Date:
March 12th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 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
075/02:53:23
433 -2
1 8
0 8
0
N/A 5
0 -0
3 186
3
000/00:11:26
867 -5
9 0
0 178
1
Coasting Arc #1 (Orbit 3470)
---------------------------------------
Vector Time (GMT): 2007/066/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1843279
18 A = 6715315
51 meter
Y = 5975224
96 meter E =
0016451
Z = -2439780
13 I = 51
32593
XDOT = -4324
631504 Wp = 281
41374
YDOT = -3520
510058 meter/sec RA = 268
94658 deg
ZDOT = -5321
256189 TA = 286
33406
MA = 286
51490
Ha = 184
352 n
mi
Hp = 174
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6047503
86 X = -1898106
08
Y = 19603756
43 feet Y = 5954305
64 meter
Z = -8004527
98 Z = -2448868
36
XDOT = -14188
423568 XDOT = -4259
093724
YDOT = -11550
229848 feet/sec YDOT = -3568
504487 meter/sec
ZDOT = -17458
189596 ZDOT = -5342
105626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15229190
49 X = -4641857
26
Y = 13726493
12 feet Y = 4183835
10 meter
Z = -8037859
24 Z = -2449939
50
XDOT = -5144
972027 XDOT = -1568
187474
YDOT = -16041
415410 feet/sec YDOT = -4889
423417 meter/sec
ZDOT = -17536
987871 ZDOT = -5345
273903
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 07066
48505197
00020000 00000-0 20000-3 0 9007
2 25544 51
6332 269
5244 0021287 288
9593 70
9266 15
79017562 34716
Satellite: ISS
Catalog Number: 25544
Epoch time: 07066
48505197 = yrday
fracday
Element set: 900
Inclination: 51
6332 deg
RA of node: 269
5244 deg
Eccentricity:
0021287
Arg of perigee: 288
9593 deg
Mean anomaly: 70
9266 deg
Mean motion: 15
79017562 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3471
Checksum: 315
Coasting Arc #2 (Orbit 3486)
---------------------------------------
Vector Time (GMT): 2007/067/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3414163
78 A = 6711886
57 meter
Y = 4516915
16 meter E =
0012207
Z = 3619412
88 I = 51
31756
XDOT = -2878
009032 Wp = 320
51692
YDOT = 5661
085672 meter/sec RA = 263
69990 deg
ZDOT = -4348
794075 TA = 175
85609
MA = 175
84597
Ha = 184
509 n
mi
Hp = 174
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11201324
73 X = 3345818
86
Y = 14819275
47 feet Y = 4554712
35 meter
Z = 11874714
16 Z = 3635832
51
XDOT = -9442
286849 XDOT = -2919
972638
YDOT = 18573
115722 feet/sec YDOT = 5628
667259 meter/sec
ZDOT = -14267
697096 ZDOT = -4362
877670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2246484
44 X = 684728
46
Y = 18399743
74 feet Y = 5608241
89 meter
Z = 11937008
65 Z = 3638400
24
XDOT = -16045
331708 XDOT = -4890
617105
YDOT = 11251
828827 feet/sec YDOT = 3429
557426 meter/sec
ZDOT = -14319
836055 ZDOT = -4364
686030
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 07067
49763098
00020000 00000-0 20000-3 0 9016
2 25544 51
6336 264
2833 0021427 293
2926 66
5984 15
79114479 34871
Satellite: ISS
Catalog Number: 25544
Epoch time: 07067
49763098 = yrday
fracday
Element set: 901
Inclination: 51
6336 deg
RA of node: 264
2833 deg
Eccentricity:
0021427
Arg of perigee: 293
2926 deg
Mean anomaly: 66
5984 deg
Mean motion: 15
79114479 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3487
Checksum: 329
Coasting Arc #3 (Orbit 3502)
---------------------------------------
Vector Time (GMT): 2007/068/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3171234
