Date:
June 28th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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 2983)
---------------------------------------
Vector Time (GMT): 2008/177/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6274479
02 A = 6728320
47 meter
Y = 1447428
58 meter E =
0004162
Z = -1943578
61 I = 51
50416
XDOT = 523
728044 Wp = 242
15532
YDOT = -5258
347926 meter/sec RA = 333
12032 deg
ZDOT = -5599
574251 TA = 319
51106
MA = 319
54202
Ha = 188
055 n
mi
Hp = 185
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20585561
09 X = -6280756
53
Y = 4748781
42 feet Y = 1377228
90 meter
Z = -6376570
24 Z = -1974075
02
XDOT = 1718
267861 XDOT = 609
690441
YDOT = -17251
797657 feet/sec YDOT = -5252
009962 meter/sec
ZDOT = -18371
306599 ZDOT = -5596
821839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5904963
04 X = 1799832
74
Y = 20246917
73 feet Y = 6171260
52 meter
Z = -6493891
92 Z = -1979338
26
XDOT = -15851
016448 XDOT = -4831
389813
YDOT = -1273
581028 feet/sec YDOT = -388
187497 meter/sec
ZDOT = -18361
124696 ZDOT = -5596
470807
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 08177
52784643
00020000 00000-0 20000-3 0 9001
2 25544 51
6376 333
4771 0008696 292
6787 67
3457 15
74756549 29846
Satellite: ISS
Catalog Number: 25544
Epoch time: 08177
52784643 = yrday
fracday
Element set: 900
Inclination: 51
6376 deg
RA of node: 333
4771 deg
Eccentricity:
0008696
Arg of perigee: 292
6787 deg
Mean anomaly: 67
3457 deg
Mean motion: 15
74756549 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2984
Checksum: 349
Coasting Arc #2 (Orbit 2999)
---------------------------------------
Vector Time (GMT): 2008/178/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -353861
26 A = 6720218
90 meter
Y = 4715615
26 meter E =
0007443
Z = 4778947
23 I = 51
45044
XDOT = -6991
611574 Wp = 348
90778
YDOT = 2023
021662 meter/sec RA = 327
92942 deg
ZDOT = -2507
366665 TA = 125
73878
MA = 125
66953
Ha = 188
249 n
mi
Hp = 185
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1160962
15 X = -429781
03
Y = 15471178
66 feet Y = 4711233
09 meter
Z = 15678960
73 Z = 4777044
35
XDOT = -22938
358181 XDOT = -7001
533332
YDOT = 6637
210178 feet/sec YDOT = 1944
782292 meter/sec
ZDOT = -8226
268585 ZDOT = -2541
355833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15521343
15 X = 4730905
39
Y = 105132
84 feet Y = 32044
49 meter
Z = 15672008
99 Z = 4776828
34
XDOT = 8316
160808 XDOT = 2534
765814
YDOT = 21206
964850 feet/sec YDOT = 6463
882886 meter/sec
ZDOT = -8356
991501 ZDOT = -2547
211010
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 08178
54320270
00020000 00000-0 20000-3 0 9017
2 25544 51
6374 328
2564 0008576 295
6132 64
4144 15
74715556 30004
Satellite: ISS
Catalog Number: 25544
Epoch time: 08178
54320270 = yrday
fracday
Element set: 901
Inclination: 51
6374 deg
RA of node: 328
2564 deg
Eccentricity:
0008576
Arg of perigee: 295
6132 deg
Mean anomaly: 64
4144 deg
Mean motion: 15
74715556 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3000
Checksum: 283
Coasting Arc #3 (Orbit 3015)
---------------------------------------
Vector Time (GMT): 2008/179/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5917929
23 A = 6727264
33 meter
Y = -2055002
14 meter E =
0009693
Z = 2434037
27 I = 51
45209
XDOT = -271
583697 Wp = 36
54447
YDOT = 5547
163074 meter/sec RA = 322
81595 deg
ZDOT = 5340
442402 TA = 351
04112
MA = 351
05841
Ha = 188
208 n
mi
Hp = 185
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19415778
32 X = 5928644
57
Y = -6742133
01 feet Y = -1988764
89 meter
Z = 7985686
57 Z = 2462812
