Date:
February 10th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8503 49 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 3060)
---------------------------------------
Vector Time (GMT): 2007/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4209633
79 A = 6720148
68 meter
Y = -5107260
69 meter E =
0029090
Z = -1051911
48 I = 51
86873
XDOT = 4323
154569 Wp = 172
90890
YDOT = -2346
464510 meter/sec RA = 43
33621 deg
ZDOT = -5953
718851 TA = 18
60162
MA = 18
49550
Ha = 189
714 n
mi
Hp = 173
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13811134
49 X = -4147100
88
Y = -16756104
62 feet Y = -5153985
51 meter
Z = -3451153
15 Z = -1072209
79
XDOT = 14183
577983 XDOT = 4377
993505
YDOT = -7698
374378 feet/sec YDOT = -2297
813910 meter/sec
ZDOT = -19533
198330 ZDOT = -5932
584040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 785086
01 X = 239294
22
Y = -21687825
99 feet Y = -6610449
36 meter
Z = -3527999
39 Z = -1075334
22
XDOT = 14221
528783 XDOT = 4334
721973
YDOT = 3655
680003 feet/sec YDOT = 1114
251265 meter/sec
ZDOT = -19454
127759 ZDOT = -5929
618141
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 07040
52962188
00020000 00000-0 20000-3 0 9001
2 25544 51
6321 43
7211 0021416 186
7385 173
3495 15
78062671 30615
Satellite: ISS
Catalog Number: 25544
Epoch time: 07040
52962188 = yrday
fracday
Element set: 900
Inclination: 51
6321 deg
RA of node: 43
7211 deg
Eccentricity:
0021416
Arg of perigee: 186
7385 deg
Mean anomaly: 173
3495 deg
Mean motion: 15
78062671 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3061
Checksum: 278
Coasting Arc #2 (Orbit 3076)
---------------------------------------
Vector Time (GMT): 2007/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4624424
43 A = 6710764
84 meter
Y = 1096032
04 meter E =
0017473
Z = 4728189
76 I = 51
81543
XDOT = -4135
412678 Wp = 170
48433
YDOT = -5933
773413 meter/sec RA = 38
15255 deg
ZDOT = -2684
664059 TA = 305
71193
MA = 305
87438
Ha = 189
509 n
mi
Hp = 173
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15171996
15 X = -4659305
13
Y = 3595905
65 feet Y = 1044124
00 meter
Z = 15512433
60 Z = 4705639
88
XDOT = -13567
626897 XDOT = -4055
711571
YDOT = -19467
760542 feet/sec YDOT = -5979
572204 meter/sec
ZDOT = -8807
952951 ZDOT = -2704
560216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13931898
87 X = -4246442
78
Y = -7185951
77 feet Y = -2190278
10 meter
Z = 15427893
31 Z = 4702421
88
XDOT = 1858
235952 XDOT = 566
390318
YDOT = -22565
091810 feet/sec YDOT = -6877
839984 meter/sec
ZDOT = -8883
386460 ZDOT = -2707
656193
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 07041
54280906
00020000 00000-0 20000-3 0 9016
2 25544 51
6317 38
4854 0021276 190
9647 169
1057 15
78125433 30776
Satellite: ISS
Catalog Number: 25544
Epoch time: 07041
54280906 = yrday
fracday
Element set: 901
Inclination: 51
6317 deg
RA of node: 38
4854 deg
Eccentricity:
0021276
Arg of perigee: 190
9647 deg
Mean anomaly: 169
1057 deg
Mean motion: 15
78125433 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3077
Checksum: 294
Coasting Arc #3 (Orbit 3092)
---------------------------------------
Vector Time (GMT): 2007/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2736765
16 A = 6714951
94 meter
Y = 5053553
11 meter E =
0022165
Z = 3487573
64 I = 51
80670
XDOT = -6213
514558 Wp = 161
70742
YDOT = 215
085512 meter/sec RA = 33
04458 deg
ZDOT = 4535
809127 TA = 239
60032
MA = 239
81957
Ha = 189
129 n
mi
Hp = 174
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8978888
33 X = 2663110
44
Y = 16579898
66 feet Y = 5083745
18 meter
