Date:
December 18th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 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 2184)
---------------------------------------
Vector Time (GMT): 2006/349/22:58:08
813
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6081654
99 A = 6726545
21 meter
Y = -2667098
00 meter E =
0030125
Z = 935492
32 I = 51
49091
XDOT = 1184
569293 Wp = 5
65042
YDOT = 4781
749009 meter/sec RA = 329
88442 deg
ZDOT = 5945
290549 TA = 4
61826
MA = 4
59053
Ha = 193
162 n
mi
Hp = 177
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19952936
33 X = 6106482
34
Y = -8750321
53 feet Y = -2598950
84 meter
Z = 3069200
51 Z = 965097
43
XDOT = 3886
382196 XDOT = 1102
129505
YDOT = 15688
152917 feet/sec YDOT = 4794
533919 meter/sec
ZDOT = 19505
546420 ZDOT = 5950
845550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -744781
76 X = -227009
48
Y = -21758749
22 feet Y = -6632066
76 meter
Z = 3179609
96 Z = 969145
11
XDOT = 14385
095087 XDOT = 4384
576982
YDOT = 2354
881212 feet/sec YDOT = 717
767794 meter/sec
ZDOT = 19526
864725 ZDOT = 5951
788368
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 06350
01860172
00020000 00000-0 20000-3 0 9008
2 25544 51
6320 330
0700 0023613 340
0756 19
9484 15
75844895 21859
Satellite: ISS
Catalog Number: 25544
Epoch time: 06350
01860172 = yrday
fracday
Element set: 900
Inclination: 51
6320 deg
RA of node: 330
0700 deg
Eccentricity:
0023613
Arg of perigee: 340
0756 deg
Mean anomaly: 19
9484 deg
Mean motion: 15
75844895 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2185
Checksum: 269
Coasting Arc #2 (Orbit 2199)
---------------------------------------
Vector Time (GMT): 2006/350/22:58:08
813
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -709394
21 A = 6715728
01 meter
Y = -4403545
78 meter E =
0020400
Z = -5020985
73 I = 51
43113
XDOT = 6825
870227 Wp = 18
30502
YDOT = -3099
334166 meter/sec RA = 324
69731 deg
ZDOT = 1774
821392 TA = 268
71529
MA = 268
94901
Ha = 193
228 n
mi
Hp = 176
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2327408
84 X = -635709
01
Y = -14447328
67 feet Y = -4411065
96 meter
Z = -16473050
31 Z = -5024253
62
XDOT = 22394
587360 XDOT = 6851
398211
YDOT = -10168
419181 feet/sec YDOT = -3022
860994 meter/sec
ZDOT = 5822
904828 ZDOT = 1808
043577
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14302250
52 X = -4359325
96
Y = -3027955
37 feet Y = -922920
80 meter
Z = -16485770
84 Z = -5024862
95
XDOT = -1806
142304 XDOT = -550
512174
YDOT = -23471
198698 feet/sec YDOT = -7154
021363 meter/sec
ZDOT = 5946
795787 ZDOT = 1812
583356
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 06350
96980736
00020000 00000-0 20000-3 0 9012
2 25544 51
6321 325
1705 0023377 343
9426 16
0995 15
75908673 22001
Satellite: ISS
Catalog Number: 25544
Epoch time: 06350
96980736 = yrday
fracday
Element set: 901
Inclination: 51
6321 deg
RA of node: 325
1705 deg
Eccentricity:
0023377
Arg of perigee: 343
9426 deg
Mean anomaly: 16
0995 deg
Mean motion: 15
75908673 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2200
Checksum: 295
Coasting Arc #3 (Orbit 2215)
---------------------------------------
Vector Time (GMT): 2006/351/22:58:08
813
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5793794
22 A = 6724388
47 meter
Y = 2657309
31 meter E =
0018488
Z = -2176455
20 I = 51
43902
XDOT = -406
432702 Wp = 357
30927
YDOT = -5383
672760 meter/sec RA = 319
56651 deg
ZDOT = -5471
108002 TA = 207
09952
MA = 207
19615
Ha = 193
385 n
mi
Hp = 176
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19008511
21 X = -5812505
04
Y = 8718206
39 feet Y = 2592415
