Date:
December 28th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 12 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 2287)
---------------------------------------
Vector Time (GMT): 2006/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4251107
34 A = 6714069
25 meter
Y = 679483
18 meter E =
0022252
Z = 5144480
28 I = 51
33031
XDOT = -2507
920086 Wp = 12
40776
YDOT = 7202
762837 meter/sec RA = 296
07740 deg
ZDOT = 1141
607419 TA = 66
77982
MA = 66
54564
Ha = 193
730 n
mi
Hp = 174
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13947202
56 X = 4218202
56
Y = 2229275
53 feet Y = 726836
55 meter
Z = 16878216
15 Z = 5165052
20
XDOT = -8228
084271 XDOT = -2593
821678
YDOT = 23631
111669 feet/sec YDOT = 7174
237383 meter/sec
ZDOT = 3745
431166 ZDOT = 1129
216639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2187005
25 X = -666599
20
Y = 13860176
77 feet Y = 4224581
88 meter
Z = 16955259
27 Z = 5167963
02
XDOT = -22645
392706 XDOT = -6902
315697
YDOT = -8017
261234 feet/sec YDOT = -2443
661224 meter/sec
ZDOT = 3699
899961 ZDOT = 1127
729508
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 06356
54948842
00020000 00000-0 20000-3 0 9003
2 25544 51
6349 296
4320 0023931 4
1908 355
9452 15
76259134 22882
Satellite: ISS
Catalog Number: 25544
Epoch time: 06356
54948842 = yrday
fracday
Element set: 900
Inclination: 51
6349 deg
RA of node: 296
4320 deg
Eccentricity:
0023931
Arg of perigee: 4
1908 deg
Mean anomaly: 355
9452 deg
Mean motion: 15
76259134 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2288
Checksum: 307
Coasting Arc #2 (Orbit 2302)
---------------------------------------
Vector Time (GMT): 2006/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2194354
48 A = 6725745
44 meter
Y = -6329795
86 meter E =
0034285
Z = -259021
08 I = 51
35776
XDOT = 4632
998214 Wp = 19
28063
YDOT = 1370
099812 meter/sec RA = 290
89130 deg
ZDOT = 6025
025560 TA = 337
88411
MA = 338
03167
Ha = 193
938 n
mi
Hp = 174
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7199325
71 X = 2266230
32
Y = -20767046
80 feet Y = -6304855
46 meter
Z = -849806
68 Z = -248187
40
XDOT = 15200
125375 XDOT = 4588
065082
YDOT = 4495
078124 feet/sec YDOT = 1421
656425 meter/sec
ZDOT = 19767
144226 ZDOT = 6047
423481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20908628
96 X = 6372950
11
Y = 6782021
73 feet Y = 2067160
22 meter
Z = -810006
86 Z = -246890
09
XDOT = -3693
993548 XDOT = -1125
929233
YDOT = 13653
565447 feet/sec YDOT = 4161
606748 meter/sec
ZDOT = 19851
106633 ZDOT = 6050
617302
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 06357
50047482
00020000 00000-0 20000-3 0 9011
2 25544 51
6344 291
5315 0023980 8
0444 352
1101 15
76258844 23034
Satellite: ISS
Catalog Number: 25544
Epoch time: 06357
50047482 = yrday
fracday
Element set: 901
Inclination: 51
6344 deg
RA of node: 291
5315 deg
Eccentricity:
0023980
Arg of perigee: 8
0444 deg
Mean anomaly: 352
1101 deg
Mean motion: 15
76258844 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2303
Checksum: 267
Coasting Arc #3 (Orbit 2318)
---------------------------------------
Vector Time (GMT): 2006/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3850783
79 A = 6713630
99 meter
Y = -1762556
23 meter E =
0029692
Z = -5224418
24 I = 51
30887
XDOT = 2533
887706 Wp = 41
55276
YDOT = -7237
925071 meter/sec RA = 285
71357 deg
ZDOT = 598
