Date:
May 25th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6673 62 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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
143/23:31:13
309 0
3 1
6 1
6
N/A -1
0 -0
0 183
9
000/00:02:26
618 1
1 0
0 179
7
Coasting Arc #1 (Orbit 655)
---------------------------------------
Vector Time (GMT): 2007/141/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -81639
60 A = 6715348
98 meter
Y = -5790901
78 meter E =
0011237
Z = 3400971
54 I = 51
35649
XDOT = 5616
096258 Wp = 137
22525
YDOT = 2618
518334 meter/sec RA = 241
18942 deg
ZDOT = 4576
441023 TA = 263
19102
MA = 263
31888
Ha = 184
725 n
mi
Hp = 178
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -267846
46 X = -33400
10
Y = -18999021
60 feet Y = -5791545
51 meter
Z = 11158043
09 Z = 3400691
24
XDOT = 18425
512657 XDOT = 5564
166719
YDOT = 8590
939416 feet/sec YDOT = 2681
029634 meter/sec
ZDOT = 15014
570287 ZDOT = 4603
598234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13192875
69 X = -4021188
51
Y = -13675594
20 feet Y = -4168321
11 meter
Z = 11156282
70 Z = 3400434
97
XDOT = 18278
446804 XDOT = 5571
270586
YDOT = -5255
442152 feet/sec YDOT = -1601
858768 meter/sec
ZDOT = 15117
271332 ZDOT = 4607
744302
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 07141
51457342
00020000 00000-0 20000-3 0 9003
2 25544 51
6335 241
7308 0009483 211
1829 148
8774 15
78151108 6561
Satellite: ISS
Catalog Number: 25544
Epoch time: 07141
51457342 = yrday
fracday
Element set: 900
Inclination: 51
6335 deg
RA of node: 241
7308 deg
Eccentricity:
0009483
Arg of perigee: 211
1829 deg
Mean anomaly: 148
8774 deg
Mean motion: 15
78151108 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 656
Checksum: 286
Coasting Arc #2 (Orbit 670)
---------------------------------------
Vector Time (GMT): 2007/142/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5066028
23 A = 6716556
20 meter
Y = -3277480
83 meter E =
0006049
Z = -2956934
58 I = 51
37548
XDOT = 859
783549 Wp = 191
78477
YDOT = -5819
170724 meter/sec RA = 235
95230 deg
ZDOT = 4969
329702 TA = 133
93260
MA = 133
88266
Ha = 184
472 n
mi
Hp = 178
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16620827
53 X = -5014638
23
Y = -10752889
86 feet Y = -3333844
28 meter
Z = -9701228
95 Z = -2981420
88
XDOT = 2820
812168 XDOT = 900
650423
YDOT = -19091
767466 feet/sec YDOT = -5809
328279 meter/sec
ZDOT = 16303
575139 ZDOT = 4973
605042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19388991
82 X = -5909764
71
Y = 3759770
71 feet Y = 1145978
11 meter
Z = -9793952
81 Z = -2985196
82
XDOT = -11013
855088 XDOT = -3357
023031
YDOT = -14223
605398 feet/sec YDOT = -4335
354925 meter/sec
ZDOT = 16318
980611 ZDOT = 4974
025290
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 07142
46441838
00020000 00000-0 20000-3 0 9012
2 25544 51
6334 236
8227 0009273 216
1053 143
9487 15
78129911 6717
Satellite: ISS
Catalog Number: 25544
Epoch time: 07142
46441838 = yrday
fracday
Element set: 901
Inclination: 51
6334 deg
RA of node: 236
8227 deg
Eccentricity:
0009273
Arg of perigee: 216
1053 deg
Mean anomaly: 143
9487 deg
Mean motion: 15
78129911 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 671
Checksum: 291
Coasting Arc #3 (Orbit 686)
---------------------------------------
