Date:
November 15th 2006
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) : 75 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 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 1703)
---------------------------------------
Vector Time (GMT): 2006/319/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2444697
10 A = 6718784
56 meter
Y = -5917488
51 meter E =
0015399
Z = 2002483
46 I = 51
89659
XDOT = 5280
491111 Wp = 158
46118
YDOT = 281
032504 meter/sec RA = 126
64460 deg
ZDOT = -5616
646527 TA = 359
24600
MA = 359
24832
Ha = 185
075 n
mi
Hp = 178
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8020659
78 X = 2500957
70
Y = -19414332
38 feet Y = -5889836
02 meter
Z = 6569827
63 Z = 2014496
56
XDOT = 17324
445901 XDOT = 5304
241266
YDOT = 922
022652 feet/sec YDOT = 340
214794 meter/sec
ZDOT = -18427
318003 ZDOT = -5590
935730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12074130
59 X = 3680195
00
Y = 17172115
98 feet Y = 5234060
95 meter
Z = 6613903
80 Z = 2015917
88
XDOT = -8896
725653 XDOT = -2711
721979
YDOT = 13315
198278 feet/sec YDOT = 4058
472435 meter/sec
ZDOT = -18331
257349 ZDOT = -5587
367240
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 06319
54604499
00020000 00000-0 20000-3 0 9009
2 25544 51
6280 127
3564 0011802 219
2568 140
7743 15
78092395 17044
Satellite: ISS
Catalog Number: 25544
Epoch time: 06319
54604499 = yrday
fracday
Element set: 900
Inclination: 51
6280 deg
RA of node: 127
3564 deg
Eccentricity:
0011802
Arg of perigee: 219
2568 deg
Mean anomaly: 140
7743 deg
Mean motion: 15
78092395 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1704
Checksum: 295
Coasting Arc #2 (Orbit 1719)
---------------------------------------
Vector Time (GMT): 2006/320/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3955940
63 A = 6708706
47 meter
Y = -1410135
15 meter E =
0011371
Z = 5236931
95 I = 51
87826
XDOT = 3474
863862 Wp = 206
24167
YDOT = -6831
076687 meter/sec RA = 121
51976 deg
ZDOT = 776
148278 TA = 236
34579
MA = 236
45430
Ha = 184
962 n
mi
Hp = 178
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12978807
84 X = -3965318
93
Y = -4626427
66 feet Y = -1454425
23 meter
Z = 17181535
26 Z = 5217690
74
XDOT = 11400
471989 XDOT = 3547
221180
YDOT = -22411
668922 feet/sec YDOT = -6791
814279 meter/sec
ZDOT = 2546
418235 ZDOT = 793
205151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10782944
62 X = 3286641
52
Y = -8720784
21 feet Y = -2658095
03 meter
Z = 17109484
73 Z = 5214970
95
XDOT = 12506
184785 XDOT = 3811
885123
YDOT = 20642
991118 feet/sec YDOT = 6291
983693 meter/sec
ZDOT = 2609
218119 ZDOT = 795
289683
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 06320
55923823
00020000 00000-0 20000-3 0 9018
2 25544 51
6279 122
1197 0011621 222
2507 137
7764 15
78083048 17205
Satellite: ISS
Catalog Number: 25544
Epoch time: 06320
55923823 = yrday
fracday
Element set: 901
Inclination: 51
6279 deg
RA of node: 122
1197 deg
Eccentricity:
0011621
Arg of perigee: 222
2507 deg
Mean anomaly: 137
7764 deg
Mean motion: 15
78083048 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1720
Checksum: 275
Coasting Arc #3 (Orbit 1735)
---------------------------------------
Vector Time (GMT): 2006/321/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3459602
73 A = 6720115
59 meter
Y = 5716327
36 meter E =
0002237
Z = 715666
07 I = 51
93248
XDOT = -3751
914605 Wp = 90
60605
YDOT = -3024
854486 meter/sec RA = 116
37098 deg
ZDOT = 6007
600296 TA = 277
16841
MA = 277
19385
Ha = 184
605 n
mi
Hp = 178
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11350402
66 X = -3526743