022300 TA = 234
02592
MA = 234
30163
Ha = 193
954 n
mi
Hp = 174
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12633805
09 X = -3805409
48
Y = -5782664
78 feet Y = -1805363
48 meter
Z = -17140479
77 Z = -5243015
12
XDOT = 8313
279874 XDOT = 2611
729831
YDOT = -23746
473329 feet/sec YDOT = -7209
154567 meter/sec
ZDOT = 1962
015420 ZDOT = 610
519956
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5309070
66 X = 1618204
74
Y = -12746315
54 feet Y = -3885076
98 meter
Z = -17210273
06 Z = -5245691
23
XDOT = 23111
194701 XDOT = 7044
292145
YDOT = 7020
251653 feet/sec YDOT = 2139
772704 meter/sec
ZDOT = 2007
926954 ZDOT = 612
016136
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 06358
51482846
00020000 00000-0 20000-3 0 9021
2 25544 51
6347 286
3040 0023901 11
8942 348
2781 15
76315592 23193
Satellite: ISS
Catalog Number: 25544
Epoch time: 06358
51482846 = yrday
fracday
Element set: 902
Inclination: 51
6347 deg
RA of node: 286
3040 deg
Eccentricity:
0023901
Arg of perigee: 11
8942 deg
Mean anomaly: 348
2781 deg
Mean motion: 15
76315592 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2319
Checksum: 296
Coasting Arc #4 (Orbit 2334)
---------------------------------------
Vector Time (GMT): 2006/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2241882
24 A = 6724632
37 meter
Y = 6211713
21 meter E =
0019831
Z = -1332615
31 I = 51
34037
XDOT = -4210
805877 Wp = 36
50194
YDOT = -2759
208839 meter/sec RA = 280
55505 deg
ZDOT = -5806
273817 TA = 158
17174
MA = 158
08713
Ha = 194
038 n
mi
Hp = 174
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7355256
70 X = -2304702
34
Y = 20379636
53 feet Y = 6186292
13 meter
Z = -4372097
49 Z = -1343658
25
XDOT = -13814
979911 XDOT = -4151
433533
YDOT = -9052
522439 feet/sec YDOT = -2805
963877 meter/sec
ZDOT = -19049
454779 ZDOT = -5826
585752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20749675
85 X = -6324501
20
Y = -6206757
55 feet Y = -1891819
70 meter
Z = -4412678
91 Z = -1344984
53
XDOT = 7837
447767 XDOT = 2388
854079
YDOT = -12670
095283 feet/sec YDOT = -3861
845042 meter/sec
ZDOT = -19125
790206 ZDOT = -5829
540855
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 06359
52915051
00020000 00000-0 20000-3 0 9033
2 25544 51
6349 281
0759 0023855 15
8580 344
3326 15
76372146 23352
Satellite: ISS
Catalog Number: 25544
Epoch time: 06359
52915051 = yrday
fracday
Element set: 903
Inclination: 51
6349 deg
RA of node: 281
0759 deg
Eccentricity:
0023855
Arg of perigee: 15
8580 deg
Mean anomaly: 344
3326 deg
Mean motion: 15
76372146 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2335
Checksum: 297
Coasting Arc #5 (Orbit 2350)
---------------------------------------
Vector Time (GMT): 2006/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3571549
88 A = 6715167
50 meter
Y = 3054239
93 meter E =
0029570
Z = 4794565
54 I = 51
30432
XDOT = -2579
893340 Wp = 28
19565
YDOT = 6849
993197 meter/sec RA = 275
34599 deg
ZDOT = -2409
980009 TA = 85
59464
MA = 85
25685
Ha = 194
001 n
mi
Hp = 173
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11717683
33 X = 3513840
52
Y = 10020472
20 feet Y = 3093855
93 meter
Z = 15730201
91 Z = 4811776
09
XDOT = -8464
216996 XDOT = -2644
592019
YDOT = 22473
730960 feet/sec YDOT = 6820
781839 meter/sec
ZDOT = -7906
758561 ZDOT = -2422
669652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9159569