49
XDOT = -891
022629 XDOT = -359
535829
YDOT = 18199
353918 feet/sec YDOT = 5543
633570 meter/sec
ZDOT = 17521
136491 ZDOT = 5338
910166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8475774
53 X = -2583416
08
Y = -18676474
85 feet Y = -5692589
53 meter
Z = 8096328
08 Z = 2467760
80
XDOT = 16852
231818 XDOT = 5136
560258
YDOT = -50
276114 feet/sec YDOT = -15
324159 meter/sec
ZDOT = 17515
678313 ZDOT = 5338
778750
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 08179
55854189
00020000 00000-0 20000-3 0 9021
2 25544 51
6384 323
0359 0008676 299
1302 60
8992 15
74797206 30169
Satellite: ISS
Catalog Number: 25544
Epoch time: 08179
55854189 = yrday
fracday
Element set: 902
Inclination: 51
6384 deg
RA of node: 323
0359 deg
Eccentricity:
0008676
Arg of perigee: 299
1302 deg
Mean anomaly: 60
8992 deg
Mean motion: 15
74797206 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3016
Checksum: 322
Coasting Arc #4 (Orbit 3030)
---------------------------------------
Vector Time (GMT): 2008/180/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 95265
99 A = 6721040
66 meter
Y = -4972526
82 meter E =
0002529
Z = -4521920
18 I = 51
40860
XDOT = 6543
718682 Wp = 57
90149
YDOT = -2659
957900 meter/sec RA = 317
61572 deg
ZDOT = 3065
454183 TA = 242
70506
MA = 242
73082
Ha = 188
528 n
mi
Hp = 184
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 312552
46 X = 172829
35
Y = -16314064
36 feet Y = -4971027
09 meter
Z = -14835696
13 Z = -4521269
77
XDOT = 21468
893315 XDOT = 6558
084857
YDOT = -8726
895998 feet/sec YDOT = -2586
702455 meter/sec
ZDOT = 10057
264379 ZDOT = 3097
278319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16261526
45 X = -4956513
26
Y = 1368113
16 feet Y = 417000
89 meter
Z = -14833586
50 Z = -4521277
16
XDOT = -10889
728858 XDOT = -3319
189356
YDOT = -19156
940095 feet/sec YDOT = -5839
035341 meter/sec
ZDOT = 10179
599633 ZDOT = 3102
741968
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 08180
51041297
00020000 00000-0 20000-3 0 9038
2 25544 51
6387 318
1425 0008727 303
6148 56
4182 15
74785196 30311
Satellite: ISS
Catalog Number: 25544
Epoch time: 08180
51041297 = yrday
fracday
Element set: 903
Inclination: 51
6387 deg
RA of node: 318
1425 deg
Eccentricity:
0008727
Arg of perigee: 303
6148 deg
Mean anomaly: 56
4182 deg
Mean motion: 15
74785196 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3031
Checksum: 291
Coasting Arc #5 (Orbit 3046)
---------------------------------------
Vector Time (GMT): 2008/181/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5497901
78 A = 6726070
83 meter
Y = 2546770
62 meter E =
0004560
Z = -2922456
24 I = 51
40527
XDOT = -49
294084 Wp = 323
16622
YDOT = -5852
105830 meter/sec RA = 312
50388 deg
ZDOT = -4999
453719 TA = 250
60227
MA = 250
65156
Ha = 188
714 n
mi
Hp = 184
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18037735
49 X = -5511774
67
Y = 8355546
65 feet Y = 2485212
92 meter
Z = -9588111
04 Z = -2949198
50
XDOT = -161
725998 XDOT = 40
435402
YDOT = -19199
822278 feet/sec YDOT = -5852
154410 meter/sec
ZDOT = -16402
407213 ZDOT = -4999
476351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10540300
20 X = 3212683
50
Y = 16795703
23 feet Y = 5119330
34 meter
Z = -9690890
56 Z = -2953783
44
XDOT = -17815
673582 XDOT = -5430
217308
YDOT = 1701
837056 feet/sec YDOT = 518
719935 meter/sec
ZDOT = -16402
956824 ZDOT = -4999
621240
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 08181
52572800
00020000 00000-0 20000-3 0 9040
2 25544 51
6388 312
9213 0008759 307
8321 52
2049 15
74812817 30477
Satellite: ISS
Catalog Number: 25544
