Date:
January 8th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 15 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 2555)
---------------------------------------
Vector Time (GMT): 2007/008/11:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4485655
10 A = 6714511
06 meter
Y = -1796139
85 meter E =
0030945
Z = 4643403
74 I = 51
46946
XDOT = 4992
343111 Wp = 66
73393
YDOT = 5185
341915 meter/sec RA = 208
10649 deg
ZDOT = -2790
258503 TA = 50
92179
MA = 50
64692
Ha = 193
909 n
mi
Hp = 171
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14716716
21 X = 4482850
00
Y = -5892847
27 feet Y = -1745994
78 meter
Z = 15234264
25 Z = 4665187
72
XDOT = 16379
078449 XDOT = 4947
543174
YDOT = 17012
276623 feet/sec YDOT = 5240
918787 meter/sec
ZDOT = -9154
391413 ZDOT = -2766
114574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9462522
16 X = 2884176
75
Y = 12620694
37 feet Y = 3846787
65 meter
Z = 15315643
64 Z = 4668208
18
XDOT = -11286
796467 XDOT = -3440
215563
YDOT = 19566
788373 feet/sec YDOT = 5963
957096 meter/sec
ZDOT = -9063
269819 ZDOT = -2762
484641
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 07008
53727858
00020000 00000-0 20000-3 0 9009
2 25544 51
6313 208
8598 0023088 67
8384 292
5228 15
76855738 25561
Satellite: ISS
Catalog Number: 25544
Epoch time: 07008
53727858 = yrday
fracday
Element set: 900
Inclination: 51
6313 deg
RA of node: 208
8598 deg
Eccentricity:
0023088
Arg of perigee: 67
8384 deg
Mean anomaly: 292
5228 deg
Mean motion: 15
76855738 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2556
Checksum: 332
Coasting Arc #2 (Orbit 2571)
---------------------------------------
Vector Time (GMT): 2007/009/11:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3885264
73 A = 6719526
31 meter
Y = -4418228
50 meter E =
0035682
Z = 3207509
75 I = 51
51139
XDOT = 5843
129667 Wp = 77
44377
YDOT = -1645
362353 meter/sec RA = 202
98465 deg
ZDOT = 4774
661332 TA = 320
25583
MA = 320
51672
Ha = 193
994 n
mi
Hp = 171
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12746931
52 X = -3851151
99
Y = -14495500
32 feet Y = -4461485
16 meter
Z = 10523325
96 Z = 3188717
98
XDOT = 19170
372924 XDOT = 5837
899959
YDOT = -5398
170451 feet/sec YDOT = -1580
050774 meter/sec
ZDOT = 15664
899384 ZDOT = 4803
034045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10430073
05 X = 3179086
26
Y = -16288222
67 feet Y = -4964650
27 meter
Z = 10452347
13 Z = 3185875
41
XDOT = 9234
926113 XDOT = 2814
805479
YDOT = 16111
776170 feet/sec YDOT = 4910
869377 meter/sec
ZDOT = 15770
987578 ZDOT = 4806
997014
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 07009
55126922
00020000 00000-0 20000-3 0 9018
2 25544 51
6304 203
6289 0023023 71
8660 288
5009 15
76892652 25728
Satellite: ISS
Catalog Number: 25544
Epoch time: 07009
55126922 = yrday
fracday
Element set: 901
Inclination: 51
6304 deg
RA of node: 203
6289 deg
Eccentricity:
0023023
Arg of perigee: 71
8660 deg
Mean anomaly: 288
5009 deg
Mean motion: 15
76892652 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2572
Checksum: 288
Coasting Arc #3 (Orbit 2586)
---------------------------------------
Vector Time (GMT): 2007/010/11:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5633019
70 A = 6718479
10 meter
Y = 1119283
26 meter E =
0028139
Z = -3505226
23 I = 51
53466
XDOT = -3768
110460 Wp = 79
80389
YDOT = -4965
805863 meter/sec RA = 197
76614 deg
ZDOT = 4505
277939 TA = 238
48623
MA = 238
76142
Ha = 193
964 n
mi
Hp = 170
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18481035
76 X = -5628089
45
Y = 3672189
16 feet Y = 1056319
49 meter