Vector Time (GMT): 2007/143/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1696048
56 A = 6709516
65 meter
Y = 4192942
58 meter E =
0007652
Z = -4960378
56 I = 51
36939
XDOT = -5815
420780 Wp = 120
16817
YDOT = -4658
854128 meter/sec RA = 230
80651 deg
ZDOT = -1955
696780 TA = 130
90135
MA = 130
83505
Ha = 184
186 n
mi
Hp = 178
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5564463
79 X = -1718712
02
Y = 13756373
28 feet Y = 4173850
23 meter
Z = -16274207
89 Z = -4968672
55
XDOT = -19079
464501 XDOT = -5753
392176
YDOT = -15284
954488 feet/sec YDOT = -4723
538392 meter/sec
ZDOT = -6416
328018 ZDOT = -1983
797886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5844224
30 X = 1781319
57
Y = 13603093
50 feet Y = 4146222
90 meter
Z = -16304962
28 Z = -4969752
50
XDOT = -23284
262490 XDOT = -7097
043207
YDOT = 2208
726920 feet/sec YDOT = 673
219965 meter/sec
ZDOT = -6522
863281 ZDOT = -1988
168728
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 07143
47756140
00020000 00000-0 20000-3 0 9020
2 25544 51
6335 231
5869 0009300 219
9390 140
1092 15
78178512 6877
Satellite: ISS
Catalog Number: 25544
Epoch time: 07143
47756140 = yrday
fracday
Element set: 902
Inclination: 51
6335 deg
RA of node: 231
5869 deg
Eccentricity:
0009300
Arg of perigee: 219
9390 deg
Mean anomaly: 140
1092 deg
Mean motion: 15
78178512 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 687
Checksum: 289
Coasting Arc #4 (Orbit 694)
---------------------------------------
Vector Time (GMT): 2007/143/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5239515
56 A = 6719834
77 meter
Y = -3872202
61 meter E =
0002019
Z = -1641984
28 I = 51
41096
XDOT = 1784
872316 Wp = 299
96698
YDOT = -4841
949031 meter/sec RA = 228
06782 deg
ZDOT = 5718
797690 TA = 41
81355
MA = 41
79813
Ha = 183
900 n
mi
Hp = 179
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17190011
67 X = -5187850
15
Y = -12704076
80 feet Y = -3930504
77 meter
Z = -5387087
53 Z = -1667312
73
XDOT = 5855
880303 XDOT = 1811
102170
YDOT = -15885
659549 feet/sec YDOT = -4821
843501 meter/sec
ZDOT = 18762
459612 ZDOT = 5727
531824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20411300
67 X = 6221364
44
Y = -6263023
59 feet Y = -1908969
59 meter
Z = -5483075
85 Z = -1671241
52
XDOT = 8910
099627 XDOT = 2715
798366
YDOT = 12571
959141 feet/sec YDOT = 3831
933146 meter/sec
ZDOT = 18794
791922 ZDOT = 5728
652578
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 07143
98412456
00020000 00000-0 20000-3 0 9036
2 25544 51
6328 228
9716 0008328 231
3887 128
6533 15
77914445 6950
Satellite: ISS
Catalog Number: 25544
Epoch time: 07143
98412456 = yrday
fracday
Element set: 903
Inclination: 51
6328 deg
RA of node: 228
9716 deg
Eccentricity:
0008328
Arg of perigee: 231
3887 deg
Mean anomaly: 128
6533 deg
Mean motion: 15
77914445 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 695
Checksum: 318
Coasting Arc #5 (Orbit 710)
---------------------------------------
Vector Time (GMT): 2007/144/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2525477
40 A = 6708873
44 meter
Y = 3359876
10 meter E =
0009027
Z = -5235774
10 I = 51
39530
XDOT = -5844
046214 Wp = 115
16811
YDOT = -5001
143267 meter/sec RA = 222
90419 deg
ZDOT = -394
745134 TA = 151
