Date:
May 19th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4897 58 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
143/23:30:02
907 0
4 3
5 3
5
N/A -2
4 -0
0 184
0
000/00:05:05
815 2
4 0
1 180
9
Coasting Arc #1 (Orbit 576)
---------------------------------------
Vector Time (GMT): 2007/136/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3309449
39 A = 6712464
43 meter
Y = -3876967
06 meter E =
0014696
Z = 4368989
49 I = 51
30503
XDOT = 2972
221708 Wp = 152
73872
YDOT = 6289
445388 meter/sec RA = 267
12732 deg
ZDOT = 3312
431093 TA = 263
75314
MA = 263
92057
Ha = 185
828 n
mi
Hp = 177
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10857773
59 X = 3331331
98
Y = -12719708
21 feet Y = -3839837
14 meter
Z = 14333955
02 Z = 4385119
84
XDOT = 9751
383555 XDOT = 2885
579748
YDOT = 20634
663347 feet/sec YDOT = 6322
197581 meter/sec
ZDOT = 10867
556080 ZDOT = 3326
660816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 648077
31 X = 197533
96
Y = -16659217
64 feet Y = -5077729
54 meter
Z = 14394268
09 Z = 4387372
92
XDOT = 19133
857641 XDOT = 5831
999809
YDOT = 10230
185364 feet/sec YDOT = 3118
160499 meter/sec
ZDOT = 10921
926886 ZDOT = 3329
003315
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
51171899
00020000 00000-0 20000-3 0 9007
2 25544 51
6325 267
5754 0009982 191
9759 168
1170 15
77983249 5777
Satellite: ISS
Catalog Number: 25544
Epoch time: 07136
51171899 = yrday
fracday
Element set: 900
Inclination: 51
6325 deg
RA of node: 267
5754 deg
Eccentricity:
0009982
Arg of perigee: 191
9759 deg
Mean anomaly: 168
1170 deg
Mean motion: 15
77983249 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 577
Checksum: 336
Coasting Arc #2 (Orbit 591)
---------------------------------------
Vector Time (GMT): 2007/137/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2237260
52 A = 6719580
01 meter
Y = -6109015
19 meter E =
0004046
Z = -1692017
28 I = 51
33307
XDOT = 4158
396353 Wp = 147
91999
YDOT = -3098
204684 meter/sec RA = 261
89807 deg
ZDOT = 5690
469781 TA = 193
27360
MA = 193
28425
Ha = 185
702 n
mi
Hp = 177
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7340093
57 X = -2160562
67
Y = -20042700
76 feet Y = -6133604
39 meter
Z = -5551237
78 Z = -1702700
75
XDOT = 13643
032654 XDOT = 4165
088059
YDOT = -10164
713529 feet/sec YDOT = -3051
666643 meter/sec
ZDOT = 18669
520280 ZDOT = 5710
687435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18299685
02 X = -5577744
00
Y = -10965929
47 feet Y = -3342415
30 meter
Z = -5592225
59 Z = -1704510
36
XDOT = 3315
518729 XDOT = 1010
570108
YDOT = -15087
578809 feet/sec YDOT = -4598
694021 meter/sec
ZDOT = 18745
335997 ZDOT = 5713
578412
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
46166287
00020000 00000-0 20000-3 0 9018
2 25544 51
6337 262
6678 0009868 194
9934 165
0940 15
77986072 5927
Satellite: ISS
Catalog Number: 25544
Epoch time: 07137
46166287 = yrday
fracday
Element set: 901
Inclination: 51
6337 deg
RA of node: 262
6678 deg
Eccentricity:
0009868
Arg of perigee: 194
9934 deg
Mean anomaly: 165
0940 deg
Mean motion: 15
77986072 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 592
Checksum: 337
Coasting Arc #3 (Orbit 607)
---------------------------------------
Vector Time (GMT): 2007/138/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3969736