Z = -11500086
05 Z = -3532579
11
XDOT = -12362
567126 XDOT = -3734
187661
YDOT = -16292
013986 feet/sec YDOT = -5007
753592 meter/sec
ZDOT = 14781
095602 ZDOT = 4487
054724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8866238
02 X = -2702429
35
Y = -16554731
44 feet Y = -5045882
14 meter
Z = -11602427
57 Z = -3536419
92
XDOT = 10764
995149 XDOT = 3281
170521
YDOT = -15995
651342 feet/sec YDOT = -4875
474529 meter/sec
ZDOT = 14712
169952 ZDOT = 4484
269401
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 07010
50186816
00020000 00000-0 20000-3 0 9024
2 25544 51
6299 198
7243 0023148 75
6194 284
7538 15
76901049 25879
Satellite: ISS
Catalog Number: 25544
Epoch time: 07010
50186816 = yrday
fracday
Element set: 902
Inclination: 51
6299 deg
RA of node: 198
7243 deg
Eccentricity:
0023148
Arg of perigee: 75
6194 deg
Mean anomaly: 284
7538 deg
Mean motion: 15
76901049 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2587
Checksum: 315
Coasting Arc #4 (Orbit 2602)
---------------------------------------
Vector Time (GMT): 2007/011/11:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2547825
77 A = 6714922
82 meter
Y = 4269966
10 meter E =
0033195
Z = -4544477
01 I = 51
55011
XDOT = -6983
685966 Wp = 76
81780
YDOT = 922
537185 meter/sec RA = 192
65003 deg
ZDOT = -3059
836707 TA = 162
66043
MA = 162
54679
Ha = 193
998 n
mi
Hp = 170
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8359008
45 X = 2521965
14
Y = 14009075
14 feet Y = 4298313
05 meter
Z = -14909701
49 Z = -4532162
27
XDOT = -22912
355531 XDOT = -6978
618839
YDOT = 3026
696802 feet/sec YDOT = 844
470276 meter/sec
ZDOT = -10038
834342 ZDOT = -3093
750839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10740514
39 X = -3273708
79
Y = 12335272
42 feet Y = 3759791
03 meter
Z = -14863001
44 Z = -4530242
84
XDOT = -8998
944610 XDOT = -2742
878317
YDOT = -20039
673519 feet/sec YDOT = -6108
092488 meter/sec
ZDOT = -10165
793999 ZDOT = -3098
534011
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 07011
51581975
00020000 00000-0 20000-3 0 9032
2 25544 51
6297 193
4932 0023252 79
4551 280
9231 15
76941213 26033
Satellite: ISS
Catalog Number: 25544
Epoch time: 07011
51581975 = yrday
fracday
Element set: 903
Inclination: 51
6297 deg
RA of node: 193
4932 deg
Eccentricity:
0023252
Arg of perigee: 79
4551 deg
Mean anomaly: 280
9231 deg
Mean motion: 15
76941213 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2603
Checksum: 287
Coasting Arc #5 (Orbit 2618)
---------------------------------------
Vector Time (GMT): 2007/012/11:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6456387
44 A = 6722263
32 meter
Y = -554450
94 meter E =
0035815
Z = 1749654
21 I = 51
60394
XDOT = 1981
992089 Wp = 95
09159
YDOT = 4809
361905 meter/sec RA = 187
44684 deg
ZDOT = -5693
428155 TA = 65
48197
MA = 65
10899
Ha = 193
792 n
mi
Hp = 170
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21182373
48 X = 6453608
07
Y = -1819064
76 feet Y = -482267
71 meter
Z = 5740335
35 Z = 1781012
39
XDOT = 6502
598716 XDOT = 1955
723325
YDOT = 15778
746406 feet/sec YDOT = 4831
379260 meter/sec
ZDOT = -18679
226229 ZDOT = -5683
863073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8560685
79 X = 2609297
03
Y = 19425615
21 feet Y = 5920927
52 meter
Z = 5857774
79 Z = 1785449
76
XDOT = -11378
348040 XDOT = -3468
120483
YDOT = 10729
360550 feet/sec YDOT = 3270
309096 meter/sec
ZDOT = -18642
757804 ZDOT = -5682
312579
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 07012
52974864
00020000 00000-0 20000-3 0 9048
2 25544 51
6298 188
2614 0022999 82
8086 277
5692 15
