Date:
July 12th 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) : 82 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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
202/01:19:29
699 -0
9 3
4 3
4
N/A 3
3 0
1 186
9
000/00:04:59
398 0
1 0
2 172
7
Coasting Arc #1 (Orbit 1460)
---------------------------------------
Vector Time (GMT): 2007/192/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6073021
00 A = 6714540
04 meter
Y = -8705
75 meter E =
0011341
Z = -2877746
09 I = 51
51864
XDOT = 2392
925372 Wp = 73
41073
YDOT = -5297
401090 meter/sec RA = 337
95449 deg
ZDOT = -5047
042575 TA = 139
75214
MA = 139
66813
Ha = 185
384 n
mi
Hp = 173
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19924609
57 X = -6058492
76
Y = -28562
17 feet Y = -76535
83 meter
Z = -9441424
18 Z = -2907213
46
XDOT = 7850
805027 XDOT = 2476
501385
YDOT = -17379
924835 feet/sec YDOT = -5270
173675 meter/sec
ZDOT = -16558
538633 ZDOT = -5035
215906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1095104
86 X = 333787
96
Y = 19841229
80 feet Y = 6047606
84 meter
Z = -9552890
58 Z = -2911721
05
XDOT = -16354
373829 XDOT = -4984
813143
YDOT = -7027
873846 feet/sec YDOT = -2142
095948 meter/sec
ZDOT = -16514
350653 ZDOT = -5033
574079
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 07192
48413469
00020000 00000-0 20000-3 0 9007
2 25544 51
6320 338
2981 0008386 53
2939 306
8996 15
78907763 14615
Satellite: ISS
Catalog Number: 25544
Epoch time: 07192
48413469 = yrday
fracday
Element set: 900
Inclination: 51
6320 deg
RA of node: 338
2981 deg
Eccentricity:
0008386
Arg of perigee: 53
2939 deg
Mean anomaly: 306
8996 deg
Mean motion: 15
78907763 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1461
Checksum: 324
Coasting Arc #2 (Orbit 1476)
---------------------------------------
Vector Time (GMT): 2007/193/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3443119
89 A = 6713581
62 meter
Y = 4722454
90 meter E =
0020140
Z = 3291362
32 I = 51
48820
XDOT = -6020
179746 Wp = 78
08528
YDOT = -1098
188940 meter/sec RA = 332
72089 deg
ZDOT = -4693
875125 TA = 63
07727
MA = 62
87163
Ha = 185
436 n
mi
Hp = 173
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11296325
10 X = -3511659
87
Y = 15493618
44 feet Y = 4683568
04 meter
Z = 10798432
81 Z = 3274470
36
XDOT = -19751
245886 XDOT = -5984
650417
YDOT = -3602
982088 feet/sec YDOT = -1165
310275 meter/sec
ZDOT = -15399
852771 ZDOT = -4723
034846
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16288525
75 X = 4964742
65
Y = 10183741
28 feet Y = 3104004
34 meter
Z = 10735020
58 Z = 3272034
27
XDOT = -1401
071308 XDOT = -427
046535
YDOT = 18688
957651 feet/sec YDOT = 5696
394292 meter/sec
ZDOT = -15510
276171 ZDOT = -4727
532177
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 07193
49681036
00020000 00000-0 20000-3 0 9017
2 25544 51
6315 333
0579 0008239 57
5465 302
6496 15
78902702 14777
Satellite: ISS
Catalog Number: 25544
Epoch time: 07193
49681036 = yrday
fracday
Element set: 901
Inclination: 51
6315 deg
RA of node: 333
0579 deg
Eccentricity:
0008239
Arg of perigee: 57
5465 deg
Mean anomaly: 302
6496 deg
Mean motion: 15
78902702 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1477
Checksum: 306
Coasting Arc #3 (Orbit 1492)
---------------------------------------
