Date:
May 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) : 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
143/23:31:57
261 0
5 2
5 2
5
N/A -1
6 -0
0 184
1
000/00:03:54
522 1
9 0
0 180
4
Coasting Arc #1 (Orbit 609)
---------------------------------------
Vector Time (GMT): 2007/138/13:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1778709
30 A = 6720836
87 meter
Y = 6464699
64 meter E =
0018857
Z = 224263
91 I = 51
34401
XDOT = -4594
618893 Wp = 161
03736
YDOT = 1477
262034 meter/sec RA = 256
14929 deg
ZDOT = -6019
155489 TA = 16
50920
MA = 16
44788
Ha = 185
463 n
mi
Hp = 177
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5835660
44 X = 1705198
45
Y = 21209644
48 feet Y = 6484179
10 meter
Z = 735773
98 Z = 232727
57
XDOT = -15074
208966 XDOT = -4581
556036
YDOT = 4846
660218 feet/sec YDOT = 1425
956530 meter/sec
ZDOT = -19747
885461 ZDOT = -6041
444442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21895389
97 X = 6673714
86
Y = -2108722
07 feet Y = -642738
49 meter
Z = 768442
67 Z = 234221
32
XDOT = 2055
687040 XDOT = 626
573410
YDOT = 13976
494147 feet/sec YDOT = 4260
035416 meter/sec
ZDOT = -19831
710814 ZDOT = -6044
705456
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 07138
60158216
00020000 00000-0 20000-3 0 9007
2 25544 51
6343 256
7816 0009764 199
3919 160
6876 15
77988871 6108
Satellite: ISS
Catalog Number: 25544
Epoch time: 07138
60158216 = yrday
fracday
Element set: 900
Inclination: 51
6343 deg
RA of node: 256
7816 deg
Eccentricity:
0009764
Arg of perigee: 199
3919 deg
Mean anomaly: 160
6876 deg
Mean motion: 15
77988871 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 610
Checksum: 327
Coasting Arc #2 (Orbit 625)
---------------------------------------
Vector Time (GMT): 2007/139/13:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4335631
42 A = 6709050
87 meter
Y = -3193
90 meter E =
0006381
Z = 5119220
10 I = 51
31359
XDOT = 1497
675279 Wp = 184
94640
YDOT = 7454
231002 meter/sec RA = 250
95190 deg
ZDOT = -1270
172959 TA = 277
20371
MA = 277
27625
Ha = 185
044 n
mi
Hp = 177
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14224512
55 X = 4310476
51
Y = -10478
68 feet Y = 45148
00 meter
Z = 16795341
53 Z = 5140221
63
XDOT = 4913
632806 XDOT = 1420
379982
YDOT = 24456
138458 feet/sec YDOT = 7470
546891 meter/sec
ZDOT = -4167
234116 ZDOT = -1263
083636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2172422
98 X = 662154
52
Y = -13962527
57 feet Y = -4255778
40 meter
Z = 16874500
48 Z = 5143347
75
XDOT = 23907
058610 XDOT = 7286
871464
YDOT = -1258
040807 feet/sec YDOT = -383
450838 meter/sec
ZDOT = -4139
620585 ZDOT = -1261
756354
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 07139
61482318
00020000 00000-0 20000-3 0 9013
2 25544 51
6347 251
5462 0009585 204
3893 155
6820 15
78067649 6263
Satellite: ISS
Catalog Number: 25544
Epoch time: 07139
61482318 = yrday
fracday
Element set: 901
Inclination: 51
6347 deg
RA of node: 251
5462 deg
Eccentricity:
0009585
Arg of perigee: 204
3893 deg
Mean anomaly: 155
6820 deg
Mean motion: 15
78067649 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 626
Checksum: 308
Coasting Arc #3 (Orbit 641)
---------------------------------------
Vector Time (GMT): 2007/140/13:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -718884