77004420 26192
Satellite: ISS
Catalog Number: 25544
Epoch time: 07012
52974864 = yrday
fracday
Element set: 904
Inclination: 51
6298 deg
RA of node: 188
2614 deg
Eccentricity:
0022999
Arg of perigee: 82
8086 deg
Mean anomaly: 277
5692 deg
Mean motion: 15
77004420 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2619
Checksum: 322
Coasting Arc #6 (Orbit 2634)
---------------------------------------
Vector Time (GMT): 2007/013/11:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -864311
94 A = 6711959
32 meter
Y = -4147327
36 meter E =
0026190
Z = 5183763
83 I = 51
59649
XDOT = 7658
067073 Wp = 91
79089
YDOT = -428
343542 meter/sec RA = 182
31015 deg
ZDOT = 929
346333 TA = 349
35202
MA = 349
40737
Ha = 194
019 n
mi
Hp = 170
799
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2835669
09 X = -843053
38
Y = -13606717
05 feet Y = -4156874
25 meter
Z = 17007099
19 Z = 5179616
23
XDOT = 25124
891971 XDOT = 7657
773131
YDOT = -1405
326583 feet/sec YDOT = -342
708516 meter/sec
ZDOT = 3049
036527 ZDOT = 966
548310
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11803150
60 X = 3597600
30
Y = -7376727
66 feet Y = -2248426
59 meter
Z = 16991018
68 Z = 5178862
49
XDOT = 9310
403687 XDOT = 2837
811044
YDOT = 22277
502230 feet/sec YDOT = 6790
182680 meter/sec
ZDOT = 3188
404373 ZDOT = 971
825653
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 07013
54366132
00020000 00000-0 20000-3 0 9055
2 25544 51
6290 183
0302 0023234 87
0623 273
3200 15
76964086 26357
Satellite: ISS
Catalog Number: 25544
Epoch time: 07013
54366132 = yrday
fracday
Element set: 905
Inclination: 51
6290 deg
RA of node: 183
0302 deg
Eccentricity:
0023234
Arg of perigee: 87
0623 deg
Mean anomaly: 273
3200 deg
Mean motion: 15
76964086 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2635
Checksum: 264
Coasting Arc #7 (Orbit 2650)
---------------------------------------
Vector Time (GMT): 2007/014/11:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6712228
50 A = 6723546
14 meter
Y = 195446
60 meter E =
0033359
Z = 176047
47 I = 51
66550
XDOT = 43
852924 Wp = 76
14345
YDOT = -4785
008534 meter/sec RA = 177
14428 deg
ZDOT = 6041
099533 TA = 285
77122
MA = 286
13885
Ha = 193
843 n
mi
Hp = 170
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22021747
05 X = -6714770
35
Y = 641229
01 feet Y = 120372
49 meter
Z = 577583
57 Z = 143433
49
XDOT = 143
874423 XDOT = 68
009900
YDOT = -15698
846896 feet/sec YDOT = -4784
383825 meter/sec
ZDOT = 19819
880358 ZDOT = 6041
370655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8434038
30 X = -2570694
87
Y = -20355877
76 feet Y = -6204471
54 meter
Z = 455366
79 Z = 138795
80
XDOT = 13199
770632 XDOT = 4023
290089
YDOT = -4937
865600 feet/sec YDOT = -1505
061435 meter/sec
ZDOT = 19820
280273 ZDOT = 6041
221427
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 07014
55754865
00020000 00000-0 20000-3 0 9062
2 25544 51
6296 177
7989 0023204 91
2580 269
1243 15
77038528 26512
Satellite: ISS
Catalog Number: 25544
Epoch time: 07014
55754865 = yrday
fracday
Element set: 906
Inclination: 51
6296 deg
RA of node: 177
7989 deg
Eccentricity:
0023204
Arg of perigee: 91
2580 deg
Mean anomaly: 269
1243 deg
Mean motion: 15
77038528 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2651
Checksum: 316
Coasting Arc #8 (Orbit 2665)
---------------------------------------
Vector Time (GMT): 2007/015/11:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -981772
88 A = 6712034
70 meter
Y = 4243848
16 meter E =
0037300
Z = -5139263
05 I = 51
65577
XDOT = -7548
611742 Wp = 97
25769
YDOT = -54
679689 meter/sec RA = 171