17 A = 6707856
63 meter
Y = -3523773
75 meter E =
0013947
Z = 4754050
84 I = 51
30676
XDOT = 3376
247503 Wp = 295
86207
YDOT = 6441
768597 meter/sec RA = 258
54681 deg
ZDOT = 2534
333288 TA = 129
26460
MA = 129
14078
Ha = 184
730 n
mi
Hp = 174
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10404311
57 X = 3187307
57
Y = -11560937
51 feet Y = -3488221
15 meter
Z = 15597279
66 Z = 4769495
85
XDOT = 11076
927503 XDOT = 3291
652499
YDOT = 21134
411406 feet/sec YDOT = 6479
050805 meter/sec
ZDOT = 8314
741760 ZDOT = 2550
529271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14626413
33 X = 4458130
78
Y = -5116112
74 feet Y = -1559391
16 meter
Z = 15654824
55 Z = 4771590
52
XDOT = -961
115302 XDOT = -292
947944
YDOT = 22765
876244 feet/sec YDOT = 6939
039079 meter/sec
ZDOT = 8376
459717 ZDOT = 2553
144922
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 07068
51019186
00020000 00000-0 20000-3 0 9023
2 25544 51
6324 259
0417 0021263 297
3809 62
5193 15
79064484 35038
Satellite: ISS
Catalog Number: 25544
Epoch time: 07068
51019186 = yrday
fracday
Element set: 902
Inclination: 51
6324 deg
RA of node: 259
0417 deg
Eccentricity:
0021263
Arg of perigee: 297
3809 deg
Mean anomaly: 62
5193 deg
Mean motion: 15
79064484 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3503
Checksum: 293
Coasting Arc #4 (Orbit 3517)
---------------------------------------
Vector Time (GMT): 2007/069/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2345117
11 A = 6717506
11 meter
Y = -6254809
18 meter E =
0022323
Z = -564420
20 I = 51
34608
XDOT = 4350
312200 Wp = 329
93001
YDOT = -2179
245072 meter/sec RA = 253
32253 deg
ZDOT = 5992
170167 TA = 23
88077
MA = 23
77737
Ha = 184
926 n
mi
Hp = 174
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7693953
77 X = -2272258
80
Y = -20521027
49 feet Y = -6280626
23 meter
Z = -1851772
31 Z = -575635
59
XDOT = 14272
677820 XDOT = 4345
248733
YDOT = -7149
754173 feet/sec YDOT = -2130
625591 meter/sec
ZDOT = 19659
350941 ZDOT = 6013
291666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2845665
42 X = 867358
82
Y = -21726726
37 feet Y = -6622306
20 meter
Z = -1894757
00 Z = -577521
93
XDOT = 14277
652653 XDOT = 4351
828529
YDOT = 125
541222 feet/sec YDOT = 38
264965 meter/sec
ZDOT = 19738
407466 ZDOT = 6016
266596
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 07069
45944276
00020000 00000-0 20000-3 0 9035
2 25544 51
6315 254
1281 0021382 300
7675 59
1385 15
79120381 35185
Satellite: ISS
Catalog Number: 25544
Epoch time: 07069
45944276 = yrday
fracday
Element set: 903
Inclination: 51
6315 deg
RA of node: 254
1281 deg
Eccentricity:
0021382
Arg of perigee: 300
7675 deg
Mean anomaly: 59
1385 deg
Mean motion: 15
79120381 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3518
Checksum: 292
Coasting Arc #5 (Orbit 3533)
---------------------------------------
Vector Time (GMT): 2007/070/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4334586
61 A = 6705897
54 meter
Y = 182744
34 meter E =
0010207
Z = -5108652
96 I = 51
31619
XDOT = -1837
649650 Wp = 340
46586
YDOT = -7377
478800 meter/sec RA = 248
11923 deg
ZDOT = 1304
060306 TA = 301
99196
MA = 302
09112
Ha = 184
976 n
mi
Hp = 174
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14221084
