Date:
June 15th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4843 76 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 979)
---------------------------------------
Vector Time (GMT): 2007/162/00:43:42
491
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4386470
42 A = 6719697
62 meter
Y = 5047705
89 meter E =
0012624
Z = -566857
40 I = 51
87747
XDOT = -3940
648453 Wp = 2
77324
YDOT = -2749
094316 meter/sec RA = 134
80479 deg
ZDOT = 6031
595466 TA = 351
06334
MA = 351
08579
Ha = 182
876 n
mi
Hp = 179
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14391307
15 X = -4439834
86
Y = 16560714
86 feet Y = 4998355
62 meter
Z = -1859768
36 Z = -588296
07
XDOT = -12928
636658 XDOT = -3938
915585
YDOT = -9019
338307 feet/sec YDOT = -2793
152014 meter/sec
ZDOT = 19788
699037 ZDOT = 6012
455364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16352780
36 X = -4984327
45
Y = -14616709
79 feet Y = -4455173
14 meter
Z = -1940130
40 Z = -591351
75
XDOT = 8139
618072 XDOT = 2480
955588
YDOT = -11715
908950 feet/sec YDOT = -3571
009048 meter/sec
ZDOT = 19716
076603 ZDOT = 6009
460149
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 07162
03148993
00020000 00000-0 20000-3 0 9002
2 25544 51
6304 135
7187 0007837 303
0486 56
9926 15
78341521 9803
Satellite: ISS
Catalog Number: 25544
Epoch time: 07162
03148993 = yrday
fracday
Element set: 900
Inclination: 51
6304 deg
RA of node: 135
7187 deg
Eccentricity:
0007837
Arg of perigee: 303
0486 deg
Mean anomaly: 56
9926 deg
Mean motion: 15
78341521 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 980
Checksum: 297
Coasting Arc #2 (Orbit 995)
---------------------------------------
Vector Time (GMT): 2007/163/00:43:42
491
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2423132
55 A = 6707941
86 meter
Y = 3480445
71 meter E =
0008666
Z = -5203867
07 I = 51
85766
XDOT = -5464
147580 Wp = 71
64677
YDOT = 5331
324802 meter/sec RA = 129
65003 deg
ZDOT = 1025
417781 TA = 208
07503
MA = 208
12179
Ha = 183
035 n
mi
Hp = 179
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7949909
93 X = 2409313
43
Y = 11418785
12 feet Y = 3507466
15 meter
Z = -17073054
68 Z = -5192128
28
XDOT = -17926
993372 XDOT = -5528
338493
YDOT = 17491
223105 feet/sec YDOT = 5269
862556 meter/sec
ZDOT = 3364
231565 ZDOT = 998
717529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11395787
59 X = -3473436
06
Y = 8077866
90 feet Y = 2462133
83 meter
Z = -17028300
24 Z = -5190225
91
XDOT = -16953
422152 XDOT = -5167
403072
YDOT = -17064
424538 feet/sec YDOT = -5201
236599 meter/sec
ZDOT = 3264
014660 ZDOT = 994
871668
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 07163
04451563
00020000 00000-0 20000-3 0 9015
2 25544 51
6304 130
4826 0007807 307
1029 52
9423 15
78389643 9962
Satellite: ISS
Catalog Number: 25544
Epoch time: 07163
04451563 = yrday
fracday
Element set: 901
Inclination: 51
6304 deg
RA of node: 130
4826 deg
Eccentricity:
0007807
Arg of perigee: 307
1029 deg
Mean anomaly: 52
9423 deg
Mean motion: 15
78389643 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 996
Checksum: 289
Coasting Arc #3 (Orbit 1011)
---------------------------------------
Vector Time (GMT): 2007/164/00:43:42
491
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4913235
99 A = 6717416
51 meter
Y = -3962003
74 meter E =
0002066
Z = -2299155
08 I = 51
90732
XDOT = 1625
765046 Wp = 295
14860
YDOT = 5186
431191 meter/sec RA = 124
52585 deg
ZDOT = -5458
615041 TA = 270
63003
MA = 270
65370
Ha = 183
134 n
mi
Hp = 178
983
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16119540
66 X = 4968343
57
Y = -12998699
