Date:
June 5th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5704 87 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 876)
---------------------------------------
Vector Time (GMT): 2007/155/11:56:02
145
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1542637
78 A = 6709785
10 meter
Y = 4289040
37 meter E =
0004786
Z = -4928328
93 I = 51
67980
XDOT = -7400
156146 Wp = 117
34607
YDOT = -212
041835 meter/sec RA = 168
49024 deg
ZDOT = 2131
233012 TA = 173
30431
MA = 173
29792
Ha = 181
912 n
mi
Hp = 180
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5061147
56 X = -1566542
90
Y = 14071654
75 feet Y = 4271657
03 meter
Z = -16169058
16 Z = -4935880
28
XDOT = -24278
727514 XDOT = -7407
588198
YDOT = -695
675311 feet/sec YDOT = -294
836501 meter/sec
ZDOT = 6992
234291 ZDOT = 2095
264997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11657719
42 X = 3553272
88
Y = 9317648
13 feet Y = 2840019
15 meter
Z = -16197040
93 Z = -4936858
08
XDOT = -7966
384446 XDOT = -2428
153979
YDOT = 21889
094761 feet/sec YDOT = 6671
796083 meter/sec
ZDOT = 6856
433327 ZDOT = 2089
840878
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 07155
50951866
00020000 00000-0 20000-3 0 9007
2 25544 51
6319 169
4278 0008165 278
7586 81
2655 15
78134196 8771
Satellite: ISS
Catalog Number: 25544
Epoch time: 07155
50951866 = yrday
fracday
Element set: 900
Inclination: 51
6319 deg
RA of node: 169
4278 deg
Eccentricity:
0008165
Arg of perigee: 278
7586 deg
Mean anomaly: 81
2655 deg
Mean motion: 15
78134196 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 877
Checksum: 330
Coasting Arc #2 (Orbit 892)
---------------------------------------
Vector Time (GMT): 2007/156/11:56:02
145
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5910695
47 A = 6716250
16 meter
Y = 778928
46 meter E =
0003614
Z = -3090265
07 I = 51
72885
XDOT = -3223
107912 Wp = 278
05533
YDOT = 4997
176870 meter/sec RA = 163
36907 deg
ZDOT = -4899
849735 TA = 297
83036
MA = 297
86698
Ha = 182
134 n
mi
Hp = 180
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19392045
49 X = 5916557
96
Y = 2555539
57 feet Y = 845058
50 meter
Z = -10138664
93 Z = -3061536
65
XDOT = -10574
501022 XDOT = -3254
945041
YDOT = 16394
937237 feet/sec YDOT = 4960
957128 meter/sec
ZDOT = -16075
622491 ZDOT = -4915
583980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8500087
70 X = 2590826
73
Y = -17678239
29 feet Y = -5388327
34 meter
Z = -10030109
77 Z = -3057177
46
XDOT = 11012
755492 XDOT = 3356
687874
YDOT = 14459
430570 feet/sec YDOT = 4407
234438 meter/sec
ZDOT = -16134
413867 ZDOT = -4917
769347
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 07156
52266649
00020000 00000-0 20000-3 0 9019
2 25544 51
6310 164
1913 0008104 282
5922 77
4337 15
78170950 8930
Satellite: ISS
Catalog Number: 25544
Epoch time: 07156
52266649 = yrday
fracday
Element set: 901
Inclination: 51
6310 deg
RA of node: 164
1913 deg
Eccentricity:
0008104
Arg of perigee: 282
5922 deg
Mean anomaly: 77
4337 deg
Mean motion: 15
78170950 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 893
Checksum: 291
Coasting Arc #3 (Orbit 908)
---------------------------------------
Vector Time (GMT): 2007/157/11:56:02
145
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3895374
58 A = 6715330
87 meter
Y = -4362340
59 meter E =
0005386
Z = 3298397
99 I = 51
75361
XDOT = 5860
699888 Wp = 65
89574
YDOT = 1658
694615 meter/sec RA = 158
15795 deg
ZDOT = -4719
524344 TA = 75
38526
MA = 75
32555
Ha = 182
329 n
mi
Hp = 180
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12780100
34 X = 3927842
46
Y = -14312141
04 feet Y = -4318599