11 A = 6708689
55 meter
Y = 1416438
34 meter E =
0014444
Z = -5228966
77 I = 51
30212
XDOT = -2093
336265 Wp = 125
24968
YDOT = -7397
387819 meter/sec RA = 256
72953 deg
ZDOT = -423
650293 TA = 140
75996
MA = 140
65517
Ha = 185
374 n
mi
Hp = 177
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13024068
60 X = -3959878
18
Y = 4647107
40 feet Y = 1372102
56 meter
Z = -17155402
80 Z = -5248227
82
XDOT = -6867
901131 XDOT = -2008
403974
YDOT = -24269
645076 feet/sec YDOT = -7420
321723 meter/sec
ZDOT = -1389
928782 ZDOT = -433
614848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6912534
24 X = -2106940
44
Y = 11872185
90 feet Y = 3618642
26 meter
Z = -17227823
07 Z = -5251040
47
XDOT = -19994
122462 XDOT = -6094
208526
YDOT = -13671
325107 feet/sec YDOT = -4167
019893 meter/sec
ZDOT = -1428
364642 ZDOT = -435
365543
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
47491670
00020000 00000-0 20000-3 0 9028
2 25544 51
6337 257
4337 0009723 199
0018 161
0785 15
78033608 6080
Satellite: ISS
Catalog Number: 25544
Epoch time: 07138
47491670 = yrday
fracday
Element set: 902
Inclination: 51
6337 deg
RA of node: 257
4337 deg
Eccentricity:
0009723
Arg of perigee: 199
0018 deg
Mean anomaly: 161
0785 deg
Mean motion: 15
78033608 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 608
Checksum: 300
Coasting Arc #4 (Orbit 623)
---------------------------------------
Vector Time (GMT): 2007/139/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1344484
13 A = 6720264
70 meter
Y = 6500240
81 meter E =
0016867
Z = -978185
45 I = 51
34900
XDOT = -4944
783947 Wp = 172
20332
YDOT = 136
318643 meter/sec RA = 251
54563 deg
ZDOT = -5918
934999 TA = 18
55579
MA = 18
49435
Ha = 185
201 n
mi
Hp = 177
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4411037
18 X = 1276449
45
Y = 21326249
36 feet Y = 6514895
35 meter
Z = -3209269
86 Z = -971818
01
XDOT = -16223
044444 XDOT = -4917
187464
YDOT = 447
239641 feet/sec YDOT = 81
178651 meter/sec
ZDOT = -19419
078081 ZDOT = -5942
889873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17334724
35 X = 5283623
98
Y = 13188324
95 feet Y = 4019801
45 meter
Z = -3184492
21 Z = -970633
23
XDOT = -10905
730267 XDOT = -3324
066585
YDOT = 9646
335224 feet/sec YDOT = 2940
202976 meter/sec
ZDOT = -19509
351624 ZDOT = -5946
450375
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
48815169
00020000 00000-0 20000-3 0 9034
2 25544 51
6334 252
1976 0009693 203
4000 156
6725 15
78052486 6242
Satellite: ISS
Catalog Number: 25544
Epoch time: 07139
48815169 = yrday
fracday
Element set: 903
Inclination: 51
6334 deg
RA of node: 252
1976 deg
Eccentricity:
0009693
Arg of perigee: 203
4000 deg
Mean anomaly: 156
6725 deg
Mean motion: 15
78052486 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 624
Checksum: 298
Coasting Arc #5 (Orbit 639)
---------------------------------------
Vector Time (GMT): 2007/140/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4624764
10 A = 6710808
44 meter
Y = 1128388
39 meter E =
0005379
Z = 4726167
24 I = 51
32798
XDOT = 890
497864 Wp = 156
48486
YDOT = 7205
232651 meter/sec RA = 246
32806 deg
ZDOT = -2595
522640 TA = 319
03767
MA = 319
07807
Ha = 184
971 n
mi
Hp = 178
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15173110
55 X = 4588843
67
Y = 3702061