93 feet Y = -3906752
59 meter
Z = -7543159
73 Z = -2275153
19
XDOT = 5333
874822 XDOT = 1594
166116
YDOT = 17015
850365 feet/sec YDOT = 5204
435833 meter/sec
ZDOT = -17908
841999 ZDOT = -5450
792668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13320277
13 X = 4060020
47
Y = 15897443
75 feet Y = 4845540
85 meter
Z = -7452955
72 Z = -2271660
90
XDOT = -15744
213662 XDOT = -4798
836324
YDOT = 4802
859429 feet/sec YDOT = 1463
911554 meter/sec
ZDOT = -17878
683523 ZDOT = -5449
422738
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 07164
05752352
00020000 00000-0 20000-3 0 9028
2 25544 51
6306 125
2441 0007878 310
9019 49
1463 15
78404591 10120
Satellite: ISS
Catalog Number: 25544
Epoch time: 07164
05752352 = yrday
fracday
Element set: 902
Inclination: 51
6306 deg
RA of node: 125
2441 deg
Eccentricity:
0007878
Arg of perigee: 310
9019 deg
Mean anomaly: 49
1463 deg
Mean motion: 15
78404591 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1012
Checksum: 270
Coasting Arc #4 (Orbit 1027)
---------------------------------------
Vector Time (GMT): 2007/165/00:43:42
491
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -485257
36 A = 6712947
80 meter
Y = -5422673
11 meter E =
0009213
Z = 3928299
26 I = 51
90850
XDOT = 5576
842747 Wp = 35
88840
YDOT = -3442
663085 meter/sec RA = 119
32934 deg
ZDOT = -4051
331308 TA = 96
08428
MA = 95
97930
Ha = 183
277 n
mi
Hp = 178
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1592051
72 X = -443667
32
Y = -17790922
28 feet Y = -5427867
88 meter
Z = 12888120
94 Z = 3926041
64
XDOT = 18296
728173 XDOT = 5634
605448
YDOT = -11294
826393 feet/sec YDOT = -3379
975812 meter/sec
ZDOT = -13291
769382 ZDOT = -4024
099211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17716611
82 X = 5400023
28
Y = -2325759
97 feet Y = -708891
64 meter
Z = 12878963
92 Z = 3925508
20
XDOT = 11801
770629 XDOT = 3597
179688
YDOT = 16645
298211 feet/sec YDOT = 5073
486895 meter/sec
ZDOT = -13189
283874 ZDOT = -4020
093725
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 07165
07051453
00020000 00000-0 20000-3 0 9036
2 25544 51
6315 120
0072 0007796 314
5954 45
4574 15
78402622 10282
Satellite: ISS
Catalog Number: 25544
Epoch time: 07165
07051453 = yrday
fracday
Element set: 903
Inclination: 51
6315 deg
RA of node: 120
0072 deg
Eccentricity:
0007796
Arg of perigee: 314
5954 deg
Mean anomaly: 45
4574 deg
Mean motion: 15
78402622 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1028
Checksum: 270
Coasting Arc #5 (Orbit 1043)
---------------------------------------
Vector Time (GMT): 2007/166/00:43:42
491
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4657947
98 A = 6710742
87 meter
Y = 1788903
80 meter E =
0003915
Z = 4483571
27 I = 51
91609
XDOT = 396
062527 Wp = 51
20603
YDOT = -7000
908624 meter/sec RA = 114
22846 deg
ZDOT = 3205
308132 TA = 6
91404
MA = 6
90864
Ha = 183
451 n
mi
Hp = 178
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15281981
58 X = -4699386
03
Y = 5869106
94 feet Y = 1736583
24 meter
Z = 14709879
49 Z = 4460842
65
XDOT = 1299
417738 XDOT = 458
747417
YDOT = -22968
860315 feet/sec YDOT = -6996
129914 meter/sec
ZDOT = 10516
102794 ZDOT = 3207
382786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6696777
46 X = -2041177
77
Y = -15021710
54 feet Y = -4578617
37 meter
Z = 14624203
09 Z = 4457457
10
XDOT = 21906
965240 XDOT = 6677
243005
YDOT = 476
659659 feet/sec YDOT = 145
285864 meter/sec
ZDOT = 10523
140494 ZDOT = 3207
453223
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 07166
08348480
00020000 00000-0 20000-3 0 9048
2 25544 51
6328 114
7698 0007927 318
1673 41
8886 15
