Date:
June 20th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4574 66 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
There are no maneuvers
Coasting Arc #1 (Orbit 1110)
---------------------------------------
Vector Time (GMT): 2007/170/07:33:18
296
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3665789
27 A = 6710420
58 meter
Y = 2904382
44 meter E =
0009062
Z = -4817625
45 I = 51
93852
XDOT = -2220
406482 Wp = 65
03771
YDOT = 6938
676043 meter/sec RA = 92
15216 deg
ZDOT = 2500
935072 TA = 229
27732
MA = 229
35605
Ha = 184
764 n
mi
Hp = 177
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12026867
68 X = 3656442
45
Y = 9528813
76 feet Y = 2945323
91 meter
Z = -15805857
76 Z = -4799839
47
XDOT = -7284
798170 XDOT = -2309
979684
YDOT = 22764
685179 feet/sec YDOT = 6913
344953 meter/sec
ZDOT = 8205
167558 ZDOT = 2489
932092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14621790
52 X = 4456721
75
Y = 4876304
17 feet Y = 1486297
51 meter
Z = -15738293
34 Z = -4797031
81
XDOT = 1145
727395 XDOT = 349
217710
YDOT = 22836
541674 feet/sec YDOT = 6960
577902 meter/sec
ZDOT = 8164
359121 ZDOT = 2488
496660
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 07170
32634916
00020000 00000-0 20000-3 0 9008
2 25544 51
6316 92
8575 0008058 337
6468 22
4345 15
78120571 11119
Satellite: ISS
Catalog Number: 25544
Epoch time: 07170
32634916 = yrday
fracday
Element set: 900
Inclination: 51
6316 deg
RA of node: 92
8575 deg
Eccentricity:
0008058
Arg of perigee: 337
6468 deg
Mean anomaly: 22
4345 deg
Mean motion: 15
78120571 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1111
Checksum: 279
Coasting Arc #2 (Orbit 1126)
---------------------------------------
Vector Time (GMT): 2007/171/07:33:18
296
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2369057
62 A = 6715422
86 meter
Y = -5308274
28 meter E =
0007930
Z = -3372345
11 I = 51
95530
XDOT = 3903
280085 Wp = 16
92907
YDOT = 4712
806951 meter/sec RA = 87
05112 deg
ZDOT = -4671
515771 TA = 202
65406
MA = 202
68908
Ha = 184
772 n
mi
Hp = 177
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7772498
75 X = 2444621
51
Y = -17415598
04 feet Y = -5281359
14 meter
Z = -11064124
37 Z = -3360653
61
XDOT = 12806
037023 XDOT = 3872
983819
YDOT = 15461
965061 feet/sec YDOT = 4756
286927 meter/sec
ZDOT = -15326
495313 ZDOT = -4652
626718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1163146
67 X = 354527
11
Y = -19061079
17 feet Y = -5809816
93 meter
Z = -11020525
87 Z = -3359056
29
XDOT = 16139
730644 XDOT = 4919
389900
YDOT = 9813
520205 feet/sec YDOT = 2991
160959 meter/sec
ZDOT = -15254
553384 ZDOT = -4649
587872
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 07171
33950300
00020000 00000-0 20000-3 0 9019
2 25544 51
6313 87
6208 0008067 341
9186 18
1692 15
78166543 11279
Satellite: ISS
Catalog Number: 25544
Epoch time: 07171
33950300 = yrday
fracday
Element set: 901
Inclination: 51
6313 deg
RA of node: 87
6208 deg
Eccentricity:
0008067
Arg of perigee: 341
9186 deg
Mean anomaly: 18
1692 deg
Mean motion: 15
78166543 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1127
Checksum: 280
Coasting Arc #3 (Orbit 1142)
---------------------------------------
Vector Time (GMT): 2007/172/07:33:18
296
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3129510
68 A = 6716258
19 meter
Y = -5108904
74 meter E =
0012777
Z = 3033921
22 I = 51
95543
XDOT = 3219
211633 Wp = 59
25094
YDOT = -4933
620400 meter/sec RA = 81
85545 deg
ZDOT = -4965
494343 TA = 85
74356
MA = 85
59756
Ha = 184
874 n
mi
Hp = 177
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10267423
48 X = -3086887