04
Y = 18754354
84 feet Y = 5677264
73 meter
Z = 2347985
78 Z = 698695
97
XDOT = -12309
431118 XDOT = -3746
996023
YDOT = -9924
063273 feet/sec YDOT = -3066
783182 meter/sec
ZDOT = 19709
974724 ZDOT = 5989
384851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10371202
02 X = -3161142
38
Y = -19320606
46 feet Y = -5888920
85 meter
Z = 2285352
89 Z = 696575
56
XDOT = 13450
929283 XDOT = 4099
843245
YDOT = -4890
673881 feet/sec YDOT = -1490
677399 meter/sec
ZDOT = 19641
542304 ZDOT = 5986
742094
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 06321
57240229
00020000 00000-0 20000-3 0 9024
2 25544 51
6289 116
8830 0011748 225
7799 134
2402 15
78174320 17363
Satellite: ISS
Catalog Number: 25544
Epoch time: 06321
57240229 = yrday
fracday
Element set: 902
Inclination: 51
6289 deg
RA of node: 116
8830 deg
Eccentricity:
0011748
Arg of perigee: 225
7799 deg
Mean anomaly: 134
2402 deg
Mean motion: 15
78174320 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1736
Checksum: 289
Coasting Arc #4 (Orbit 1750)
---------------------------------------
Vector Time (GMT): 2006/322/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2598153
11 A = 6710020
69 meter
Y = 3835971
74 meter E =
0011432
Z = -4860160
25 I = 51
91060
XDOT = -4298
202870 Wp = 166
15179
YDOT = 5933
341965 meter/sec RA = 111
19780 deg
ZDOT = 2375
533980 TA = 126
97196
MA = 126
86724
Ha = 184
337 n
mi
Hp = 178
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8524124
37 X = 2578676
11
Y = 12585209
12 feet Y = 3864917
08 meter
Z = -15945407
65 Z = -4847585
16
XDOT = -14101
715453 XDOT = -4375
771131
YDOT = 19466
345028 feet/sec YDOT = 5884
843247 meter/sec
ZDOT = 7793
746652 ZDOT = 2354
464577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15196253
88 X = -4631818
18
Y = 1278125
44 feet Y = 389572
63 meter
Z = -15897939
28 Z = -4845691
89
XDOT = -9855
155237 XDOT = -3003
851316
YDOT = -20801
590381 feet/sec YDOT = -6340
324748 meter/sec
ZDOT = 7715
818883 ZDOT = 2351
781596
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 06322
52222339
00020000 00000-0 20000-3 0 9033
2 25544 51
6294 111
9743 0011632 229
7563 130
2586 15
78191461 17514
Satellite: ISS
Catalog Number: 25544
Epoch time: 06322
52222339 = yrday
fracday
Element set: 903
Inclination: 51
6294 deg
RA of node: 111
9743 deg
Eccentricity:
0011632
Arg of perigee: 229
7563 deg
Mean anomaly: 130
2586 deg
Mean motion: 15
78191461 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1751
Checksum: 279
Coasting Arc #5 (Orbit 1766)
---------------------------------------
Vector Time (GMT): 2006/323/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3928024
45 A = 6715495
80 meter
Y = -4335953
68 meter E =
0008621
Z = -3284903
61 I = 51
93881
XDOT = 2248
365549 Wp = 213
37080
YDOT = 5638
374972 meter/sec RA = 106
09388 deg
ZDOT = -4755
098851 TA = 5
07664
MA = 5
06790
Ha = 184
072 n
mi
Hp = 179
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12887219
32 X = 3992175
71
Y = -14225569
81 feet Y = -4291669
40 meter
Z = -10777242
83 Z = -3265665
17
XDOT = 7376
527393 XDOT = 2208
249475
YDOT = 18498
605550 feet/sec YDOT = 5663
293493 meter/sec
ZDOT = -15600
718014 ZDOT = -4744
272981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6295307
54 X = 1918809
74
Y = 18175485
47 feet Y = 5539887
97 meter
Z = -10705935
36 Z = -3263169
10
XDOT = -18488
885471 XDOT = -5635
412292
YDOT = -2758
877541 feet/sec YDOT = -840
905875 meter/sec
ZDOT = -15559
556553 ZDOT = -4742
552837
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 06323
53534040
00020000 00000-0 20000-3 0 9041
2 25544 51
6296 106
7372 0011568 234
