Date:
August 9th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 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
230/20:37:31
477 1
7 4
0 4
0
N/A -2
9 -0
0 191
9
000/00:10:58
953 2
2 0
3 191
4
Coasting Arc #1 (Orbit 3107)
---------------------------------------
Vector Time (GMT): 2010/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6555221
90 A = 6738891
21 meter
Y = -1206682
88 meter E =
0010625
Z = 981940
12 I = 51
56606
XDOT = 9
471319 Wp = 87
94988
YDOT = 4912
932162 meter/sec RA = 342
85618 deg
ZDOT = 5919
478201 TA = 282
77316
MA = 282
89188
Ha = 195
252 n
mi
Hp = 187
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21506633
54 X = 6563457
99
Y = -3958933
32 feet Y = -1133332
51 meter
Z = 3221588
33 Z = 1013805
14
XDOT = 31
073880 XDOT = -74
222305
YDOT = 16118
543838 feet/sec YDOT = 4912
569571 meter/sec
ZDOT = 19420
860241 ZDOT = 5919
321378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17358746
35 X = -5290945
89
Y = -13268201
38 feet Y = -4044147
78 meter
Z = 3349004
01 Z = 1020776
42
XDOT = 11035
962336 XDOT = 3363
761320
YDOT = -9492
943340 feet/sec YDOT = -2893
449130 meter/sec
ZDOT = 19420
179222 ZDOT = 5919
270627
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 10216
56162348
00016717 00000-0 10270-3 0 9002
2 25544 51
6463 343
0501 0007409 186
1183 173
9890 15
71485243 31080
Satellite: ISS
Catalog Number: 25544
Epoch time: 10216
56162348 = yrday
fracday
Element set: 900
Inclination: 51
6463 deg
RA of node: 343
0501 deg
Eccentricity:
0007409
Arg of perigee: 186
1183 deg
Mean anomaly: 173
9890 deg
Mean motion: 15
71485243 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3108
Checksum: 296
Coasting Arc #2 (Orbit 3122)
---------------------------------------
Vector Time (GMT): 2010/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1362219
49 A = 6727205
77 meter
Y = -3971039
13 meter E =
0015730
Z = -5268565
08 I = 51
49845
XDOT = 7173
081090 Wp = 118
75312
YDOT = -2754
390260 meter/sec RA = 337
72153 deg
ZDOT = 214
454534 TA = 153
33041
MA = 153
24942
Ha = 195
018 n
mi
Hp = 187
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4469224
03 X = -1292119
82
Y = -13028343
60 feet Y = -3985879
77 meter
Z = -17285318
51 Z = -5275012
85
XDOT = 23533
730610 XDOT = 7202
306292
YDOT = -9036
713450 feet/sec YDOT = -2674
013195 meter/sec
ZDOT = 703
590990 ZDOT = 249
371786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6518136
42 X = -1986727
98
Y = 12096909
30 feet Y = 3687137
95 meter
Z = -17311054
83 Z = -5276409
51
XDOT = -21803
314005 XDOT = -6645
650109
YDOT = -10508
939141 feet/sec YDOT = -3203
124650 meter/sec
ZDOT = 843
229522 ZDOT = 257
016358
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 10217
51549047
00016717 00000-0 10270-3 0 9014
2 25544 51
6464 338
1712 0007245 190
0358 170
0661 15
71518891 31233
Satellite: ISS
Catalog Number: 25544
Epoch time: 10217
51549047 = yrday
fracday
Element set: 901
Inclination: 51
6464 deg
RA of node: 338
1712 deg
Eccentricity:
0007245
Arg of perigee: 190
0358 deg
Mean anomaly: 170
0661 deg
Mean motion: 15
71518891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3123
Checksum: 291
Coasting Arc #3 (Orbit 3138)
---------------------------------------
Vector Time (GMT): 2010/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5709343
94 A = 6739108
41 meter
Y = 3507070
64 meter E =
0017558
Z = 610213
46 I = 51
51117
XDOT = -2988
850372 Wp = 150
66609
YDOT = -3813
757427 meter/sec RA = 332
59142 deg
ZDOT = -5988
440188 TA = 22
68009
MA = 22
60260
Ha = 194
886 n
mi
Hp = 187
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18731443
37 X = -5751100
58
Y = 11506137
