Date:
April 1st 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6243 07 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 3833)
---------------------------------------
Vector Time (GMT): 2007/089/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1774895
84 A = 6712187
45 meter
Y = 4893864
94 meter E =
0015738
Z = -4238114
09 I = 51
78735
XDOT = -6775
147399 Wp = 39
98510
YDOT = 653
847362 meter/sec RA = 149
79635 deg
ZDOT = 3611
579603 TA = 266
54666
MA = 266
72669
Ha = 187
835 n
mi
Hp = 174
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5823149
07 X = -1808900
07
Y = 16055987
34 feet Y = 4873826
60 meter
Z = -13904573
79 Z = -4246819
42
XDOT = -22228
173881 XDOT = -6799
499475
YDOT = 2145
168509 feet/sec YDOT = 577
947997 meter/sec
ZDOT = 11849
014444 ZDOT = 3578
607114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7997088
24 X = -2437512
50
Y = 15061796
56 feet Y = 4590835
59 meter
Z = -13936636
29 Z = -4247886
74
XDOT = -21272
094488 XDOT = -6483
734400
YDOT = -503
393931 feet/sec YDOT = -153
434470 meter/sec
ZDOT = 11725
033455 ZDOT = 3573
790197
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
46778858
00020000 00000-0 20000-3 0 9006
2 25544 51
6330 150
7235 0015242 7
8801 352
2601 15
78258609 38349
Satellite: ISS
Catalog Number: 25544
Epoch time: 07089
46778858 = yrday
fracday
Element set: 900
Inclination: 51
6330 deg
RA of node: 150
7235 deg
Eccentricity:
0015242
Arg of perigee: 7
8801 deg
Mean anomaly: 352
2601 deg
Mean motion: 15
78258609 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3834
Checksum: 297
Coasting Arc #2 (Orbit 3849)
---------------------------------------
Vector Time (GMT): 2007/090/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5262648
96 A = 6712610
26 meter
Y = 298665
09 meter E =
0020540
Z = -4176979
97 I = 51
81193
XDOT = -3279
400877 Wp = 31
00710
YDOT = 5890
616185 meter/sec RA = 144
68975 deg
ZDOT = -3701
364852 TA = 201
19517
MA = 201
28039
Ha = 187
990 n
mi
Hp = 174
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17265908
67 X = 5279208
99
Y = 979872
33 feet Y = 357607
20 meter
Z = -13704002
54 Z = -4151374
01
XDOT = -10759
189228 XDOT = -3327
046429
YDOT = 19326
168586 feet/sec YDOT = 5853
677362 meter/sec
ZDOT = -12143
585472 ZDOT = -3717
412315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17077383
19 X = 5205186
40
Y = 3172944
41 feet Y = 967113
45 meter
Z = -13607602
46 Z = -4147597
23
XDOT = -12826
244434 XDOT = -3909
439303
YDOT = 16567
884732 feet/sec YDOT = 5049
891266 meter/sec
ZDOT = -12203
137166 ZDOT = -3719
516208
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
48088481
00020000 00000-0 20000-3 0 9017
2 25544 51
6323 145
4867 0015282 11
6085 348
5430 15
78254517 38504
Satellite: ISS
Catalog Number: 25544
Epoch time: 07090
48088481 = yrday
fracday
Element set: 901
Inclination: 51
6323 deg
RA of node: 145
4867 deg
Eccentricity:
0015282
Arg of perigee: 11
6085 deg
Mean anomaly: 348
5430 deg
Mean motion: 15
78254517 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3850
Checksum: 293
Coasting Arc #3 (Orbit 3865)
---------------------------------------
Vector Time (GMT): 2007/091/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3737755
76 A = 6718142
91 meter
Y = -5226130
32 meter E =
0019799
Z = 1967889
14 I = 51
85452
XDOT = 5056
076744 Wp = 60
82652
YDOT = 1481
881397 meter/sec RA = 139
49121 deg
ZDOT = -5616
284175 TA = 97
31159
MA = 97
08651
Ha = 188
052 n
mi
Hp = 173
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12262978
21 X = 3786357
67
Y = -17146096
86 feet Y = -5184060
72 meter
Z = 6456329