09647
MA = 151
04644
Ha = 183
539 n
mi
Hp = 179
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8285687
01 X = -2537425
81
Y = 11023215
55 feet Y = 3331568
46 meter
Z = -17177736
55 Z = -5248071
63
XDOT = -19173
379966 XDOT = -5785
770753
YDOT = -16407
950351 feet/sec YDOT = -5066
168799 meter/sec
ZDOT = -1295
095583 ZDOT = -422
994492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4231723
80 X = -1289829
41
Y = -13064285
04 feet Y = -3981994
08 meter
Z = -17223689
89 Z = -5249780
68
XDOT = 23528
806000 XDOT = 7171
580069
YDOT = -5791
253685 feet/sec YDOT = -1765
174123 meter/sec
ZDOT = -1402
247842 ZDOT = -427
405142
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 07144
99742203
00020000 00000-0 20000-3 0 9045
2 25544 51
6336 223
7364 0008227 235
5355 124
5033 15
77967511 7116
Satellite: ISS
Catalog Number: 25544
Epoch time: 07144
99742203 = yrday
fracday
Element set: 904
Inclination: 51
6336 deg
RA of node: 223
7364 deg
Eccentricity:
0008227
Arg of perigee: 235
5355 deg
Mean anomaly: 124
5033 deg
Mean motion: 15
77967511 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 711
Checksum: 283
Coasting Arc #6 (Orbit 726)
---------------------------------------
Vector Time (GMT): 2007/145/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4735936
73 A = 6720547
08 meter
Y = 4654200
15 meter E =
0012136
Z = -982895
64 I = 51
45686
XDOT = -4029
097416 Wp = 184
96992
YDOT = 2850
099840 meter/sec RA = 217
72885 deg
ZDOT = -5924
308856 TA = 5
82044
MA = 5
80635
Ha = 183
471 n
mi
Hp = 180
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15537850
15 X = 4688315
56
Y = 15269685
54 feet Y = 4706893
88 meter
Z = -3224723
23 Z = -960003
56
XDOT = -13218
823542 XDOT = -4031
888772
YDOT = 9350
721261 feet/sec YDOT = 2805
029128 meter/sec
ZDOT = -19436
708844 ZDOT = -5943
888881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21391783
42 X = -6520215
59
Y = 4187203
57 feet Y = 1276259
65 meter
Z = -3137810
06 Z = -956404
51
XDOT = 12
456084 XDOT = 3
796614
YDOT = -14540
571703 feet/sec YDOT = -4431
966255 meter/sec
ZDOT = -19510
190493 ZDOT = -5946
706062
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 07146
01069727
00020000 00000-0 20000-3 0 9054
2 25544 51
6338 218
5013 0008347 239
3554 120
6789 15
77956373 7273
Satellite: ISS
Catalog Number: 25544
Epoch time: 07146
01069727 = yrday
fracday
Element set: 905
Inclination: 51
6338 deg
RA of node: 218
5013 deg
Eccentricity:
0008347
Arg of perigee: 239
3554 deg
Mean anomaly: 120
6789 deg
Mean motion: 15
77956373 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 727
Checksum: 309
Coasting Arc #7 (Orbit 742)
---------------------------------------
Vector Time (GMT): 2007/146/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4460553
85 A = 6710732
14 meter
Y = -1636146
43 meter E =
0001104
Z = 4740243
08 I = 51
44834
XDOT = 4759
787425 Wp = 278
09924
YDOT = 5480
236318 meter/sec RA = 212
51942 deg
ZDOT = -2587
740745 TA = 197
32760
MA = 197
33137
Ha = 182
943 n
mi
Hp = 180
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14634363
03 X = 4455490
46
Y = -5367934
47 feet Y = -1586294
77 meter
Z = 15551978
60 Z = 4761900
24
XDOT = 15616
100477 XDOT = 4710
723784
YDOT = 17979
777945 feet/sec YDOT = 5533
188847 meter/sec
ZDOT = -8489