Vector Time (GMT): 2007/194/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4117467
86 A = 6707456
33 meter
Y = 2002696
16 meter E =
0012368
Z = 4890786
42 I = 51
44417
XDOT = -5158
957573 Wp = 86
89802
YDOT = 5317
788570 meter/sec RA = 327
57825 deg
ZDOT = 2161
674275 TA = 342
09275
MA = 342
13629
Ha = 185
200 n
mi
Hp = 173
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13508752
82 X = 4071009
21
Y = 6570525
46 feet Y = 2048479
18 meter
Z = 16045887
21 Z = 4910676
37
XDOT = -16925
713822 XDOT = -5228
539305
YDOT = 17446
812894 feet/sec YDOT = 5259
708693 meter/sec
ZDOT = 7092
107200 ZDOT = 2136
444567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5324191
88 X = 1622813
69
Y = -13960084
06 feet Y = -4255033
62 meter
Z = 16121344
17 Z = 4913785
70
XDOT = 17897
980128 XDOT = 5455
304343
YDOT = 14921
696226 feet/sec YDOT = 4548
133010 meter/sec
ZDOT = 6997
211151 ZDOT = 2132
749959
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 07194
50946295
00020000 00000-0 20000-3 0 9022
2 25544 51
6324 327
8183 0008195 60
6737 299
5246 15
78974845 14939
Satellite: ISS
Catalog Number: 25544
Epoch time: 07194
50946295 = yrday
fracday
Element set: 902
Inclination: 51
6324 deg
RA of node: 327
8183 deg
Eccentricity:
0008195
Arg of perigee: 60
6737 deg
Mean anomaly: 299
5246 deg
Mean motion: 15
78974845 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1493
Checksum: 333
Coasting Arc #4 (Orbit 1507)
---------------------------------------
Vector Time (GMT): 2007/195/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5173561
44 A = 6717995
21 meter
Y = -4264625
80 meter E =
0019767
Z = -274714
65 I = 51
45740
XDOT = 3239
770629 Wp = 51
72198
YDOT = 3561
794881 meter/sec RA = 322
37141 deg
ZDOT = 6023
845157 TA = 305
27767
MA = 305
46242
Ha = 185
370 n
mi
Hp = 173
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16973626
78 X = 5222199
09
Y = -13991554
45 feet Y = -4206500
12 meter
Z = -901294
78 Z = -249464
70
XDOT = 10629
168731 XDOT = 3170
439176
YDOT = 11685
678742 feet/sec YDOT = 3597
634973 meter/sec
ZDOT = 19763
271512 ZDOT = 6039
415949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15742903
94 X = -4798437
12
Y = -15368504
64 feet Y = -4684320
21 meter
Z = -806210
37 Z = -245732
92
XDOT = 9360
971640 XDOT = 2853
224156
YDOT = -10570
464228 feet/sec YDOT = -3221
877497 meter/sec
ZDOT = 19822
558362 ZDOT = 6041
915789
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 07195
45880661
00020000 00000-0 20000-3 0 9032
2 25544 51
6337 322
9068 0008322 64
7395 295
4632 15
78986908 15082
Satellite: ISS
Catalog Number: 25544
Epoch time: 07195
45880661 = yrday
fracday
Element set: 903
Inclination: 51
6337 deg
RA of node: 322
9068 deg
Eccentricity:
0008322
Arg of perigee: 64
7395 deg
Mean anomaly: 295
4632 deg
Mean motion: 15
78986908 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1508
Checksum: 326
Coasting Arc #5 (Orbit 1523)
---------------------------------------
Vector Time (GMT): 2007/196/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1439579
66 A = 6706694
40 meter
Y = -4177524
70 meter E =
0021105
Z = -5063411
41 I = 51
39755
XDOT = 6307
351385 Wp = 89
20507
YDOT = -4105
047536 meter/sec RA = 317
17230 deg
ZDOT = 1599
611465 TA = 196
19018
MA = 196
25771
Ha = 185
323 n
mi
Hp = 173