60 meter
Z = -7140601
06 Z = -2204646
90
XDOT = -1333
440622 XDOT = -319
623485
YDOT = -17662
968372 feet/sec YDOT = -5387
731497 meter/sec
ZDOT = -17949
829403 ZDOT = -5472
872449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1789600
76 X = 545470
31
Y = 20799410
08 feet Y = 6339660
19 meter
Z = -7245734
89 Z = -2208499
99
XDOT = -15522
758706 XDOT = -4731
336853
YDOT = -4942
567929 feet/sec YDOT = -1506
494705 meter/sec
ZDOT = -17957
036532 ZDOT = -5473
304735
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 06351
98439422
00020000 00000-0 20000-3 0 9027
2 25544 51
6323 319
9440 0023496 348
0687 11
9918 15
75992191 22161
Satellite: ISS
Catalog Number: 25544
Epoch time: 06351
98439422 = yrday
fracday
Element set: 902
Inclination: 51
6323 deg
RA of node: 319
9440 deg
Eccentricity:
0023496
Arg of perigee: 348
0687 deg
Mean anomaly: 11
9918 deg
Mean motion: 15
75992191 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2216
Checksum: 310
Coasting Arc #4 (Orbit 2231)
---------------------------------------
Vector Time (GMT): 2006/352/22:58:08
813
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 37279
97 A = 6717928
32 meter
Y = 5042485
42 meter E =
0026796
Z = 4448672
79 I = 51
39566
XDOT = -6381
649844 Wp = 10
64680
YDOT = 2885
669716 meter/sec RA = 314
35520 deg
ZDOT = -3188
347484 TA = 111
51387
MA = 111
22800
Ha = 193
463 n
mi
Hp = 176
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 122309
62 X = -40719
66
Y = 16543587
35 feet Y = 5042465
42 meter
Z = 14595383
18 Z = 4448665
32
XDOT = -20937
171405 XDOT = -6397
954926
YDOT = 9467
420329 feet/sec YDOT = 2814
215954 meter/sec
ZDOT = -10460
457626 ZDOT = -3219
388988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15676030
22 X = 4778054
01
Y = 5286921
86 feet Y = 1611453
78 meter
Z = 14595923
61 Z = 4448837
52
XDOT = 2626
981559 XDOT = 800
703979
YDOT = 21672
178583 feet/sec YDOT = 6605
680032 meter/sec
ZDOT = -10576
231472 ZDOT = -3223
635353
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 06352
99894957
00020000 00000-0 20000-3 0 9038
2 25544 51
6319 314
7164 0023180 351
7786 8
2995 15
75987382 22321
Satellite: ISS
Catalog Number: 25544
Epoch time: 06352
99894957 = yrday
fracday
Element set: 903
Inclination: 51
6319 deg
RA of node: 314
7164 deg
Eccentricity:
0023180
Arg of perigee: 351
7786 deg
Mean anomaly: 8
2995 deg
Mean motion: 15
75987382 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2232
Checksum: 331
Coasting Arc #5 (Orbit 2247)
---------------------------------------
Vector Time (GMT): 2006/353/22:58:08
813
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5333371
82 A = 6721319
70 meter
Y = -2316322
59 meter E =
0025392
Z = 3338315
29 I = 51
39004
XDOT = -231
531396 Wp = 24
79012
YDOT = 6156
590972 meter/sec RA = 309
23538 deg
ZDOT = 4651
737297 TA = 14
79156
MA = 14
71741
Ha = 193
336 n
mi
Hp = 176
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17497939
05 X = 5342659
85
Y = -7599483
55 feet Y = -2256630
56 meter
Z = 10952477
98 Z = 3364247
10
XDOT = -759
617440 XDOT = -322
955489
YDOT = 20198
789278 feet/sec YDOT = 6153
489809 meter/sec
ZDOT = 15261
605305 ZDOT = 4650
391595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1906914
11 X = -581227
42
Y = -18925257
56 feet Y = -5768418
50 meter
Z = 11049212
65 Z = 3367800
02
XDOT = 17594
260912 XDOT = 5362
730726
YDOT = 7115
873644 feet/sec YDOT = 2168
918287 meter/sec
ZDOT = 15257
265876 ZDOT = 4650
414639
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 06354
01346985
00020000 00000-0 20000-3 0 9047
2 25544 51
6328 309
4895 0023058 355
6762 4
4199 15
76074277 22486
