Date:
May 16th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6189 25 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 465)
---------------------------------------
Vector Time (GMT): 2007/129/11:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3419162
00 A = 6709490
86 meter
Y = -2439738
82 meter E =
0020372
Z = -5247532
71 I = 51
34415
XDOT = 4320
806696 Wp = 119
12973
YDOT = -6364
543410 meter/sec RA = 303
37157 deg
ZDOT = 134
362316 TA = 152
20622
MA = 152
09722
Ha = 187
054 n
mi
Hp = 176
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11217723
10 X = -3366134
75
Y = -8004392
47 feet Y = -2477676
86 meter
Z = -17216314
67 Z = -5264014
44
XDOT = 14175
874988 XDOT = 4391
002103
YDOT = -20881
047934 feet/sec YDOT = -6315
833259 meter/sec
ZDOT = 440
821246 ZDOT = 155
522784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13695355
32 X = -4174344
30
Y = -439422
32 feet Y = -133935
92 meter
Z = -17278693
57 Z = -5266545
80
XDOT = 83
212041 XDOT = 25
363030
YDOT = -24237
888648 feet/sec YDOT = -7387
708460 meter/sec
ZDOT = 519
790785 ZDOT = 158
432231
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 07129
48157741
00020000 00000-0 20000-3 0 9005
2 25544 51
6320 303
8876 0010026 164
4761 195
6714 15
77735273 4668
Satellite: ISS
Catalog Number: 25544
Epoch time: 07129
48157741 = yrday
fracday
Element set: 900
Inclination: 51
6320 deg
RA of node: 303
8876 deg
Eccentricity:
0010026
Arg of perigee: 164
4761 deg
Mean anomaly: 195
6714 deg
Mean motion: 15
77735273 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 466
Checksum: 295
Coasting Arc #2 (Orbit 481)
---------------------------------------
Vector Time (GMT): 2007/130/11:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4027003
22 A = 6720548
12 meter
Y = 5190547
27 meter E =
0018036
Z = -1371360
16 I = 51
36765
XDOT = -3147
406970 Wp = 156
14089
YDOT = -3967
297411 meter/sec RA = 298
20180 deg
ZDOT = -5816
503787 TA = 39
02321
MA = 38
89321
Ha = 186
744 n
mi
Hp = 176
357
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13211952
82 X = -4078083
54
Y = 17029354
57 feet Y = 5145229
55 meter
Z = -4499213
11 Z = -1391047
11
XDOT = -10326
138352 XDOT = -3074
554566
YDOT = -13016
067621 feet/sec YDOT = -4002
085746 meter/sec
ZDOT = -19083
017673 ZDOT = -5831
617236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1075140
25 X = -327702
75
Y = 21511192
90 feet Y = 6556611
59 meter
Z = -4572765
74 Z = -1393779
00
XDOT = -14259
168413 XDOT = -4346
194532
YDOT = -4752
108092 feet/sec YDOT = -1448
442546 meter/sec
ZDOT = -19140
427996 ZDOT = -5834
002453
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 07130
49498822
00020000 00000-0 20000-3 0 9017
2 25544 51
6322 298
6536 0009804 168
3443 191
7951 15
77796843 4824
Satellite: ISS
Catalog Number: 25544
Epoch time: 07130
49498822 = yrday
fracday
Element set: 901
Inclination: 51
6322 deg
RA of node: 298
6536 deg
Eccentricity:
0009804
Arg of perigee: 168
3443 deg
Mean anomaly: 191
7951 deg
Mean motion: 15
77796843 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 482
Checksum: 323
Coasting Arc #3 (Orbit 497)
---------------------------------------
Vector Time (GMT): 2007/131/11:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2110047
72 A = 6712158
40 meter
Y = 4417335
69 meter E =
0010805
Z = 4581615
52 I = 51
32599
XDOT = -4782
930221 Wp = 125
28097
YDOT = 5305
332100 meter/sec RA = 292
97977 deg
ZDOT = -2913
688825 TA = 353
64469
MA = 353
65838
Ha = 186
668 n
mi
Hp = 176
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6922728
73 X = 2038238
84
Y = 14492571
15 feet Y = 4440529
69 meter