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4723030
39 X = -1368162
41
Y = -13705789
70 feet Y = -4193222
70 meter
Z = -16612242
14 Z = -5070231
98
XDOT = 20693
410055 XDOT = 6345
015415
YDOT = -13468
003726 feet/sec YDOT = -4034
304875 meter/sec
ZDOT = 5248
069112 ZDOT = 1630
342650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13019162
09 X = -3968240
60
Y = 6307470
77 feet Y = 1922517
09 meter
Z = -16638494
75 Z = -5071413
20
XDOT = -15486
421123 XDOT = -4720
261158
YDOT = -17867
863528 feet/sec YDOT = -5446
124803 meter/sec
ZDOT = 5363
909061 ZDOT = 1634
919482
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 07196
47141801
00020000 00000-0 20000-3 0 9042
2 25544 51
6338 317
6682 0008332 68
1116 292
0935 15
79028323 15242
Satellite: ISS
Catalog Number: 25544
Epoch time: 07196
47141801 = yrday
fracday
Element set: 904
Inclination: 51
6338 deg
RA of node: 317
6682 deg
Eccentricity:
0008332
Arg of perigee: 68
1116 deg
Mean anomaly: 292
0935 deg
Mean motion: 15
79028323 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1524
Checksum: 286
Coasting Arc #6 (Orbit 1539)
---------------------------------------
Vector Time (GMT): 2007/197/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5470078
16 A = 6713986
24 meter
Y = 2568128
49 meter E =
0012141
Z = -2937629
48 I = 51
40230
XDOT = -80
765549 Wp = 84
83715
YDOT = -5861
977598 meter/sec RA = 312
01812 deg
ZDOT = -4990
841684 TA = 129
17781
MA = 129
06990
Ha = 185
286 n
mi
Hp = 173
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17946450
67 X = -5484118
67
Y = 8425618
42 feet Y = 2506880
93 meter
Z = -9637891
99 Z = -2964236
22
XDOT = -264
978834 XDOT = 9
033984
YDOT = -19232
209966 feet/sec YDOT = -5862
377937 meter/sec
ZDOT = -16374
152505 ZDOT = -4991
016775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10882655
15 X = 3317033
29
Y = 16513286
40 feet Y = 5033249
69 meter
Z = -9738289
80 Z = -2968230
73
XDOT = -17808
203787 XDOT = -5427
940514
YDOT = 2110
794182 feet/sec YDOT = 643
370067 meter/sec
ZDOT = -16375
449428 ZDOT = -4991
236986
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 07197
48400767
00020000 00000-0 20000-3 0 9054
2 25544 51
6339 312
4275 0008306 71
3741 288
8326 15
79051528 15403
Satellite: ISS
Catalog Number: 25544
Epoch time: 07197
48400767 = yrday
fracday
Element set: 905
Inclination: 51
6339 deg
RA of node: 312
4275 deg
Eccentricity:
0008306
Arg of perigee: 71
3741 deg
Mean anomaly: 288
8326 deg
Mean motion: 15
79051528 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1540
Checksum: 299
Coasting Arc #7 (Orbit 1555)
---------------------------------------
Vector Time (GMT): 2007/198/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1153055
41 A = 6713376
09 meter
Y = 5788619
53 meter E =
0021046
Z = 3182301
07 I = 51
38202
XDOT = -5871
241502 Wp = 86
02717
YDOT = 1474
950348 meter/sec RA = 306
77635 deg
ZDOT = -4781
772343 TA = 56
57117
MA = 56
37007
Ha = 185
311 n
mi
Hp = 173
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3782990
20 X = -1233157
62
Y = 18991533
91 feet Y = 5775277
16 meter
Z = 10440620
30 Z = 3176505
79
XDOT = -19262
603353 XDOT = -5864
069777
YDOT = 4839
075946 feet/sec YDOT = 1409
335508 meter/sec
ZDOT = -15688
229471 ZDOT = -4810
276615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19360769