Z = 11442170
75 Z = 3500689
97
XDOT = -20385
546450 XDOT = -6237
491715
YDOT = 705
661128 feet/sec YDOT = 145
468275 meter/sec
ZDOT = 14881
263541 ZDOT = 4505
566054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3686034
41 X = -1123503
29
Y = 18460308
81 feet Y = 5626702
12 meter
Z = 11492036
20 Z = 3502772
63
XDOT = -14883
274788 XDOT = -4536
422155
YDOT = -12222
833535 feet/sec YDOT = -3725
519662 meter/sec
ZDOT = 14767
724271 ZDOT = 4501
202358
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 07042
55597006
00020000 00000-0 20000-3 0 9021
2 25544 51
6315 33
2497 0021324 195
0980 164
9552 15
78186724 30931
Satellite: ISS
Catalog Number: 25544
Epoch time: 07042
55597006 = yrday
fracday
Element set: 902
Inclination: 51
6315 deg
RA of node: 33
2497 deg
Eccentricity:
0021324
Arg of perigee: 195
0980 deg
Mean anomaly: 164
9552 deg
Mean motion: 15
78186724 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3093
Checksum: 294
Coasting Arc #4 (Orbit 3107)
---------------------------------------
Vector Time (GMT): 2007/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6043365
61 A = 6716729
34 meter
Y = 621861
07 meter E =
0018136
Z = -2886122
23 I = 51
78754
XDOT = 1861
741722 Wp = 187
48557
YDOT = 5487
764409 meter/sec RA = 27
83774 deg
ZDOT = 5059
618508 TA = 139
41298
MA = 139
27764
Ha = 188
902 n
mi
Hp = 174
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19827315
00 X = 6049982
74
Y = 2040226
62 feet Y = 689478
51 meter
Z = -9468904
95 Z = -2856747
95
XDOT = 6108
076516 XDOT = 1775
660097
YDOT = 18004
476409 feet/sec YDOT = 5508
101870 meter/sec
ZDOT = 16599
798255 ZDOT = 5068
453898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14269860
67 X = 4349453
53
Y = 13990505
51 feet Y = 4264306
08 meter
Z = -9358522
19 Z = -2852477
56
XDOT = -5502
776242 XDOT = -1677
246199
YDOT = 16786
254774 feet/sec YDOT = 5116
450455 meter/sec
ZDOT = 16633
639267 ZDOT = 5069
933249
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 07043
50578639
00020000 00000-0 20000-3 0 9039
2 25544 51
6313 28
3404 0021127 198
2278 161
8132 15
78190197 31084
Satellite: ISS
Catalog Number: 25544
Epoch time: 07043
50578639 = yrday
fracday
Element set: 903
Inclination: 51
6313 deg
RA of node: 28
3404 deg
Eccentricity:
0021127
Arg of perigee: 198
2278 deg
Mean anomaly: 161
8132 deg
Mean motion: 15
78190197 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3108
Checksum: 285
Coasting Arc #5 (Orbit 3123)
---------------------------------------
Vector Time (GMT): 2007/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -339670
86 A = 6709119
00 meter
Y = -4436040
73 meter E =
0017177
Z = -5021749
02 I = 51
73647
XDOT = 7334
025517 Wp = 162
49972
YDOT = 1498
919697 meter/sec RA = 22
71653 deg
ZDOT = -1837
856083 TA = 89
92024
MA = 89
72340
Ha = 188
630 n
mi
Hp = 174
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1114405
72 X = -265646
96
Y = -14553939
40 feet Y = -4439424
94 meter
Z = -16475554
52 Z = -5023219
55
XDOT = 24061
763506 XDOT = 7325
647087
YDOT = 4917
715540 feet/sec YDOT = 1580
886118 meter/sec
ZDOT = -6029
711557 ZDOT = -1802
248417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8067070
06 X = 2458842
95
Y = -12156554
67 feet Y = -3705317
86 meter
Z = -16481611
21 Z = -5023595
10
XDOT = 15206
982774 XDOT = 4635
088350
YDOT = 18006
094833 feet/sec YDOT = 5488
257705 meter/sec
ZDOT = -5895
808384 ZDOT = -1797
042395
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 07044
51889713
00020000 00000-0 20000-3 0 9040
2 25544 51
6313 23
1031 0021110 202
3234 157
7014 15
78229362 31242