Z = 15031546
98 Z = 4591691
98
XDOT = -15692
028284 XDOT = -4827
745495
YDOT = 17405
945211 feet/sec YDOT = 5251
596264 meter/sec
ZDOT = -9559
346538 ZDOT = -2937
033005
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14034486
96 X = 4277711
63
Y = 7735196
82 feet Y = 2357687
99 meter
Z = 15070039
88 Z = 4593348
15
XDOT = -1906
827834 XDOT = -581
201124
YDOT = 22245
118544 feet/sec YDOT = 6780
312132 meter/sec
ZDOT = -9646
659410 ZDOT = -2940
301788
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 07131
50837513
00020000 00000-0 20000-3 0 9025
2 25544 51
6314 293
4186 0009944 172
6509 187
4803 15
77793417 4984
Satellite: ISS
Catalog Number: 25544
Epoch time: 07131
50837513 = yrday
fracday
Element set: 902
Inclination: 51
6314 deg
RA of node: 293
4186 deg
Eccentricity:
0009944
Arg of perigee: 172
6509 deg
Mean anomaly: 187
4803 deg
Mean motion: 15
77793417 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 498
Checksum: 311
Coasting Arc #4 (Orbit 513)
---------------------------------------
Vector Time (GMT): 2007/132/11:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4225008
66 A = 6715564
20 meter
Y = -3810707
16 meter E =
0016641
Z = 3566438
65 I = 51
32799
XDOT = 1745
296738 Wp = 130
23703
YDOT = 6077
682327 meter/sec RA = 287
84009 deg
ZDOT = 4402
255504 TA = 272
62786
MA = 272
81834
Ha = 186
496 n
mi
Hp = 176
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13861576
96 X = 4249981
25
Y = -12502320
08 feet Y = -3763321
25 meter
Z = 11700914
22 Z = 3587024
45
XDOT = 5726
039167 XDOT = 1655
819935
YDOT = 19939
902646 feet/sec YDOT = 6096
698751 meter/sec
ZDOT = 14443
095485 ZDOT = 4410
517131
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3537863
15 X = 1078340
69
Y = -18279077
93 feet Y = -5571462
95 meter
Z = 11778011
34 Z = 3589937
86
XDOT = 15145
543713 XDOT = 4616
361724
YDOT = 12308
867104 feet/sec YDOT = 3751
742693 meter/sec
ZDOT = 14474
955395 ZDOT = 4411
966404
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 07132
52173504
00020000 00000-0 20000-3 0 9032
2 25544 51
6311 288
1831 0009974 176
6666 183
4567 15
77871425 5148
Satellite: ISS
Catalog Number: 25544
Epoch time: 07132
52173504 = yrday
fracday
Element set: 903
Inclination: 51
6311 deg
RA of node: 288
1831 deg
Eccentricity:
0009974
Arg of perigee: 176
6666 deg
Mean anomaly: 183
4567 deg
Mean motion: 15
77871425 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 514
Checksum: 302
Coasting Arc #5 (Orbit 528)
---------------------------------------
Vector Time (GMT): 2007/133/11:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -985248
13 A = 6717587
98 meter
Y = -6013792
58 meter E =
0008886
Z = -2840700
57 I = 51
32827
XDOT = 4855
177618 Wp = 151
52505
YDOT = -3182
702712 meter/sec RA = 282
60144 deg
ZDOT = 5052
668694 TA = 175
71265
MA = 175
70503
Ha = 186
391 n
mi
Hp = 176
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3232441
37 X = -904127
98
Y = -19730290
61 feet Y = -6024356
49 meter
Z = -9319883
74 Z = -2845290
18
XDOT = 15929
060427 XDOT = 4865
860893
YDOT = -10441
938031 feet/sec YDOT = -3128
349868 meter/sec
ZDOT = 16576
997027 ZDOT = 5076
281321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14617168
58 X = -4455312
98
Y = -13628470
56 feet Y = -4153957
83 meter
Z = -9337903
98 Z = -2846193
13
XDOT = 5104
333231 XDOT = 1555
800769
YDOT = -16896
206148 feet/sec YDOT = -5149
963634 meter/sec
ZDOT = 16665
572502 ZDOT = 5079
666499
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 07133
47173877
00020000 00000-0 20000-3 0 9041
2 25544 51
6319 283
2749 0009942 179
4511 180
6667 15
77891065 5293