18 X = 5901162
45
Y = 770824
74 feet Y = 234947
38 meter
Z = 10419326
91 Z = 3175810
84
XDOT = 7884
486505 XDOT = 2403
191487
YDOT = 16748
364170 feet/sec YDOT = 5104
901399 meter/sec
ZDOT = -15795
925272 ZDOT = -4814
598023
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 07198
49657624
00020000 00000-0 20000-3 0 9063
2 25544 51
6341 307
1880 0008328 75
1547 285
0541 15
79070494 15567
Satellite: ISS
Catalog Number: 25544
Epoch time: 07198
49657624 = yrday
fracday
Element set: 906
Inclination: 51
6341 deg
RA of node: 307
1880 deg
Eccentricity:
0008328
Arg of perigee: 75
1547 deg
Mean anomaly: 285
0541 deg
Mean motion: 15
79070494 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1556
Checksum: 312
Coasting Arc #8 (Orbit 1571)
---------------------------------------
Vector Time (GMT): 2007/199/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4511607
90 A = 6706682
98 meter
Y = 219737
59 meter E =
0012891
Z = 4946933
16 I = 51
34477
XDOT = -2494
870456 Wp = 96
61275
YDOT = 7036
885325 meter/sec RA = 301
62366 deg
ZDOT = 1956
940313 TA = 334
40938
MA = 334
47313
Ha = 185
024 n
mi
Hp = 172
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14801863
19 X = 4484784
59
Y = 720923
85 feet Y = 270038
44 meter
Z = 16230095
68 Z = 4968785
02
XDOT = -8185
270525 XDOT = -2582
878806
YDOT = 23086
894110 feet/sec YDOT = 7008
493998 meter/sec
ZDOT = 6420
407850 ZDOT = 1944
607416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1880451
80 X = -573161
71
Y = -14607776
86 feet Y = -4452450
39 meter
Z = 16312806
23 Z = 4972143
34
XDOT = 23108
459102 XDOT = 7043
458334
YDOT = 4165
010421 feet/sec YDOT = 1269
495176 meter/sec
ZDOT = 6374
522987 ZDOT = 1942
954606
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 07199
50912107
00020000 00000-0 20000-3 0 9077
2 25544 51
6347 301
9482 0008227 77
9196 282
2891 15
79157564 15720
Satellite: ISS
Catalog Number: 25544
Epoch time: 07199
50912107 = yrday
fracday
Element set: 907
Inclination: 51
6347 deg
RA of node: 301
9482 deg
Eccentricity:
0008227
Arg of perigee: 77
9196 deg
Mean anomaly: 282
2891 deg
Mean motion: 15
79157564 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1572
Checksum: 319
Coasting Arc #9 (Orbit 1586)
---------------------------------------
Vector Time (GMT): 2007/200/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2962295
74 A = 6717584
91 meter
Y = -6021570
66 meter E =
0019723
Z = -31878
76 I = 51
36742
XDOT = 4326
504014 Wp = 59
20303
YDOT = 2111
120831 meter/sec RA = 296
41229 deg
ZDOT = 6023
329987 TA = 300
44854
MA = 300
64324
Ha = 185
233 n
mi
Hp = 172
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9718818
04 X = 3029564
53
Y = -19755809
24 feet Y = -5988068
48 meter
Z = -104589
12 Z = -17325
31
XDOT = 14194
566974 XDOT = 4273
315776
YDOT = 6926
249445 feet/sec YDOT = 2159
204281 meter/sec
ZDOT = 19761
581322 ZDOT = 6044
218843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21260031
22 X = -6480057
52
Y = -5724239
23 feet Y = -1744748
12 meter
Z = -50195
58 Z = -15299
61
XDOT = 3660
819829 XDOT = 1115
817884
YDOT = -13605
121769 feet/sec YDOT = -4146
841115 meter/sec
ZDOT = 19840
860491 ZDOT = 6047
494278
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 07200
45836550
00020000 00000-0 20000-3 0 9082