963075 ZDOT = -2564
736089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3545180
88 X = -1080571
13
Y = 15095372
54 feet Y = 4601069
55 meter
Z = 15633450
05 Z = 4765075
58
XDOT = -22535
886599 XDOT = -6868
938236
YDOT = 3408
211550 feet/sec YDOT = 1038
822880 meter/sec
ZDOT = -8402
516861 ZDOT = -2561
087139
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 07147
02394785
00020000 00000-0 20000-3 0 9062
2 25544 51
6337 213
2661 0008253 245
1544 114
8763 15
78056733 7430
Satellite: ISS
Catalog Number: 25544
Epoch time: 07147
02394785 = yrday
fracday
Element set: 906
Inclination: 51
6337 deg
RA of node: 213
2661 deg
Eccentricity:
0008253
Arg of perigee: 245
1544 deg
Mean anomaly: 114
8763 deg
Mean motion: 15
78056733 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 743
Checksum: 294
Coasting Arc #8 (Orbit 758)
---------------------------------------
Vector Time (GMT): 2007/147/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3311983
41 A = 6715727
92 meter
Y = -4755662
94 meter E =
0005785
Z = 3392155
83 I = 51
49010
XDOT = 6104
005507 Wp = 120
62409
YDOT = -962
112240 meter/sec RA = 207
38633 deg
ZDOT = 4602
198711 TA = 279
58396
MA = 279
64932
Ha = 182
827 n
mi
Hp = 180
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10866087
31 X = -3275037
46
Y = -15602568
69 feet Y = -4792493
19 meter
Z = 11129120
18 Z = 3376155
20
XDOT = 20026
264786 XDOT = 6091
953341
YDOT = -3156
536222 feet/sec YDOT = -893
921719 meter/sec
ZDOT = 15099
077136 ZDOT = 4631
823034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19030556
01 X = 5800513
47
Y = -838278
76 feet Y = -255507
37 meter
Z = 11068177
18 Z = 3373580
41
XDOT = -8108
714548 XDOT = -2471
536194
YDOT = 17128
978160 feet/sec YDOT = 5220
912543 meter/sec
ZDOT = 15210
687170 ZDOT = 4636
217450
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 07148
03717883
00020000 00000-0 20000-3 0 9073
2 25544 51
6340 208
0302 0008141 249
1367 110
8927 15
78044205 7597
Satellite: ISS
Catalog Number: 25544
Epoch time: 07148
03717883 = yrday
fracday
Element set: 907
Inclination: 51
6340 deg
RA of node: 208
0302 deg
Eccentricity:
0008141
Arg of perigee: 249
1367 deg
Mean anomaly: 110
8927 deg
Mean motion: 15
78044205 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 759
Checksum: 282
Coasting Arc #9 (Orbit 773)
---------------------------------------
Vector Time (GMT): 2007/148/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6006530
64 A = 6716539
27 meter
Y = 129303
04 meter E =
0003758
Z = -3000847
65 I = 51
51965
XDOT = -2590
747328 Wp = 255
33298
YDOT = -5304
420756 meter/sec RA = 202
15918 deg
ZDOT = 4951
025744 TA = 69
86026
MA = 69
81984
Ha = 182
523 n
mi
Hp = 180
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19706465
35 X = -5992952
28
Y = 424222
57 feet Y = 62210
95 meter
Z = -9845300
68 Z = -3029994
88
XDOT = -8499
827190 XDOT = -2555
291572
YDOT = -17402
955235 feet/sec YDOT = -5333
194337 meter/sec
ZDOT = 16243
522781 ZDOT = 4938
525117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9905839
09 X = 3019299
75
Y = -16977118
66 feet Y = -5174625
77 meter
Z = -9955223
79 Z = -3034352
21
XDOT = 18089
029612 XDOT = 5513
536226
YDOT = 1046
033285 feet/sec YDOT = 318
830945 meter/sec
ZDOT = 16195
711030 ZDOT = 4936
452722