19 Z = 1986165
63
XDOT = 16588
178294 XDOT = 5066
413190
YDOT = 4861
815608 feet/sec YDOT = 1538
478571 meter/sec
ZDOT = -18426
129182 ZDOT = -5591
696837
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14035993
89 X = 4278170
94
Y = -15699584
78 feet Y = -4785233
44 meter
Z = 6524367
55 Z = 1988627
23
XDOT = 14910
775882 XDOT = 4544
804489
YDOT = 5642
163155 feet/sec YDOT = 1719
731330 meter/sec
ZDOT = -18333
392093 ZDOT = -5588
017910
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
49395575
00020000 00000-0 20000-3 0 9025
2 25544 51
6326 140
2499 0015534 15
4259 344
7377 15
78336161 38667
Satellite: ISS
Catalog Number: 25544
Epoch time: 07091
49395575 = yrday
fracday
Element set: 902
Inclination: 51
6326 deg
RA of node: 140
2499 deg
Eccentricity:
0015534
Arg of perigee: 15
4259 deg
Mean anomaly: 344
7377 deg
Mean motion: 15
78336161 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3866
Checksum: 314
Coasting Arc #4 (Orbit 3881)
---------------------------------------
Vector Time (GMT): 2007/092/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3443762
44 A = 6707838
04 meter
Y = -2366898
40 meter E =
0015308
Z = 5239360
00 I = 51
84038
XDOT = 4995
013387 Wp = 30
60330
YDOT = -5844
037518 meter/sec RA = 134
36100 deg
ZDOT = 655
190225 TA = 53
26713
MA = 53
12664
Ha = 188
178 n
mi
Hp = 173
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11298433
21 X = -3442491
43
Y = -7765414
71 feet Y = -2405400
94 meter
Z = 17189501
33 Z = 5222633
45
XDOT = 16387
839197 XDOT = 5056
808211
YDOT = -19173
351438 feet/sec YDOT = -5787
834915 meter/sec
ZDOT = 2149
574228 ZDOT = 679
606651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10624947
71 X = -3238484
06
Y = -8788529
91 feet Y = -2678743
92 meter
Z = 17126220
92 Z = 5220072
14
XDOT = 17441
863643 XDOT = 5316
280038
YDOT = -16797
741839 feet/sec YDOT = -5119
951712 meter/sec
ZDOT = 2240
637939 ZDOT = 682
946444
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
50700319
00020000 00000-0 20000-3 0 9035
2 25544 51
6321 135
0129 0015428 19
3430 340
8318 15
78361768 38821
Satellite: ISS
Catalog Number: 25544
Epoch time: 07092
50700319 = yrday
fracday
Element set: 903
Inclination: 51
6321 deg
RA of node: 135
0129 deg
Eccentricity:
0015428
Arg of perigee: 19
3430 deg
Mean anomaly: 340
8318 deg
Mean motion: 15
78361768 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3882
Checksum: 278
Coasting Arc #5 (Orbit 3897)
---------------------------------------
Vector Time (GMT): 2007/093/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4708319
04 A = 6719585
87 meter
Y = 4690483
48 meter E =
0028373
Z = 870890
65 I = 51
89815
XDOT = -2827
718396 Wp = 37
80442
YDOT = -3965
666567 meter/sec RA = 129
21085 deg
ZDOT = 5991
165294 TA = 331
69936
MA = 331
85321
Ha = 188
393 n
mi
Hp = 173
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15447240
95 X = -4764649
43
Y = 15388725
34 feet Y = 4637517
53 meter
Z = 2857252
79 Z = 847880
31
XDOT = -9277
291327 XDOT = -2812
267790
YDOT = -13010
717084 feet/sec YDOT = -3997
200883 meter/sec
ZDOT = 19656
054114 ZDOT = 5977
465952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16581680
97 X = -5054096
36
Y = 14176096
39 feet Y = 4320874
18 meter
Z = 2771310
45 Z = 844695
42
XDOT = -7342
773675 XDOT = -2238
077416
YDOT = -12473
929469 feet/sec YDOT = -3802
053702 meter/sec
ZDOT = 19603
943816 ZDOT = 5975
282075
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
52002962
00020000 00000-0 20000-3 0 9048
2 25544 51
6314 129
7757 0015788 23
6843 336
5046 15
78332849 38980
Satellite: ISS
Catalog Number: 25544
