Date:
July 24th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7750 02 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
205/16:28:18
127 -10
4 11
2 11
2
N/A -3
4 0
0 193
9
000/00:20:36
255 2
5 0
3 185
5
Coasting Arc #1 (Orbit 3394)
---------------------------------------
Vector Time (GMT): 2008/203/13:37:38
230
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5946796
25 A = 6724697
25 meter
Y = -582141
83 meter E =
0020139
Z = 3076947
41 I = 51
53802
XDOT = 3046
126455 Wp = 70
26679
YDOT = 5116
933855 meter/sec RA = 198
55439 deg
ZDOT = -4886
585330 TA = 73
95291
MA = 73
73122
Ha = 191
410 n
mi
Hp = 179
329
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19510486
37 X = 5937916
88
Y = -1909914
14 feet Y = -515691
27 meter
Z = 10094971
82 Z = 3105814
82
XDOT = 9993
853198 XDOT = 3012
419419
YDOT = 16787
840733 feet/sec YDOT = 5150
809367 meter/sec
ZDOT = -16032
104100 ZDOT = -4871
868918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16746521
25 X = -5104339
68
Y = -10079751
40 feet Y = -3072308
23 meter
Z = 10206269
86 Z = 3110871
05
XDOT = 1195
031886 XDOT = 364
245719
YDOT = -18267
712876 feet/sec YDOT = -5567
998885 meter/sec
ZDOT = -15974
828887 ZDOT = -4869
127845
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 08203
60596818
00020000 00000-0 20000-3 0 9005
2 25544 51
6370 199
3787 0009922 36
4172 323
7665 15
75150960 33954
Satellite: ISS
Catalog Number: 25544
Epoch time: 08203
60596818 = yrday
fracday
Element set: 900
Inclination: 51
6370 deg
RA of node: 199
3787 deg
Eccentricity:
0009922
Arg of perigee: 36
4172 deg
Mean anomaly: 323
7665 deg
Mean motion: 15
75150960 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3395
Checksum: 311
Coasting Arc #2 (Orbit 3410)
---------------------------------------
Vector Time (GMT): 2008/204/13:37:38
230
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2595526
61 A = 6720092
33 meter
Y = -4273983
53 meter E =
0015152
Z = 4474906
75 I = 51
55175
XDOT = 6973
565311 Wp = 74
85142
YDOT = -915
818138 meter/sec RA = 193
45233 deg
ZDOT = 3165
132557 TA = 343
52369
MA = 343
57289
Ha = 191
448 n
mi
Hp = 179
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8515507
25 X = -2569279
33
Y = -14022255
67 feet Y = -4302861
77 meter
Z = 14681452
60 Z = 4462361
29
XDOT = 22879
151282 XDOT = 6967
912413
YDOT = -3004
652683 feet/sec YDOT = -837
867568 meter/sec
ZDOT = 10384
293165 ZDOT = 3198
995881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1189366
40 X = -362518
88
Y = 16405918
35 feet Y = 5000523
91 meter
Z = 14632628
58 Z = 4460025
19
XDOT = -19094
810499 XDOT = -5820
098240
YDOT = -10777
178283 feet/sec YDOT = -3284
883941 meter/sec
ZDOT = 10514
837957 ZDOT = 3204
922609
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 08204
62105746
00020000 00000-0 20000-3 0 9015
2 25544 51
6378 194
1573 0009757 40
1449 320
0434 15
75193560 34119
Satellite: ISS
Catalog Number: 25544
Epoch time: 08204
62105746 = yrday
fracday
Element set: 901
Inclination: 51
6378 deg
RA of node: 194
1573 deg
Eccentricity:
0009757
Arg of perigee: 40
1449 deg
Mean anomaly: 320
0434 deg
Mean motion: 15
75193560 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3411
Checksum: 276
Coasting Arc #3 (Orbit 3425)
---------------------------------------
Vector Time (GMT): 2008/205/13:37:38
230
Vector Time (MET): N/A
Weight (LBS) : 661904
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6185955
83 A = 6726236
27 meter
Y = 1039863
47 meter E =
0015380
Z = -2419576
62 I = 51
60133
XDOT = -2879
090394 Wp = 45
80884
YDOT = -4715
143758 meter/sec RA = 188
25863 deg
ZDOT = 5365
814817 TA = 286
85526
MA = 287
02388
Ha = 191
518 n
mi
Hp = 179
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20295130
67 X = -6185370
23
Y = 3411625
55 feet Y = 970692
00 meter
Z = -7938243
50 Z = -2449626
24
XDOT = -9445
834625 XDOT = -2852
216859
YDOT = -15469
631753 feet/sec YDOT = -4747
189516 meter/sec
ZDOT = 17604