78487195 10446
Satellite: ISS
Catalog Number: 25544
Epoch time: 07166
08348480 = yrday
fracday
Element set: 904
Inclination: 51
6328 deg
RA of node: 114
7698 deg
Eccentricity:
0007927
Arg of perigee: 318
1673 deg
Mean anomaly: 41
8886 deg
Mean motion: 15
78487195 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1044
Checksum: 326
Coasting Arc #6 (Orbit 1058)
---------------------------------------
Vector Time (GMT): 2007/167/00:43:42
491
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1052932
62 A = 6718608
33 meter
Y = 6471661
84 meter E =
0013239
Z = -1426352
99 I = 51
95373
XDOT = -5004
874157 Wp = 1
50531
YDOT = 471
637740 meter/sec RA = 109
04297 deg
ZDOT = 5848
671031 TA = 342
83501
MA = 342
87975
Ha = 183
613 n
mi
Hp = 178
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3454503
33 X = -1118292
49
Y = 21232486
36 feet Y = 6459522
26 meter
Z = -4679635
81 Z = -1431625
33
XDOT = -16420
190803 XDOT = -5038
187792
YDOT = 1547
367912 feet/sec YDOT = 415
482765 meter/sec
ZDOT = 19188
553252 ZDOT = 5824
276621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21423483
87 X = -6529877
88
Y = -1899064
98 feet Y = -578835
01 meter
Z = -4698824
60 Z = -1432201
74
XDOT = -2865
303171 XDOT = -873
344407
YDOT = -14811
803731 feet/sec YDOT = -4514
637777 meter/sec
ZDOT = 19096
418909 ZDOT = 5820
588483
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 07167
03313101
00020000 00000-0 20000-3 0 9057
2 25544 51
6334 109
8605 0008034 322
8628 37
1980 15
78462884 10595
Satellite: ISS
Catalog Number: 25544
Epoch time: 07167
03313101 = yrday
fracday
Element set: 905
Inclination: 51
6334 deg
RA of node: 109
8605 deg
Eccentricity:
0008034
Arg of perigee: 322
8628 deg
Mean anomaly: 37
1980 deg
Mean motion: 15
78462884 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1059
Checksum: 284
Coasting Arc #7 (Orbit 1074)
---------------------------------------
Vector Time (GMT): 2007/168/00:43:42
491
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3998676
94 A = 6707247
92 meter
Y = 1077374
55 meter E =
0012504
Z = -5285099
67 I = 51
92443
XDOT = -1912
038206 Wp = 58
56640
YDOT = 7459
245628 meter/sec RA = 103
90815 deg
ZDOT = 80
457317 TA = 212
15590
MA = 212
23222
Ha = 183
701 n
mi
Hp = 177
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13119018
83 X = 4012006
22
Y = 3534693
40 feet Y = 1122165
72 meter
Z = -17339565
84 Z = -5265641
64
XDOT = -6273
091227 XDOT = -1995
697319
YDOT = 24472
590642 feet/sec YDOT = 7437
396365 meter/sec
ZDOT = 263
967577 ZDOT = 70
967190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2347834
38 X = -715619
92
Y = 13477372
39 feet Y = 4107903
10 meter
Z = -17265901
75 Z = -5262646
85
XDOT = -23950
110635 XDOT = -7299
993722
YDOT = -3906
454203 feet/sec YDOT = -1190
687241 meter/sec
ZDOT = 228
944635 ZDOT = 69
782325
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 07168
04606809
00020000 00000-0 20000-3 0 9060
2 25544 51
6338 104
6240 0008011 326
4759 33
5898 15
78520448 10754
Satellite: ISS
Catalog Number: 25544
Epoch time: 07168
04606809 = yrday
fracday
Element set: 906
Inclination: 51
6338 deg
RA of node: 104
6240 deg
Eccentricity:
0008011
Arg of perigee: 326
4759 deg
Mean anomaly: 33
5898 deg
Mean motion: 15
78520448 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1075
Checksum: 296
Coasting Arc #8 (Orbit 1090)
---------------------------------------
Vector Time (GMT): 2007/169/00:43:42
491
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2196637
83 A = 6718213
78 meter
Y = -6150776
35 meter E =
0001031
Z = -1575767
83 I = 51
96726
XDOT = 4127
441526 Wp = 67
84533
YDOT = 2957