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 07148
98706061
00020000 00000-0 20000-3 0 9084
2 25544 51
6338 203
1218 0008275 253
5859 106
4397 15
78089276 7745
Satellite: ISS
Catalog Number: 25544
Epoch time: 07148
98706061 = yrday
fracday
Element set: 908
Inclination: 51
6338 deg
RA of node: 203
1218 deg
Eccentricity:
0008275
Arg of perigee: 253
5859 deg
Mean anomaly: 106
4397 deg
Mean motion: 15
78089276 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 774
Checksum: 321
Coasting Arc #10 (Orbit 789)
---------------------------------------
Vector Time (GMT): 2007/149/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1020307
52 A = 6709753
52 meter
Y = 4423049
53 meter E =
0004566
Z = -4945453
49 I = 51
52353
XDOT = -7406
929345 Wp = 68
92634
YDOT = -572
448191 meter/sec RA = 197
02519 deg
ZDOT = -2040
010108 TA = 181
30321
MA = 181
30440
Ha = 182
210 n
mi
Hp = 180
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3347465
61 X = 994797
05
Y = 14511317
35 feet Y = 4434317
28 meter
Z = -16225241
10 Z = -4940558
05
XDOT = -24300
949293 XDOT = -7390
067465
YDOT = -1878
110863 feet/sec YDOT = -655
182043 meter/sec
ZDOT = -6692
946547 ZDOT = -2075
952755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14247300
90 X = -4342577
32
Y = -4406239
63 feet Y = -1343021
84 meter
Z = -16206226
43 Z = -4939657
82
XDOT = 13616
269369 XDOT = 4150
238904
YDOT = -18910
334217 feet/sec YDOT = -5763
869869 meter/sec
ZDOT = -6828
600098 ZDOT = -2081
357310
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 07150
00024707
00020000 00000-0 20000-3 0 9091
2 25544 51
6332 197
8860 0008291 258
0089 102
0147 15
78141315 7900
Satellite: ISS
Catalog Number: 25544
Epoch time: 07150
00024707 = yrday
fracday
Element set: 909
Inclination: 51
6332 deg
RA of node: 197
8860 deg
Eccentricity:
0008291
Arg of perigee: 258
0089 deg
Mean anomaly: 102
0147 deg
Mean motion: 15
78141315 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 790
Checksum: 273
Coasting Arc #11 (Orbit 805)
---------------------------------------
Vector Time (GMT): 2007/150/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6618601
08 A = 6720392
84 meter
Y = 1043238
90 meter E =
0010018
Z = 423615
21 I = 51
58706
XDOT = -370
501013 Wp = 169
70153
YDOT = 4800
283957 meter/sec RA = 191
83103 deg
ZDOT = -6020
837276 TA = 5
67961
MA = 5
66826
Ha = 182
041 n
mi
Hp = 180
962
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21714570
47 X = 6604385
64
Y = 3422699
80 feet Y = 1117172
25 meter
Z = 1389813
69 Z = 455734
58
XDOT = -1215
554505 XDOT = -394
902317
YDOT = 15748
963113 feet/sec YDOT = 4796
005400 meter/sec
ZDOT = -19753
403137 ZDOT = -6022
695653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13676257
86 X = -4168523
40
Y = 17200160
68 feet Y = 5242608
98 meter
Z = 1511115
52 Z = 460588
01
XDOT = -11904
476101 XDOT = -3628
484316
YDOT = -7726
330801 feet/sec YDOT = -2354
985628 meter/sec
ZDOT = -19759
822778 ZDOT = -6022
793983
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 07151
01341361
00020000 00000-0 20000-3 0 9103
2 25544 51
6330 192
6505 0008252 260
4801 99
5432 15
78119008 8062
Satellite: ISS
Catalog Number: 25544
Epoch time: 07151
01341361 = yrday
fracday
Element set: 910
Inclination: 51
6330 deg
RA of node: 192
6505 deg