27 feet Y = 3442991
80 meter
Z = 2002012
67 Z = 582376
78
XDOT = -9805
939541 XDOT = -2916
891703
YDOT = -12512
327516 feet/sec YDOT = -3846
777521 meter/sec
ZDOT = -19647
113478 ZDOT = -6002
785490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21310128
45 X = 6495327
15
Y = 5437830
30 feet Y = 1657450
68 meter
Z = 1890673
77 Z = 576277
37
XDOT = -1835
578842 XDOT = -559
484431
YDOT = 14113
744119 feet/sec YDOT = 4301
869208 meter/sec
ZDOT = -19704
431260 ZDOT = -6005
910648
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 10218
53293198
00016717 00000-0 10270-3 0 9021
2 25544 51
6466 332
9655 0007278 194
2584 165
8373 15
71519317 31399
Satellite: ISS
Catalog Number: 25544
Epoch time: 10218
53293198 = yrday
fracday
Element set: 902
Inclination: 51
6466 deg
RA of node: 332
9655 deg
Eccentricity:
0007278
Arg of perigee: 194
2584 deg
Mean anomaly: 165
8373 deg
Mean motion: 15
71519317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3139
Checksum: 334
Coasting Arc #4 (Orbit 3154)
---------------------------------------
Vector Time (GMT): 2010/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3685008
23 A = 6727802
58 meter
Y = 2443731
46 meter E =
0009769
Z = 5071509
05 I = 51
44840
XDOT = -5571
795419 Wp = 169
77549
YDOT = 5063
092779 meter/sec RA = 327
48253 deg
ZDOT = 1598
910939 TA = 264
76365
MA = 264
87513
Ha = 194
539 n
mi
Hp = 187
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12089922
00 X = 3632772
06
Y = 8017491
68 feet Y = 2484646
82 meter
Z = 16638809
22 Z = 5089283
89
XDOT = -18280
168697 XDOT = -5635
764823
YDOT = 16611
196780 feet/sec YDOT = 5000
427789 meter/sec
ZDOT = 5245
770797 ZDOT = 1571
688792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2840308
51 X = -865726
03
Y = -14142475
55 feet Y = -4310626
55 meter
Z = 16709859
14 Z = 5093165
07
XDOT = 23665
060402 XDOT = 7213
110411
YDOT = 1354
971730 feet/sec YDOT = 412
995383 meter/sec
ZDOT = 5136
873026 ZDOT = 1565
718898
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 10219
55035475
00016717 00000-0 10270-3 0 9037
2 25544 51
6475 327
7603 0007167 198
8154 161
2744 15
71585938 31556
Satellite: ISS
Catalog Number: 25544
Epoch time: 10219
55035475 = yrday
fracday
Element set: 903
Inclination: 51
6475 deg
RA of node: 327
7603 deg
Eccentricity:
0007167
Arg of perigee: 198
8154 deg
Mean anomaly: 161
2744 deg
Mean motion: 15
71585938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3155
Checksum: 327
Coasting Arc #5 (Orbit 3169)
---------------------------------------
Vector Time (GMT): 2010/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3834254
06 A = 6737213
46 meter
Y = -5112678
99 meter E =
0002177
Z = -2137196
03 I = 51
45489
XDOT = 5145
222259 Wp = 135
93448
YDOT = 1561
094751 meter/sec RA = 322
32074 deg
ZDOT = 5498
137650 TA = 200
14234
MA = 200
15093
Ha = 194
469 n
mi
Hp = 188
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12579573
69 X = 3901521
88
Y = -16773881
19 feet Y = -5069425
76 meter
Z = -7011797
99 Z = -2118406
69
XDOT = 16880
650455 XDOT = 5100
675050
YDOT = 5121
701940 feet/sec YDOT = 1618
382150 meter/sec
ZDOT = 18038
509349 ZDOT = 5523
024513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20724564
59 X = -6316847
29
Y = 3339124
96 feet Y = 1017765
29 meter
Z = -6936623
26 Z = -2114282
77
XDOT = -8293
735218 XDOT = -2527
930494
YDOT = -13808
802832 feet/sec YDOT = -4208
923103 meter/sec
ZDOT = 18138
011170 ZDOT = 5528
465805
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 10220
50417554
00016717 00000-0 10270-3 0 9047
2 25544 51
6476 322
8809 0006940 203
0259 157
0593 15
71550694 31707
Satellite: ISS
Catalog Number: 25544