50 A = 6718164
91 meter
Y = -6241140
29 meter E =
0010070
Z = 2380100
08 I = 51
35429
XDOT = 5343
487140 Wp = 116
88426
YDOT = 1436
443455 meter/sec RA = 245
79577 deg
ZDOT = 5358
718105 TA = 270
09125
MA = 270
20664
Ha = 184
994 n
mi
Hp = 178
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2358544
95 X = -660603
84
Y = -20476182
04 feet Y = -6248853
79 meter
Z = 7808727
31 Z = 2376748
27
XDOT = 17531
125786 XDOT = 5300
995769
YDOT = 4712
740994 feet/sec YDOT = 1495
958852 meter/sec
ZDOT = 17581
096145 ZDOT = 5384
573828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20612038
45 X = -6282549
32
Y = -435357
62 feet Y = -132697
00 meter
Z = 7795339
79 Z = 2376019
57
XDOT = 7032
476557 XDOT = 2143
498855
YDOT = -15116
340692 feet/sec YDOT = -4607
460643 meter/sec
ZDOT = 17678
736477 ZDOT = 5388
478878
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 07140
62804898
00020000 00000-0 20000-3 0 9028
2 25544 51
6340 246
3113 0009519 207
9161 152
1495 15
78069139 6429
Satellite: ISS
Catalog Number: 25544
Epoch time: 07140
62804898 = yrday
fracday
Element set: 902
Inclination: 51
6340 deg
RA of node: 246
3113 deg
Eccentricity:
0009519
Arg of perigee: 207
9161 deg
Mean anomaly: 152
1495 deg
Mean motion: 15
78069139 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 642
Checksum: 289
Coasting Arc #4 (Orbit 656)
---------------------------------------
Vector Time (GMT): 2007/141/13:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4925520
45 A = 6713792
63 meter
Y = -2388536
50 meter E =
0010154
Z = -3896169
46 I = 51
35209
XDOT = -8
018454 Wp = 171
20417
YDOT = -6563
164774 meter/sec RA = 240
56141 deg
ZDOT = 4025
149882 TA = 140
85371
MA = 140
78021
Ha = 184
726 n
mi
Hp = 178
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16159843
99 X = -4879518
56
Y = -7836405
83 feet Y = -2443358
65 meter
Z = -12782708
21 Z = -3919986
21
XDOT = -26
307265 XDOT = 45
818992
YDOT = -21532
692827 feet/sec YDOT = -6562
954011 meter/sec
ZDOT = 13205
872316 ZDOT = 4025
240736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9716387
32 X = -2961554
85
Y = 15027659
91 feet Y = 4580430
74 meter
Z = -12872789
06 Z = -3923626
11
XDOT = -20292
322573 XDOT = -6185
099920
YDOT = -1784
728771 feet/sec YDOT = -543
985329 meter/sec
ZDOT = 13205
416430 ZDOT = 4025
010928
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
57793239
00020000 00000-0 20000-3 0 9030
2 25544 51
6330 241
4036 0009407 211
5096 148
5507 15
78108426 6574
Satellite: ISS
Catalog Number: 25544
Epoch time: 07141
57793239 = yrday
fracday
Element set: 903
Inclination: 51
6330 deg
RA of node: 241
4036 deg
Eccentricity:
0009407
Arg of perigee: 211
5096 deg
Mean anomaly: 148
5507 deg
Mean motion: 15
78108426 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 657
Checksum: 286
Coasting Arc #5 (Orbit 672)
---------------------------------------
Vector Time (GMT): 2007/142/13:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -829725
70 A = 6712060
71 meter
Y = 4998278
41 meter E =
0005371
Z = -4402812
25 I = 51
36056
XDOT = -5823
923878 Wp = 142
07133
YDOT = -3842
385032 meter/sec RA = 235
42414 deg
ZDOT = -3270
802141 TA = 95
04288
MA = 94
98156
Ha = 184
509 n
mi
Hp = 178
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2722197
19 X = -864167
51
Y = 16398551
21 feet Y = 4988807
93 meter