Epoch time: 08181
52572800 = yrday
fracday
Element set: 904
Inclination: 51
6388 deg
RA of node: 312
9213 deg
Eccentricity:
0008759
Arg of perigee: 307
8321 deg
Mean anomaly: 52
2049 deg
Mean motion: 15
74812817 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3047
Checksum: 289
Coasting Arc #6 (Orbit 3062)
---------------------------------------
Vector Time (GMT): 2008/182/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 205863
44 A = 6722249
89 meter
Y = 5254957
74 meter E =
0009221
Z = 4189849
78 I = 51
37386
XDOT = -6026
251688 Wp = 20
91475
YDOT = 3133
788280 meter/sec RA = 307
29494 deg
ZDOT = -3623
396799 TA = 106
18280
MA = 106
08130
Ha = 188
906 n
mi
Hp = 184
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 675404
99 X = 126732
73
Y = 17240675
01 feet Y = 5256816
47 meter
Z = 13746226
32 Z = 4190658
81
XDOT = -19771
166956 XDOT = -6043
244420
YDOT = 10281
457612 feet/sec YDOT = 3066
305064 meter/sec
ZDOT = -11887
784774 ZDOT = -3652
713087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16980677
90 X = 5175710
62
Y = -3042461
91 feet Y = -927342
39 meter
Z = 13749755
95 Z = 4190925
61
XDOT = 12756
730145 XDOT = 3888
251348
YDOT = 16802
606873 feet/sec YDOT = 5121
434575 meter/sec
ZDOT = -12000
437692 ZDOT = -3657
733409
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 08182
54103071
00020000 00000-0 20000-3 0 9054
2 25544 51
6394 307
7007 0008690 311
9980 48
0443 15
74805481 30636
Satellite: ISS
Catalog Number: 25544
Epoch time: 08182
54103071 = yrday
fracday
Element set: 905
Inclination: 51
6394 deg
RA of node: 307
7007 deg
Eccentricity:
0008690
Arg of perigee: 311
9980 deg
Mean anomaly: 48
0443 deg
Mean motion: 15
74805481 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3063
Checksum: 282
Coasting Arc #7 (Orbit 3078)
---------------------------------------
Vector Time (GMT): 2008/183/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5025712
09 A = 6724543
76 meter
Y = -2889020
21 meter E =
0008764
Z = 3396522
65 I = 51
36686
XDOT = 447
387356 Wp = 45
53355
YDOT = 6174
404314 meter/sec RA = 302
18441 deg
ZDOT = 4588
641684 TA = 354
79422
MA = 354
80333
Ha = 188
860 n
mi
Hp = 184
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16488556
74 X = 5041144
37
Y = -9478412
78 feet Y = -2832734
34 meter
Z = 11143447
00 Z = 3420974
35
XDOT = 1467
806285 XDOT = 356
020166
YDOT = 20257
232000 feet/sec YDOT = 6178
895308 meter/sec
ZDOT = 15054
598701 ZDOT = 4590
594623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11972285
88 X = -3649152
74
Y = -14706277
44 feet Y = -4482473
36 meter
Z = 11237392
83 Z = 3425157
33
XDOT = 18706
567939 XDOT = 5701
761908
YDOT = -3716
213416 feet/sec YDOT = -1132
701849 meter/sec
ZDOT = 15062
607458 ZDOT = 4591
082753
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 08183
55631690
00020000 00000-0 20000-3 0 9060
2 25544 51
6404 302
4798 0008823 315
7404 44
3053 15
74887866 30798
Satellite: ISS
Catalog Number: 25544
Epoch time: 08183
55631690 = yrday
fracday
Element set: 906
Inclination: 51
6404 deg
RA of node: 302
4798 deg
Eccentricity:
0008823
Arg of perigee: 315
7404 deg
Mean anomaly: 44
3053 deg
Mean motion: 15
74887866 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3079
Checksum: 310
Coasting Arc #8 (Orbit 3093)
---------------------------------------
Vector Time (GMT): 2008/184/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -605799
92 A = 6723430
59 meter
Y = -5510501
46 meter E =
0005323
Z = -3800035
26 I = 51
34825
XDOT = 5487
048384 Wp = 2
53684
YDOT = -3462
137344 meter/sec RA = 296
97114 deg
ZDOT = 4151
230743 TA = 311
07976