Satellite: ISS
Catalog Number: 25544
Epoch time: 07044
51889713 = yrday
fracday
Element set: 904
Inclination: 51
6313 deg
RA of node: 23
1031 deg
Eccentricity:
0021110
Arg of perigee: 202
3234 deg
Mean anomaly: 157
7014 deg
Mean motion: 15
78229362 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3124
Checksum: 244
Coasting Arc #6 (Orbit 3139)
---------------------------------------
Vector Time (GMT): 2007/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6433717
94 A = 6720022
53 meter
Y = -1864581
95 meter E =
0027476
Z = 204118
84 I = 51
74710
XDOT = 1154
965310 Wp = 179
88828
YDOT = -4645
799536 meter/sec RA = 17
53900 deg
ZDOT = -6060
082354 TA = 357
88886
MA = 357
90044
Ha = 188
279 n
mi
Hp = 174
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21107998
48 X = -6413381
30
Y = -6117394
86 feet Y = -1936413
68 meter
Z = 669681
24 Z = 172913
97
XDOT = 3789
256266 XDOT = 1236
267466
YDOT = -15242
124461 feet/sec YDOT = -4632
429183 meter/sec
ZDOT = -19882
159954 ZDOT = -6054
274436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13300481
41 X = -4053986
73
Y = -17498879
80 feet Y = -5333658
56 meter
Z = 552261
74 Z = 168329
38
XDOT = 10942
816478 XDOT = 3335
370462
YDOT = -8940
967499 feet/sec YDOT = -2725
206894 meter/sec
ZDOT = -19860
907938 ZDOT = -6053
604739
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 07045
53198069
00020000 00000-0 20000-3 0 9051
2 25544 51
6318 17
8667 0021024 206
4627 153
5466 15
78283006 31405
Satellite: ISS
Catalog Number: 25544
Epoch time: 07045
53198069 = yrday
fracday
Element set: 905
Inclination: 51
6318 deg
RA of node: 17
8667 deg
Eccentricity:
0021024
Arg of perigee: 206
4627 deg
Mean anomaly: 153
5466 deg
Mean motion: 15
78283006 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3140
Checksum: 288
Coasting Arc #7 (Orbit 3155)
---------------------------------------
Vector Time (GMT): 2007/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2377472
33 A = 6708506
68 meter
Y = 3623756
97 meter E =
0016980
Z = 5123188
34 I = 51
68083
XDOT = -7084
256842 Wp = 203
58614
YDOT = -2688
243447 meter/sec RA = 12
36604 deg
ZDOT = -1402
937233 TA = 259
73588
MA = 259
92739
Ha = 188
041 n
mi
Hp = 174
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7800106
06 X = -2442703
75
Y = 11888966
45 feet Y = 3596805
86 meter
Z = 16808360
71 Z = 5111480
61
XDOT = -23242
312474 XDOT = -7046
855005
YDOT = -8819
696348 feet/sec YDOT = -2767
254391 meter/sec
ZDOT = -4602
812443 ZDOT = -1437
260725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13340422
94 X = -4066160
91
Y = 5067920
26 feet Y = 1544702
10 meter
Z = 16764828
29 Z = 5109919
66
XDOT = -13367
450557 XDOT = -4074
398930
YDOT = -19717
302077 feet/sec YDOT = -6009
833673 meter/sec
ZDOT = -4732
051617 ZDOT = -1442
329333
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 07046
54503752
00020000 00000-0 20000-3 0 9063
2 25544 51
6319 12
6303 0021034 210
4318 149
5628 15
78314922 31563
Satellite: ISS
Catalog Number: 25544
Epoch time: 07046
54503752 = yrday
fracday
Element set: 906
Inclination: 51
6319 deg
RA of node: 12
6303 deg
Eccentricity:
0021034
Arg of perigee: 210
4318 deg
Mean anomaly: 149
5628 deg
Mean motion: 15
78314922 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3156
Checksum: 268
Coasting Arc #8 (Orbit 3171)
---------------------------------------
Vector Time (GMT): 2007/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5558395
63 A = 6716702
48 meter
Y = 2764694
83 meter E =
0014606
Z = 2584858
60 I = 51
68180
XDOT = -4268
893479 Wp = 173
39719
YDOT = 3648
456089 meter/sec RA = 7