Satellite: ISS
Catalog Number: 25544
Epoch time: 07133
47173877 = yrday
fracday
Element set: 904
Inclination: 51
6319 deg
RA of node: 283
2749 deg
Eccentricity:
0009942
Arg of perigee: 179
4511 deg
Mean anomaly: 180
6667 deg
Mean motion: 15
77891065 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 529
Checksum: 326
Coasting Arc #6 (Orbit 544)
---------------------------------------
Vector Time (GMT): 2007/134/11:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4227354
09 A = 6710056
84 meter
Y = 1569638
17 meter E =
0013966
Z = -4977705
39 I = 51
29884
XDOT = -552
390770 Wp = 117
95260
YDOT = -7444
211166 meter/sec RA = 277
45239 deg
ZDOT = -1888
774095 TA = 133
78571
MA = 133
67008
Ha = 186
084 n
mi
Hp = 176
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13869271
95 X = -4220410
54
Y = 5149731
51 feet Y = 1522404
64 meter
Z = -16331054
43 Z = -4998225
34
XDOT = -1812
305675 XDOT = -459
931954
YDOT = -24423
264981 feet/sec YDOT = -7449
871235 meter/sec
ZDOT = -6196
765402 ZDOT = -1891
233515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7503363
54 X = -2287025
21
Y = 12651131
04 feet Y = 3856064
74 meter
Z = -16408174
70 Z = -5001211
65
XDOT = -15777
029311 XDOT = -4808
838534
YDOT = -17363
143751 feet/sec YDOT = -5292
286215 meter/sec
ZDOT = -6206
932718 ZDOT = -1891
873092
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 07134
48505042
00020000 00000-0 20000-3 0 9057
2 25544 51
6324 278
0404 0009798 182
9339 177
1770 15
77944801 5456
Satellite: ISS
Catalog Number: 25544
Epoch time: 07134
48505042 = yrday
fracday
Element set: 905
Inclination: 51
6324 deg
RA of node: 278
0404 deg
Eccentricity:
0009798
Arg of perigee: 182
9339 deg
Mean anomaly: 177
1770 deg
Mean motion: 15
77944801 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 545
Checksum: 305
Coasting Arc #7 (Orbit 560)
---------------------------------------
Vector Time (GMT): 2007/135/11:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 16412
80 A = 6720812
52 meter
Y = 6699221
67 meter E =
0019970
Z = 348095
04 I = 51
33260
XDOT = -4826
385690 Wp = 155
18639
YDOT = 329
658144 meter/sec RA = 272
24265 deg
ZDOT = -6010
602475 TA = 21
00297
MA = 20
92107
Ha = 185
842 n
mi
Hp = 177
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 53847
77 X = -60191
11
Y = 21979073
73 feet Y = 6698976
87 meter
Z = 1142044
11 Z = 347989
31
XDOT = -15834
598721 XDOT = -4800
514159
YDOT = 1081
555591 feet/sec YDOT = 275
831989 meter/sec
ZDOT = -19719
824392 ZDOT = -6033
986738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14111088
85 X = 4301059
88
Y = 16851077
66 feet Y = 5136208
47 meter
Z = 1142453
46 Z = 348219
81
XDOT = -10155
902264 XDOT = -3095
519010
YDOT = 9871
087014 feet/sec YDOT = 3008
707322 meter/sec
ZDOT = -19807
889330 ZDOT = -6037
444668
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 07135
49833603
00020000 00000-0 20000-3 0 9067
2 25544 51
6319 272
8039 0009674 187
9575 172
1438 15
77987429 5613
Satellite: ISS
Catalog Number: 25544
Epoch time: 07135
49833603 = yrday
fracday
Element set: 906
Inclination: 51
6319 deg
RA of node: 272
8039 deg
Eccentricity:
0009674
Arg of perigee: 187
9575 deg
Mean anomaly: 172
1438 deg
Mean motion: 15
77987429 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 561
Checksum: 332
Coasting Arc #8 (Orbit 576)
---------------------------------------
Vector Time (GMT): 2007/136/11:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4180315
99 A = 6709220
98 meter
Y = 1026683
20 meter E =
0007486
Z = 5143915
64 I = 51
29443
XDOT = -503
610729 Wp = 169
23559
YDOT = 7611
968716 meter/sec RA = 267
04704 deg