379321 ZDOT = 5351
893263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18593164
23 X = 5667196
46
Y = 8716273
17 feet Y = 2656720
06 meter
Z = -8054070
61 Z = -2454880
72
XDOT = -316
155557 XDOT = -96
364214
YDOT = 16797
186838 feet/sec YDOT = 5119
782548 meter/sec
ZDOT = 17550
197430 ZDOT = 5349
300177
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 08205
57269524
00020000 00000-0 20000-3 0 9026
2 25544 51
6378 189
2615 0009972 43
9108 316
2847 15
75163130 34264
Satellite: ISS
Catalog Number: 25544
Epoch time: 08205
57269524 = yrday
fracday
Element set: 902
Inclination: 51
6378 deg
RA of node: 189
2615 deg
Eccentricity:
0009972
Arg of perigee: 43
9108 deg
Mean anomaly: 316
2847 deg
Mean motion: 15
75163130 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3426
Checksum: 302
Coasting Arc #4 (Orbit 3427)
---------------------------------------
Vector Time (GMT): 2008/205/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5825066
20 A = 6732092
27 meter
Y = 1591237
76 meter E =
0011385
Z = -2963541
96 I = 51
60323
XDOT = -3762
026291 Wp = 9
15906
YDOT = -4495
729870 meter/sec RA = 187
60969 deg
ZDOT = 4994
273833 TA = 316
63605
MA = 316
72557
Ha = 193
871 n
mi
Hp = 185
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19111109
57 X = -5828030
50
Y = 5220596
34 feet Y = 1526082
16 meter
Z = -9722906
68 Z = -2991846
99
XDOT = -12342
605943 XDOT = -3735
735808
YDOT = -14749
769914 feet/sec YDOT = -4537
652359 meter/sec
ZDOT = 16385
412837 ZDOT = 4976
061599
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17756818
00 X = 5412278
13
Y = -8663269
98 feet Y = -2640564
69 meter
Z = -9831948
79 Z = -2996777
99
XDOT = 14323
529584 XDOT = 4365
811817
YDOT = 10893
180547 feet/sec YDOT = 3320
241431 meter/sec
ZDOT = 16314
698892 ZDOT = 4972
720222
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 08205
69958161
00020000 00000-0 20000-3 0 9032
2 25544 51
6404 188
6096 0010051 345
4181 14
6690 15
72657715 34282
Satellite: ISS
Catalog Number: 25544
Epoch time: 08205
69958161 = yrday
fracday
Element set: 903
Inclination: 51
6404 deg
RA of node: 188
6096 deg
Eccentricity:
0010051
Arg of perigee: 345
4181 deg
Mean anomaly: 14
6690 deg
Mean motion: 15
72657715 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3428
Checksum: 296
Coasting Arc #5 (Orbit 3443)
---------------------------------------
Vector Time (GMT): 2008/206/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4068207
53 A = 6728662
81 meter
Y = 3445092
32 meter E =
0013536
Z = -4118783
38 I = 51
62147
XDOT = -6124
623186 Wp = 23
45222
YDOT = 2716
966286 meter/sec RA = 182
53215 deg
ZDOT = -3768
905602 TA = 207
80029
MA = 207
87269
Ha = 194
093 n
mi
Hp = 185
382
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13347137
57 X = 4049389
84
Y = 11302796
34 feet Y = 3490480
47 meter
Z = -13513068
84 Z = -4099065
53
XDOT = -20093
908090 XDOT = -6136
240940
YDOT = 8913
931384 feet/sec YDOT = 2648
412570 meter/sec
ZDOT = -12365
175861 ZDOT = -3798
686929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15433072
00 X = -4704000
35
Y = -8353389
89 feet Y = -2546113
24 meter
Z = -13436646
96 Z = -4095489
99
XDOT = 17196
563691 XDOT = 5241
512613
YDOT = -11654
751928 feet/sec YDOT = -3552
368388 meter/sec
ZDOT = -12479
808942 ZDOT = -3803
845766
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 08206
71628161
00020000 00000-0 20000-3 0 9041
2 25544 51
6411 183
3989 0010118 349
5251 10
5699 15
72684426 34441
Satellite: ISS
Catalog Number: 25544
Epoch time: 08206
71628161 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 183
3989 deg
Eccentricity:
0010118
Arg of perigee: 349
5251 deg
Mean anomaly: 10
5699 deg
Mean motion: 15
72684426 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3444
Checksum: 294
Coasting Arc #6 (Orbit 3459)
---------------------------------------
Vector Time (GMT): 2008/207/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4777990