Z = -14444922
07 Z = -4406926
08
XDOT = -19107
361803 XDOT = -5764
636001
YDOT = -12606
250106 feet/sec YDOT = -3907
179508 meter/sec
ZDOT = -10730
978154 ZDOT = -3298
951164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16037994
28 X = 4888380
66
Y = 4321457
07 feet Y = 1317180
11 meter
Z = -14459818
85 Z = -4407352
79
XDOT = -14191
339786 XDOT = -4325
520367
YDOT = 16473
392578 feet/sec YDOT = 5021
090058 meter/sec
ZDOT = -10837
582469 ZDOT = -3303
295137
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
59112495
00020000 00000-0 20000-3 0 9043
2 25544 51
6323 236
1677 0009337 216
0623 143
9914 15
78092552 6737
Satellite: ISS
Catalog Number: 25544
Epoch time: 07142
59112495 = yrday
fracday
Element set: 904
Inclination: 51
6323 deg
RA of node: 236
1677 deg
Eccentricity:
0009337
Arg of perigee: 216
0623 deg
Mean anomaly: 143
9914 deg
Mean motion: 15
78092552 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 673
Checksum: 292
Coasting Arc #6 (Orbit 688)
---------------------------------------
Vector Time (GMT): 2007/143/13:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5073354
41 A = 6719216
63 meter
Y = 4086154
65 meter E =
0014850
Z = 1606217
81 I = 51
40334
XDOT = -2005
365210 Wp = 153
16768
YDOT = 4748
432416 meter/sec RA = 230
19898 deg
ZDOT = -5738
264100 TA = 8
99526
MA = 8
96869
Ha = 184
128 n
mi
Hp = 178
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16644863
55 X = 5019482
67
Y = 13406019
19 feet Y = 4142586
36 meter
Z = 5269743
47 Z = 1630733
71
XDOT = -6579
282184 XDOT = -2030
438423
YDOT = 15578
846509 feet/sec YDOT = 4725
867717 meter/sec
ZDOT = -18826
325787 ZDOT = -5748
066549
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14788062
82 X = 4507401
55
Y = -15397979
65 feet Y = -4693304
20 meter
Z = 5362690
55 Z = 1634548
08
XDOT = 13840
184965 XDOT = 4218
488377
YDOT = 6714
228506 feet/sec YDOT = 2046
496849 meter/sec
ZDOT = -18862
698937 ZDOT = -5749
350636
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
60429995
00020000 00000-0 20000-3 0 9053
2 25544 51
6328 230
9319 0009087 220
5197 139
5292 15
78155380 6891
Satellite: ISS
Catalog Number: 25544
Epoch time: 07143
60429995 = yrday
fracday
Element set: 905
Inclination: 51
6328 deg
RA of node: 230
9319 deg
Eccentricity:
0009087
Arg of perigee: 220
5197 deg
Mean anomaly: 139
5292 deg
Mean motion: 15
78155380 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 689
Checksum: 316
Coasting Arc #7 (Orbit 694)
---------------------------------------
Vector Time (GMT): 2007/143/23:33:54
522
Vector Time (MET): N/A
Weight (LBS) : 480645
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5079551
97 A = 6721106
04 meter
Y = -4234574
66 meter E =
0002924
Z = -1189006
68 I = 51
41305
XDOT = 2315
565490 Wp = 337
48718
YDOT = -4424
995843 meter/sec RA = 228
06451 deg
ZDOT = 5864
947118 TA = 9
42843
MA = 9
42294
Ha = 184
054 n
mi
Hp = 180
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16665196
74 X = -5026046
84
Y = -13892961
49 feet Y = -4291077
78 meter
Z = -3900940
56 Z = -1213553
60
XDOT = 7596
999638 XDOT = 2336
383503
YDOT = -14517
702896 feet/sec YDOT = -4398
986078 meter/sec
ZDOT = 19241
952486 ZDOT = 5876
246255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21027796
95 X = 6409272
51
Y = -5276362
65 feet Y = -1608235
34 meter