2 25544 51
6348 297
0360 0008387 80
5088 279
7025 15
79140928 15870
Satellite: ISS
Catalog Number: 25544
Epoch time: 07200
45836550 = yrday
fracday
Element set: 908
Inclination: 51
6348 deg
RA of node: 297
0360 deg
Eccentricity:
0008387
Arg of perigee: 80
5088 deg
Mean anomaly: 279
7025 deg
Mean motion: 15
79140928 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1587
Checksum: 314
Coasting Arc #10 (Orbit 1602)
---------------------------------------
Vector Time (GMT): 2007/201/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2931709
58 A = 6706553
98 meter
Y = -3444938
24 meter E =
0021176
Z = -4970081
94 I = 51
31889
XDOT = 4072
477749 Wp = 96
48179
YDOT = -6236
746829 meter/sec RA = 291
20053 deg
ZDOT = 1925
331038 TA = 192
19052
MA = 192
24184
Ha = 185
138 n
mi
Hp = 172
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9618469
76 X = -2868826
38
Y = -11302290
80 feet Y = -3477370
21 meter
Z = -16306043
11 Z = -4984171
61
XDOT = 13361
147469 XDOT = 4132
562485
YDOT = -20461
767812 feet/sec YDOT = -6190
870318 meter/sec
ZDOT = 6316
702879 ZDOT = 1945
260301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9051671
35 X = -2758949
43
Y = 11686303
74 feet Y = 3561985
38 meter
Z = -16359747
26 Z = -4986450
96
XDOT = -21950
118824 XDOT = -6690
396218
YDOT = -8075
504422 feet/sec YDOT = -2461
413748 meter/sec
ZDOT = 6391
409032 ZDOT = 1948
101473
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 07201
47087101
00020000 00000-0 20000-3 0 9096
2 25544 51
6346 291
7964 0008391 84
2964 275
9159 15
79209267 16035
Satellite: ISS
Catalog Number: 25544
Epoch time: 07201
47087101 = yrday
fracday
Element set: 909
Inclination: 51
6346 deg
RA of node: 291
7964 deg
Eccentricity:
0008391
Arg of perigee: 84
2964 deg
Mean anomaly: 275
9159 deg
Mean motion: 15
79209267 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1603
Checksum: 313
Coasting Arc #11 (Orbit 1612)
---------------------------------------
Vector Time (GMT): 2007/202/01:21:59
398
Vector Time (MET): N/A
Weight (LBS) : 508908
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3816030
28 A = 6707079
68 meter
Y = 1765725
33 meter E =
0013639
Z = 5214006
51 I = 51
30941
XDOT = -2728
056025 Wp = 80
58311
YDOT = 7207
686765 meter/sec RA = 288
10402 deg
ZDOT = -441
090806 TA = 13
63355
MA = 13
59675
Ha = 186
925 n
mi
Hp = 172
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12519784
39 X = 3770673
58
Y = 5793062
10 feet Y = 1808144
23 meter
Z = 17106320
59 Z = 5232434
64
XDOT = -8950
315044 XDOT = -2806
307965
YDOT = 23647
266288 feet/sec YDOT = 7176
742621 meter/sec
ZDOT = -1447
148313 ZDOT = -454
532982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5400226
47 X = 1645989
03
Y = 12599392
23 feet Y = 3840294
75 meter
Z = 17176252
30 Z = 5235321
70
XDOT = -21509
126045 XDOT = -6555
981618
YDOT = 11274
277468 feet/sec YDOT = 3436
399772 meter/sec
ZDOT = -1497
195494 ZDOT = -456
345187
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 07202
10370047
00020000 00000-0 20000-3 0 9103
2 25544 51
6350 288
5239 0011035 83
5274 276
7148 15
78599115 16135
Satellite: ISS
Catalog Number: 25544
Epoch time: 07202
10370047 = yrday
fracday
Element set: 910
Inclination: 51
6350 deg
RA of node: 288
5239 deg
Eccentricity:
0011035
Arg of perigee: 83
5274 deg
Mean anomaly: 276