75 A = 6730219
27 meter
Y = -3076495
06 meter E =
0015358
Z = 3606479
86 I = 51
65551
XDOT = 5421
164251 Wp = 44
81441
YDOT = 3234
512179 meter/sec RA = 177
35559 deg
ZDOT = -4400
915451 TA = 92
09092
MA = 91
91504
Ha = 194
185 n
mi
Hp = 185
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15675822
68 X = 4794517
88
Y = -10093487
74 feet Y = -3022972
77 meter
Z = 11832283
00 Z = 3629731
17
XDOT = 17785
971952 XDOT = 5405
971348
YDOT = 10611
916597 feet/sec YDOT = 3295
050239 meter/sec
ZDOT = -14438
698985 ZDOT = -4374
616027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13017091
02 X = -3967609
34
Y = 13268058
36 feet Y = 4044104
19 meter
Z = 11921694
56 Z = 3633732
50
XDOT = -18791
635037 XDOT = -5727
690359
YDOT = -5489
618858 feet/sec YDOT = -1673
235828 meter/sec
ZDOT = -14336
898126 ZDOT = -4369
886549
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 08207
73297214
00020000 00000-0 20000-3 0 9056
2 25544 51
6404 178
1879 0010094 353
4327 6
6702 15
72678206 34602
Satellite: ISS
Catalog Number: 25544
Epoch time: 08207
73297214 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 178
1879 deg
Eccentricity:
0010094
Arg of perigee: 353
4327 deg
Mean anomaly: 6
6702 deg
Mean motion: 15
72678206 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3460
Checksum: 290
Coasting Arc #7 (Orbit 3475)
---------------------------------------
Vector Time (GMT): 2008/208/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5305467
92 A = 6730533
57 meter
Y = -2108299
33 meter E =
0015150
Z = 3545642
27 I = 51
68600
XDOT = 4661
948907 Wp = 50
93380
YDOT = -4200
007568 meter/sec RA = 172
28343 deg
ZDOT = 4475
105208 TA = 351
31956
MA = 351
34573
Ha = 194
438 n
mi
Hp = 184
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17406390
81 X = -5298722
35
Y = -6916992
55 feet Y = -2167590
85 meter
Z = 11632684
61 Z = 3519884
42
XDOT = 15295
107962 XDOT = 4686
828325
YDOT = -13779
552390 feet/sec YDOT = -4147
736434 meter/sec
ZDOT = 14682
103700 ZDOT = 4497
812861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18611054
51 X = 5672649
41
Y = 2600645
71 feet Y = 792676
81 meter
Z = 11533077
22 Z = 3515281
94
XDOT = -11342
097211 XDOT = -3457
071230
YDOT = 15621
281854 feet/sec YDOT = 4761
366709 meter/sec
ZDOT = 14769
318099 ZDOT = 4501
688157
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 08208
74965154
00020000 00000-0 20000-3 0 9064
2 25544 51
6408 172
9764 0010170 357
1875 2
9228 15
72690651 34762
Satellite: ISS
Catalog Number: 25544
Epoch time: 08208
74965154 = yrday
fracday
Element set: 906
Inclination: 51
6408 deg
RA of node: 172
9764 deg
Eccentricity:
0010170
Arg of perigee: 357
1875 deg
Mean anomaly: 2
9228 deg
Mean motion: 15
72690651 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3476
Checksum: 308
Coasting Arc #8 (Orbit 3490)
---------------------------------------
Vector Time (GMT): 2008/209/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3272911
45 A = 6728170
66 meter
Y = 4134715
29 meter E =
0010620
Z = -4180280
57 I = 51
70756
XDOT = -6583
898675 Wp = 46
27819
YDOT = -1487
461418 meter/sec RA = 167
11127 deg
ZDOT = 3696
563921 TA = 261
39627
MA = 261
51661
Ha = 194
367 n
mi
Hp = 184
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10737898
47 X = -3298596
26
Y = 13565338
87 feet Y = 4097972
73 meter
Z = -13714831
28 Z = -4196242
10
XDOT = -21600
717439 XDOT = -6584
733505
YDOT = -4880
122763 feet/sec YDOT = -1561
091580 meter/sec
ZDOT = 12127
834385 ZDOT = 3664
577165
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6888004
37 X = 2099463
73
Y = -15817517
78 feet Y = -4821179
42 meter
Z = -13776030
14 Z = -4198933
99
XDOT = 21046
247291 XDOT = 6414
896174
YDOT = -1252
957279 feet/sec YDOT = -381
901379 meter/sec
ZDOT = 12004
236797 ZDOT = 3658
891376
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 08209
70277809
00020000 00000-0 20000-3 0 9075
2 25544 51
6409 168
0912 0010208 359
8659