66 feet Y = 1179903
46 meter
Z = 15505798
04 Z = 4748547
33
XDOT = 2921
580920 XDOT = 822
470321
YDOT = 23639
214735 feet/sec YDOT = 7214
810771 meter/sec
ZDOT = -8515
494225 ZDOT = -2591
360626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13689749
24 X = 4172635
57
Y = -7341095
75 feet Y = -2237565
98 meter
Z = 15590298
15 Z = 4751922
87
XDOT = 17486
053062 XDOT = 5329
748973
YDOT = 14585
690208 feet/sec YDOT = 4445
718375 meter/sec
ZDOT = -8498
937278 ZDOT = -2590
476082
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
50136928
00020000 00000-0 20000-3 0 9049
2 25544 51
6340 246
9630 0009587 206
8087 153
2584 15
78044357 6403
Satellite: ISS
Catalog Number: 25544
Epoch time: 07140
50136928 = yrday
fracday
Element set: 904
Inclination: 51
6340 deg
RA of node: 246
9630 deg
Eccentricity:
0009587
Arg of perigee: 206
8087 deg
Mean anomaly: 153
2584 deg
Mean motion: 15
78044357 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 640
Checksum: 294
Coasting Arc #6 (Orbit 655)
---------------------------------------
Vector Time (GMT): 2007/141/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -77459
88 A = 6715381
08 meter
Y = -5788868
25 meter E =
0011218
Z = 3404803
02 I = 51
35729
XDOT = 5616
172033 Wp = 138
10707
YDOT = 2624
332731 meter/sec RA = 241
18602 deg
ZDOT = 4572
779185 TA = 262
36263
MA = 262
49006
Ha = 184
771 n
mi
Hp = 178
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -254133
45 X = -29262
04
Y = -18992349
89 feet Y = -5789465
47 meter
Z = 11170613
57 Z = 3404542
93
XDOT = 18425
761263 XDOT = 5564
195260
YDOT = 8610
015523 feet/sec YDOT = 2686
844615 meter/sec
ZDOT = 15002
556382 ZDOT = 4599
936650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13178346
15 X = -4016759
91
Y = -13680012
80 feet Y = -4169667
90 meter
Z = 11168929
59 Z = 3404289
74
XDOT = 18291
359441 XDOT = 5575
206358
YDOT = -5242
759808 feet/sec YDOT = -1597
993189 meter/sec
ZDOT = 15105
259093 ZDOT = 4604
082972
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 07141
51456438
00020000 00000-0 20000-3 0 9053
2 25544 51
6343 241
7273 0009626 211
5845 148
4743 15
78135811 6567
Satellite: ISS
Catalog Number: 25544
Epoch time: 07141
51456438 = yrday
fracday
Element set: 905
Inclination: 51
6343 deg
RA of node: 241
7273 deg
Eccentricity:
0009626
Arg of perigee: 211
5845 deg
Mean anomaly: 148
4743 deg
Mean motion: 15
78135811 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 656
Checksum: 292
Coasting Arc #7 (Orbit 670)
---------------------------------------
Vector Time (GMT): 2007/142/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5066473
35 A = 6716624
46 meter
Y = -3275591
26 meter E =
0006173
Z = -2958423
90 I = 51
37631
XDOT = 857
393109 Wp = 192
83530
YDOT = -5820
442891 meter/sec RA = 235
94913 deg
ZDOT = 4968
189434 TA = 132
86325
MA = 132
81138
Ha = 184
538 n
mi
Hp = 178
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16622287
90 X = -5015097
21
Y = -10746690
50 feet Y = -3331959
77 meter
Z = -9706115
15 Z = -2982912
39
XDOT = 2812
969518 XDOT = 898
279926
YDOT = -19095
941243 feet/sec YDOT = -5810
627066 meter/sec
ZDOT = 16299
834100 ZDOT = 4972
453209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19385719
95 X = -5908767
44
Y = 3765227
90 feet Y = 1147641
46 meter
Z = -9798847
06 Z = -2986688
59
XDOT = -11021