67 X = -4311491
16
Y = 599554
93 feet Y = 134401
63 meter
Z = -16760672
43 Z = -5129654
16
XDOT = -6029
034285 XDOT = -1761
351899
YDOT = -24204
326772 feet/sec YDOT = -7397
601805 meter/sec
ZDOT = 4278
413079 ZDOT = 1295
318491
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12859696
73 X = -3919635
56
Y = -5880177
13 feet Y = -1792277
99 meter
Z = -16839553
80 Z = -5132696
00
XDOT = 5168
114339 XDOT = 1575
241251
YDOT = -23376
076141 feet/sec YDOT = -7125
028008 meter/sec
ZDOT = 4244
565057 ZDOT = 1293
743429
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 07070
47195676
00020000 00000-0 20000-3 0 9042
2 25544 51
6306 248
8869 0021213 304
6477 55
2689 15
79185018 35343
Satellite: ISS
Catalog Number: 25544
Epoch time: 07070
47195676 = yrday
fracday
Element set: 904
Inclination: 51
6306 deg
RA of node: 248
8869 deg
Eccentricity:
0021213
Arg of perigee: 304
6477 deg
Mean anomaly: 55
2689 deg
Mean motion: 15
79185018 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3534
Checksum: 317
Coasting Arc #6 (Orbit 3549)
---------------------------------------
Vector Time (GMT): 2007/071/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 661494
25 A = 6714099
28 meter
Y = 6099529
13 meter E =
0016543
Z = -2731560
80 I = 51
35605
XDOT = -5482
657216 Wp = 310
78368
YDOT = -1717
109192 meter/sec RA = 242
95727 deg
ZDOT = -5131
076627 TA = 260
59917
MA = 260
78624
Ha = 185
349 n
mi
Hp = 174
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2170256
72 X = 606508
58
Y = 20011578
52 feet Y = 6106618
87 meter
Z = -8961813
64 Z = -2728480
89
XDOT = -17987
720526 XDOT = -5438
123162
YDOT = -5633
560341 feet/sec YDOT = -1778
170361 meter/sec
ZDOT = -16834
240903 ZDOT = -5157
602944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6782966
69 X = -2067448
25
Y = 18957500
88 feet Y = 5778246
27 meter
Z = -8949408
69 Z = -2727779
77
XDOT = -12226
886975 XDOT = -3726
755150
YDOT = -12416
946043 feet/sec YDOT = -3784
685154 meter/sec
ZDOT = -16934
149166 ZDOT = -5161
528666
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 07071
48444698
00020000 00000-0 20000-3 0 9056
2 25544 51
6305 243
6470 0021305 308
8692 51
0572 15
79225333 35508
Satellite: ISS
Catalog Number: 25544
Epoch time: 07071
48444698 = yrday
fracday
Element set: 905
Inclination: 51
6305 deg
RA of node: 243
6470 deg
Eccentricity:
0021305
Arg of perigee: 308
8692 deg
Mean anomaly: 51
0572 deg
Mean motion: 15
79225333 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3550
Checksum: 286
Coasting Arc #7 (Orbit 3565)
---------------------------------------
Vector Time (GMT): 2007/072/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5025086
60 A = 6712353
06 meter
Y = 2978914
77 meter E =
0014607
Z = 3323820
33 I = 51
36475
XDOT = -537
777851 Wp = 347
51765
YDOT = 6108
043615 meter/sec RA = 237
71098 deg
ZDOT = -4650
929682 TA = 153
20337
MA = 153
12784
Ha = 185
552 n
mi
Hp = 173
833
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16486504
59 X = 4975256
17
Y = 9773342
42 feet Y = 3034829
50 meter
Z = 10904922
36 Z = 3348110
82
XDOT = -1764
363027 XDOT = -583
445826
YDOT = 20039
513172 feet/sec YDOT = 6101
774511 meter/sec
ZDOT = -15258
955650 ZDOT = -4653
653136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10747412
81 X = 3275811
42
Y = 15805316