ZDOT = -1117
020192 TA = 291
42387
MA = 291
50371
Ha = 185
714 n
mi
Hp = 177
275
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13714947
46 X = 4143535
98
Y = 3368383
20 feet Y = 1073223
54 meter
Z = 16876363
66 Z = 5164134
88
XDOT = -1652
266172 XDOT = -583
265032
YDOT = 24973
650644 feet/sec YDOT = 7605
891830 meter/sec
ZDOT = -3664
764411 ZDOT = -1119
659317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12511072
95 X = 3813375
04
Y = -6351174
90 feet Y = -1935838
11 meter
Z = 16952671
48 Z = 5167174
27
XDOT = 14621
546245 XDOT = 4456
647296
YDOT = 19057
638746 feet/sec YDOT = 5808
768290 meter/sec
ZDOT = -3673
795620 ZDOT = -1119
772905
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 07136
51159956
00020000 00000-0 20000-3 0 9074
2 25544 51
6328 267
5688 0009668 190
7763 169
3196 15
77967972 5775
Satellite: ISS
Catalog Number: 25544
Epoch time: 07136
51159956 = yrday
fracday
Element set: 907
Inclination: 51
6328 deg
RA of node: 267
5688 deg
Eccentricity:
0009668
Arg of perigee: 190
7763 deg
Mean anomaly: 169
3196 deg
Mean motion: 15
77967972 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 577
Checksum: 361
Coasting Arc #9 (Orbit 592)
---------------------------------------
Vector Time (GMT): 2007/137/11:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 926609
88 A = 6718377
75 meter
Y = -6262009
34 meter E =
0011905
Z = 2250527
27 I = 51
33043
XDOT = 4768
937392 Wp = 115
28336
YDOT = 2666
731513 meter/sec RA = 261
88716 deg
ZDOT = 5429
193875 TA = 270
12360
MA = 270
26002
Ha = 185
515 n
mi
Hp = 177
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3040058
65 X = 985630
84
Y = -20544650
06 feet Y = -6251317
82 meter
Z = 7383619
65 Z = 2255171
21
XDOT = 15646
120053 XDOT = 4712
388623
YDOT = 8749
119138 feet/sec YDOT = 2719
743411 meter/sec
ZDOT = 17812
315862 ZDOT = 5452
224884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11455231
22 X = -3491554
47
Y = -17316310
81 feet Y = -5278011
54 meter
Z = 7400371
57 Z = 2255633
26
XDOT = 16158
940186 XDOT = 4925
244969
YDOT = -3001
731896 feet/sec YDOT = -914
927882 meter/sec
ZDOT = 17899
421555 ZDOT = 5455
743690
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 07137
52483284
00020000 00000-0 20000-3 0 9081
2 25544 51
6340 262
3336 0009757 195
6430 164
4435 15
78080077 5939
Satellite: ISS
Catalog Number: 25544
Epoch time: 07137
52483284 = yrday
fracday
Element set: 908
Inclination: 51
6340 deg
RA of node: 262
3336 deg
Eccentricity:
0009757
Arg of perigee: 195
6430 deg
Mean anomaly: 164
4435 deg
Mean motion: 15
78080077 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 593
Checksum: 302
Coasting Arc #10 (Orbit 607)
---------------------------------------
Vector Time (GMT): 2007/138/11:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4115291
73 A = 6713595
56 meter
Y = -3508446
79 meter E =
0011820
Z = -3989762
90 I = 51
31980
XDOT = 1684
989381 Wp = 162
19272
YDOT = -6419
577694 meter/sec RA = 256
65195 deg
ZDOT = 3899
068538 TA = 148
29868
MA = 148
22745
Ha = 185
282 n
mi
Hp = 177
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13501613
29 X = -4056372
11
Y = -11510652
19 feet Y = -3554136
15 meter
Z = -13089773
29 Z = -4009612
75
XDOT = 5528
180385 XDOT = 1737
707581
YDOT = -21061
606606 feet/sec YDOT = -6400
441119 meter/sec
ZDOT = 12792
219612 ZDOT = 3907
381257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17673817
67 X = -5386979
63
Y = 670656
93 feet Y = 204416
23 meter
Z = -13165000
12 Z = -4012692
04
XDOT = -10249
467445 XDOT = -3124
037677
YDOT = -17876
609058 feet/sec YDOT = -5448
790441 meter/sec
ZDOT = 12822