Epoch time: 10220
50417554 = yrday
fracday
Element set: 904
Inclination: 51
6476 deg
RA of node: 322
8809 deg
Eccentricity:
0006940
Arg of perigee: 203
0259 deg
Mean anomaly: 157
0593 deg
Mean motion: 15
71550694 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3170
Checksum: 298
Coasting Arc #6 (Orbit 3185)
---------------------------------------
Vector Time (GMT): 2010/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5049457
64 A = 6730345
43 meter
Y = -167130
34 meter E =
0006631
Z = -4450235
31 I = 51
40899
XDOT = 3033
606269 Wp = 115
52921
YDOT = -6297
797669 meter/sec RA = 317
23199 deg
ZDOT = -3212
095435 TA = 122
21387
MA = 122
14956
Ha = 194
222 n
mi
Hp = 188
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16566462
08 X = -5025595
58
Y = -548327
87 feet Y = -223462
72 meter
Z = -14600509
55 Z = -4474707
01
XDOT = 9952
776472 XDOT = 3119
407317
YDOT = -20662
065842 feet/sec YDOT = -6263
394148 meter/sec
ZDOT = -10538
370849 ZDOT = -3197
150496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11697749
32 X = 3565473
99
Y = 11620840
20 feet Y = 3542032
09 meter
Z = -14698365
30 Z = -4480061
74
XDOT = -20554
894680 XDOT = -6265
131898
YDOT = 7464
266789 feet/sec YDOT = 2275
108517 meter/sec
ZDOT = -10478
568697 ZDOT = -3193
867739
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 10221
52156698
00016717 00000-0 10270-3 0 9050
2 25544 51
6475 317
6760 0007055 206
6376 153
4424 15
71588981 31861
Satellite: ISS
Catalog Number: 25544
Epoch time: 10221
52156698 = yrday
fracday
Element set: 905
Inclination: 51
6475 deg
RA of node: 317
6760 deg
Eccentricity:
0007055
Arg of perigee: 206
6376 deg
Mean anomaly: 153
4424 deg
Mean motion: 15
71588981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3186
Checksum: 325
Coasting Arc #7 (Orbit 3201)
---------------------------------------
Vector Time (GMT): 2010/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1385835
50 A = 6733882
43 meter
Y = 5620500
54 meter E =
0010798
Z = 3426513
33 I = 51
39923
XDOT = -6068
647091 Wp = 122
32309
YDOT = 1288
744732 meter/sec RA = 312
04999 deg
ZDOT = -4563
588279 TA = 17
00109
MA = 16
96494
Ha = 194
100 n
mi
Hp = 188
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4546704
38 X = -1465226
94
Y = 18439962
42 feet Y = 5604559
32 meter
Z = 11241841
63 Z = 3419588
40
XDOT = -19910
259485 XDOT = -6060
438494
YDOT = 4228
165132 feet/sec YDOT = 1220
927497 meter/sec
ZDOT = -14972
402489 ZDOT = -4593
049073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15752074
72 X = 4801232
38
Y = -10639515
34 feet Y = -3242924
28 meter
Z = 11214124
71 Z = 3418065
21
XDOT = 16797
516940 XDOT = 5119
883163
YDOT = 8947
427140 feet/sec YDOT = 2727
175792 meter/sec
ZDOT = -15090
215726 ZDOT = -4599
497753
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 10222
53894201
00016717 00000-0 10270-3 0 9062
2 25544 51
6472 312
4711 0006841 209
6304 150
4471 15
71621294 32026
Satellite: ISS
Catalog Number: 25544
Epoch time: 10222
53894201 = yrday
fracday
Element set: 906
Inclination: 51
6472 deg
RA of node: 312
4711 deg
Eccentricity:
0006841
Arg of perigee: 209
6304 deg
Mean anomaly: 150
4471 deg
Mean motion: 15
71621294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3202
Checksum: 272
Coasting Arc #8 (Orbit 3217)
---------------------------------------
Vector Time (GMT): 2010/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5258531
84 A = 6733565
02 meter
Y = -2405631
36 meter E =
0010391
Z = 3448493
13 I = 51
37924
XDOT = -141
838772 Wp = 125
19020
YDOT = 6214
171785 meter/sec RA = 306
96578 deg
ZDOT = 4535
695094 TA = 275
77227
MA = 275
89073
Ha = 193