05 feet Y = 4817460
33 meter
Z = 10996612
65 Z = 3351767
54
XDOT = -8848
400081 XDOT = -2696
992345
YDOT = 16663
044418 feet/sec YDOT = 5078
895939 meter/sec
ZDOT = -15268
352358 ZDOT = -4653
793799
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 07072
49691277
00020000 00000-0 20000-3 0 9066
2 25544 51
6304 238
4050 0021399 312
3070 47
6282 15
79259080 35668
Satellite: ISS
Catalog Number: 25544
Epoch time: 07072
49691277 = yrday
fracday
Element set: 906
Inclination: 51
6304 deg
RA of node: 238
4050 deg
Eccentricity:
0021399
Arg of perigee: 312
3070 deg
Mean anomaly: 47
6282 deg
Mean motion: 15
79259080 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3566
Checksum: 296
Coasting Arc #8 (Orbit 3581)
---------------------------------------
Vector Time (GMT): 2007/073/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1738782
45 A = 6706580
14 meter
Y = -4208818
43 meter E =
0015344
Z = 4927856
11 I = 51
36088
XDOT = 5708
499680 Wp = 321
83517
YDOT = 4749
435285 meter/sec RA = 232
55692 deg
ZDOT = 2057
496423 TA = 108
25923
MA = 108
09220
Ha = 185
750 n
mi
Hp = 173
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5704666
83 X = 1761778
61
Y = -13808459
43 feet Y = -4189245
75 meter
Z = 16167506
92 Z = 4936358
89
XDOT = 18728
673492 XDOT = 5644
971774
YDOT = 15582
136762 feet/sec YDOT = 4812
915748 meter/sec
ZDOT = 6750
316347 ZDOT = 2085
073458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10754014
13 X = 3277823
51
Y = -10322426
58 feet Y = -3146275
62 meter
Z = 16198880
98 Z = 4937418
92
XDOT = 9966
673705 XDOT = 3037
842145
YDOT = 21061
668228 feet/sec YDOT = 6419
596476 meter/sec
ZDOT = 6854
615429 ZDOT = 2089
286783
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 07073
50935723
00020000 00000-0 20000-3 0 9077
2 25544 51
6296 233
1627 0021268 316
7163 43
2331 15
79261337 35829
Satellite: ISS
Catalog Number: 25544
Epoch time: 07073
50935723 = yrday
fracday
Element set: 907
Inclination: 51
6296 deg
RA of node: 233
1627 deg
Eccentricity:
0021268
Arg of perigee: 316
7163 deg
Mean anomaly: 43
2331 deg
Mean motion: 15
79261337 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3582
Checksum: 288
Coasting Arc #9 (Orbit 3596)
---------------------------------------
Vector Time (GMT): 2007/074/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4574833
87 A = 6717090
31 meter
Y = -4895036
77 meter E =
0025414
Z = -59763
14 I = 51
41598
XDOT = 3479
719175 Wp = 348
86502
YDOT = -3330
668921 meter/sec RA = 227
34434 deg
ZDOT = 6036
291642 TA = 10
48120
MA = 10
42832
Ha = 185
869 n
mi
Hp = 173
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15009297
46 X = -4519466
54
Y = -16059831
92 feet Y = -4945885
55 meter
Z = -196073
31 Z = -81852
59
XDOT = 11416
401493 XDOT = 3487
381947
YDOT = -10927
391474 feet/sec YDOT = -3291
713709 meter/sec
ZDOT = 19804
106438 ZDOT = 6053
214502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7517910
99 X = -2291459
27
Y = -20655226
75 feet Y = -6295713
11 meter
Z = -279782
90 Z = -85277
83
XDOT = 13176
731183 XDOT = 4016
267665
YDOT = -5077
497214 feet/sec YDOT = -1547
621151 meter/sec
ZDOT = 19867
248189 ZDOT = 6055
537248
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 07074
45849919
00020000 00000-0 20000-3 0 9084
2 25544 51
6301 228
2486 0021143 320
2327 39