97360 deg
ZDOT = 1400
938522 TA = 186
17250
MA = 186
21859
Ha = 193
831 n
mi
Hp = 170
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3221039
64 X = -1004189
83
Y = 13923386
34 feet Y = 4232744
81 meter
Z = -16861099
25 Z = -5144086
32
XDOT = -24765
786554 XDOT = -7554
244726
YDOT = -179
395305 feet/sec YDOT = -139
124157 meter/sec
ZDOT = 4596
254994 ZDOT = 1364
253984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14088241
46 X = -4294096
00
Y = 2272789
84 feet Y = 692746
34 meter
Z = -16878635
32 Z = -5144608
05
XDOT = -8883
744990 XDOT = -2707
765473
YDOT = -22053
582518 feet/sec YDOT = -6721
931952 meter/sec
ZDOT = 4458
731771 ZDOT = 1359
021444
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 07015
50805016
00020000 00000-0 20000-3 0 9074
2 25544 51
6301 172
8946 0023247 94
7643 265
6177 15
77056818 26668
Satellite: ISS
Catalog Number: 25544
Epoch time: 07015
50805016 = yrday
fracday
Element set: 907
Inclination: 51
6301 deg
RA of node: 172
8946 deg
Eccentricity:
0023247
Arg of perigee: 94
7643 deg
Mean anomaly: 265
6177 deg
Mean motion: 15
77056818 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2666
Checksum: 304
Coasting Arc #9 (Orbit 2681)
---------------------------------------
Vector Time (GMT): 2007/016/11:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6329951
19 A = 6721194
95 meter
Y = 338776
66 meter E =
0028213
Z = -2242653
68 I = 51
71527
XDOT = -2182
474069 Wp = 106
39399
YDOT = 4949
372539 meter/sec RA = 166
84806 deg
ZDOT = -5476
821788 TA = 98
75088
MA = 98
43124
Ha = 193
764 n
mi
Hp = 170
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20767556
40 X = 6336586
75
Y = 1111471
99 feet Y = 409599
13 meter
Z = -7357787
66 Z = -2211887
01
XDOT = -7160
347994 XDOT = -2211
051394
YDOT = 16238
098880 feet/sec YDOT = 4924
807935 meter/sec
ZDOT = -17968
575420 ZDOT = -5487
492781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7041955
12 X = 2146387
92
Y = 19611791
80 feet Y = 5977674
14 meter
Z = -7242395
91 Z = -2207482
27
XDOT = -16275
375773 XDOT = -4960
734535
YDOT = -726
909855 feet/sec YDOT = -221
562124 meter/sec
ZDOT = -18007
948717 ZDOT = -5488
822769
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 07016
52189633
00020000 00000-0 20000-3 0 9088
2 25544 51
6300 167
6618 0023210 98
2099 262
1699 15
77113652 26828
Satellite: ISS
Catalog Number: 25544
Epoch time: 07016
52189633 = yrday
fracday
Element set: 908
Inclination: 51
6300 deg
RA of node: 167
6618 deg
Eccentricity:
0023210
Arg of perigee: 98
2099 deg
Mean anomaly: 262
1699 deg
Mean motion: 15
77113652 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2682
Checksum: 298
Coasting Arc #10 (Orbit 2697)
---------------------------------------
Vector Time (GMT): 2007/017/11:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2723034
16 A = 6715442
08 meter
Y = -4420375
46 meter E =
0032208
Z = 4230599
46 I = 51
72367
XDOT = 6800
103889 Wp = 93
77854
YDOT = 730
776264 meter/sec RA = 161
64933 deg
ZDOT = -3592
155015 TA = 32
64257
MA = 32
44390
Ha = 193
690 n
mi
Hp = 170
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8933839
11 X = 2751709
95
Y = -14502544
17 feet Y = -4389765
27 meter
Z = 13879919
50 Z = 4243896
71
XDOT = 22310
052130 XDOT = 6808
876556
YDOT = 2397
559921 feet/sec YDOT = 806
868393 meter/sec
ZDOT = -11785
285481 ZDOT = -3559
099317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16843175
71 X = 5133799
96
Y = 2252524
58 feet Y = 686569
49 meter
Z = 13929213
87 Z = 4245624
39
XDOT = 6997
978139 XDOT = 2132
983737
YDOT = 20212
282836 feet/sec YDOT = 6160
703808 meter/sec