831 n
mi
Hp = 188
378
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17252401
04 X = 5268289
41
Y = -7892491
34 feet Y = -2346772
75 meter
Z = 11313953
83 Z = 3474062
24
XDOT = -465
350303 XDOT = -233
349365
YDOT = 20387
702708 feet/sec YDOT = 6212
073998 meter/sec
ZDOT = 14880
889416 ZDOT = 4534
783779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18153701
26 X = -5533248
14
Y = -5296764
92 feet Y = -1614453
95 meter
Z = 11416204
47 Z = 3479659
12
XDOT = 13389
607916 XDOT = 4081
152493
YDOT = -13716
483156 feet/sec YDOT = -4180
784066 meter/sec
ZDOT = 14877
227746 ZDOT = 4534
579017
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 10223
55629826
00016717 00000-0 10270-3 0 9075
2 25544 51
6470 307
2651 0006858 214
5371 145
5346 15
71672187 32186
Satellite: ISS
Catalog Number: 25544
Epoch time: 10223
55629826 = yrday
fracday
Element set: 907
Inclination: 51
6470 deg
RA of node: 307
2651 deg
Eccentricity:
0006858
Arg of perigee: 214
5371 deg
Mean anomaly: 145
5346 deg
Mean motion: 15
71672187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3218
Checksum: 315
Coasting Arc #9 (Orbit 3232)
---------------------------------------
Vector Time (GMT): 2010/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1073026
93 A = 6730245
64 meter
Y = -4972644
39 meter E =
0009773
Z = -4415375
93 I = 51
35008
XDOT = 5617
670131 Wp = 151
29603
YDOT = -4113
739314 meter/sec RA = 301
78011 deg
ZDOT = 3262
278118 TA = 151
63600
MA = 151
58277
Ha = 193
628 n
mi
Hp = 188
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3520429
56 X = -995893
39
Y = -16314450
09 feet Y = -4984212
39 meter
Z = -14486141
50 Z = -4420401
20
XDOT = 18430
676282 XDOT = 5647
405885
YDOT = -13496
520058 feet/sec YDOT = -4050
752865 meter/sec
ZDOT = 10703
012199 ZDOT = 3289
640611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7842355
86 X = -2390350
07
Y = 14712912
35 feet Y = 4484495
68 meter
Z = -14506228
54 Z = -4421498
46
XDOT = -21673
545465 XDOT = -6606
096658
YDOT = -874
402969 feet/sec YDOT = -266
518025 meter/sec
ZDOT = 10812
430366 ZDOT = 3295
628776
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 10224
51005655
00016717 00000-0 10270-3 0 9081
2 25544 51
6461 302
3855 0006695 217
9734 142
0957 15
71707417 32339
Satellite: ISS
Catalog Number: 25544
Epoch time: 10224
51005655 = yrday
fracday
Element set: 908
Inclination: 51
6461 deg
RA of node: 302
3855 deg
Eccentricity:
0006695
Arg of perigee: 217
9734 deg
Mean anomaly: 142
0957 deg
Mean motion: 15
71707417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3233
Checksum: 304
Coasting Arc #10 (Orbit 3248)
---------------------------------------
Vector Time (GMT): 2010/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4322605
82 A = 6736570
69 meter
Y = 4660833
90 meter E =
0009310
Z = -2212526
67 I = 51
35552
XDOT = -2443
342661 Wp = 181
98501
YDOT = -4851
743741 meter/sec RA = 296
68536 deg
ZDOT = -5455
448291 TA = 22
90472
MA = 22
86323
Ha = 193
378 n
mi
Hp = 188
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14181777
64 X = -4363654
91
Y = 15291449
81 feet Y = 4612266
40 meter
Z = -7258945
78 Z = -2233625
42
XDOT = -8016
216079 XDOT = -2362
406665
YDOT = -15917
794426 feet/sec YDOT = -4878
614165 meter/sec
ZDOT = -17898
452397 ZDOT = -5467
121301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20608750
55 X = 6281547
17
Y = -2999786
19 feet Y = -914334
83 meter
Z = -7343312
02 Z = -2238241
50
XDOT = -4077
499903 XDOT = -1242
821970
YDOT = 15848
642156 feet/sec YDOT = 4830
666129 meter/sec
ZDOT = -17945
124854 ZDOT = -5469
674055
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 10225
52738254