984554 XDOT = -3359
500892
YDOT = -14221
418805 feet/sec YDOT = -4334
688452 meter/sec
ZDOT = 16315
195811 ZDOT = 4972
871683
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 07142
46442185
00020000 00000-0 20000-3 0 9063
2 25544 51
6342 236
8194 0009429 216
4500 143
6024 15
78104521 6716
Satellite: ISS
Catalog Number: 25544
Epoch time: 07142
46442185 = yrday
fracday
Element set: 906
Inclination: 51
6342 deg
RA of node: 236
8194 deg
Eccentricity:
0009429
Arg of perigee: 216
4500 deg
Mean anomaly: 143
6024 deg
Mean motion: 15
78104521 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 671
Checksum: 271
Coasting Arc #8 (Orbit 686)
---------------------------------------
Vector Time (GMT): 2007/143/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1684278
17 A = 6709633
82 meter
Y = 4202170
74 meter E =
0007544
Z = -4956551
26 I = 51
37029
XDOT = -5820
089287 Wp = 121
37030
YDOT = -4647
694262 meter/sec RA = 230
80376 deg
ZDOT = -1968
675777 TA = 129
56917
MA = 129
50251
Ha = 184
269 n
mi
Hp = 178
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5525847
00 X = -1707064
28
Y = 13786649
39 feet Y = 4183209
33 meter
Z = -16261651
13 Z = -4964788
37
XDOT = -19094
781125 XDOT = -5758
122078
YDOT = -15248
340753 feet/sec YDOT = -4712
431073 meter/sec
ZDOT = -6458
910028 ZDOT = -1996
799710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5892894
33 X = 1796154
19
Y = 13597291
24 feet Y = 4144454
37 meter
Z = -16292189
89 Z = -4965859
48
XDOT = -23269
491973 XDOT = -7092
541153
YDOT = 2241
744199 feet/sec YDOT = 683
283632 meter/sec
ZDOT = -6565
529986 ZDOT = -2001
173540
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 07143
47758449
00020000 00000-0 20000-3 0 9079
2 25544 51
6343 231
5837 0009464 220
2400 139
8066 15
78143107 6877
Satellite: ISS
Catalog Number: 25544
Epoch time: 07143
47758449 = yrday
fracday
Element set: 907
Inclination: 51
6343 deg
RA of node: 231
5837 deg
Eccentricity:
0009464
Arg of perigee: 220
2400 deg
Mean anomaly: 139
8066 deg
Mean motion: 15
78143107 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 687
Checksum: 298
Coasting Arc #9 (Orbit 694)
---------------------------------------
Vector Time (GMT): 2007/143/23:32:35
815
Vector Time (MET): N/A
Weight (LBS) : 480590
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5228677
09 A = 6721024
08 meter
Y = -3901847
71 meter E =
0003497
Z = -1606706
53 I = 51
41198
XDOT = 1826
871506 Wp = 311
55031
YDOT = -4810
932517 meter/sec RA = 228
06492 deg
ZDOT = 5732
338261 TA = 30
63570
MA = 30
61528
Ha = 184
049 n
mi
Hp = 180
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17154452
40 X = -5176852
37
Y = -12801337
63 feet Y = -3960027
78 meter
Z = -5271346
89 Z = -1631981
94
XDOT = 5993
672921 XDOT = 1852
685630
YDOT = -15783
899333 feet/sec YDOT = -4790
359654 meter/sec
ZDOT = 18806
884057 ZDOT = 5741
275421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20464679
36 X = 6237634
27
Y = -6190904
52 feet Y = -1886987
70 meter
Z = -5367138
92 Z = -1635903
94
XDOT = 8761
269453 XDOT = 2670
434929
YDOT = 12612
133033 feet/sec YDOT = 3844
178149 meter/sec
ZDOT = 18839
985775 ZDOT = 5742
427664
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 07143
98415953
00020000 00000-0 20000-3 0 9086
2 25544 51
6336 228
9686 0008439 241
8061 118
2252 15