2902 125
7187 15
78233724 17674
Satellite: ISS
Catalog Number: 25544
Epoch time: 06323
53534040 = yrday
fracday
Element set: 904
Inclination: 51
6296 deg
RA of node: 106
7372 deg
Eccentricity:
0011568
Arg of perigee: 234
2902 deg
Mean anomaly: 125
7187 deg
Mean motion: 15
78233724 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1767
Checksum: 287
Coasting Arc #6 (Orbit 1782)
---------------------------------------
Vector Time (GMT): 2006/324/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1368486
11 A = 6715882
13 meter
Y = -5784868
32 meter E =
0007920
Z = 3113792
47 I = 51
94737
XDOT = 4629
481016 Wp = 155
68797
YDOT = -3734
330452 meter/sec RA = 100
89663 deg
ZDOT = -4905
785371 TA = 348
20788
MA = 348
22641
Ha = 183
781 n
mi
Hp = 179
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4489783
83 X = -1318823
90
Y = -18979226
78 feet Y = -5799894
12 meter
Z = 10215854
55 Z = 3107264
22
XDOT = 15188
586009 XDOT = 4694
726891
YDOT = -12251
740328 feet/sec YDOT = -3682
195740 meter/sec
ZDOT = -16095
096360 ZDOT = -4883
136538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18925351
99 X = 5768447
29
Y = 4765798
97 feet Y = 1452615
53 meter
Z = 10190736
21 Z = 3106136
40
XDOT = 4125
379956 XDOT = 1257
415811
YDOT = 17835
232229 feet/sec YDOT = 5436
178783 meter/sec
ZDOT = -16010
960239 ZDOT = -4880
140681
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 06324
54843304
00020000 00000-0 20000-3 0 9050
2 25544 51
6300 101
5004 0011551 238
0299 121
9743 15
78253073 17831
Satellite: ISS
Catalog Number: 25544
Epoch time: 06324
54843304 = yrday
fracday
Element set: 905
Inclination: 51
6300 deg
RA of node: 101
5004 deg
Eccentricity:
0011551
Arg of perigee: 238
0299 deg
Mean anomaly: 121
9743 deg
Mean motion: 15
78253073 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1783
Checksum: 263
Coasting Arc #7 (Orbit 1798)
---------------------------------------
Vector Time (GMT): 2006/325/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4096016
06 A = 6709242
26 meter
Y = 1944015
30 meter E =
0010126
Z = 4952574
92 I = 51
93131
XDOT = -920
648189 Wp = 210
30914
YDOT = -7347
921882 meter/sec RA = 95
79135 deg
ZDOT = 2116
139621 TA = 219
22786
MA = 219
30129
Ha = 183
328 n
mi
Hp = 179
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13438372
91 X = -4141509
28
Y = 6378002
96 feet Y = 1897956
42 meter
Z = 16248605
39 Z = 4932565
64
XDOT = -3020
499309 XDOT = -848
694389
YDOT = -24107
355256 feet/sec YDOT = -7357
815021 meter/sec
ZDOT = 6942
715292 ZDOT = 2111
840883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 359510
24 X = 109578
72
Y = -14951769
19 feet Y = -4557299
25 meter
Z = 16174093
98 Z = 4929863
84
XDOT = 21832
345515 XDOT = 6654
498913
YDOT = 8040
737618 feet/sec YDOT = 2450
816826 meter/sec
ZDOT = 6925
739118 ZDOT = 2110
965283
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 06325
56149817
00020000 00000-0 20000-3 0 9062
2 25544 51
6315 96
2636 0011584 242
8785 117
1199 15
78341780 17999
Satellite: ISS
Catalog Number: 25544
Epoch time: 06325
56149817 = yrday
fracday
Element set: 906
Inclination: 51
6315 deg
RA of node: 96
2636 deg
Eccentricity:
0011584
Arg of perigee: 242
8785 deg
Mean anomaly: 117
1199 deg
Mean motion: 15
78341780 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1799
Checksum: 323
Coasting Arc #8 (Orbit 1813)
---------------------------------------
Vector Time (GMT): 2006/326/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 257308
44 A = 6719760
61 meter
Y = 6698694
15 meter E =
0004955
Z = -422156
91 I = 51
96937
XDOT = -4738
153866 Wp = 324
18265
YDOT = 565