00016717 00000-0 10270-3 0 9092
2 25544 51
6451 297
1793 0006650 222
4217 137
6432 15
71694687 32497
Satellite: ISS
Catalog Number: 25544
Epoch time: 10225
52738254 = yrday
fracday
Element set: 909
Inclination: 51
6451 deg
RA of node: 297
1793 deg
Eccentricity:
0006650
Arg of perigee: 222
4217 deg
Mean anomaly: 137
6432 deg
Mean motion: 15
71694687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3249
Checksum: 323
Coasting Arc #11 (Orbit 3264)
---------------------------------------
Vector Time (GMT): 2010/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3030489
99 A = 6727508
10 meter
Y = 3287998
27 meter E =
0001506
Z = 5026525
98 I = 51
31357
XDOT = -3997
982539 Wp = 202
73312
YDOT = 6343
091362 meter/sec RA = 291
51108 deg
ZDOT = -1740
364264 TA = 264
09590
MA = 264
11307
Ha = 193
038 n
mi
Hp = 188
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9942552
46 X = 2969079
96
Y = 10787395
90 feet Y = 3321543
63 meter
Z = 16491226
98 Z = 5041098
86
XDOT = -13116
740613 XDOT = -4060
160687
YDOT = 20810
667198 feet/sec YDOT = 6298
035882 meter/sec
ZDOT = -5709
856508 ZDOT = -1759
937327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1122203
12 X = -342047
51
Y = -14561512
24 feet Y = -4438348
93 meter
Z = 16549496
93 Z = 5044286
66
XDOT = 22056
116597 XDOT = 6722
704339
YDOT = -8272
380907 feet/sec YDOT = -2521
421701 meter/sec
ZDOT = -5788
118439 ZDOT = -1764
218500
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 10226
54468971
00016717 00000-0 10270-3 0 9103
2 25544 51
6456 291
9728 0006659 228
1009 131
9585 15
71762199 32651
Satellite: ISS
Catalog Number: 25544
Epoch time: 10226
54468971 = yrday
fracday
Element set: 910
Inclination: 51
6456 deg
RA of node: 291
9728 deg
Eccentricity:
0006659
Arg of perigee: 228
1009 deg
Mean anomaly: 131
9585 deg
Mean motion: 15
71762199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3265
Checksum: 338
Coasting Arc #12 (Orbit 3280)
---------------------------------------
Vector Time (GMT): 2010/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2503872
21 A = 6738375
23 meter
Y = -6198854
78 meter E =
0007220
Z = 815781
91 I = 51
33902
XDOT = 4217
532270 Wp = 55
57188
YDOT = 2489
070072 meter/sec RA = 286
39271 deg
ZDOT = 5935
442073 TA = 313
35178
MA = 313
41192
Ha = 192
993 n
mi
Hp = 189
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8214803
85 X = 2569039
95
Y = -20337450
06 feet Y = -6170490
63 meter
Z = 2676449
83 Z = 828103
80
XDOT = 13837
048131 XDOT = 4160
552409
YDOT = 8166
240393 feet/sec YDOT = 2535
914307 meter/sec
ZDOT = 19473
235146 ZDOT = 5955
792403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18785216
60 X = -5725734
02
Y = 11311249
77 feet Y = 3447668
93 meter
Z = 2725715
86 Z = 830798
19
XDOT = -5221
234965 XDOT = -1591
432417
YDOT = -13409
222744 feet/sec YDOT = -4087
131092 meter/sec
ZDOT = 19554
607945 ZDOT = 5960
244502
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 10227
56198485
00016717 00000-0 10270-3 0 9117
2 25544 51
6449 286
7662 0006320 231
9411 128
1181 15
71719758 32817
Satellite: ISS
Catalog Number: 25544
Epoch time: 10227
56198485 = yrday
fracday
Element set: 911
Inclination: 51
6449 deg
RA of node: 286
7662 deg
Eccentricity:
0006320
Arg of perigee: 231
9411 deg
Mean anomaly: 128
1181 deg
Mean motion: 15
71719758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3281
Checksum: 318
Coasting Arc #13 (Orbit 3295)
---------------------------------------
Vector Time (GMT): 2010/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4100800
47 A = 6726506
34 meter
Y = -961776
76 meter E =
0010492
Z = -5252929
91 I = 51
29185
XDOT = 1597