20 X = -2791836
69
Y = 12319672
84 feet Y = 3755036
28 meter
Z = 15794972
97 Z = 4814307
76
XDOT = -22121
924169 XDOT = -6742
762487
YDOT = -6117
190666 feet/sec YDOT = -1864
519715 meter/sec
ZDOT = -7953
418756 ZDOT = -2424
202037
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 06360
54344123
00020000 00000-0 20000-3 0 9044
2 25544 51
6343 275
8478 0023822 19
6501 340
5576 15
76427218 23518
Satellite: ISS
Catalog Number: 25544
Epoch time: 06360
54344123 = yrday
fracday
Element set: 904
Inclination: 51
6343 deg
RA of node: 275
8478 deg
Eccentricity:
0023822
Arg of perigee: 19
6501 deg
Mean anomaly: 340
5576 deg
Mean motion: 15
76427218 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2351
Checksum: 284
Coasting Arc #6 (Orbit 2366)
---------------------------------------
Vector Time (GMT): 2006/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2269008
09 A = 6721735
79 meter
Y = -5643641
41 meter E =
0033121
Z = 2808789
72 I = 51
32561
XDOT = 4055
706862 Wp = 43
48748
YDOT = 4167
689404 meter/sec RA = 270
21105 deg
ZDOT = 5086
133881 TA = 348
99119
MA = 349
06349
Ha = 194
048 n
mi
Hp = 173
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7444252
25 X = 2318302
88
Y = -18515883
90 feet Y = -5617992
69 meter
Z = 9215189
38 Z = 2819931
85
XDOT = 13306
124875 XDOT = 3984
094273
YDOT = 13673
521666 feet/sec YDOT = 4212
641780 meter/sec
ZDOT = 16686
790949 ZDOT = 5105
662840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19100084
35 X = 5821705
71
Y = 5717000
27 feet Y = 1742541
68 meter
Z = 9256200
58 Z = 2821289
94
XDOT = -12027
178264 XDOT = -3665
883935
YDOT = 12984
336839 feet/sec YDOT = 3957
625869 meter/sec
ZDOT = 16760
377003 ZDOT = 5108
562910
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 06361
55770214
00020000 00000-0 20000-3 0 9051
2 25544 51
6346 270
6191 0023807 23
6365 336
5888 15
76451575 23673
Satellite: ISS
Catalog Number: 25544
Epoch time: 06361
55770214 = yrday
fracday
Element set: 905
Inclination: 51
6346 deg
RA of node: 270
6191 deg
Eccentricity:
0023807
Arg of perigee: 23
6365 deg
Mean anomaly: 336
5888 deg
Mean motion: 15
76451575 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2367
Checksum: 306
Coasting Arc #7 (Orbit 2381)
---------------------------------------
Vector Time (GMT): 2006/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3524630
76 A = 6718214
48 meter
Y = -4154369
85 meter E =
0025789
Z = -3931446
35 I = 51
31621
XDOT = 2679
578757 Wp = 42
49383
YDOT = -6018
144310 meter/sec RA = 264
98345 deg
ZDOT = 3991
027614 TA = 268
94765
MA = 269
24314
Ha = 194
026 n
mi
Hp = 173
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11563749
21 X = -3458815
75
Y = -13629822
33 feet Y = -4193415
89 meter
Z = -12898446
03 Z = -3948409
55
XDOT = 8791
268889 XDOT = 2727
287604
YDOT = -19744
567946 feet/sec YDOT = -5987
913366 meter/sec
ZDOT = 13093
922619 ZDOT = 4004
160400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12334054
82 X = 3759419
91
Y = -12872789
05 feet Y = -3923626
10 meter
Z = -12962432
51 Z = -3950949
43
XDOT = 19619
254567 XDOT = 5979
948792
YDOT = 5675
897517 feet/sec YDOT = 1730
013563 meter/sec
ZDOT = 13142
337254 ZDOT = 4005
784395
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 06362
50854272
00020000 00000-0 20000-3 0 9065
2 25544 51
6351 265
7174 0023727 27
1047 333
1351 15
76512496 23827
Satellite: ISS