Epoch time: 07093
52002962 = yrday
fracday
Element set: 904
Inclination: 51
6314 deg
RA of node: 129
7757 deg
Eccentricity:
0015788
Arg of perigee: 23
6843 deg
Mean anomaly: 336
5046 deg
Mean motion: 15
78332849 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3898
Checksum: 320
Coasting Arc #6 (Orbit 3912)
---------------------------------------
Vector Time (GMT): 2007/094/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1483681
81 A = 6709770
43 meter
Y = 4491014
67 meter E =
0020902
Z = -4770628
39 I = 51
88327
XDOT = -5586
639901 Wp = 60
73639
YDOT = 4605
167749 meter/sec RA = 124
03029 deg
ZDOT = 2616
315879 TA = 234
75862
MA = 234
95442
Ha = 188
337 n
mi
Hp = 173
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4867722
46 X = 1456527
46
Y = 14734300
09 feet Y = 4507453
94 meter
Z = -15651667
96 Z = -4763486
80
XDOT = -18328
871066 XDOT = -5650
430061
YDOT = 15108
818074 feet/sec YDOT = 4542
338287 meter/sec
ZDOT = 8583
713513 ZDOT = 2589
020504
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4085727
21 X = 1245329
65
Y = 14998706
78 feet Y = 4571605
83 meter
Z = -15624169
07 Z = -4762246
73
XDOT = -18133
814948 XDOT = -5527
186796
YDOT = 13711
628581 feet/sec YDOT = 4179
304391 meter/sec
ZDOT = 8481
622698 ZDOT = 2585
198598
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
46971506
00020000 00000-0 20000-3 0 9052
2 25544 51
6317 124
8656 0015674 27
2758 332
9227 15
78404420 39130
Satellite: ISS
Catalog Number: 25544
Epoch time: 07094
46971506 = yrday
fracday
Element set: 905
Inclination: 51
6317 deg
RA of node: 124
8656 deg
Eccentricity:
0015674
Arg of perigee: 27
2758 deg
Mean anomaly: 332
9227 deg
Mean motion: 15
78404420 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3913
Checksum: 304
Coasting Arc #7 (Orbit 3928)
---------------------------------------
Vector Time (GMT): 2007/095/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4847519
82 A = 6714120
88 meter
Y = -3039015
51 meter E =
0019296
Z = -3538270
28 I = 51
91391
XDOT = 603
613424 Wp = 44
18610
YDOT = 6204
509917 meter/sec RA = 118
92470 deg
ZDOT = -4503
190826 TA = 177
74661
MA = 177
73791
Ha = 188
326 n
mi
Hp = 172
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15903936
43 X = 4898330
74
Y = -9970523
32 feet Y = -2984523
85 meter
Z = -11608498
30 Z = -3514597
22
XDOT = 1980
359001 XDOT = 556
064790
YDOT = 20356
003666 feet/sec YDOT = 6210
993851 meter/sec
ZDOT = -14774
248117 ZDOT = -4500
374144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16365859
04 X = 4988313
83
Y = -9303563
19 feet Y = -2835726
06 meter
Z = -11519814
75 Z = -3511239
54
XDOT = 543
166793 XDOT = 165
557238
YDOT = 19230
456224 feet/sec YDOT = 5861
443057 meter/sec
ZDOT = -14762
798347 ZDOT = -4499
700936
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
48269097
00020000 00000-0 20000-3 0 9061
2 25544 51
6321 119
6276 0015711 31
6916 328
5192 15
78468036 39294
Satellite: ISS
Catalog Number: 25544
Epoch time: 07095
48269097 = yrday
fracday
Element set: 906
Inclination: 51
6321 deg
RA of node: 119
6276 deg
Eccentricity:
0015711
Arg of perigee: 31
6916 deg
Mean anomaly: 328
5192 deg
Mean motion: 15
78468036 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3929
Checksum: 317
Coasting Arc #8 (Orbit 3944)
---------------------------------------
Vector Time (GMT): 2007/096/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 322631
52 A = 6716024
24 meter
Y = -6110959
43 meter E =
0024794
Z = 2762296
30 I = 51
93269
XDOT = 5329
959913 Wp = 65
23213
YDOT = -2074
076213 meter/sec RA = 113
72510 deg
ZDOT = -5164