Satellite: ISS
Catalog Number: 25544
Epoch time: 06354
01346985 = yrday
fracday
Element set: 904
Inclination: 51
6328 deg
RA of node: 309
4895 deg
Eccentricity:
0023058
Arg of perigee: 355
6762 deg
Mean anomaly: 4
4199 deg
Mean motion: 15
76074277 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2248
Checksum: 315
Coasting Arc #6 (Orbit 2262)
---------------------------------------
Vector Time (GMT): 2006/354/22:58:08
813
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 379549
61 A = 6720602
83 meter
Y = -5668351
91 meter E =
0022838
Z = -3574356
67 I = 51
37192
XDOT = 5859
105327 Wp = 12
82572
YDOT = -2374
665899 meter/sec RA = 304
01399 deg
ZDOT = 4415
312842 TA = 304
19945
MA = 304
41570
Ha = 193
526 n
mi
Hp = 175
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1245241
50 X = 460269
29
Y = -18596955
08 feet Y = -5663655
57 meter
Z = -11726891
97 Z = -3572317
83
XDOT = 19222
786507 XDOT = 5863
774916
YDOT = -7790
898620 feet/sec YDOT = -2309
120865 meter/sec
ZDOT = 14485
934521 ZDOT = 4443
787285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17423368
67 X = -5310642
77
Y = -6632297
66 feet Y = -2021524
33 meter
Z = -11719906
65 Z = -3572227
55
XDOT = -2405
917649 XDOT = -733
323699
YDOT = -19306
858081 feet/sec YDOT = -5884
730343 meter/sec
ZDOT = 14592
181571 ZDOT = 4447
696943
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 06354
96455355
00020000 00000-0 20000-3 0 9054
2 25544 51
6339 304
5901 0023008 359
5172
5966 15
76106349 22637
Satellite: ISS
Catalog Number: 25544
Epoch time: 06354
96455355 = yrday
fracday
Element set: 905
Inclination: 51
6339 deg
RA of node: 304
5901 deg
Eccentricity:
0023008
Arg of perigee: 359
5172 deg
Mean anomaly:
5966 deg
Mean motion: 15
76106349 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2263
Checksum: 293
Coasting Arc #7 (Orbit 2278)
---------------------------------------
Vector Time (GMT): 2006/355/22:58:08
813
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4881435
37 A = 6717857
63 meter
Y = 1709767
89 meter E =
0027840
Z = -4310903
77 I = 51
34857
XDOT = 646
720541 Wp = 20
12777
YDOT = -6847
523558 meter/sec RA = 298
89307 deg
ZDOT = -3428
957268 TA = 214
93924
MA = 215
12226
Ha = 193
596 n
mi
Hp = 175
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16015207
90 X = -4879249
95
Y = 5609474
69 feet Y = 1655193
97 meter
Z = -14143385
08 Z = -4334612
04
XDOT = 2121
786553 XDOT = 739
899613
YDOT = -22465
628470 feet/sec YDOT = -6839
769952 meter/sec
ZDOT = -11249
859802 ZDOT = -3425
590438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1051324
61 X = 320443
74
Y = 16862283
27 feet Y = 5139623
94 meter
Z = -14231885
02 Z = -4337878
55
XDOT = -19789
028396 XDOT = -6031
695855
YDOT = -8303
976280 feet/sec YDOT = -2531
051970 meter/sec
ZDOT = -11238
045056 ZDOT = -3425
356133
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 06355
97900959
00020000 00000-0 20000-3 0 9062
2 25544 51
6340 299
3635 0022991 3
4046 356
7271 15
76167587 22792
Satellite: ISS
Catalog Number: 25544
Epoch time: 06355
97900959 = yrday
fracday
Element set: 906
Inclination: 51
6340 deg
RA of node: 299
3635 deg
Eccentricity:
0022991
Arg of perigee: 3
4046 deg
Mean anomaly: 356
7271 deg
Mean motion: 15
76167587 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2279
Checksum: 326
Coasting Arc #8 (Orbit 2294)
---------------------------------------
Vector Time (GMT): 2006/356/22:58:08
813
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -710917
53 A = 6723539
73 meter
Y = 6271625
97 meter E =
0024674
Z = 2335172
75 I = 51
35505
XDOT = -5315
571316 Wp = 40
90087
YDOT = 1418