Catalog Number: 25544
Epoch time: 06362
50854272 = yrday
fracday
Element set: 906
Inclination: 51
6351 deg
RA of node: 265
7174 deg
Eccentricity:
0023727
Arg of perigee: 27
1047 deg
Mean anomaly: 333
1351 deg
Mean motion: 15
76512496 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2382
Checksum: 284
Coasting Arc #8 (Orbit 2397)
---------------------------------------
Vector Time (GMT): 2006/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2481248
52 A = 6717567
46 meter
Y = 4741009
63 meter E =
0029964
Z = -4093637
80 I = 51
31872
XDOT = -4017
815161 Wp = 40
21898
YDOT = -5356
912167 meter/sec RA = 259
85648 deg
ZDOT = -3761
591487 TA = 190
89056
MA = 190
95558
Ha = 194
088 n
mi
Hp = 172
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8140579
14 X = -2514192
49
Y = 15554493
52 feet Y = 4713079
18 meter
Z = -13430570
21 Z = -4105771
27
XDOT = -13181
808272 XDOT = -3939
341577
YDOT = -17575
171150 feet/sec YDOT = -5401
402424 meter/sec
ZDOT = -12341
179419 ZDOT = -3780
920118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16429474
20 X = -5007703
74
Y = -6089122
19 feet Y = -1855964
44 meter
Z = -13475402
85 Z = -4107302
79
XDOT = 15382
465359 XDOT = 4688
575441
YDOT = -13979
626029 feet/sec YDOT = -4260
990014 meter/sec
ZDOT = -12414
167718 ZDOT = -3783
838321
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 06363
52274407
00020000 00000-0 20000-3 0 9075
2 25544 51
6356 260
4883 0023684 30
8502 329
4049 15
76568459 23989
Satellite: ISS
Catalog Number: 25544
Epoch time: 06363
52274407 = yrday
fracday
Element set: 907
Inclination: 51
6356 deg
RA of node: 260
4883 deg
Eccentricity:
0023684
Arg of perigee: 30
8502 deg
Mean anomaly: 329
4049 deg
Mean motion: 15
76568459 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2398
Checksum: 316
Coasting Arc #9 (Orbit 2413)
---------------------------------------
Vector Time (GMT): 2006/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3519393
85 A = 6721980
35 meter
Y = 5133232
07 meter E =
0031397
Z = 2541181
87 I = 51
33967
XDOT = -3057
800149 Wp = 59
09250
YDOT = 4728
020642 meter/sec RA = 254
63032 deg
ZDOT = -5251
879842 TA = 91
95498
MA = 91
59538
Ha = 194
116 n
mi
Hp = 172
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11546567
76 X = 3449387
09
Y = 16841312
56 feet Y = 5172196
11 meter
Z = 8337210
84 Z = 2558109
84
XDOT = -10032
152719 XDOT = -3084
929467
YDOT = 15511
878748 feet/sec YDOT = 4693
675665 meter/sec
ZDOT = -17230
576909 ZDOT = -5266
799954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15062630
30 X = -4591089
71
Y = 13747700
73 feet Y = 4190299
18 meter
Z = 8401191
20 Z = 2560683
08
XDOT = -15749
346755 XDOT = -4800
400891
YDOT = -6565
198398 feet/sec YDOT = -2001
072472 meter/sec
ZDOT = -17285
845143 ZDOT = -5268
725600
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 06364
53691700
00020000 00000-0 20000-3 0 9087
2 25544 51
6351 255
2590 0023618 34
9164 325
3544 15
76586311 24148
Satellite: ISS
Catalog Number: 25544
Epoch time: 06364
53691700 = yrday
fracday
Element set: 908
Inclination: 51
6351 deg
RA of node: 255
2590 deg
Eccentricity:
0023618
Arg of perigee: 34
9164 deg
Mean anomaly: 325
3544 deg
Mean motion: 15
76586311 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2414
Checksum: 287
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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