77513337 6956
Satellite: ISS
Catalog Number: 25544
Epoch time: 07143
98415953 = yrday
fracday
Element set: 908
Inclination: 51
6336 deg
RA of node: 228
9686 deg
Eccentricity:
0008439
Arg of perigee: 241
8061 deg
Mean anomaly: 118
2252 deg
Mean motion: 15
77513337 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 695
Checksum: 314
Coasting Arc #10 (Orbit 710)
---------------------------------------
Vector Time (GMT): 2007/144/23:32:35
815
Vector Time (MET): N/A
Weight (LBS) : 480590
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2429485
27 A = 6710072
25 meter
Y = 3441493
26 meter E =
0007632
Z = -5228974
18 I = 51
39628
XDOT = -5896
935548 Wp = 107
96919
YDOT = -4928
402292 meter/sec RA = 222
90519 deg
ZDOT = -506
760803 TA = 157
21803
MA = 157
18415
Ha = 183
684 n
mi
Hp = 181
090
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7970752
18 X = -2442386
50
Y = 11290988
38 feet Y = 3414253
73 meter
Z = -17155427
09 Z = -5240807
68
XDOT = -19346
901405 XDOT = -5838
925404
YDOT = -16169
298858 feet/sec YDOT = -4994
020735 meter/sec
ZDOT = -1662
601060 ZDOT = -535
267736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4641120
69 X = -1414613
59
Y = -12959978
56 feet Y = -3950201
46 meter
Z = -17199620
41 Z = -5242444
30
XDOT = 23437
127433 XDOT = 7143
636442
YDOT = -6055
837517 feet/sec YDOT = -1845
819275 meter/sec
ZDOT = -1770
715527 ZDOT = -539
714093
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 07144
99771795
00020000 00000-0 20000-3 0 9098
2 25544 51
6344 223
7353 0008349 245
9827 114
0464 15
77557714 7119
Satellite: ISS
Catalog Number: 25544
Epoch time: 07144
99771795 = yrday
fracday
Element set: 909
Inclination: 51
6344 deg
RA of node: 223
7353 deg
Eccentricity:
0008349
Arg of perigee: 245
9827 deg
Mean anomaly: 114
0464 deg
Mean motion: 15
77557714 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 711
Checksum: 319
Coasting Arc #11 (Orbit 726)
---------------------------------------
Vector Time (GMT): 2007/145/23:32:35
815
Vector Time (MET): N/A
Weight (LBS) : 480590
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4889964
59 A = 6721909
58 meter
Y = 4539568
61 meter E =
0011205
Z = -750661
97 I = 51
45825
XDOT = -3780
567043 Wp = 186
24996
YDOT = 3085
966042 meter/sec RA = 217
72993 deg
ZDOT = -5967
897648 TA = 1
96790
MA = 1
96349
Ha = 183
630 n
mi
Hp = 181
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16043190
91 X = 4842485
64
Y = 14893597
81 feet Y = 4593985
54 meter
Z = -2462801
73 Z = -727021
27
XDOT = -12403
435181 XDOT = -3785
802613
YDOT = 10124
560505 feet/sec YDOT = 3043
660873 meter/sec
ZDOT = -19579
716693 ZDOT = -5986
276220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21361941
06 X = -6511119
64
Y = 4827482
65 feet Y = 1471416
71 meter
Z = -2373079
82 Z = -723314
73
XDOT = -1051
343475 XDOT = -320
449491
YDOT = -14306
651064 feet/sec YDOT = -4360
667244 meter/sec
ZDOT = -19648
637900 ZDOT = -5988
904832
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 07146
01126078
00020000 00000-0 20000-3 0 9103
2 25544 51
6346 218
5021 0008462 249
5713 110
4544 15
77536006 7272
Satellite: ISS
Catalog Number: 25544
Epoch time: 07146
01126078 = yrday
fracday
Element set: 910
Inclination: 51
6346 deg
RA of node: 218
5021 deg
Eccentricity:
0008462
Arg of perigee: 249
5713 deg