106379 meter/sec RA = 293
67376 deg
ZDOT = -5376
405469 TA = 112
72285
MA = 112
46187
Ha = 193
646 n
mi
Hp = 175
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2332406
60 X = -792338
63
Y = 20576200
68 feet Y = 6263220
46 meter
Z = 7661327
92 Z = 2331522
41
XDOT = -17439
538438 XDOT = -5304
916369
YDOT = 4652
579984 feet/sec YDOT = 1358
725169 meter/sec
ZDOT = -17639
125554 ZDOT = -5402
202154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19281807
68 X = 5877094
98
Y = 7565055
60 feet Y = 2305828
95 meter
Z = 7648393
75 Z = 2331230
41
XDOT = 608
118590 XDOT = 185
354546
YDOT = 16548
679805 feet/sec YDOT = 5044
037605 meter/sec
ZDOT = -17735
478083 ZDOT = -5405
773720
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
99343244
00020000 00000-0 20000-3 0 9074
2 25544 51
6336 294
1355 0022852 7
2333 352
9156 15
76208244 22950
Satellite: ISS
Catalog Number: 25544
Epoch time: 06356
99343244 = yrday
fracday
Element set: 907
Inclination: 51
6336 deg
RA of node: 294
1355 deg
Eccentricity:
0022852
Arg of perigee: 7
2333 deg
Mean anomaly: 352
9156 deg
Mean motion: 15
76208244 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2295
Checksum: 296
Coasting Arc #9 (Orbit 2310)
---------------------------------------
Vector Time (GMT): 2006/357/22:58:08
813
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4438860
66 A = 6714684
58 meter
Y = -707961
22 meter E =
0021130
Z = 4975270
24 I = 51
31683
XDOT = -903
600138 Wp = 24
45995
YDOT = 7428
598176 meter/sec RA = 288
53560 deg
ZDOT = 1879
400998 TA = 47
44711
MA = 47
26893
Ha = 193
494 n
mi
Hp = 174
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14563191
13 X = 4422278
61
Y = -2322707
43 feet Y = -658416
83 meter
Z = 16323065
08 Z = 4996793
59
XDOT = -2964
567381 XDOT = -995
730290
YDOT = 24372
041260 feet/sec YDOT = 7417
978230 meter/sec
ZDOT = 6166
013772 ZDOT = 1874
788613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1209883
31 X = 368772
43
Y = -14607696
91 feet Y = -4452426
02 meter
Z = 16403515
86 Z = 4999791
64
XDOT = 21879
944147 XDOT = 6669
006976
YDOT = 8658
590778 feet/sec YDOT = 2639
138469 meter/sec
ZDOT = 6149
623816 ZDOT = 1874
405339
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
00782050
00020000 00000-0 20000-3 0 9081
2 25544 51
6346 288
9083 0022807 10
8534 349
3118 15
76301051 23110
Satellite: ISS
Catalog Number: 25544
Epoch time: 06358
00782050 = yrday
fracday
Element set: 908
Inclination: 51
6346 deg
RA of node: 288
9083 deg
Eccentricity:
0022807
Arg of perigee: 10
8534 deg
Mean anomaly: 349
3118 deg
Mean motion: 15
76301051 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2311
Checksum: 273
Coasting Arc #10 (Orbit 2325)
---------------------------------------
Vector Time (GMT): 2006/358/22:58:08
813
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 818232
48 A = 6725294
38 meter
Y = -6594669
24 meter E =
0032406
Z = -906461
01 I = 51
34501
XDOT = 4927
783232 Wp = 21
94913
YDOT = -191
564150 meter/sec RA = 283
33668 deg
ZDOT = 5939
397241 TA = 328
08436
MA = 328
28027
Ha = 193
720 n
mi
Hp = 174
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2684489
76 X = 896317
56
Y = -21636053
93 feet Y = -6585082
61 meter
Z = -2973953
46 Z = -902297
15
XDOT = 16167
267822 XDOT = 4900
706914
YDOT = -628
491307 feet/sec YDOT = -136
610992 meter/sec
ZDOT = 19486
211420 ZDOT = 5963
270342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20491258
52 X = -6245735
60
Y = -7451271
44 feet Y = -2271147
54 meter
Z = -2959153
96 Z = -901950
13
XDOT = 2420
031119 XDOT = 737
625485
YDOT = -14301
493301 feet/sec YDOT = -4359
095158 meter/sec