Z = -3994026
97 Z = -1217379
42
XDOT = 6942
836774 XDOT = 2116
176649
YDOT = 13066
772595 feet/sec YDOT = 3982
752287 meter/sec
ZDOT = 19284
008580 ZDOT = 5877
765815
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
98423735
00020000 00000-0 20000-3 0 9061
2 25544 51
6330 228
9689 0008173 235
5183 124
5211 15
77667912 6957
Satellite: ISS
Catalog Number: 25544
Epoch time: 07143
98423735 = yrday
fracday
Element set: 906
Inclination: 51
6330 deg
RA of node: 228
9689 deg
Eccentricity:
0008173
Arg of perigee: 235
5183 deg
Mean anomaly: 124
5211 deg
Mean motion: 15
77667912 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 695
Checksum: 310
Coasting Arc #8 (Orbit 710)
---------------------------------------
Vector Time (GMT): 2007/144/23:33:54
522
Vector Time (MET): N/A
Weight (LBS) : 480645
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2895037
14 A = 6709541
71 meter
Y = 3029043
41 meter E =
0009107
Z = -5247355
52 I = 51
39532
XDOT = -5614
398592 Wp = 117
41086
YDOT = -5271
395103 meter/sec RA = 222
89495 deg
ZDOT = 50
554605 TA = 153
09406
MA = 153
04681
Ha = 183
711 n
mi
Hp = 180
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9498153
35 X = -2903202
40
Y = 9937806
46 feet Y = 2996624
30 meter
Z = -17215733
35 Z = -5261439
22
XDOT = -18419
942886 XDOT = -5555
281395
YDOT = -17294
603357 feet/sec YDOT = -5333
847920 meter/sec
ZDOT = 165
861566 ZDOT = 23
422899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2730472
57 X = -832248
04
Y = -13405262
90 feet Y = -4085924
13 meter
Z = -17268463
60 Z = -5263427
70
XDOT = 23761
720683 XDOT = 7242
572464
YDOT = -4938
085552 feet/sec YDOT = -1505
128476 meter/sec
ZDOT = 62
890118 ZDOT = 19
168908
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
99769459
00020000 00000-0 20000-3 0 9070
2 25544 51
6337 223
7348 0008100 239
5647 120
4718 15
77711237 7114
Satellite: ISS
Catalog Number: 25544
Epoch time: 07144
99769459 = yrday
fracday
Element set: 907
Inclination: 51
6337 deg
RA of node: 223
7348 deg
Eccentricity:
0008100
Arg of perigee: 239
5647 deg
Mean anomaly: 120
4718 deg
Mean motion: 15
77711237 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 711
Checksum: 306
Coasting Arc #9 (Orbit 726)
---------------------------------------
Vector Time (GMT): 2007/145/23:33:54
522
Vector Time (MET): N/A
Weight (LBS) : 480645
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4526449
13 A = 6721009
26 meter
Y = 4790343
73 meter E =
0011100
Z = -1279019
79 I = 51
45610
XDOT = -4335
940462 Wp = 189
77991
YDOT = 2536
452272 meter/sec RA = 217
72822 deg
ZDOT = -5848
429147 TA = 4
31810
MA = 4
30853
Ha = 183
664 n
mi
Hp = 180
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14850554
90 X = 4478759
69
Y = 15716350
82 feet Y = 4840694
49 meter
Z = -4196259
15 Z = -1257145
56
XDOT = -14225
526451 XDOT = -4335
570373
YDOT = 8321
693807 feet/sec YDOT = 2487
967939 meter/sec
ZDOT = -19187
759667 ZDOT = -5869
492174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21352251
61 X = -6508166
29
Y = 3509196
52 feet Y = 1069603
10 meter
Z = -4113167
37 Z = -1253693
41
XDOT = 1277
033397 XDOT = 389
239779
YDOT = -14799
349674 feet/sec YDOT = -4510
841781 meter/sec
ZDOT = -19266
873280 ZDOT = -5872
542976
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
01113700
00020000 00000-0 20000-3 0 9088