133239 meter/sec RA = 98
77519 deg
ZDOT = -5791
645387 TA = 129
47801
MA = 129
46889
Ha = 183
733 n
mi
Hp = 177
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7206817
03 X = 2272908
16
Y = -20179712
44 feet Y = -6125785
55 meter
Z = -5169841
95 Z = -1564912
68
XDOT = 13541
474822 XDOT = 4122
202095
YDOT = 9701
880705 feet/sec YDOT = 3003
260488 meter/sec
ZDOT = -19001
461244 ZDOT = -5771
606636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20832345
39 X = 6349698
87
Y = 5058440
07 feet Y = 1541812
53 meter
Z = -5129506
95 Z = -1563473
72
XDOT = -7833
611754 XDOT = -2387
684863
YDOT = 13078
922997 feet/sec YDOT = 3986
455730 meter/sec
ZDOT = -18925
381843 ZDOT = -5768
456386
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 07169
05898723
00020000 00000-0 20000-3 0 9071
2 25544 51
6337 99
3866 0007948 330
1251 29
9459 15
78541266 10915
Satellite: ISS
Catalog Number: 25544
Epoch time: 07169
05898723 = yrday
fracday
Element set: 907
Inclination: 51
6337 deg
RA of node: 99
3866 deg
Eccentricity:
0007948
Arg of perigee: 330
1251 deg
Mean anomaly: 29
9459 deg
Mean motion: 15
78541266 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1091
Checksum: 328
Coasting Arc #9 (Orbit 1106)
---------------------------------------
Vector Time (GMT): 2007/170/00:43:42
491
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3187369
15 A = 6710875
51 meter
Y = -3962224
73 meter E =
0011830
Z = 4380545
57 I = 51
94615
XDOT = 3047
615210 Wp = 27
55262
YDOT = -6213
572600 meter/sec RA = 93
58814 deg
ZDOT = -3388
822401 TA = 96
46602
MA = 96
33131
Ha = 183
912 n
mi
Hp = 177
418
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10457247
86 X = -3164105
70
Y = -12999424
97 feet Y = -3997738
39 meter
Z = 14371868
67 Z = 4365117
32
XDOT = 9998
737567 XDOT = 3133
331858
YDOT = -20385
736878 feet/sec YDOT = -6179
012586 meter/sec
ZDOT = -11118
183730 ZDOT = -3373
810179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11605093
95 X = 3537232
64
Y = -12055982
04 feet Y = -3674663
33 meter
Z = 14313098
30 Z = 4362632
36
XDOT = 20588
971064 XDOT = 6275
518380
YDOT = 6631
477065 feet/sec YDOT = 2021
274209 meter/sec
ZDOT = -11062
138203 ZDOT = -3371
739724
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
07188796
00020000 00000-0 20000-3 0 9088
2 25544 51
6340 94
1490 0008024 334
8242 25
2532 15
78574070 11070
Satellite: ISS
Catalog Number: 25544
Epoch time: 07170
07188796 = yrday
fracday
Element set: 908
Inclination: 51
6340 deg
RA of node: 94
1490 deg
Eccentricity:
0008024
Arg of perigee: 334
8242 deg
Mean anomaly: 25
2532 deg
Mean motion: 15
78574070 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1107
Checksum: 280
Coasting Arc #10 (Orbit 1122)
---------------------------------------
Vector Time (GMT): 2007/171/00:43:42
491
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3081744
81 A = 6711832
09 meter
Y = 4336904
23 meter E =
0008798
Z = 4082146
24 I = 51
95019
XDOT = -3171
700039 Wp = 56
01032
YDOT = -5881
193132 meter/sec RA = 88
48888 deg
ZDOT = 3852
761252 TA = 354
61561
MA = 354
62506
Ha = 184
016 n
mi
Hp = 177
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10110711
31 X = -3149841
76
Y = 14228688
42 feet Y = 4302061
04 meter
Z = 13392868
24 Z = 4067010
56
XDOT = -10405
840023 XDOT = -3124
415750
YDOT = -19295
253058 feet/sec YDOT = -5916
397083 meter/sec
ZDOT = 12640
292822 ZDOT = 3837
467242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15514611
58 X = -4728853
61
Y = -8092908
48 feet Y = -2466718
51 meter
Z = 13336140
25 Z = 4064855
55
XDOT = 17048
213453 XDOT = 5196
295460
YDOT = -11943
506485 feet/sec YDOT = -3640