ZDOT = 19575
518928 ZDOT = 5966
618169
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
95878157
00020000 00000-0 20000-3 0 9090
2 25544 51
6349 284
0083 0022885 14
7693 345
4135 15
76299615 23269
Satellite: ISS
Catalog Number: 25544
Epoch time: 06358
95878157 = yrday
fracday
Element set: 909
Inclination: 51
6349 deg
RA of node: 284
0083 deg
Eccentricity:
0022885
Arg of perigee: 14
7693 deg
Mean anomaly: 345
4135 deg
Mean motion: 15
76299615 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2326
Checksum: 331
Coasting Arc #11 (Orbit 2341)
---------------------------------------
Vector Time (GMT): 2006/359/22:58:08
813
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4185025
88 A = 6713350
45 meter
Y = -446048
68 meter E =
0031262
Z = -5249851
98 I = 51
29992
XDOT = 994
262882 Wp = 45
50533
YDOT = -7622
396069 meter/sec RA = 278
17119 deg
ZDOT = -123
836467 TA = 223
18914
MA = 223
43474
Ha = 193
701 n
mi
Hp = 174
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13730399
88 X = -4154224
47
Y = -1463414
32 feet Y = -492675
29 meter
Z = -17223923
81 Z = -5270107
88
XDOT = 3262
017331 XDOT = 1080
025263
YDOT = -25007
861118 feet/sec YDOT = -7610
798136 meter/sec
ZDOT = -406
287623 ZDOT = -118
798738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4239200
77 X = -1292108
39
Y = 13041317
83 feet Y = 3974993
68 meter
Z = -17299775
14 Z = -5272971
46
XDOT = -22849
017713 XDOT = -6964
380599
YDOT = -8034
005155 feet/sec YDOT = -2448
764771 meter/sec
ZDOT = -388
350021 ZDOT = -118
369086
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
97310678
00020000 00000-0 20000-3 0 9104
2 25544 51
6346 278
7813 0022813 18
6294 341
5700 15
76377037 23426
Satellite: ISS
Catalog Number: 25544
Epoch time: 06359
97310678 = yrday
fracday
Element set: 910
Inclination: 51
6346 deg
RA of node: 278
7813 deg
Eccentricity:
0022813
Arg of perigee: 18
6294 deg
Mean anomaly: 341
5700 deg
Mean motion: 15
76377037 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2342
Checksum: 302
Coasting Arc #12 (Orbit 2357)
---------------------------------------
Vector Time (GMT): 2006/360/22:58:08
813
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -932469
28 A = 6725023
49 meter
Y = 6630061
69 meter E =
0020086
Z = -730289
48 I = 51
33700
XDOT = -4695
113491 Wp = 50
14663
YDOT = -1304
675160 meter/sec RA = 272
99916 deg
ZDOT = -5945
501563 TA = 137
83562
MA = 137
68095
Ha = 193
751 n
mi
Hp = 173
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3059282
41 X = -1002990
66
Y = 21752170
89 feet Y = 6619240
05 meter
Z = -2395962
85 Z = -734990
18
XDOT = -15403
915654 XDOT = -4651
293442
YDOT = -4280
430314 feet/sec YDOT = -1356
933066 meter/sec
ZDOT = -19506
238725 ZDOT = -5968
203983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20784274
82 X = 6335046
97
Y = 7102769
47 feet Y = 2164924
13 meter
Z = -2412751
78 Z = -735406
74
XDOT = -6576
460263 XDOT = -2004
505088
YDOT = 12695
102875 feet/sec YDOT = 3869
467356 meter/sec
ZDOT = -19591
351464 ZDOT = -5971
443926
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
98739943
00020000 00000-0 20000-3 0 9118
2 25544 51
6345 273
5522 0022736 22
5554 337
6604 15
76428489 23586
Satellite: ISS
Catalog Number: 25544
Epoch time: 06360
98739943 = yrday
fracday
Element set: 911
Inclination: 51
6345 deg
RA of node: 273
5522 deg
Eccentricity:
0022736
Arg of perigee: 22
5554 deg
Mean anomaly: 337
6604 deg
Mean motion: 15
76428489 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2358
Checksum: 316
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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