30 meter
Z = 10821515
71 Z = 3317399
83
XDOT = 19228
018006 XDOT = 5864
643030
YDOT = 5441
911467 feet/sec YDOT = 1724
255021 meter/sec
ZDOT = -15484
003753 ZDOT = -4691
043359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9908678
68 X = -3020165
26
Y = -16384142
90 feet Y = -4993886
76 meter
Z = 10892726
76 Z = 3320103
12
XDOT = 9717
501138 XDOT = 2961
894347
YDOT = -16117
244269 feet/sec YDOT = -4912
536053 meter/sec
ZDOT = -15376
263029 ZDOT = -4686
684971
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 07157
53579474
00020000 00000-0 20000-3 0 9025
2 25544 51
6307 158
9548 0008176 287
6514 72
3758 15
78237760 9095
Satellite: ISS
Catalog Number: 25544
Epoch time: 07157
53579474 = yrday
fracday
Element set: 902
Inclination: 51
6307 deg
RA of node: 158
9548 deg
Eccentricity:
0008176
Arg of perigee: 287
6514 deg
Mean anomaly: 72
3758 deg
Mean motion: 15
78237760 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 909
Checksum: 332
Coasting Arc #4 (Orbit 924)
---------------------------------------
Vector Time (GMT): 2007/158/11:56:02
145
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4095076
63 A = 6710012
87 meter
Y = -2197640
76 meter E =
0001748
Z = 4841562
46 I = 51
76117
XDOT = 5453
839365 Wp = 249
13586
YDOT = -4889
771742 meter/sec RA = 153
04294 deg
ZDOT = 2393
506628 TA = 177
57052
MA = 177
56967
Ha = 182
610 n
mi
Hp = 180
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13435290
79 X = -4093717
30
Y = -7210107
48 feet Y = -2243427
24 meter
Z = 15884391
26 Z = 4821671
64
XDOT = 17893
173771 XDOT = 5496
484977
YDOT = -16042
558208 feet/sec YDOT = -4828
545723 meter/sec
ZDOT = 7852
712034 ZDOT = 2420
104251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10701157
23 X = -3261712
72
Y = 10971187
64 feet Y = 3344017
99 meter
Z = 15809011
66 Z = 4818586
75
XDOT = -9617
512985 XDOT = -2931
417958
YDOT = -20839
701278 feet/sec YDOT = -6351
940950 meter/sec
ZDOT = 7952
545276 ZDOT = 2423
935800
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 07158
54890572
00020000 00000-0 20000-3 0 9033
2 25544 51
6302 153
7181 0008191 291
4795 68
5496 15
78231731 9253
Satellite: ISS
Catalog Number: 25544
Epoch time: 07158
54890572 = yrday
fracday
Element set: 903
Inclination: 51
6302 deg
RA of node: 153
7181 deg
Eccentricity:
0008191
Arg of perigee: 291
4795 deg
Mean anomaly: 68
5496 deg
Mean motion: 15
78231731 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 925
Checksum: 308
Coasting Arc #5 (Orbit 939)
---------------------------------------
Vector Time (GMT): 2007/159/11:56:02
145
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5332360
69 A = 6719705
11 meter
Y = 4013383
63 meter E =
0011475
Z = -714124
00 I = 51
81990
XDOT = -3395
316212 Wp = 357
41415
YDOT = -3443
927858 meter/sec RA = 147
85987 deg
ZDOT = 6005
422094 TA = 354
80699
MA = 354
81889
Ha = 182
538 n
mi
Hp = 179
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17494621
68 X = -5373373
53
Y = 13167269
14 feet Y = 3953524
96 meter
Z = -2342926
50 Z = -740127
79
XDOT = -11139
488884 XDOT = -3385
726647
YDOT = -11298
975913 feet/sec YDOT = -3481
843274 meter/sec
ZDOT = 19702
828393 ZDOT = 5988
950516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8110300
14 X = 2472019
48
Y = 20327184
17 feet Y = 6195725
74 meter
Z = -2440631
94 Z = -743904
61
XDOT = -12376
006219 XDOT = -3772
206696
YDOT = 7293
181256 feet/sec YDOT = 2222
961647 meter/sec
ZDOT = 19640
202521 ZDOT = 5986
333728
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 07159
49867853
00020000 00000-0 20000-3 0 9045
2 25544 51
6302 148
8095 0008021 294
3468 65
6859 15
78307176 9408