MA = 311
12573
Ha = 189
216 n
mi
Hp = 183
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1987532
55 X = -525675
87
Y = -18079073
02 feet Y = -5516826
96 meter
Z = -12467307
29 Z = -3802784
91
XDOT = 18002
127245 XDOT = 5505
188985
YDOT = -11358
718321 feet/sec YDOT = -3400
677588 meter/sec
ZDOT = 13619
523436 ZDOT = 4177
929850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17458836
15 X = -5321453
26
Y = 5071199
43 feet Y = 1545701
59 meter
Z = -12478337
03 Z = -3803397
13
XDOT = -13968
704944 XDOT = -4257
661267
YDOT = -14369
775993 feet/sec YDOT = -4379
907723 meter/sec
ZDOT = 13722
087365 ZDOT = 4182
492229
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 08184
50813916
00020000 00000-0 20000-3 0 9070
2 25544 51
6404 297
5865 0009019 319
9854 40
0644 15
74858109 30944
Satellite: ISS
Catalog Number: 25544
Epoch time: 08184
50813916 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 297
5865 deg
Eccentricity:
0009019
Arg of perigee: 319
9854 deg
Mean anomaly: 40
0644 deg
Mean motion: 15
74858109 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3094
Checksum: 316
Coasting Arc #9 (Orbit 3109)
---------------------------------------
Vector Time (GMT): 2008/185/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4562623
58 A = 6723140
04 meter
Y = 3105566
64 meter E =
0009097
Z = -3847172
32 I = 51
33573
XDOT = -936
709577 Wp = 6
23750
YDOT = -6450
863809 meter/sec RA = 291
85999 deg
ZDOT = -4088
434542 TA = 220
84644
MA = 220
91465
Ha = 189
357 n
mi
Hp = 183
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14969237
46 X = -4578322
83
Y = 10188866
94 feet Y = 3054457
85 meter
Z = -12621956
42 Z = -3869374
66
XDOT = -3073
194149 XDOT = -844
644804
YDOT = -21164
251343 feet/sec YDOT = -6460
822960 meter/sec
ZDOT = -13413
499153 ZDOT = -4092
762827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12873186
74 X = 3923747
32
Y = 12649591
70 feet Y = 3855595
55 meter
Z = -12707232
45 Z = -3873164
45
XDOT = -19265
180224 XDOT = -5872
026932
YDOT = 6087
591353 feet/sec YDOT = 1855
497844 meter/sec
ZDOT = -13430
694068 ZDOT = -4093
675552
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 08185
52340238
00020000 00000-0 20000-3 0 9086
2 25544 51
6407 292
3660 0008940 323
9638 36
0922 15
74885384 31108
Satellite: ISS
Catalog Number: 25544
Epoch time: 08185
52340238 = yrday
fracday
Element set: 908
Inclination: 51
6407 deg
RA of node: 292
3660 deg
Eccentricity:
0008940
Arg of perigee: 323
9638 deg
Mean anomaly: 36
0922 deg
Mean motion: 15
74885384 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3110
Checksum: 296
Coasting Arc #10 (Orbit 3125)
---------------------------------------
Vector Time (GMT): 2008/186/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1055396
59 A = 6724809
81 meter
Y = 5751381
72 meter E =
0010949
Z = 3322165
60 I = 51
33132
XDOT = -4962
699719 Wp = 47
23233
YDOT = 3606
815255 meter/sec RA = 286
64469 deg
ZDOT = -4650
571680 TA = 93
51909
MA = 93
39385
Ha = 189
546 n
mi
Hp = 183
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3462587
22 X = 974867
12
Y = 18869362
60 feet Y = 5762732
86 meter
Z = 10899493
43 Z = 3327098
14
XDOT = -16281
823224 XDOT = -4980
071663
YDOT = 11833
383383 feet/sec YDOT = 3551
223284 meter/sec
ZDOT = -15257
781103 ZDOT = -4674
721506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17735231
17 X = 5405698
46
Y = -7285531
10 feet Y = -2220629
88 meter
Z = 10918970
83 Z = 3328102
31
XDOT = 14437
834137 XDOT = 4400
651845
YDOT = 12056
411412 feet/sec YDOT = 3674
794198 meter/sec
ZDOT = -15350
520157 ZDOT = -4678
838544