239392 meter/sec RA = 90
62351 deg
ZDOT = 6049
658883 TA = 31
24080
MA = 31
21136
Ha = 182
950 n
mi
Hp = 179
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 844187
79 X = 184434
39
Y = 21977343
00 feet Y = 6701164
11 meter
Z = -1385029
24 Z = -421082
97
XDOT = -15545
124231 XDOT = -4773
511160
YDOT = 1854
459948 feet/sec YDOT = 512
056204 meter/sec
ZDOT = 19847
962216 ZDOT = 6026
554561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20182821
43 X = -6151723
97
Y = -8739757
20 feet Y = -2663877
99 meter
Z = -1380191
25 Z = -420682
29
XDOT = 4463
315085 XDOT = 1360
418438
YDOT = -13444
345629 feet/sec YDOT = -4097
836548 meter/sec
ZDOT = 19761
706893 ZDOT = 6023
368261
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 06326
51122618
00020000 00000-0 20000-3 0 9079
2 25544 51
6324 91
3545 0011388 246
8579 113
1387 15
78343792 18149
Satellite: ISS
Catalog Number: 25544
Epoch time: 06326
51122618 = yrday
fracday
Element set: 907
Inclination: 51
6324 deg
RA of node: 91
3545 deg
Eccentricity:
0011388
Arg of perigee: 246
8579 deg
Mean anomaly: 113
1387 deg
Mean motion: 15
78343792 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1814
Checksum: 300
Coasting Arc #9 (Orbit 1829)
---------------------------------------
Vector Time (GMT): 2006/327/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4148727
49 A = 6708010
84 meter
Y = 1000794
63 meter E =
0006904
Z = -5179295
74 I = 51
92965
XDOT = -336
447250 Wp = 149
80422
YDOT = 7604
380170 meter/sec RA = 85
47156 deg
ZDOT = 1194
733844 TA = 131
58476
MA = 131
52556
Ha = 182
568 n
mi
Hp = 179
509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13611310
67 X = 4162388
69
Y = 3283446
96 feet Y = 1047265
14 meter
Z = -16992440
10 Z = -5159107
50
XDOT = -1103
829560 XDOT = -427
259399
YDOT = 24948
753838 feet/sec YDOT = 7600
109900 meter/sec
ZDOT = 3919
730459 ZDOT = 1192
879874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8699997
67 X = -2651759
29
Y = 11086974
66 feet Y = 3379309
88 meter
Z = -16916880
80 Z = -5156265
27
XDOT = -21397
708328 XDOT = -6522
021498
YDOT = -10793
235838 feet/sec YDOT = -3289
778284 meter/sec
ZDOT = 3913
731101 ZDOT = 1192
905240
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 06327
52424378
00020000 00000-0 20000-3 0 9080
2 25544 51
6327 86
1187 0011309 251
0183 108
9757 15
78416605 18303
Satellite: ISS
Catalog Number: 25544
Epoch time: 06327
52424378 = yrday
fracday
Element set: 908
Inclination: 51
6327 deg
RA of node: 86
1187 deg
Eccentricity:
0011309
Arg of perigee: 251
0183 deg
Mean anomaly: 108
9757 deg
Mean motion: 15
78416605 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1830
Checksum: 295
Coasting Arc #10 (Orbit 1845)
---------------------------------------
Vector Time (GMT): 2006/328/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 878388
60 A = 6717026
36 meter
Y = -6192541
06 meter E =
0009581
Z = -2432593
11 I = 51
95716
XDOT = 4752
937371 Wp = 226
22267
YDOT = 2794
101830 meter/sec RA = 80
35509 deg
ZDOT = -5390
004526 TA = 341
18156
MA = 341
21695
Ha = 182
206 n
mi
Hp = 179
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2881852
36 X = 959386
44
Y = -20316735
77 feet Y = -6182265
20 meter
Z = -7980948
51 Z = -2428129
98
XDOT = 15593
626546 XDOT = 4747
524117
YDOT = 9167
000755 feet/sec YDOT = 2847
222321 meter/sec
ZDOT = -17683
741884 ZDOT = -5366
927175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17434248
72 X = 5313959
01
Y = 10834010
23 feet Y = 3302206
32 meter
Z = -7965020
94 Z = -2427738
38
XDOT = -13903
997576 XDOT = -4237
938461
YDOT = 9421
444233 feet/sec YDOT = 2871
656202 meter/sec