Satellite: ISS
Catalog Number: 25544
Epoch time: 07159
49867853 = yrday
fracday
Element set: 904
Inclination: 51
6302 deg
RA of node: 148
8095 deg
Eccentricity:
0008021
Arg of perigee: 294
3468 deg
Mean anomaly: 65
6859 deg
Mean motion: 15
78307176 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 940
Checksum: 325
Coasting Arc #6 (Orbit 955)
---------------------------------------
Vector Time (GMT): 2007/160/11:56:02
145
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1762425
76 A = 6708134
66 meter
Y = 3826679
24 meter E =
0007894
Z = -5226240
02 I = 51
80379
XDOT = -6465
213434 Wp = 72
34500
YDOT = 4104
886401 meter/sec RA = 142
70336 deg
ZDOT = 828
743545 TA = 205
50386
MA = 205
54283
Ha = 182
919 n
mi
Hp = 179
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5782236
76 X = 1744892
58
Y = 12554721
91 feet Y = 3846290
24 meter
Z = -17146456
77 Z = -5217720
25
XDOT = -21211
330165 XDOT = -6514
660275
YDOT = 13467
475070 feet/sec YDOT = 4032
312191 meter/sec
ZDOT = 2718
974884 ZDOT = 797
215702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13615422
56 X = 4149980
80
Y = -2606525
10 feet Y = -794468
85 meter
Z = -17113812
53 Z = -5216290
06
XDOT = 7637
744225 XDOT = 2327
984440
YDOT = 22895
417002 feet/sec YDOT = 6978
523102 meter/sec
ZDOT = 2600
411213 ZDOT = 792
605338
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 07160
51175120
00020000 00000-0 20000-3 0 9050
2 25544 51
6297 143
5721 0008212 299
2572 60
7771 15
78279718 9567
Satellite: ISS
Catalog Number: 25544
Epoch time: 07160
51175120 = yrday
fracday
Element set: 905
Inclination: 51
6297 deg
RA of node: 143
5721 deg
Eccentricity:
0008212
Arg of perigee: 299
2572 deg
Mean anomaly: 60
7771 deg
Mean motion: 15
78279718 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 956
Checksum: 299
Coasting Arc #7 (Orbit 971)
---------------------------------------
Vector Time (GMT): 2007/161/11:56:02
145
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5664418
81 A = 6717966
14 meter
Y = -2922902
91 meter E =
0002657
Z = -2118942
66 I = 51
85960
XDOT = 657
977623 Wp = 263
22507
YDOT = 5302
478031 meter/sec RA = 137
57412 deg
ZDOT = -5549
801540 TA = 300
42123
MA = 300
44749
Ha = 183
007 n
mi
Hp = 179
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18584051
21 X = 5706975
70
Y = -9589576
46 feet Y = -2859321
98 meter
Z = -6951911
61 Z = -2091321
60
XDOT = 2158
719235 XDOT = 625
595867
YDOT = 17396
581467 feet/sec YDOT = 5309
655560 meter/sec
ZDOT = -18208
010303 ZDOT = -5546
683027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5060537
28 X = -1542451
76
Y = -20326154
98 feet Y = -6195412
04 meter
Z = -6847948
40 Z = -2087254
67
XDOT = 15968
960920 XDOT = 4867
339289
YDOT = 2160
691305 feet/sec YDOT = 658
578710 meter/sec
ZDOT = -18195
587943 ZDOT = -5546
015205
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 07161
52480371
00020000 00000-0 20000-3 0 9060
2 25544 51
6297 138
3348 0008252 303
8534 56
1846 15
78334607 9727
Satellite: ISS
Catalog Number: 25544
Epoch time: 07161
52480371 = yrday
fracday
Element set: 906
Inclination: 51
6297 deg
RA of node: 138
3348 deg
Eccentricity:
0008252
Arg of perigee: 303
8534 deg
Mean anomaly: 56
1846 deg
Mean motion: 15
78334607 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 972
Checksum: 299
Coasting Arc #8 (Orbit 987)
---------------------------------------
Vector Time (GMT): 2007/162/11:56:02
145
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 524385
03 A = 6712536
75 meter
Y = -5314719
79 meter E =
0008395
Z = 4068748
51 I = 51
86168
XDOT = 6242
018788 Wp = 25
95342
YDOT = -2346
229441 meter/sec RA = 132