23432 deg
ZDOT = 5260
218476 TA = 215
93855
MA = 216
03687
Ha = 187
695 n
mi
Hp = 174
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18236206
14 X = 5514510
96
Y = 9070521
10 feet Y = 2826606
53 meter
Z = 8480507
21 Z = 2611753
79
XDOT = -14005
556033 XDOT = -4334
926101
YDOT = 11970
000291 feet/sec YDOT = 3600
349716 meter/sec
ZDOT = 17257
934631 ZDOT = 5239
320509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9811516
66 X = 2990550
28
Y = 17799953
72 feet Y = 5425425
89 meter
Z = 8581862
18 Z = 2615751
59
XDOT = -17107
316125 XDOT = -5214
309955
YDOT = 1119
960403 feet/sec YDOT = 341
363931 meter/sec
ZDOT = 17179
889754 ZDOT = 5236
430397
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 07047
55806488
00020000 00000-0 20000-3 0 9078
2 25544 51
6325 7
3931 0021173 214
3076 145
6723 15
78401225 31720
Satellite: ISS
Catalog Number: 25544
Epoch time: 07047
55806488 = yrday
fracday
Element set: 907
Inclination: 51
6325 deg
RA of node: 7
3931 deg
Eccentricity:
0021173
Arg of perigee: 214
3076 deg
Mean anomaly: 145
6723 deg
Mean motion: 15
78401225 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3172
Checksum: 280
Coasting Arc #9 (Orbit 3186)
---------------------------------------
Vector Time (GMT): 2007/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4903353
75 A = 6713874
12 meter
Y = -2744209
22 meter E =
0019036
Z = -3683728
20 I = 51
64347
XDOT = 5269
440123 Wp = 202
45514
YDOT = 3597
878682 meter/sec RA = 2
01762 deg
ZDOT = 4309
223517 TA = 113
18436
MA = 112
98373
Ha = 187
410 n
mi
Hp = 175
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16087118
59 X = 4951569
76
Y = -9003311
08 feet Y = -2689107
70 meter
Z = -12085722
44 Z = -3659791
30
XDOT = 17288
189381 XDOT = 5207
883757
YDOT = 11804
063917 feet/sec YDOT = 3656
460451 meter/sec
ZDOT = 14137
872430 ZDOT = 4334
671992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18436217
46 X = 5619359
08
Y = 1455272
48 feet Y = 443567
05 meter
Z = -11996155
61 Z = -3656428
23
XDOT = 7892
478560 XDOT = 2405
627465
YDOT = 18017
054889 feet/sec YDOT = 5491
598330 meter/sec
ZDOT = 14233
900391 ZDOT = 4338
492839
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 07048
50775583
00020000 00000-0 20000-3 0 9086
2 25544 51
6327 2
4831 0020978 218
2552 141
7126 15
78392286 31877
Satellite: ISS
Catalog Number: 25544
Epoch time: 07048
50775583 = yrday
fracday
Element set: 908
Inclination: 51
6327 deg
RA of node: 2
4831 deg
Eccentricity:
0020978
Arg of perigee: 218
2552 deg
Mean anomaly: 141
7126 deg
Mean motion: 15
78392286 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3187
Checksum: 305
Coasting Arc #10 (Orbit 3202)
---------------------------------------
Vector Time (GMT): 2007/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3363744
58 A = 6710030
60 meter
Y = -3492043
56 meter E =
0012480
Z = -4629867
73 I = 51
60363
XDOT = 6661
460948 Wp = 196
92040
YDOT = -2633
683779 meter/sec RA = 356
89513 deg
ZDOT = -2863
149735 TA = 44
86367
MA = 44
76285
Ha = 186
965 n
mi
Hp = 175
093
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11035907
41 X = -3301955
64
Y = -11456835
82 feet Y = -3529313
61 meter
Z = -15189854
77 Z = -4646058
05
XDOT = 21855
186836 XDOT = 6704
324347
YDOT = -8640
694813 feet/sec YDOT = -2558
952105 meter/sec
ZDOT = -9393
535875 ZDOT = -2830
685039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3037078
46 X = -925701
51
Y = -15555132
89 feet Y = -4741204
50 meter
Z = -15251099
06 Z = -4648534
99
XDOT = 21971
932564 XDOT = 6697
045046
YDOT = 4769
293534 feet/sec YDOT = 1453
680669 meter/sec
ZDOT = -9271