7288 15
79318936 35973
Satellite: ISS
Catalog Number: 25544
Epoch time: 07074
45849919 = yrday
fracday
Element set: 908
Inclination: 51
6301 deg
RA of node: 228
2486 deg
Eccentricity:
0021143
Arg of perigee: 320
2327 deg
Mean anomaly: 39
7288 deg
Mean motion: 15
79318936 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3597
Checksum: 319
Coasting Arc #10 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2007/075/02:59:06
867
Vector Time (MET): N/A
Weight (LBS) : 478751
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4347879
52 A = 6721183
94 meter
Y = 5065135
71 meter E =
0005393
Z = -796345
13 I = 51
43092
XDOT = -4132
972612 Wp = 302
34104
YDOT = 2607
229919 meter/sec RA = 223
89872 deg
ZDOT = -5949
824406 TA = 246
37327
MA = 246
42990
Ha = 186
253 n
mi
Hp = 178
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14264696
59 X = 4294785
72
Y = 16617899
31 feet Y = 5113459
23 meter
Z = -2612680
87 Z = -775352
79
XDOT = -13559
621430 XDOT = -4132
917291
YDOT = 8553
903934 feet/sec YDOT = 2561
012716 meter/sec
ZDOT = -19520
421280 ZDOT = -5969
901964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21434750
99 X = -6533312
10
Y = -4538424
24 feet Y = -1383311
71 meter
Z = -2533061
92 Z = -772077
27
XDOT = 5165
688857 XDOT = 1574
501964
YDOT = -13399
638005 feet/sec YDOT = -4084
209664 meter/sec
ZDOT = -19595
522738 ZDOT = -5972
715331
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 07075
15456134
00020000 00000-0 20000-3 0 9096
2 25544 51
6325 224
6503 0015688 314
4882 45
4999 15
77777549 36080
Satellite: ISS
Catalog Number: 25544
Epoch time: 07075
15456134 = yrday
fracday
Element set: 909
Inclination: 51
6325 deg
RA of node: 224
6503 deg
Eccentricity:
0015688
Arg of perigee: 314
4882 deg
Mean anomaly: 45
4999 deg
Mean motion: 15
77777549 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3608
Checksum: 328
Coasting Arc #11 (Orbit 3623)
---------------------------------------
Vector Time (GMT): 2007/076/02:59:06
867
Vector Time (MET): N/A
Weight (LBS) : 478751
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4449586
04 A = 6710993
53 meter
Y = -1382528
69 meter E =
0016092
Z = 4839401
01 I = 51
41858
XDOT = 4378
349261 Wp = 343
11207
YDOT = 5888
413029 meter/sec RA = 218
69202 deg
ZDOT = -2330
221697 TA = 129
73816
MA = 129
59626
Ha = 186
413 n
mi
Hp = 177
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14598379
38 X = 4441206
49
Y = -4535855
28 feet Y = -1332817
40 meter
Z = 15877299
90 Z = 4860996
43
XDOT = 14364
662930 XDOT = 4323
498350
YDOT = 19318
940383 feet/sec YDOT = 5937
067308 meter/sec
ZDOT = -7645
084307 ZDOT = -2309
085794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8562467
98 X = -2609840
24
Y = 12561556
12 feet Y = 3828762
31 meter
Z = 15958282
05 Z = 4864084
37
XDOT = -22370
292575 XDOT = -6818
465177
YDOT = -5583
239479 feet/sec YDOT = -1701
771393 meter/sec
ZDOT = -7564
796280 ZDOT = -2305
749906
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 07076
16794410
00020000 00000-0 20000-3 0 9102
2 25544 51
6324 219
4158 0015788 318
6530 41
3439 15
77827964 36243
Satellite: ISS
Catalog Number: 25544
Epoch time: 07076
16794410 = yrday
fracday
Element set: 910
Inclination: 51
6324 deg
RA of node: 219
4158 deg
Eccentricity:
0015788
Arg of perigee: 318
6530 deg
Mean anomaly: 41