37602 deg
ZDOT = -3858
819778 TA = 103
64700
MA = 103
55351
Ha = 183
145 n
mi
Hp = 179
205
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1720423
33 X = 564010
50
Y = -17436744
71 feet Y = -5308634
89 meter
Z = 13348912
45 Z = 4071391
45
XDOT = 20479
064265 XDOT = 6286
536464
YDOT = -7697
603152 feet/sec YDOT = -2276
178183 meter/sec
ZDOT = -12660
169876 ZDOT = -3828
387831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16687833
21 X = -5086451
56
Y = -5316632
80 feet Y = -1620509
68 meter
Z = 13358256
80 Z = 4071596
67
XDOT = -3538
594710 XDOT = -1078
563668
YDOT = -20499
620753 feet/sec YDOT = -6248
284405 meter/sec
ZDOT = -12545
509126 ZDOT = -3823
871182
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 07162
53783573
00020000 00000-0 20000-3 0 9073
2 25544 51
6293 133
0977 0008407 307
3281 52
7117 15
78367736 9882
Satellite: ISS
Catalog Number: 25544
Epoch time: 07162
53783573 = yrday
fracday
Element set: 907
Inclination: 51
6293 deg
RA of node: 133
0977 deg
Eccentricity:
0008407
Arg of perigee: 307
3281 deg
Mean anomaly: 52
7117 deg
Mean motion: 15
78367736 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 988
Checksum: 317
Coasting Arc #9 (Orbit 1003)
---------------------------------------
Vector Time (GMT): 2007/163/11:56:02
145
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5016640
97 A = 6711428
58 meter
Y = 952829
83 meter E =
0003471
Z = 4351733
76 I = 51
87752
XDOT = 1706
299009 Wp = 49
99816
YDOT = -6688
976539 meter/sec RA = 127
27356 deg
ZDOT = 3431
983473 TA = 5
53996
MA = 5
53613
Ha = 183
306 n
mi
Hp = 178
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16458795
82 X = -5048063
05
Y = 3126082
12 feet Y = 896554
44 meter
Z = 14277341
73 Z = 4327286
40
XDOT = 5598
093863 XDOT = 1764
297102
YDOT = -21945
461086 feet/sec YDOT = -6669
572100 meter/sec
ZDOT = 11259
788296 ZDOT = 3440
412439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -173445
99 X = -52866
34
Y = 16830313
96 feet Y = 5129879
70 meter
Z = 14185107
85 Z = 4323620
87
XDOT = -19209
231144 XDOT = -5854
973653
YDOT = -9713
119071 feet/sec YDOT = -2960
558693 meter/sec
ZDOT = 11290
836064 ZDOT = 3441
446832
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 07163
55084657
00020000 00000-0 20000-3 0 9084
2 25544 51
6300 127
8606 0008418 310
1647 49
8781 15
78427772 10042
Satellite: ISS
Catalog Number: 25544
Epoch time: 07163
55084657 = yrday
fracday
Element set: 908
Inclination: 51
6300 deg
RA of node: 127
8606 deg
Eccentricity:
0008418
Arg of perigee: 310
1647 deg
Mean anomaly: 49
8781 deg
Mean motion: 15
78427772 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1004
Checksum: 298
Coasting Arc #10 (Orbit 1018)
---------------------------------------
Vector Time (GMT): 2007/164/11:56:02
145
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2272289
13 A = 6718391
39 meter
Y = 6089093
48 meter E =
0012147
Z = -1670232
49 I = 51
91750
XDOT = -5117
848386 Wp = 354
65263
YDOT = -332
460290 meter/sec RA = 122
08179 deg
ZDOT = 5759
117692 TA = 346
91317
MA = 346
94466
Ha = 183
421 n
mi
Hp = 178
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7455016
83 X = -2332095
60
Y = 19977340
82 feet Y = 6063349
43 meter
Z = -5479765
39 Z = -1681415
37
XDOT = -16790
841162 XDOT = -5141
727490
YDOT = -1090
748982 feet/sec YDOT = -389
825695 meter/sec
ZDOT = 18894
743084 ZDOT = 5734
196795
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18326347
92 X = 5585870
85
Y = 10879312
78 feet Y = 3316014
54 meter
Z = -5521302
03 Z = -1682892
86
XDOT = -3303
399236 XDOT = -1006
876087
YDOT = 15091
926179 feet/sec YDOT = 4600
019099 meter/sec