2 25544 51
6340 218
5009 0008225 243
3433 116
6890 15
77691674 7275
Satellite: ISS
Catalog Number: 25544
Epoch time: 07146
01113700 = yrday
fracday
Element set: 908
Inclination: 51
6340 deg
RA of node: 218
5009 deg
Eccentricity:
0008225
Arg of perigee: 243
3433 deg
Mean anomaly: 116
6890 deg
Mean motion: 15
77691674 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 727
Checksum: 275
Coasting Arc #10 (Orbit 742)
---------------------------------------
Vector Time (GMT): 2007/146/23:33:54
522
Vector Time (MET): N/A
Weight (LBS) : 480645
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4626598
49 A = 6711915
51 meter
Y = -1440322
64 meter E =
0000902
Z = 4645131
89 I = 51
44986
XDOT = 4547
162535 Wp = 322
52744
YDOT = 5551
592135 meter/sec RA = 212
51687 deg
ZDOT = -2807
209057 TA = 155
23835
MA = 155
23402
Ha = 183
145 n
mi
Hp = 180
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15179128
90 X = 4619795
06
Y = -4725467
98 feet Y = -1388623
90 meter
Z = 15239934
01 Z = 4667591
50
XDOT = 14918
512255 XDOT = 4498
382935
YDOT = 18213
884958 feet/sec YDOT = 5602
168583 meter/sec
ZDOT = -9210
003467 ZDOT = -2785
236648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4285005
47 X = -1306069
67
Y = 15224695
61 feet Y = 4640487
22 meter
Z = 15324456
35 Z = 4670894
29
XDOT = -22323
103812 XDOT = -6804
082042
YDOT = 2904
765733 feet/sec YDOT = 885
372596 meter/sec
ZDOT = -9126
441261 ZDOT = -2781
739296
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
02456239
00020000 00000-0 20000-3 0 9098
2 25544 51
6339 213
2669 0008132 249
0778 110
9517 15
77777648 7436
Satellite: ISS
Catalog Number: 25544
Epoch time: 07147
02456239 = yrday
fracday
Element set: 909
Inclination: 51
6339 deg
RA of node: 213
2669 deg
Eccentricity:
0008132
Arg of perigee: 249
0778 deg
Mean anomaly: 110
9517 deg
Mean motion: 15
77777648 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 743
Checksum: 316
Coasting Arc #11 (Orbit 758)
---------------------------------------
Vector Time (GMT): 2007/147/23:33:54
522
Vector Time (MET): N/A
Weight (LBS) : 480645
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3188869
47 A = 6716269
59 meter
Y = -4774204
12 meter E =
0005427
Z = 3483803
51 I = 51
48936
XDOT = 6189
450318 Wp = 120
39512
YDOT = -836
414280 meter/sec RA = 207
38742 deg
ZDOT = 4511
330572 TA = 281
13131
MA = 281
19232
Ha = 183
032 n
mi
Hp = 181
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10462170
19 X = -3152170
56
Y = -15663399
34 feet Y = -4809659
03 meter
Z = 11429801
53 Z = 3468400
37
XDOT = 20306
595532 XDOT = 6176
427656
YDOT = -2744
141339 feet/sec YDOT = -767
273683 meter/sec
ZDOT = 14800
953320 ZDOT = 4541
367649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18862461
87 X = 5749278
38
Y = -587233
53 feet Y = -178988
78 meter
Z = 11371109
71 Z = 3465914
24
XDOT = -8470
756324 XDOT = -2581
886528
YDOT = 17212
018630 feet/sec YDOT = 5246
223278 meter/sec
ZDOT = 14914
135827 ZDOT = 4545
828600
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
03797519
00020000 00000-0 20000-3 0 9101
2 25544 51
6341 208
0322 0008040 253
0772 106
9512 15
77756164 7591
Satellite: ISS
Catalog Number: 25544
Epoch time: 07148
03797519 = yrday
fracday
Element set: 910
Inclination: 51
6341 deg
RA of node: 208
0322 deg
Eccentricity:
0008040
Arg of perigee: 253