ZDOT = -11661
243553 ZDOT = -3554
347035
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 07017
53572243
00020000 00000-0 20000-3 0 9094
2 25544 51
6302 162
4302 0023218 102
3242 258
0524 15
77106036 26984
Satellite: ISS
Catalog Number: 25544
Epoch time: 07017
53572243 = yrday
fracday
Element set: 909
Inclination: 51
6302 deg
RA of node: 162
4302 deg
Eccentricity:
0023218
Arg of perigee: 102
3242 deg
Mean anomaly: 258
0524 deg
Mean motion: 15
77106036 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2698
Checksum: 260
Coasting Arc #11 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2007/018/11:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5373130
42 A = 6716628
46 meter
Y = -1003569
33 meter E =
0034359
Z = 3881265
32 I = 51
75641
XDOT = 3952
539740 Wp = 104
09856
YDOT = -5222
631947 meter/sec RA = 156
54840 deg
ZDOT = 4083
226442 TA = 303
39186
MA = 303
72013
Ha = 193
625 n
mi
Hp = 170
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17628380
64 X = -5380363
04
Y = -3292550
29 feet Y = -1063695
63 meter
Z = 12733810
12 Z = 3855145
59
XDOT = 12967
650067 XDOT = 3990
811107
YDOT = -17134
619250 feet/sec YDOT = -5178
219016 meter/sec
ZDOT = 13396
412211 ZDOT = 4102
519661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4428880
45 X = -1349922
76
Y = -17449184
64 feet Y = -5318511
48 meter
Z = 12635726
52 Z = 3851369
44
XDOT = 19688
567777 XDOT = 6001
075458
YDOT = 4846
963446 feet/sec YDOT = 1477
354458 meter/sec
ZDOT = 13468
095108 ZDOT = 4105
075389
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 07018
54952388
00020000 00000-0 20000-3 0 9100
2 25544 51
6317 157
1991 0023077 106
2192 254
1514 15
77190733 27147
Satellite: ISS
Catalog Number: 25544
Epoch time: 07018
54952388 = yrday
fracday
Element set: 910
Inclination: 51
6317 deg
RA of node: 157
1991 deg
Eccentricity:
0023077
Arg of perigee: 106
2192 deg
Mean anomaly: 254
1514 deg
Mean motion: 15
77190733 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2714
Checksum: 289
Coasting Arc #12 (Orbit 2728)
---------------------------------------
Vector Time (GMT): 2007/019/11:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4054135
03 A = 6719854
60 meter
Y = 4642636
94 meter E =
0026352
Z = -2706675
06 I = 51
79443
XDOT = -5401
956502 Wp = 101
44804
YDOT = -1709
364612 meter/sec RA = 151
34941 deg
ZDOT = 5196
587919 TA = 227
77610
MA = 228
00001
Ha = 193
501 n
mi
Hp = 170
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13300967
95 X = -4092600
19
Y = 15231748
48 feet Y = 4597086
58 meter
Z = -8880167
51 Z = -2726462
39
XDOT = -17722
954402 XDOT = -5407
684018
YDOT = -5608
151615 feet/sec YDOT = -1769
804900 meter/sec
ZDOT = 17049
172961 ZDOT = 5170
331865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19477785
12 X = -5936828
90
Y = -5312712
74 feet Y = -1619314
84 meter
Z = -8953784
42 Z = -2729113
49
XDOT = -3081
908776 XDOT = -939
365795
YDOT = -17063
431427 feet/sec YDOT = -5200
933899 meter/sec
ZDOT = 16950
473395 ZDOT = 5166
504291
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 07019
49994523
00020000 00000-0 20000-3 0 9113
2 25544 51
6327 152
2949 0023104 109
3847 250
9818 15
77191158 27298
Satellite: ISS
Catalog Number: 25544
Epoch time: 07019
49994523 = yrday
fracday
Element set: 911
Inclination: 51
6327 deg
RA of node: 152
2949 deg
Eccentricity:
0023104
Arg of perigee: 109
3847 deg
Mean anomaly: 250
9818 deg
Mean motion: 15
77191158 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2729
Checksum: 313
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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