380777 meter/sec
ZDOT = 12581
809924 ZDOT = 3834
935665
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
08476906
00020000 00000-0 20000-3 0 9094
2 25544 51
6338 88
9109 0008007 337
8011 22
2807 15
78618088 11231
Satellite: ISS
Catalog Number: 25544
Epoch time: 07171
08476906 = yrday
fracday
Element set: 909
Inclination: 51
6338 deg
RA of node: 88
9109 deg
Eccentricity:
0008007
Arg of perigee: 337
8011 deg
Mean anomaly: 22
2807 deg
Mean motion: 15
78618088 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1123
Checksum: 297
Coasting Arc #11 (Orbit 1137)
---------------------------------------
Vector Time (GMT): 2007/172/00:43:42
491
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2305149
62 A = 6717355
79 meter
Y = 5963061
81 meter E =
0013035
Z = -2036934
42 I = 51
96617
XDOT = -4009
206236 Wp = 7
24501
YDOT = 3459
334644 meter/sec RA = 83
29697 deg
ZDOT = 5606
467825 TA = 330
08496
MA = 330
15939
Ha = 184
212 n
mi
Hp = 176
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7562826
84 X = 2248193
44
Y = 19563851
08 feet Y = 5988521
11 meter
Z = -6682855
72 Z = -2025873
61
XDOT = -13153
563768 XDOT = -4074
826020
YDOT = 11349
523110 feet/sec YDOT = 3414
133768 meter/sec
ZDOT = 18393
923312 ZDOT = 5586
832361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18127747
08 X = -5525337
31
Y = 10577877
46 feet Y = 3224137
05 meter
Z = -6640366
97 Z = -2023983
85
XDOT = -12518
905245 XDOT = -3815
762319
YDOT = -9987
747033 feet/sec YDOT = -3044
265296 meter/sec
ZDOT = 18320
081561 ZDOT = 5583
960860
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
03433020
00020000 00000-0 20000-3 0 9102
2 25544 51
6335 84
0012 0008245 341
3502 18
7360 15
78588153 11386
Satellite: ISS
Catalog Number: 25544
Epoch time: 07172
03433020 = yrday
fracday
Element set: 910
Inclination: 51
6335 deg
RA of node: 84
0012 deg
Eccentricity:
0008245
Arg of perigee: 341
3502 deg
Mean anomaly: 18
7360 deg
Mean motion: 15
78588153 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1138
Checksum: 250
Coasting Arc #12 (Orbit 1153)
---------------------------------------
Vector Time (GMT): 2007/173/00:43:42
491
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3895273
15 A = 6707058
61 meter
Y = -1503778
01 meter E =
0015640
Z = -5260441
19 I = 51
92634
XDOT = 2032
562879 Wp = 54
42590
YDOT = 7400
958024 meter/sec RA = 78
17141 deg
ZDOT = -602
942411 TA = 209
81984
MA = 209
90906
Ha = 184
228 n
mi
Hp = 176
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12779767
55 X = 3937353
26
Y = -4933654
90 feet Y = -1459982
91 meter
Z = -17258665
31 Z = -5241416
02
XDOT = 6668
513384 XDOT = 1952
582189
YDOT = 24281
358345 feet/sec YDOT = 7423
240168 meter/sec
ZDOT = -1978
157517 ZDOT = -593
261565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7098685
34 X = 2163679
29
Y = 11821328
36 feet Y = 3603140
89 meter
Z = -17186907
80 Z = -5238569
50
XDOT = -21886
802419 XDOT = -6671
097377
YDOT = 10284
715503 feet/sec YDOT = 3134
781285 meter/sec
ZDOT = -1940
726718 ZDOT = -591
533504
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
04717709
00020000 00000-0 20000-3 0 9114
2 25544 51
6328 78
7631 0008159 344
9926 15
0996 15
78629464 11542
Satellite: ISS
Catalog Number: 25544
Epoch time: 07173
04717709 = yrday
fracday
Element set: 911
Inclination: 51
6328 deg
RA of node: 78
7631 deg
Eccentricity:
0008159
Arg of perigee: 344
9926 deg
Mean anomaly: 15
0996 deg
Mean motion: 15
78629464 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1154
Checksum: 318
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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