ZDOT = 18800
558461 ZDOT = 5730
410219
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 07164
50052773
00020000 00000-0 20000-3 0 9095
2 25544 51
6299 122
9503 0008369 315
0797 44
9690 15
78418674 10198
Satellite: ISS
Catalog Number: 25544
Epoch time: 07164
50052773 = yrday
fracday
Element set: 909
Inclination: 51
6299 deg
RA of node: 122
9503 deg
Eccentricity:
0008369
Arg of perigee: 315
0797 deg
Mean anomaly: 44
9690 deg
Mean motion: 15
78418674 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1019
Checksum: 315
Coasting Arc #11 (Orbit 1034)
---------------------------------------
Vector Time (GMT): 2007/165/11:56:02
145
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3809902
51 A = 6707470
79 meter
Y = 1641090
10 meter E =
0011671
Z = -5279118
40 I = 51
89619
XDOT = -3323
939821 Wp = 54
13565
YDOT = 6943
170292 meter/sec RA = 116
94890 deg
ZDOT = -234
145081 TA = 213
61302
MA = 213
68711
Ha = 183
604 n
mi
Hp = 178
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12499680
15 X = 3816913
62
Y = 5384153
87 feet Y = 1683735
01 meter
Z = -17319942
26 Z = -5260592
35
XDOT = -10905
314373 XDOT = -3400
194881
YDOT = 22779
430091 feet/sec YDOT = 6905
573825 meter/sec
ZDOT = -768
192522 ZDOT = -250
476485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7353653
30 X = 2241393
52
Y = -11557732
84 feet Y = -3522796
97 meter
Z = -17249756
86 Z = -5257725
89
XDOT = 19869
838000 XDOT = 6056
326623
YDOT = 13910
822638 feet/sec YDOT = 4240
018740 meter/sec
ZDOT = -829
097894 ZDOT = -252
709038
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 07165
51349960
00020000 00000-0 20000-3 0 9106
2 25544 51
6311 117
7128 0008468 318
5749 41
4773 15
78449296 10359
Satellite: ISS
Catalog Number: 25544
Epoch time: 07165
51349960 = yrday
fracday
Element set: 910
Inclination: 51
6311 deg
RA of node: 117
7128 deg
Eccentricity:
0008468
Arg of perigee: 318
5749 deg
Mean anomaly: 41
4773 deg
Mean motion: 15
78449296 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1035
Checksum: 307
Coasting Arc #12 (Orbit 1050)
---------------------------------------
Vector Time (GMT): 2007/166/11:56:02
145
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3360783
56 A = 6718707
95 meter
Y = -5671661
68 meter E =
0000538
Z = -1294231
07 I = 51
94750
XDOT = 3574
105570 Wp = 148
46624
YDOT = 3459
559561 meter/sec RA = 111
80960 deg
ZDOT = -5881
211685 TA = 45
69411
MA = 45
68971
Ha = 183
650 n
mi
Hp = 178
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11026192
79 X = 3430242
27
Y = -18607813
91 feet Y = -5633690
84 meter
Z = -4246164
92 Z = -1277737
03
XDOT = 11726
068142 XDOT = 3563
724496
YDOT = 11350
261028 feet/sec YDOT = 3499
470593 meter/sec
ZDOT = -19295
313927 ZDOT = -5863
873050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16808948
41 X = -5123367
48
Y = -13631101
47 feet Y = -4154759
73 meter
Z = -4184484
25 Z = -1275430
80
XDOT = 11952
253632 XDOT = 3643
046907
YDOT = -8837
225706 feet/sec YDOT = -2693
586395 meter/sec
ZDOT = -19229
400269 ZDOT = -5861
121202
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 07166
52645051
00020000 00000-0 20000-3 0 9119
2 25544 51
6321 112
4756 0008511 322
5053 37
5518 15
78493031 10518
Satellite: ISS
Catalog Number: 25544
Epoch time: 07166
52645051 = yrday
fracday
Element set: 911
Inclination: 51
6321 deg
RA of node: 112
4756 deg
Eccentricity:
0008511
Arg of perigee: 322
5053 deg
Mean anomaly: 37
5518 deg
Mean motion: 15
78493031 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1051
Checksum: 259
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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