69
Y = -16761498
48 feet Y = -5143662
78 meter
Z = 9953809
76 Z = 3018821
00
XDOT = 10561
717956 XDOT = 3298
262128
YDOT = -16186
418634 feet/sec YDOT = -4897
178697 meter/sec
ZDOT = -16290
991940 ZDOT = -4949
664191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15791774
86 X = -4813332
98
Y = -11752968
72 feet Y = -3582304
87 meter
Z = 9896146
62 Z = 3016345
49
XDOT = 3051
263492 XDOT = 930
025113
YDOT = -17827
472904 feet/sec YDOT = -5433
813741 meter/sec
ZDOT = -16231
701662 ZDOT = -4947
422666
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 07172
35264009
00020000 00000-0 20000-3 0 9027
2 25544 51
6311 82
3845 0008255 344
7707 15
3208 15
78208583 11436
Satellite: ISS
Catalog Number: 25544
Epoch time: 07172
35264009 = yrday
fracday
Element set: 902
Inclination: 51
6311 deg
RA of node: 82
3845 deg
Eccentricity:
0008255
Arg of perigee: 344
7707 deg
Mean anomaly: 15
3208 deg
Mean motion: 15
78208583 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1143
Checksum: 275
Coasting Arc #4 (Orbit 1158)
---------------------------------------
Vector Time (GMT): 2007/173/07:33:18
296
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3270837
25 A = 6709423
12 meter
Y = 3094595
43 meter E =
0005702
Z = 4969895
80 I = 51
92757
XDOT = -3226
620148 Wp = 34
40856
YDOT = -6697
052644 meter/sec RA = 76
75031 deg
ZDOT = 2049
980707 TA = 35
87429
MA = 35
83601
Ha = 185
037 n
mi
Hp = 177
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10731093
33 X = -3329341
13
Y = 10152872
15 feet Y = 3057691
33 meter
Z = 16305432
40 Z = 4953864
43
XDOT = -10586
024109 XDOT = -3161
451314
YDOT = -21971
957492 feet/sec YDOT = -6732
770413 meter/sec
ZDOT = 6725
658488 ZDOT = 2034
463259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6065929
02 X = -1848895
16
Y = 13542644
74 feet Y = 4127798
12 meter
Z = 16245171
02 Z = 4951528
13
XDOT = -17292
020722 XDOT = -5270
607916
YDOT = -15728
132059 feet/sec YDOT = -4793
934652 meter/sec
ZDOT = 6666
242031 ZDOT = 2031
870571
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 07173
36576222
00020000 00000-0 20000-3 0 9033
2 25544 51
6314 77
1483 0008244 348
0182 12
0786 15
78232244 11594
Satellite: ISS
Catalog Number: 25544
Epoch time: 07173
36576222 = yrday
fracday
Element set: 903
Inclination: 51
6314 deg
RA of node: 77
1483 deg
Eccentricity:
0008244
Arg of perigee: 348
0182 deg
Mean anomaly: 12
0786 deg
Mean motion: 15
78232244 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1159
Checksum: 279
Coasting Arc #5 (Orbit 1173)
---------------------------------------
Vector Time (GMT): 2007/174/07:33:18
296
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2415151
35 A = 6720034
97 meter
Y = 6246249
16 meter E =
0017866
Z = -406466
89 I = 51
95565
XDOT = -4311
767054 Wp = 21
50351
YDOT = 2054
891658 meter/sec RA = 71
58302 deg
ZDOT = 6057
421462 TA = 334
08450
MA = 334
17386
Ha = 185
050 n
mi
Hp = 176
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7923724
90 X = 2347099
92
Y = 20492943
44 feet Y = 6272876
30 meter
Z = -1333552
78 Z = -394898
53
XDOT = -14146
217370 XDOT = -4363
850557
YDOT = 6741
770530 feet/sec YDOT = 2006
383027 meter/sec
ZDOT = 19873
429993 ZDOT = 6036
348655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15495236
20 X = 4722947
99
Y = 15580767
94 feet Y = 4749018
07 meter
Z = -1289122
04 Z = -392924
40
XDOT = -9211
885794 XDOT = -2807
782790
YDOT = 10771
159287 feet/sec YDOT = 3283
049351 meter/sec
ZDOT = 19793
989248 ZDOT = 6033
207923
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 07174
31555036
00020000 00000-0 20000-3 0 9040
2 25544 51
6314 72
2392 0008161 352