7148 deg
Mean motion: 15
78599115 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1613
Checksum: 280
Coasting Arc #12 (Orbit 1628)
---------------------------------------
Vector Time (GMT): 2007/203/01:21:59
398
Vector Time (MET): N/A
Weight (LBS) : 508908
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2849720
74 A = 6717639
32 meter
Y = -5782532
37 meter E =
0024879
Z = 1854025
97 I = 51
33704
XDOT = 3775
291738 Wp = 75
22799
YDOT = 3683
480242 meter/sec RA = 282
93158 deg
ZDOT = 5629
188277 TA = 305
50251
MA = 305
73436
Ha = 187
050 n
mi
Hp = 172
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9349477
49 X = 2905163
60
Y = -18971562
88 feet Y = -5750355
39 meter
Z = 6082762
35 Z = 1868003
90
XDOT = 12386
127748 XDOT = 3706
476496
YDOT = 12084
908931 feet/sec YDOT = 3725
312316 meter/sec
ZDOT = 18468
465476 ZDOT = 5647
361790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19450175
05 X = 5928413
36
Y = -8269548
30 feet Y = -2520558
32 meter
Z = 6134996
89 Z = 1869947
05
XDOT = 793
730348 XDOT = 241
929010
YDOT = 15755
775222 feet/sec YDOT = 4802
360288 meter/sec
ZDOT = 18537
653970 ZDOT = 5650
276930
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 07203
11658559
00020000 00000-0 20000-3 0 9113
2 25544 51
6348 283
2858 0011079 86
6119 273
6314 15
78587762 16294
Satellite: ISS
Catalog Number: 25544
Epoch time: 07203
11658559 = yrday
fracday
Element set: 911
Inclination: 51
6348 deg
RA of node: 283
2858 deg
Eccentricity:
0011079
Arg of perigee: 86
6119 deg
Mean anomaly: 273
6314 deg
Mean motion: 15
78587762 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1629
Checksum: 319
Coasting Arc #13 (Orbit 1643)
---------------------------------------
Vector Time (GMT): 2007/204/01:21:59
398
Vector Time (MET): N/A
Weight (LBS) : 508908
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2744687
35 A = 6711466
76 meter
Y = -4518719
78 meter E =
0018679
Z = -4151932
17 I = 51
31127
XDOT = 3732
342712 Wp = 98
46696
YDOT = -5634
729375 meter/sec RA = 277
69441 deg
ZDOT = 3676
577719 TA = 209
22895
MA = 209
33359
Ha = 186
952 n
mi
Hp = 172
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9004879
75 X = -2673785
10
Y = -14825196
12 feet Y = -4549015
47 meter
Z = -13621824
70 Z = -4165094
15
XDOT = 12245
218870 XDOT = 3777
213603
YDOT = -18486
644931 feet/sec YDOT = -5592
741781 meter/sec
ZDOT = 12062
262856 ZDOT = 3694
817687
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2638956
76 X = 804354
02
Y = -17103704
27 feet Y = -5213209
06 meter
Z = -13672147
41 Z = -4167270
53
XDOT = 19945
274404 XDOT = 6079
319638
YDOT = -6589
718637 feet/sec YDOT = -2008
546241 meter/sec
ZDOT = 12130
642493 ZDOT = 3697
419832
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 07204
06614545
00020000 00000-0 20000-3 0 9126
2 25544 51
6347 278
3750 0010939 90
1190 270
1228 15
78626865 16443
Satellite: ISS
Catalog Number: 25544
Epoch time: 07204
06614545 = yrday
fracday
Element set: 912
Inclination: 51
6347 deg
RA of node: 278
3750 deg
Eccentricity:
0010939
Arg of perigee: 90
1190 deg
Mean anomaly: 270
1228 deg
Mean motion: 15
78626865 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1644
Checksum: 291
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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