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 08186
53865302
00020000 00000-0 20000-3 0 9093
2 25544 51
6403 287
1459 0008922 328
9594 31
1041 15
74897927 31269
Satellite: ISS
Catalog Number: 25544
Epoch time: 08186
53865302 = yrday
fracday
Element set: 909
Inclination: 51
6403 deg
RA of node: 287
1459 deg
Eccentricity:
0008922
Arg of perigee: 328
9594 deg
Mean anomaly: 31
1041 deg
Mean motion: 15
74897927 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3126
Checksum: 314
Coasting Arc #11 (Orbit 3141)
---------------------------------------
Vector Time (GMT): 2008/187/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4123367
11 A = 6721460
17 meter
Y = -3161664
45 meter E =
0007157
Z = 4256265
17 I = 51
31362
XDOT = 1506
004436 Wp = 45
90359
YDOT = 6691
607488 meter/sec RA = 281
52929 deg
ZDOT = 3512
985232 TA = 8
36982
MA = 8
35789
Ha = 189
513 n
mi
Hp = 182
944
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13528107
32 X = 4137739
14
Y = -10372914
86 feet Y = -3115474
94 meter
Z = 13964124
59 Z = 4276330
48
XDOT = 4940
959436 XDOT = 1414
000789
YDOT = 21954
092807 feet/sec YDOT = 6707
933492 meter/sec
ZDOT = 11525
542100 ZDOT = 3520
078892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13151498
89 X = -4008576
86
Y = -10746516
80 feet Y = -3275538
32 meter
Z = 14041163
75 Z = 4279746
71
XDOT = 19493
722955 XDOT = 5941
686757
YDOT = -8766
186998 feet/sec YDOT = -2671
933797 meter/sec
ZDOT = 11553
436931 ZDOT = 3521
487577
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 08187
55388835
00020000 00000-0 20000-3 0 9109
2 25544 51
6404 281
9245 0009048 332
5811 27
4874 15
74960532 31421
Satellite: ISS
Catalog Number: 25544
Epoch time: 08187
55388835 = yrday
fracday
Element set: 910
Inclination: 51
6404 deg
RA of node: 281
9245 deg
Eccentricity:
0009048
Arg of perigee: 332
5811 deg
Mean anomaly: 27
4874 deg
Mean motion: 15
74960532 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3142
Checksum: 302
Coasting Arc #12 (Orbit 3156)
---------------------------------------
Vector Time (GMT): 2008/188/12:00:00
010
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1597786
75 A = 6726101
88 meter
Y = -5898854
27 meter E =
0010776
Z = -2794690
23 I = 51
32392
XDOT = 4502
898603 Wp = 1
89838
YDOT = -3627
131697 meter/sec RA = 276
31621 deg
ZDOT = 5092
690595 TA = 325
91388
MA = 325
98304
Ha = 189
828 n
mi
Hp = 182
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5242082
52 X = -1518130
23
Y = -19353196
43 feet Y = -5916275
87 meter
Z = -9168931
19 Z = -2802259
47
XDOT = 14773
289380 XDOT = 4518
384182
YDOT = -11900
038376 feet/sec YDOT = -3576
691826 meter/sec
ZDOT = 16708
302478 ZDOT = 5114
602393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17507835
21 X = -5336388
17
Y = 9744554
72 feet Y = 2970140
28 meter
Z = -9198603
16 Z = -2803734
24
XDOT = -14404
286796 XDOT = -4390
426615
YDOT = -10062
792296 feet/sec YDOT = -3067
139092 meter/sec
ZDOT = 16792
413394 ZDOT = 5118
327602
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 08188
50566242
00020000 00000-0 20000-3 0 9116
2 25544 51
6400 277
0309 0009277 336
2518 23
8217 15
74930063 31576
Satellite: ISS
Catalog Number: 25544
Epoch time: 08188
50566242 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 277
0309 deg
Eccentricity:
0009277
Arg of perigee: 336
2518 deg
Mean anomaly: 23
8217 deg
Mean motion: 15
74930063 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3157
Checksum: 284
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics 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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