5099 7
5943 15
78253487 11747
Satellite: ISS
Catalog Number: 25544
Epoch time: 07174
31555036 = yrday
fracday
Element set: 904
Inclination: 51
6314 deg
RA of node: 72
2392 deg
Eccentricity:
0008161
Arg of perigee: 352
5099 deg
Mean anomaly: 7
5943 deg
Mean motion: 15
78253487 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1174
Checksum: 289
Coasting Arc #6 (Orbit 1189)
---------------------------------------
Vector Time (GMT): 2007/175/07:33:18
296
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4244330
39 A = 6708458
75 meter
Y = -439748
97 meter E =
0014816
Z = -5186959
78 I = 51
90708
XDOT = 2177
964042 Wp = 65
82441
YDOT = 7290
792915 meter/sec RA = 66
42929 deg
ZDOT = 1172
592208 TA = 215
28497
MA = 215
38313
Ha = 185
206 n
mi
Hp = 176
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13924968
47 X = 4274129
68
Y = -1442745
97 feet Y = -392119
11 meter
Z = -17017584
59 Z = -5166268
43
XDOT = 7145
551319 XDOT = 2090
579195
YDOT = 23919
924261 feet/sec YDOT = 7314
659367 meter/sec
ZDOT = 3847
087296 ZDOT = 1182
961605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12138065
51 X = 3699682
37
Y = -7162987
00 feet Y = -2183278
44 meter
Z = -16939404
69 Z = -5163130
55
XDOT = 15935
572303 XDOT = 4857
162438
YDOT = 17877
863395 feet/sec YDOT = 5449
172763 meter/sec
ZDOT = 3887
093420 ZDOT = 1184
786074
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 07175
32864229
00020000 00000-0 20000-3 0 9050
2 25544 51
6323 67
0025 0008315 355
6008 4
5083 15
78255763 11906
Satellite: ISS
Catalog Number: 25544
Epoch time: 07175
32864229 = yrday
fracday
Element set: 905
Inclination: 51
6323 deg
RA of node: 67
0025 deg
Eccentricity:
0008315
Arg of perigee: 355
6008 deg
Mean anomaly: 4
5083 deg
Mean motion: 15
78255763 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1190
Checksum: 278
Coasting Arc #7 (Orbit 1205)
---------------------------------------
Vector Time (GMT): 2007/176/07:33:18
296
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1234494
18 A = 6717457
24 meter
Y = -6158947
74 meter E =
0006019
Z = -2391751
93 I = 51
92605
XDOT = 5385
339720 Wp = 40
26288
YDOT = 1018
883402 meter/sec RA = 61
31168 deg
ZDOT = -5406
345254 TA = 166
61086
MA = 166
59488
Ha = 185
227 n
mi
Hp = 176
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4050177
77 X = -1153913
41
Y = -20206521
47 feet Y = -6172301
61 meter
Z = -7846955
16 Z = -2397554
42
XDOT = 17668
437400 XDOT = 5399
809362
YDOT = 3342
793313 feet/sec YDOT = 1079
187079 meter/sec
ZDOT = -17737
353194 ZDOT = -5380
147803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12360086
40 X = -3767354
33
Y = -16479696
66 feet Y = -5023011
54 meter
Z = -7869562
73 Z = -2398642
72
XDOT = 16261
317313 XDOT = 4956
449517
YDOT = -3778
230001 feet/sec YDOT = -1151
604504 meter/sec
ZDOT = -17638
194820 ZDOT = -5376
121781
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 07176
34171854
00020000 00000-0 20000-3 0 9069
2 25544 51
6331 61
7660 0008404 359
2045
9105 15
78298542 12066
Satellite: ISS
Catalog Number: 25544
Epoch time: 07176
34171854 = yrday
fracday
Element set: 906
Inclination: 51
6331 deg
RA of node: 61
7660 deg
Eccentricity:
0008404
Arg of perigee: 359
2045 deg
Mean anomaly:
9105 deg
Mean motion: 15
78298542 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1206
Checksum: 277
Coasting Arc #8 (Orbit 1221)
---------------------------------------
Vector Time (GMT): 2007/177/07:33:18
296
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5064894
27 A = 6713412
28 meter
Y = -2082096
05 meter E =
0015420
Z = 3881720
16 I = 51
89786
XDOT = -489
054331 Wp = 48
34356
YDOT = -6503