930258 ZDOT = -2826
084343
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 07049
52073137
00020000 00000-0 20000-3 0 9096
2 25544 51
6336 357
2461 0020950 222
1361 137
8195 15
78461605 32032
Satellite: ISS
Catalog Number: 25544
Epoch time: 07049
52073137 = yrday
fracday
Element set: 909
Inclination: 51
6336 deg
RA of node: 357
2461 deg
Eccentricity:
0020950
Arg of perigee: 222
1361 deg
Mean anomaly: 137
8195 deg
Mean motion: 15
78461605 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3203
Checksum: 280
Coasting Arc #11 (Orbit 3218)
---------------------------------------
Vector Time (GMT): 2007/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6361783
76 A = 6718969
57 meter
Y = 1809342
06 meter E =
0022548
Z = 1099176
64 I = 51
60579
XDOT = -2269
143042 Wp = 188
58440
YDOT = -4406
829662 meter/sec RA = 351
69116 deg
ZDOT = -5916
624541 TA = 339
34183
MA = 339
43284
Ha = 186
776 n
mi
Hp = 175
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20871993
96 X = -6386882
74
Y = 5936161
60 feet Y = 1738060
78 meter
Z = 3606222
57 Z = 1068210
72
XDOT = -7444
695019 XDOT = -2190
955366
YDOT = -14458
102566 feet/sec YDOT = -4431
767745 meter/sec
ZDOT = -19411
497838 ZDOT = -5927
457551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20896820
18 X = -6369350
79
Y = -5918171
71 feet Y = -1803858
74 meter
Z = 3490148
65 Z = 1063797
31
XDOT = 916
380323 XDOT = 279
312722
YDOT = -14632
929739 feet/sec YDOT = -4460
116985 meter/sec
ZDOT = -19452
736336 ZDOT = -5929
194035
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 07050
53367973
00020000 00000-0 20000-3 0 9105
2 25544 51
6342 352
0095 0020983 225
9121 134
0318 15
78481550 32190
Satellite: ISS
Catalog Number: 25544
Epoch time: 07050
53367973 = yrday
fracday
Element set: 910
Inclination: 51
6342 deg
RA of node: 352
0095 deg
Eccentricity:
0020983
Arg of perigee: 225
9121 deg
Mean anomaly: 134
0318 deg
Mean motion: 15
78481550 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3219
Checksum: 277
Coasting Arc #12 (Orbit 3234)
---------------------------------------
Vector Time (GMT): 2007/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 470926
01 A = 6707237
07 meter
Y = 4169817
06 meter E =
0018427
Z = 5243083
45 I = 51
53876
XDOT = -7551
562200 Wp = 226
94774
YDOT = 1426
268805 meter/sec RA = 346
52332 deg
ZDOT = -469
441322 TA = 227
44030
MA = 227
59597
Ha = 186
342 n
mi
Hp = 175
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1545032
83 X = 398793
99
Y = 13680502
15 feet Y = 4174680
27 meter
Z = 17201717
35 Z = 5245195
67
XDOT = -24775
466537 XDOT = -7564
669274
YDOT = 4679
359597 feet/sec YDOT = 1341
749700 meter/sec
ZDOT = -1540
161819 ZDOT = -506
158125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5735743
78 X = -1748254
70
Y = 12504139
85 feet Y = 3811261
83 meter
Z = 17210173
60 Z = 5245660
91
XDOT = -22774
430056 XDOT = -6941
646281
YDOT = -8197
931758 feet/sec YDOT = -2498
729600 meter/sec
ZDOT = -1677
877255 ZDOT = -511
416987
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 07051
54659848
00020000 00000-0 20000-3 0 9113
2 25544 51
6343 346
7727 0021007 230
1657 129
7661 15
78555751 32358
Satellite: ISS
Catalog Number: 25544
Epoch time: 07051
54659848 = yrday
fracday
Element set: 911
Inclination: 51
6343 deg
RA of node: 346
7727 deg
Eccentricity:
0021007
Arg of perigee: 230
1657 deg
Mean anomaly: 129
7661 deg
Mean motion: 15
78555751 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3235
Checksum: 303
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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