Eccentricity:
0008252
Arg of perigee: 260
4801 deg
Mean anomaly: 99
5432 deg
Mean motion: 15
78119008 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 806
Checksum: 257
Coasting Arc #12 (Orbit 821)
---------------------------------------
Vector Time (GMT): 2007/151/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1707210
83 A = 6708526
17 meter
Y = -3928223
95 meter E =
0005377
Z = 5167882
39 I = 51
57574
XDOT = 7417
957769 Wp = 286
01151
YDOT = 1756
018485 meter/sec RA = 186
65367 deg
ZDOT = -1115
231448 TA = 174
63935
MA = 174
63359
Ha = 181
581 n
mi
Hp = 181
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5601085
39 X = 1725904
92
Y = -12887873
85 feet Y = -3909029
42 meter
Z = 16954994
71 Z = 5176220
80
XDOT = 24337
131788 XDOT = 7403
188063
YDOT = 5761
215503 feet/sec YDOT = 1838
887876 meter/sec
ZDOT = -3658
895828 ZDOT = -1079
230029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8690570
59 X = 2648885
92
Y = 10995086
81 feet Y = 3351302
46 meter
Z = 16985974
93 Z = 5177325
16
XDOT = -15897
461426 XDOT = -4845
546243
YDOT = 18010
312569 feet/sec YDOT = 5489
543271 meter/sec
ZDOT = -3522
845432 ZDOT = -1073
763288
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 07152
02655519
00020000 00000-0 20000-3 0 9119
2 25544 51
6324 187
4137 0008326 265
8278 94
1935 15
78204983 8221
Satellite: ISS
Catalog Number: 25544
Epoch time: 07152
02655519 = yrday
fracday
Element set: 911
Inclination: 51
6324 deg
RA of node: 187
4137 deg
Eccentricity:
0008326
Arg of perigee: 265
8278 deg
Mean anomaly: 94
1935 deg
Mean motion: 15
78204983 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 822
Checksum: 302
Coasting Arc #13 (Orbit 837)
---------------------------------------
Vector Time (GMT): 2007/152/23:32:26
618
Vector Time (MET): N/A
Weight (LBS) : 480698
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5982241
23 A = 6717872
62 meter
Y = -1987575
74 meter E =
0006501
Z = 2310525
56 I = 51
63508
XDOT = 3496
994376 Wp = 49
98066
YDOT = -4206
973126 meter/sec RA = 181
51235 deg
ZDOT = 5429
301805 TA = 336
05401
MA = 336
08423
Ha = 180
603 n
mi
Hp = 180
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19626775
67 X = -5970795
48
Y = -6520917
78 feet Y = -2054408
99 meter
Z = 7580464
43 Z = 2281490
93
XDOT = 11473
078663 XDOT = 3517
402626
YDOT = -13802
405268 feet/sec YDOT = -4167
754769 meter/sec
ZDOT = 17812
669963 ZDOT = 5446
339099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14880593
58 X = 4535604
92
Y = -14420587
23 feet Y = -4395394
99 meter
Z = 7470658
04 Z = 2277056
57
XDOT = 5923
311414 XDOT = 1805
425319
YDOT = 15383
430463 feet/sec YDOT = 4688
869605 meter/sec
ZDOT = 17876
448145 ZDOT = 5448
741395
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 07153
03967636
00020000 00000-0 20000-3 0 9128
2 25544 51
6312 182
1763 0008423 269
9645 90
0555 15
78242348 8383
Satellite: ISS
Catalog Number: 25544
Epoch time: 07153
03967636 = yrday
fracday
Element set: 912
Inclination: 51
6312 deg
RA of node: 182
1763 deg
Eccentricity:
0008423
Arg of perigee: 269
9645 deg
Mean anomaly: 90
0555 deg
Mean motion: 15
78242348 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 838
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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