3439 deg
Mean motion: 15
77827964 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3624
Checksum: 307
Coasting Arc #12 (Orbit 3639)
---------------------------------------
Vector Time (GMT): 2007/077/02:59:06
867
Vector Time (MET): N/A
Weight (LBS) : 478751
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3084210
85 A = 6716964
64 meter
Y = -5056365
51 meter E =
0013956
Z = 3149930
13 I = 51
46270
XDOT = 5981
223805 Wp = 14
47796
YDOT = -646
562053 meter/sec RA = 213
55581 deg
ZDOT = 4827
281346 TA = 22
41352
MA = 22
35261
Ha = 186
706 n
mi
Hp = 177
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10118802
00 X = -3042742
18
Y = -16589125
68 feet Y = -5090622
69 meter
Z = 10334416
43 Z = 3135048
51
XDOT = 19623
437679 XDOT = 5964
559514
YDOT = -2121
266579 feet/sec YDOT = -579
769336 meter/sec
ZDOT = 15837
537225 ZDOT = 4856
297273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18387107
94 X = 5604390
50
Y = 6377425
38 feet Y = 1943839
26 meter
Z = 10277748
54 Z = 3132657
75
XDOT = -13297
086142 XDOT = -4052
951856
YDOT = 12684
836386 feet/sec YDOT = 3866
338131 meter/sec
ZDOT = 15946
521989 ZDOT = 4860
499902
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 07077
18130489
00020000 00000-0 20000-3 0 9116
2 25544 51
6331 214
1803 0015823 322
8409 37
1660 15
77845894 36401
Satellite: ISS
Catalog Number: 25544
Epoch time: 07077
18130489 = yrday
fracday
Element set: 911
Inclination: 51
6331 deg
RA of node: 214
1803 deg
Eccentricity:
0015823
Arg of perigee: 322
8409 deg
Mean anomaly: 37
1660 deg
Mean motion: 15
77845894 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3640
Checksum: 289
Coasting Arc #13 (Orbit 3654)
---------------------------------------
Vector Time (GMT): 2007/078/02:59:06
867
Vector Time (MET): N/A
Weight (LBS) : 478751
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5833297
68 A = 6716213
61 meter
Y = -154152
51 meter E =
0013947
Z = -3307641
09 I = 51
48656
XDOT = -2505
893148 Wp = 343
77105
YDOT = -5589
466193 meter/sec RA = 208
32765 deg
ZDOT = 4688
302464 TA = 337
16291
MA = 337
22488
Ha = 186
724 n
mi
Hp = 177
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19138115
75 X = -5815072
60
Y = -505749
70 feet Y = -219282
18 meter
Z = -10851840
86 Z = -3335934
72
XDOT = -8221
434211 XDOT = -2465
979423
YDOT = -18338
143677 feet/sec YDOT = -5617
264788 meter/sec
ZDOT = 15381
569763 ZDOT = 4676
226531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14870282
75 X = 4532462
18
Y = -11961506
09 feet Y = -3645867
06 meter
Z = -10958228
44 Z = -3340068
03
XDOT = 17328
893208 XDOT = 5281
846650
YDOT = 7518
966047 feet/sec YDOT = 2291
780851 meter/sec
ZDOT = 15335
367547 ZDOT = 4674
220028
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 07078
13130871
00020000 00000-0 20000-3 0 9128
2 25544 51
6340 209
2727 0015888 326
4186 33
5971 15
77899403 36550
Satellite: ISS
Catalog Number: 25544
Epoch time: 07078
13130871 = yrday
fracday
Element set: 912
Inclination: 51
6340 deg
RA of node: 209
2727 deg
Eccentricity:
0015888
Arg of perigee: 326
4186 deg
Mean anomaly: 33
5971 deg
Mean motion: 15
77899403 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3655
Checksum: 310
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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