850434 TA = 83
26230
MA = 82
98020
Ha = 188
352 n
mi
Hp = 172
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1058502
38 X = 377522
28
Y = -20049079
49 feet Y = -6107044
64 meter
Z = 9062651
91 Z = 2763997
07
XDOT = 17486
745122 XDOT = 5377
846609
YDOT = -6804
711986 feet/sec YDOT = -2014
205936 meter/sec
ZDOT = -16945
047355 ZDOT = -5138
840834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1489633
06 X = 454040
16
Y = -20019138
78 feet Y = -6101833
50 meter
Z = 9068227
55 Z = 2763995
76
XDOT = 16279
537388 XDOT = 4962
002996
YDOT = -6488
625032 feet/sec YDOT = -1977
732910 meter/sec
ZDOT = -16847
428486 ZDOT = -5135
096203
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
49564122
00020000 00000-0 20000-3 0 9071
2 25544 51
6312 114
3897 0015771 35
3532 324
8676 15
78516991 39454
Satellite: ISS
Catalog Number: 25544
Epoch time: 07096
49564122 = yrday
fracday
Element set: 907
Inclination: 51
6312 deg
RA of node: 114
3897 deg
Eccentricity:
0015771
Arg of perigee: 35
3532 deg
Mean anomaly: 324
8676 deg
Mean motion: 15
78516991 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3945
Checksum: 317
Coasting Arc #9 (Orbit 3960)
---------------------------------------
Vector Time (GMT): 2007/097/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4338900
27 A = 6708019
98 meter
Y = 394934
35 meter E =
0016835
Z = 5086417
43 I = 51
91611
XDOT = 1189
564264 Wp = 56
60312
YDOT = -7459
176529 meter/sec RA = 108
61149 deg
ZDOT = 1599
237147 TA = 18
16955
MA = 18
10947
Ha = 188
537 n
mi
Hp = 172
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14235237
12 X = -4367703
16
Y = 1295716
39 feet Y = 346253
27 meter
Z = 16687721
23 Z = 5065268
88
XDOT = 3902
769894 XDOT = 1265
116555
YDOT = -24472
363939 feet/sec YDOT = -7445
451730 meter/sec
ZDOT = 5246
841034 ZDOT = 1605
199587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14336510
50 X = -4369768
40
Y = 1197575
84 feet Y = 365021
12 meter
Z = 16608165
93 Z = 5062168
97
XDOT = 4128
040776 XDOT = 1258
226828
YDOT = -23399
919257 feet/sec YDOT = -7132
295389 meter/sec
ZDOT = 5268
287963 ZDOT = 1605
774171
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
50856722
00020000 00000-0 20000-3 0 9085
2 25544 51
6311 109
1517 0015779 39
6271 320
6044 15
78542135 39619
Satellite: ISS
Catalog Number: 25544
Epoch time: 07097
50856722 = yrday
fracday
Element set: 908
Inclination: 51
6311 deg
RA of node: 109
1517 deg
Eccentricity:
0015779
Arg of perigee: 39
6271 deg
Mean anomaly: 320
6044 deg
Mean motion: 15
78542135 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3961
Checksum: 296
Coasting Arc #10 (Orbit 3976)
---------------------------------------
Vector Time (GMT): 2007/098/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1635602
59 A = 6719189
04 meter
Y = 6502052
33 meter E =
0028246
Z = 100110
63 I = 51
96303
XDOT = -4586
637445 Wp = 44
43970
YDOT = -1262
751958 meter/sec RA = 103
45058 deg
ZDOT = 6077
464256 TA = 316
64646
MA = 316
86832
Ha = 188
409 n
mi
Hp = 171
988
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5366150
24 X = -1708674
24
Y = 21332192
69 feet Y = 6483353
54 meter
Z = 328446
94 Z = 91987
43
XDOT = -15048
023112 XDOT = -4601
699713
YDOT = -4142
887001 feet/sec YDOT = -1314
126628 meter/sec
ZDOT = 19939
187193 ZDOT = 6055
145605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5146507
66 X = -1568655
54
Y = 21386680
70 feet Y = 6518660
28 meter
Z = 298727
61 Z = 91052
18
XDOT = -13641
468307 XDOT = -4157
919540
YDOT = -3610
429554 feet/sec YDOT = -1100
458928 meter/sec
ZDOT = 19855
000582 ZDOT = 6051
804177