0772 deg
Mean anomaly: 106
9512 deg
Mean motion: 15
77756164 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 759
Checksum: 284
Coasting Arc #12 (Orbit 773)
---------------------------------------
Vector Time (GMT): 2007/148/23:33:54
522
Vector Time (MET): N/A
Weight (LBS) : 480645
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6016879
64 A = 6717438
19 meter
Y = 108594
69 meter E =
0003723
Z = -2982061
21 I = 51
51998
XDOT = -2559
860668 Wp = 265
14242
YDOT = -5305
090477 meter/sec RA = 202
16244 deg
ZDOT = 4966
208424 TA = 60
30310
MA = 60
26604
Ha = 182
740 n
mi
Hp = 181
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19740418
77 X = -6003160
21
Y = 356281
80 feet Y = 41387
66 meter
Z = -9783665
38 Z = -3011258
38
XDOT = -8398
493006 XDOT = -2524
473476
YDOT = -17405
152484 feet/sec YDOT = -5333
519052 meter/sec
ZDOT = 16293
334726 ZDOT = 4953
857681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9872700
03 X = 3009198
97
Y = -17034497
38 feet Y = -5192114
80 meter
Z = -9893779
42 Z = -3015623
97
XDOT = 18045
417983 XDOT = 5500
243401
YDOT = 1012
163126 feet/sec YDOT = 308
507321 meter/sec
ZDOT = 16246
088234 ZDOT = 4951
807694
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
98803411
00020000 00000-0 20000-3 0 9115
2 25544 51
6340 203
1251 0008190 257
4617 102
5633 15
77789947 7747
Satellite: ISS
Catalog Number: 25544
Epoch time: 07148
98803411 = yrday
fracday
Element set: 911
Inclination: 51
6340 deg
RA of node: 203
1251 deg
Eccentricity:
0008190
Arg of perigee: 257
4617 deg
Mean anomaly: 102
5633 deg
Mean motion: 15
77789947 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 774
Checksum: 294
Coasting Arc #13 (Orbit 789)
---------------------------------------
Vector Time (GMT): 2007/149/23:33:54
522
Vector Time (MET): N/A
Weight (LBS) : 480645
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1115516
48 A = 6710754
50 meter
Y = 4430688
85 meter E =
0004619
Z = -4919346
84 I = 51
52407
XDOT = -7388
236295 Wp = 60
65469
YDOT = -498
256891 meter/sec RA = 197
03130 deg
ZDOT = -2123
390614 TA = 188
72600
MA = 188
73403
Ha = 182
403 n
mi
Hp = 181
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3659830
97 X = 1089786
69
Y = 14536380
74 feet Y = 4443020
05 meter
Z = -16139589
36 Z = -4913989
40
XDOT = -24239
620390 XDOT = -7371
800368
YDOT = -1634
701087 feet/sec YDOT = -580
784076 meter/sec
ZDOT = -6966
504638 ZDOT = -2159
243472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14453557
48 X = -4405444
32
Y = -4057713
16 feet Y = -1236790
97 meter
Z = -16118830
99 Z = -4913019
69
XDOT = 13271
467800 XDOT = 4045
143385
YDOT = -19052
114584 feet/sec YDOT = -5807
084525 meter/sec
ZDOT = -7101
810295 ZDOT = -2164
631778
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
00141647
00020000 00000-0 20000-3 0 9128
2 25544 51
6333 197
8906 0008218 261
8521 98
1712 15
77830190 7902
Satellite: ISS
Catalog Number: 25544
Epoch time: 07150
00141647 = yrday
fracday
Element set: 912
Inclination: 51
6333 deg
RA of node: 197
8906 deg
Eccentricity:
0008218
Arg of perigee: 261
8521 deg
Mean anomaly: 98
1712 deg
Mean motion: 15
77830190 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 790
Checksum: 282
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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