2499 15
72717185 34915
Satellite: ISS
Catalog Number: 25544
Epoch time: 08209
70277809 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 168
0912 deg
Eccentricity:
0010208
Arg of perigee: 359
8659 deg
Mean anomaly:
2499 deg
Mean motion: 15
72717185 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3491
Checksum: 312
Coasting Arc #9 (Orbit 3506)
---------------------------------------
Vector Time (GMT): 2008/210/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6057675
47 A = 6732244
04 meter
Y = 453558
77 meter E =
0009349
Z = -2916611
46 I = 51
74925
XDOT = -2806
359470 Wp = 30
35542
YDOT = 5084
153521 meter/sec RA = 162
04027 deg
ZDOT = -5037
160094 TA = 183
09080
MA = 183
09658
Ha = 194
479 n
mi
Hp = 184
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19874263
36 X = 6066321
75
Y = 1488053
70 feet Y = 521348
00 meter
Z = -9568935
23 Z = -2887162
41
XDOT = -9207
216110 XDOT = -2838
533287
YDOT = 16680
293705 feet/sec YDOT = 5052
592151 meter/sec
ZDOT = -16526
115795 ZDOT = -5050
870584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19593712
28 X = -5972163
50
Y = 3930709
91 feet Y = 1198080
38 meter
Z = -9455216
98 Z = -2881950
13
XDOT = 4573
494275 XDOT = 1394
001055
YDOT = -17088
552272 feet/sec YDOT = -5208
590732 meter/sec
ZDOT = -16578
544915 ZDOT = -5053
140490
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 08210
71943690
00020000 00000-0 20000-3 0 9087
2 25544 51
6410 162
8798 0010109 3
0608 357
0615 15
72712071 35073
Satellite: ISS
Catalog Number: 25544
Epoch time: 08210
71943690 = yrday
fracday
Element set: 908
Inclination: 51
6410 deg
RA of node: 162
8798 deg
Eccentricity:
0010109
Arg of perigee: 3
0608 deg
Mean anomaly: 357
0615 deg
Mean motion: 15
72712071 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3507
Checksum: 272
Coasting Arc #10 (Orbit 3522)
---------------------------------------
Vector Time (GMT): 2008/211/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1597843
42 A = 6726350
35 meter
Y = -4631221
97 meter E =
0016289
Z = 4608069
12 I = 51
75811
XDOT = 7094
251561 Wp = 32
35181
YDOT = -503
434098 meter/sec RA = 156
87643 deg
ZDOT = -2947
612530 TA = 86
91659
MA = 86
73021
Ha = 194
493 n
mi
Hp = 184
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5242268
42 X = 1627126
87
Y = -15194297
79 feet Y = -4613191
01 meter
Z = 15118337
00 Z = 4615901
68
XDOT = 23275
103548 XDOT = 7113
672548
YDOT = -1651
686673 feet/sec YDOT = -423
993019 meter/sec
ZDOT = -9670
644784 ZDOT = -2913
102047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -600270
12 X = -182962
33
Y = 16033904
61 feet Y = 4887134
12 meter
Z = 15148127
14 Z = 4617149
15
XDOT = -20716
657393 XDOT = -6314
437173
YDOT = 8291
528821 feet/sec YDOT = 2527
257985 meter/sec
ZDOT = -9537
461529 ZDOT = -2907
018274
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 08211
73608345
00020000 00000-0 20000-3 0 9096
2 25544 51
6413 157
6682 0010303 6
7896 353
3404 15
72796145 35232
Satellite: ISS
Catalog Number: 25544
Epoch time: 08211
73608345 = yrday
fracday
Element set: 909
Inclination: 51
6413 deg
RA of node: 157
6682 deg
Eccentricity:
0010303
Arg of perigee: 6
7896 deg
Mean anomaly: 353
3404 deg
Mean motion: 15
72796145 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3523
Checksum: 290
Coasting Arc #11 (Orbit 3538)
---------------------------------------
Vector Time (GMT): 2008/212/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6200676
95 A = 6733652
69 meter
Y = 1350144
08 meter E =
0021125
Z = 2211911
22 I = 51
80848
XDOT = 805
392830 Wp = 46
15494
YDOT = -5341
291124 meter/sec RA = 151
80165 deg
ZDOT = 5500
058998 TA = 338
60218
MA = 338
69037
Ha = 194
755 n
mi
Hp = 184
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20343428
33 X = -6226058
48
Y = 4429606
57 feet Y = 1280662
29 meter
Z = 7256926
56 Z = 2181727
49
XDOT = 2642
364928 XDOT = 838
342396
YDOT = -17523
921010 feet/sec YDOT = -5332
101377 meter/sec
