter
Z = 9607535
23 Z = 2928376
74
XDOT = -10365
201423 XDOT = -3159
313394
YDOT = -14575
195154 feet/sec YDOT = -4442
519483 meter/sec
ZDOT = -16469
981622 ZDOT = -5020
050398
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 08099
49600256
00020000 00000-0 20000-3 0 9119
2 25544 51
6411 15
6447 0001392 353
3156 6
7990 15
77020310 17531
Satellite: ISS
Catalog Number: 25544
Epoch time: 08099
49600256 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 15
6447 deg
Eccentricity:
0001392
Arg of perigee: 353
3156 deg
Mean anomaly: 6
7990 deg
Mean motion: 15
77020310 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1753
Checksum: 272
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics 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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