367998 meter/sec RA = 56
11568 deg
ZDOT = -4105
982205 TA = 84
35863
MA = 84
18280
Ha = 185
344 n
mi
Hp = 176
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16617107
20 X = -5060092
35
Y = -6831023
78 feet Y = -2138708
40 meter
Z = 12735302
36 Z = 3857126
02
XDOT = -1604
508959 XDOT = -396
350124
YDOT = -21336
509181 feet/sec YDOT = -6508
317793 meter/sec
ZDOT = -13471
070226 ZDOT = -4108
134054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17979415
00 X = -5480125
69
Y = 1377409
56 feet Y = 419834
43 meter
Z = 12642090
13 Z = 3853309
07
XDOT = -10833
882109 XDOT = -3302
167267
YDOT = -17074
336990 feet/sec YDOT = -5204
257914 meter/sec
ZDOT = -13479
903975 ZDOT = -4108
674732
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 07177
35477946
00020000 00000-0 20000-3 0 9073
2 25544 51
6335 56
5299 0008430 2
5448 357
5758 15
78325301 12221
Satellite: ISS
Catalog Number: 25544
Epoch time: 07177
35477946 = yrday
fracday
Element set: 907
Inclination: 51
6335 deg
RA of node: 56
5299 deg
Eccentricity:
0008430
Arg of perigee: 2
5448 deg
Mean anomaly: 357
5758 deg
Mean motion: 15
78325301 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1222
Checksum: 306
Coasting Arc #9 (Orbit 1237)
---------------------------------------
Vector Time (GMT): 2007/178/07:33:18
296
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -526617
62 A = 6710950
19 meter
Y = 4950620
81 meter E =
0010178
Z = 4489922
22 I = 51
87349
XDOT = -6074
219733 Wp = 61
63459
YDOT = -3533
742199 meter/sec RA = 51
01435 deg
ZDOT = 3183
222860 TA = 356
72570
MA = 356
73236
Ha = 185
326 n
mi
Hp = 176
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1727748
09 X = -603748
39
Y = 16242194
27 feet Y = 4944299
71 meter
Z = 14730715
94 Z = 4487177
55
XDOT = -19928
542432 XDOT = -6049
717060
YDOT = -11593
642386 feet/sec YDOT = -3601
531175 meter/sec
ZDOT = 10443
644554 ZDOT = 3153
772941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5928090
86 X = 1806882
09
Y = 15229639
67 feet Y = 4641994
17 meter
Z = 14720862
55 Z = 4486918
91
XDOT = -21973
491713 XDOT = -6697
520274
YDOT = -1435
766173 feet/sec YDOT = -437
621529 meter/sec
ZDOT = 10331
916819 ZDOT = 3149
168246
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 07178
36782416
00020000 00000-0 20000-3 0 9087
2 25544 51
6340 51
2937 0008310 5
8380 354
2880 15
78368973 12385
Satellite: ISS
Catalog Number: 25544
Epoch time: 07178
36782416 = yrday
fracday
Element set: 908
Inclination: 51
6340 deg
RA of node: 51
2937 deg
Eccentricity:
0008310
Arg of perigee: 5
8380 deg
Mean anomaly: 354
2880 deg
Mean motion: 15
78368973 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1238
Checksum: 304
Coasting Arc #10 (Orbit 1252)
---------------------------------------
Vector Time (GMT): 2007/179/07:33:18
296
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5311084
37 A = 6718954
71 meter
Y = 3837698
27 meter E =
0016624
Z = -1446398
70 I = 51
88066
XDOT = -1817
764664 Wp = 23
05547
YDOT = 4701
483709 meter/sec RA = 45
82527 deg
ZDOT = 5836
975845 TA = 321
04307
MA = 321
16272
Ha = 185
529 n
mi
Hp = 175
953
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17424817
50 X = 5274802
30
Y = 12590873
60 feet Y = 3896887
25 meter
Z = -4745402
55 Z = -1420684
67
XDOT = -5963
794829 XDOT = -1898
557278
YDOT = 15424
815319 feet/sec YDOT = 4680
703436 meter/sec
ZDOT = 19150
183219 ZDOT = 5827
949902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21349549
94 X = 6507342
82
Y = 2695957
06 feet Y = 821727
71 meter
Z = -4647767
31 Z = -1416639
48
XDOT = 2253
961755 XDOT = 687
007543
YDOT = 14891
454918 feet/sec YDOT = 4538