ZDOT = -17597
161475 ZDOT = -5363
614818
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 06328
53723630
00020000 00000-0 20000-3 0 9096
2 25544 51
6332 80
8815 0011335 255
2066 104
7844 15
78429156 18466
Satellite: ISS
Catalog Number: 25544
Epoch time: 06328
53723630 = yrday
fracday
Element set: 909
Inclination: 51
6332 deg
RA of node: 80
8815 deg
Eccentricity:
0011335
Arg of perigee: 255
2066 deg
Mean anomaly: 104
7844 deg
Mean motion: 15
78429156 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1846
Checksum: 294
Coasting Arc #11 (Orbit 1861)
---------------------------------------
Vector Time (GMT): 2006/329/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4082077
29 A = 6713229
83 meter
Y = -3709340
33 meter E =
0000630
Z = 3826125
33 I = 51
93852
XDOT = 1739
516403 Wp = 138
56651
YDOT = -6231
842187 meter/sec RA = 75
16041 deg
ZDOT = -4185
817971 TA = 355
05487
MA = 355
05549
Ha = 181
842 n
mi
Hp = 179
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13392642
02 X = -4058882
34
Y = -12169751
75 feet Y = -3754859
20 meter
Z = 12552904
64 Z = 3806350
26
XDOT = 5707
074814 XDOT = 1829
406589
YDOT = -20445
676465 feet/sec YDOT = -6211
886799 meter/sec
ZDOT = -13732
998591 ZDOT = -4177
149789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16419033
59 X = 5004521
44
Y = -7729313
43 feet Y = -2355894
73 meter
Z = 12478548
89 Z = 3803461
70
XDOT = 16071
866056 XDOT = 4898
704774
YDOT = 12021
053691 feet/sec YDOT = 3664
017165 meter/sec
ZDOT = -13701
356067 ZDOT = -4176
173329
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 06329
55020424
00020000 00000-0 20000-3 0 9102
2 25544 51
6333 75
6450 0011165 259
4123 100
5785 15
78446605 18629
Satellite: ISS
Catalog Number: 25544
Epoch time: 06329
55020424 = yrday
fracday
Element set: 910
Inclination: 51
6333 deg
RA of node: 75
6450 deg
Eccentricity:
0011165
Arg of perigee: 259
4123 deg
Mean anomaly: 100
5785 deg
Mean motion: 15
78446605 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1862
Checksum: 273
Coasting Arc #12 (Orbit 1877)
---------------------------------------
Vector Time (GMT): 2006/330/12:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2226282
32 A = 6710207
60 meter
Y = 4378411
57 meter E =
0005895
Z = 4576946
52 I = 51
92105
XDOT = -4507
473370 Wp = 215
65771
YDOT = -5462
460137 meter/sec RA = 70
05903 deg
ZDOT = 3030
276976 TA = 204
34506
MA = 204
37292
Ha = 181
176 n
mi
Hp = 179
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7304075
86 X = -2297311
00
Y = 14364867
36 feet Y = 4353118
40 meter
Z = 15016228
74 Z = 4565959
12
XDOT = -14788
298458 XDOT = -4460
777010
YDOT = -17921
457143 feet/sec YDOT = -5512
604446 meter/sec
ZDOT = 9941
853595 ZDOT = 3008
492342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10617300
91 X = -3236153
32
Y = -12173235
69 feet Y = -3710402
24 meter
Z = 14975690
91 Z = 4564590
59
XDOT = 21250
867091 XDOT = 6477
264289
YDOT = -6393
914464 feet/sec YDOT = -1948
865129 meter/sec
ZDOT = 9859
770093 ZDOT = 3005
257924
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 06330
56314425
00020000 00000-0 20000-3 0 9113
2 25544 51
6337 70
4068 0011245 264
0039 95
9845 15
78533788 18788
Satellite: ISS
Catalog Number: 25544
Epoch time: 06330
56314425 = yrday
fracday
Element set: 911
Inclination: 51
6337 deg
RA of node: 70
4068 deg
Eccentricity:
0011245
Arg of perigee: 264
0039 deg
Mean anomaly: 95
9845 deg
Mean motion: 15
78533788 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1878
Checksum: 303
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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