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
52146741
00020000 00000-0 20000-3 0 9092
2 25544 51
6321 103
9145 0015772 43
1833 317
0566 15
78580781 39771
Satellite: ISS
Catalog Number: 25544
Epoch time: 07098
52146741 = yrday
fracday
Element set: 909
Inclination: 51
6321 deg
RA of node: 103
9145 deg
Eccentricity:
0015772
Arg of perigee: 43
1833 deg
Mean anomaly: 317
0566 deg
Mean motion: 15
78580781 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3977
Checksum: 305
Coasting Arc #11 (Orbit 3991)
---------------------------------------
Vector Time (GMT): 2007/099/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3606269
59 A = 6708183
50 meter
Y = 2610324
62 meter E =
0025481
Z = -5036669
72 I = 51
93154
XDOT = -2501
803704 Wp = 72
63114
YDOT = 7030
441576 meter/sec RA = 98
28512 deg
ZDOT = 1867
454373 TA = 215
24494
MA = 215
41371
Ha = 188
443 n
mi
Hp = 171
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11831593
15 X = 3601279
85
Y = 8564057
15 feet Y = 2650624
15 meter
Z = -16524506
95 Z = -5019162
47
XDOT = -8208
017400 XDOT = -2589
304960
YDOT = 23065
753201 feet/sec YDOT = 7001
975722 meter/sec
ZDOT = 6126
818810 ZDOT = 1855
088182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12155013
22 X = 3704848
03
Y = 8232290
30 feet Y = 2509202
08 meter
Z = -16458251
77 Z = -5016475
14
XDOT = -7002
816703 XDOT = -2134
458531
YDOT = 22397
759455 feet/sec YDOT = 6826
837082 meter/sec
ZDOT = 6081
185519 ZDOT = 1853
545346
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
47103774
00020000 00000-0 20000-3 0 9108
2 25544 51
6323 99
0038 0015715 46
5538 313
6932 15
78589687 39925
Satellite: ISS
Catalog Number: 25544
Epoch time: 07099
47103774 = yrday
fracday
Element set: 910
Inclination: 51
6323 deg
RA of node: 99
0038 deg
Eccentricity:
0015715
Arg of perigee: 46
5538 deg
Mean anomaly: 313
6932 deg
Mean motion: 15
78589687 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3992
Checksum: 325
Coasting Arc #12 (Orbit 4007)
---------------------------------------
Vector Time (GMT): 2007/100/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 465135
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2682933
85 A = 6714989
79 meter
Y = -5364428
27 meter E =
0018558
Z = -3043751
02 I = 51
95682
XDOT = 3631
374631 Wp = 62
53653
YDOT = 4622
622650 meter/sec RA = 93
17465 deg
ZDOT = -4960
768222 TA = 152
53581
MA = 152
43761
Ha = 188
407 n
mi
Hp = 171
683
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8802276
42 X = 2757506
25
Y = -17599830
27 feet Y = -5334009
19 meter
Z = -9986059
77 Z = -3030536
29
XDOT = 11913
958764 XDOT = 3603
512408
YDOT = 15166
084810 feet/sec YDOT = 4663
075016 meter/sec
ZDOT = -16275
486292 ZDOT = -4943
194610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8061247
38 X = 2457068
20
Y = -17978534
43 feet Y = -5479857
30 meter
Z = -9937005
37 Z = -3028799
24
XDOT = 11360
176739 XDOT = 3462
581870
YDOT = 14025
940829 feet/sec YDOT = 4275
106765 meter/sec
ZDOT = -16208
714570 ZDOT = -4940
416201
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
48388738
00020000 00000-0 20000-3 0 9118
2 25544 51
6312 93
7648 0015732 50
7869 309
4691 15
78643531 40087
Satellite: ISS
Catalog Number: 25544
Epoch time: 07100
48388738 = yrday
fracday
Element set: 911
Inclination: 51
6312 deg
RA of node: 93
7648 deg
Eccentricity:
0015732
Arg of perigee: 50
7869 deg
Mean anomaly: 309
4691 deg
Mean motion: 15
78643531 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4008
Checksum: 307
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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