782043 ZDOT = 3908
383967
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 07138
47472026
00020000 00000-0 20000-3 0 9099
2 25544 51
6342 257
4261 0009516 199
8111 160
2686 15
78070354 6084
Satellite: ISS
Catalog Number: 25544
Epoch time: 07138
47472026 = yrday
fracday
Element set: 909
Inclination: 51
6342 deg
RA of node: 257
4261 deg
Eccentricity:
0009516
Arg of perigee: 199
8111 deg
Mean anomaly: 160
2686 deg
Mean motion: 15
78070354 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 608
Checksum: 295
Coasting Arc #11 (Orbit 623)
---------------------------------------
Vector Time (GMT): 2007/139/11:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2079922
27 A = 6712280
59 meter
Y = 4694479
96 meter E =
0007130
Z = -4323919
24 I = 51
32372
XDOT = -4598
001448 Wp = 140
39038
YDOT = -5163
169544 meter/sec RA = 251
51277 deg
ZDOT = -3402
385191 TA = 95
20726
MA = 95
12589
Ha = 184
992 n
mi
Hp = 177
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6823891
96 X = -2111257
08
Y = 15401837
13 feet Y = 4671046
67 meter
Z = -14186086
74 Z = -4334098
85
XDOT = -15085
306587 XDOT = -4523
396119
YDOT = -16939
532625 feet/sec YDOT = -5214
169227 meter/sec
ZDOT = -11162
681074 ZDOT = -3424
542140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5781743
28 X = 1762275
35
Y = 15788585
63 feet Y = 4812360
90 meter
Z = -14223893
76 Z = -4335442
82
XDOT = -21414
810981 XDOT = -6527
234387
YDOT = -2265
128743 feet/sec YDOT = -690
411241 meter/sec
ZDOT = -11246
812089 ZDOT = -3428
028325
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 07139
48790815
00020000 00000-0 20000-3 0 9102
2 25544 51
6343 252
1906 0009486 204
0364 156
0360 15
78111973 6241
Satellite: ISS
Catalog Number: 25544
Epoch time: 07139
48790815 = yrday
fracday
Element set: 910
Inclination: 51
6343 deg
RA of node: 252
1906 deg
Eccentricity:
0009486
Arg of perigee: 204
0364 deg
Mean anomaly: 156
0360 deg
Mean motion: 15
78111973 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 624
Checksum: 285
Coasting Arc #12 (Orbit 639)
---------------------------------------
Vector Time (GMT): 2007/140/11:11:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3813751
22 A = 6719067
43 meter
Y = 5239927
00 meter E =
0016656
Z = 1731158
53 I = 51
35733
XDOT = -3136
312144 Wp = 149
53099
YDOT = 4164
605293 meter/sec RA = 246
28322 deg
ZDOT = -5686
616805 TA = 11
17521
MA = 11
13827
Ha = 184
779 n
mi
Hp = 177
998
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12512307
16 X = 3746464
48
Y = 17191361
55 feet Y = 5282198
00 meter
Z = 5679653
97 Z = 1749523
21
XDOT = -10289
738004 XDOT = -3155
023670
YDOT = 13663
403193 feet/sec YDOT = 4129
429624 meter/sec
ZDOT = -18656
879280 ZDOT = -5701
897790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20966175
81 X = 6390490
39
Y = 3423709
38 feet Y = 1043546
62 meter
Z = 5749512
82 Z = 1752451
51
XDOT = 2634
585235 XDOT = 803
021579
YDOT = 15345
525657 feet/sec YDOT = 4677
316220 meter/sec
ZDOT = -18713
981058 ZDOT = -5704
021426
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 07140
50107187
00020000 00000-0 20000-3 0 9112
2 25544 51
6342 246
9552 0009431 207
5844 152
4822 15
78146586 6408
Satellite: ISS
Catalog Number: 25544
Epoch time: 07140
50107187 = yrday
fracday
Element set: 911
Inclination: 51
6342 deg
RA of node: 246
9552 deg
Eccentricity:
0009431
Arg of perigee: 207
5844 deg
Mean anomaly: 152
4822 deg
Mean motion: 15
78146586 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 640
Checksum: 282
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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