915459 meter/sec
ZDOT = 19116
545818 ZDOT = 5826
723165
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 07179
31754178
00020000 00000-0 20000-3 0 9098
2 25544 51
6337 46
3844 0008508 9
3794 350
7529 15
78347059 12530
Satellite: ISS
Catalog Number: 25544
Epoch time: 07179
31754178 = yrday
fracday
Element set: 909
Inclination: 51
6337 deg
RA of node: 46
3844 deg
Eccentricity:
0008508
Arg of perigee: 9
3794 deg
Mean anomaly: 350
7529 deg
Mean motion: 15
78347059 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1253
Checksum: 320
Coasting Arc #11 (Orbit 1268)
---------------------------------------
Vector Time (GMT): 2007/180/07:33:18
296
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2716613
41 A = 6707640
05 meter
Y = -3141291
82 meter E =
0018882
Z = -5281797
35 I = 51
82243
XDOT = 5827
473404 Wp = 64
00788
YDOT = 5026
336657 meter/sec RA = 40
68455 deg
ZDOT = 16
059253 TA = 206
09655
MA = 206
19184
Ha = 185
519 n
mi
Hp = 175
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8912773
65 X = 2777195
85
Y = -10306075
53 feet Y = -3110573
19 meter
Z = -17328731
47 Z = -5268453
63
XDOT = 19119
007232 XDOT = 5770
757048
YDOT = 16490
605829 feet/sec YDOT = 5091
185613 meter/sec
ZDOT = 52
687839 ZDOT = 44
232455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2743523
45 X = 836225
95
Y = -13411219
29 feet Y = -4087739
64 meter
Z = -17278597
67 Z = -5266516
57
XDOT = 23790
701856 XDOT = 7251
405926
YDOT = 4695
558295 feet/sec YDOT = 1431
206168 meter/sec
ZDOT = 159
749369 ZDOT = 48
691608
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 07180
33055799
00020000 00000-0 20000-3 0 9107
2 25544 51
6344 41
1473 0008495 13
1828 346
9558 15
78383693 12695
Satellite: ISS
Catalog Number: 25544
Epoch time: 07180
33055799 = yrday
fracday
Element set: 910
Inclination: 51
6344 deg
RA of node: 41
1473 deg
Eccentricity:
0008495
Arg of perigee: 13
1828 deg
Mean anomaly: 346
9558 deg
Mean motion: 15
78383693 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1269
Checksum: 314
Coasting Arc #12 (Orbit 1284)
---------------------------------------
Vector Time (GMT): 2007/181/07:33:18
296
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4568219
76 A = 6718661
85 meter
Y = -4700208
68 meter E =
0007625
Z = -1487368
64 I = 51
83765
XDOT = 4413
664493 Wp = 78
19894
YDOT = -2458
452755 meter/sec RA = 35
54329 deg
ZDOT = -5810
365406 TA = 118
14823
MA = 118
07117
Ha = 185
562 n
mi
Hp = 175
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14987597
65 X = -4508096
51
Y = -15420632
16 feet Y = -4750956
57 meter
Z = -4879818
36 Z = -1509415
94
XDOT = 14480
526551 XDOT = 4469
052741
YDOT = -8065
789877 feet/sec YDOT = -2408
785658 meter/sec
ZDOT = -19062
878627 ZDOT = -5788
789995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20724936
35 X = -6316960
60
Y = -5663520
12 feet Y = -1726240
93 meter
Z = -4963684
10 Z = -1512930
91
XDOT = 8040
771865 XDOT = 2450
827264
YDOT = -12854
334803 feet/sec YDOT = -3918
001248 meter/sec
ZDOT = -18981
538216 ZDOT = -5785
572848
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 07181
34355893
00020000 00000-0 20000-3 0 9118
2 25544 51
6348 35
9103 0008505 16
8788 343
2659 15
78406122 12850
Satellite: ISS
Catalog Number: 25544
Epoch time: 07181
34355893 = yrday
fracday
Element set: 911
Inclination: 51
6348 deg
RA of node: 35
9103 deg
Eccentricity:
0008505
Arg of perigee: 16
8788 deg
Mean anomaly: 343
2659 deg
Mean motion: 15
78406122 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1285
Checksum: 300
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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