Mean anomaly: 110
4544 deg
Mean motion: 15
77536006 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 727
Checksum: 267
Coasting Arc #12 (Orbit 742)
---------------------------------------
Vector Time (GMT): 2007/146/23:32:35
815
Vector Time (MET): N/A
Weight (LBS) : 480590
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4155334
00 A = 6711325
35 meter
Y = -1972189
04 meter E =
0003150
Z = 4890183
40 I = 51
44709
XDOT = 5110
823456 Wp = 294
70892
YDOT = 5331
796415 meter/sec RA = 212
52858 deg
ZDOT = -2192
332910 TA = 176
63056
MA = 176
62843
Ha = 183
137 n
mi
Hp = 181
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13632985
55 X = 4153322
57
Y = -6470436
48 feet Y = -1925733
47 meter
Z = 16043908
79 Z = 4910365
17
XDOT = 16767
793490 XDOT = 5061
472759
YDOT = 17492
770392 feet/sec YDOT = 5388
672784 meter/sec
ZDOT = -7192
693273 ZDOT = -2167
623613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2061759
23 X = -628424
21
Y = 14867208
62 feet Y = 4531525
19 meter
Z = 16119773
85 Z = 4913307
07
XDOT = -22774
502332 XDOT = -6941
668311
YDOT = 4539
279614 feet/sec YDOT = 1383
572426 meter/sec
ZDOT = -7098
836896 ZDOT = -2163
725486
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 07147
02478518
00020000 00000-0 20000-3 0 9115
2 25544 51
6346 213
2688 0008456 255
3690 104
6538 15
77629574 7434
Satellite: ISS
Catalog Number: 25544
Epoch time: 07147
02478518 = yrday
fracday
Element set: 911
Inclination: 51
6346 deg
RA of node: 213
2688 deg
Eccentricity:
0008456
Arg of perigee: 255
3690 deg
Mean anomaly: 104
6538 deg
Mean motion: 15
77629574 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 743
Checksum: 311
Coasting Arc #13 (Orbit 758)
---------------------------------------
Vector Time (GMT): 2007/147/23:32:35
815
Vector Time (MET): N/A
Weight (LBS) : 480590
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3819394
74 A = 6718124
74 meter
Y = -4650865
67 meter E =
0005043
Z = 2981340
69 I = 51
49475
XDOT = 5700
080819 Wp = 89
00814
YDOT = -1494
280303 meter/sec RA = 207
39496 deg
ZDOT = 4964
187690 TA = 305
55089
MA = 305
59789
Ha = 182
970 n
mi
Hp = 181
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12530822
63 X = -3781587
24
Y = -15258745
65 feet Y = -4693365
22 meter
Z = 9781301
48 Z = 2962877
12
XDOT = 18701
052555 XDOT = 5692
250951
YDOT = -4902
494433 feet/sec YDOT = -1430
583126 meter/sec
ZDOT = 16286
705019 ZDOT = 4991
859915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19628939
43 X = 5982900
74
Y = -2433990
10 feet Y = -741880
18 meter
Z = 9711082
44 Z = 2959937
93
XDOT = -6024
708186 XDOT = -1836
331055
YDOT = 16903
559980 feet/sec YDOT = 5152
205082 meter/sec
ZDOT = 16390
885932 ZDOT = 4995
942032
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 07148
03829684
00020000 00000-0 20000-3 0 9122
2 25544 51
6348 208
0349 0008335 259
5736 100
4490 15
77602802 7598
Satellite: ISS
Catalog Number: 25544
Epoch time: 07148
03829684 = yrday
fracday
Element set: 912
Inclination: 51
6348 deg
RA of node: 208
0349 deg
Eccentricity:
0008335
Arg of perigee: 259
5736 deg
Mean anomaly: 100
4490 deg
Mean motion: 15
77602802 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 759
Checksum: 302
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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