ZDOT = 18044
812985 ZDOT = 5504
050726
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18093718
90 X = 5514965
52
Y = -10381228
17 feet Y = -3164198
35 meter
Z = 7140511
99 Z = 2176428
05
XDOT = 2116
756179 XDOT = 645
187283
YDOT = 16152
665493 feet/sec YDOT = 4923
332442 meter/sec
ZDOT = 18059
707829 ZDOT = 5504
598946
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 08212
75272193
00020000 00000-0 20000-3 0 9109
2 25544 51
6412 152
4564 0010309 10
6998 349
4382 15
72762912 35399
Satellite: ISS
Catalog Number: 25544
Epoch time: 08212
75272193 = yrday
fracday
Element set: 910
Inclination: 51
6412 deg
RA of node: 152
4564 deg
Eccentricity:
0010309
Arg of perigee: 10
6998 deg
Mean anomaly: 349
4382 deg
Mean motion: 15
72762912 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3539
Checksum: 290
Coasting Arc #12 (Orbit 3553)
---------------------------------------
Vector Time (GMT): 2008/213/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 177474
91 A = 6724960
48 meter
Y = 4552377
59 meter E =
0016182
Z = -4957282
37 I = 51
80482
XDOT = -6932
381272 Wp = 66
44559
YDOT = 2565
732515 meter/sec RA = 146
65064 deg
ZDOT = 2119
740212 TA = 224
02277
MA = 224
15175
Ha = 194
713 n
mi
Hp = 183
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 582266
78 X = 150637
30
Y = 14935622
01 feet Y = 4554212
79 meter
Z = -16264049
77 Z = -4956484
82
XDOT = -22744
033045 XDOT = -6970
853534
YDOT = 8417
757594 feet/sec YDOT = 2487
995266 meter/sec
ZDOT = 6954
528254 ZDOT = 2085
970413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5396628
37 X = -1644892
33
Y = -13942842
06 feet Y = -4249778
26 meter
Z = -16260526
19 Z = -4956208
38
XDOT = 17899
564802 XDOT = 5455
787352
YDOT = -14841
858066 feet/sec YDOT = -4523
798338 meter/sec
ZDOT = 6824
368749 ZDOT = 2080
067595
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 08213
70580894
00020000 00000-0 20000-3 0 9116
2 25544 51
6411 147
5705 0010243 13
9295 346
2148 15
72794951 35543
Satellite: ISS
Catalog Number: 25544
Epoch time: 08213
70580894 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 147
5705 deg
Eccentricity:
0010243
Arg of perigee: 13
9295 deg
Mean anomaly: 346
2148 deg
Mean motion: 15
72794951 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3554
Checksum: 291
Coasting Arc #13 (Orbit 3569)
---------------------------------------
Vector Time (GMT): 2008/214/16:38:36
255
Vector Time (MET): N/A
Weight (LBS) : 661018
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5796379
19 A = 6734720
43 meter
Y = -3086690
83 meter E =
0008652
Z = -1508972
23 I = 51
86114
XDOT = 1119
003005 Wp = 70
44511
YDOT = 4924
343514 meter/sec RA = 141
56940 deg
ZDOT = -5798
650008 TA = 126
09758
MA = 126
01744
Ha = 194
789 n
mi
Hp = 183
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19016992
10 X = 5837794
39
Y = -10126938
43 feet Y = -3021640
68 meter
Z = -4950696
28 Z = -1480713
85
XDOT = 3671
269702 XDOT = 1092
023103
YDOT = 16155
982658 feet/sec YDOT = 4936
706555 meter/sec
ZDOT = -19024
442285 ZDOT = -5793
279091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14556536
99 X = -4436832
48
Y = 15917722
04 feet Y = 4851721
68 meter
Z = -4841861
21 Z = -1475799
30
XDOT = -7809
054526 XDOT = -2380
199819
YDOT = -12897
173603 feet/sec YDOT = -3931
058514 meter/sec
ZDOT = -19003
215973 ZDOT = -5792
180229
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 08214
72242575
00020000 00000-0 20000-3 0 9121
2 25544 51
6412 142
3597 0010111 17
6328 342
5184 15
72772564 35701
Satellite: ISS
Catalog Number: 25544
Epoch time: 08214
72242575 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 142
3597 deg
Eccentricity:
0010111
Arg of perigee: 17
6328 deg
Mean anomaly: 342
5184 deg
Mean motion: 15
72772564 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3570
Checksum: 274
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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