956245 Wp = 111
71602
YDOT = -7521
469601 meter/sec RA = 281
24170 deg
ZDOT = 126
032231 TA = 159
50842
MA = 159
46631
Ha = 192
718 n
mi
Hp = 188
986
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13454069
79 X = -4064223
28
Y = -3155435
55 feet Y = -1007429
63 meter
Z = -17234022
00 Z = -5272762
69
XDOT = 5242
638600 XDOT = 1681
331693
YDOT = -24676
737535 feet/sec YDOT = -7503
134126 meter/sec
ZDOT = 413
491572 ZDOT = 133
997273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8945932
82 X = 2726720
32
Y = 10401887
07 feet Y = 3170495
18 meter
Z = -17313327
62 Z = -5277102
26
XDOT = -17986
722513 XDOT = -5482
353022
YDOT = 16230
047314 feet/sec YDOT = 4946
918421 meter/sec
ZDOT = 445
333308 ZDOT = 135
737592
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 10228
51568059
00016717 00000-0 10270-3 0 9122
2 25544 51
6447 281
8849 0006406 235
6738 124
3818 15
71756863 32965
Satellite: ISS
Catalog Number: 25544
Epoch time: 10228
51568059 = yrday
fracday
Element set: 912
Inclination: 51
6447 deg
RA of node: 281
8849 deg
Eccentricity:
0006406
Arg of perigee: 235
6738 deg
Mean anomaly: 124
3818 deg
Mean motion: 15
71756863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3296
Checksum: 341
Coasting Arc #14 (Orbit 3311)
---------------------------------------
Vector Time (GMT): 2010/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -238058
98 A = 6738228
06 meter
Y = 6699810
90 meter E =
0012429
Z = 593053
11 I = 51
32773
XDOT = -4846
305673 Wp = 156
49456
YDOT = 359
353958 meter/sec RA = 276
09500 deg
ZDOT = -5973
281055 TA = 17
02490
MA = 16
98324
Ha = 192
408 n
mi
Hp = 189
121
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -781033
39 X = -315840
72
Y = 21981006
88 feet Y = 6696713
85 meter
Z = 1945712
30 Z = 591708
05
XDOT = -15899
952996 XDOT = -4820
946943
YDOT = 1178
982803 feet/sec YDOT = 305
301773 meter/sec
ZDOT = -19597
378790 ZDOT = -5996
762619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13262797
14 X = 4042500
57
Y = -17546901
33 feet Y = -5348295
53 meter
Z = 1940344
98 Z = 591417
15
XDOT = 12322
817169 XDOT = 3755
994673
YDOT = 7125
154893 feet/sec YDOT = 2171
747211 meter/sec
ZDOT = -19691
277826 ZDOT = -6001
901481
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 10229
53294089
00016717 00000-0 10270-3 0 9135
2 25544 51
6452 276
6784 0006203 240
0338 120
0209 15
71823966 33127
Satellite: ISS
Catalog Number: 25544
Epoch time: 10229
53294089 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 276
6784 deg
Eccentricity:
0006203
Arg of perigee: 240
0338 deg
Mean anomaly: 120
0209 deg
Mean motion: 15
71823966 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3312
Checksum: 296
Coasting Arc #15 (Orbit 3327)
---------------------------------------
Vector Time (GMT): 2010/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4107692
69 A = 6726990
04 meter
Y = -1578009
18 meter E =
0005744
Z = 5090816
63 I = 51
28730
XDOT = 1049
371801 Wp = 197
49073
YDOT = 7480
937930 meter/sec RA = 270
97081 deg
ZDOT = 1467
184384 TA = 238
33824
MA = 238
39428
Ha = 192
206 n
mi
Hp = 189
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13476682
04 X = 4100302
98
Y = -5177195
46 feet Y = -1532116
11 meter
Z = 16702154
29 Z = 5110753
54
XDOT = 3442
820868 XDOT = 958
513352
YDOT = 24543
759612 feet/sec YDOT = 7492
164531 meter/sec
ZDOT = 4813
597060 ZDOT = 1472
061921
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13983334
14 X = -4262120
25
Y = -3197049
16 feet Y = -974460
59 meter
Z = 16781880
48 Z = 5115117
17
XDOT = 10674
006796 XDOT = 3253
437272
YDOT = -21231
051842 feet/sec YDOT = -6471
224601 meter/sec
ZDOT = 4833
122801 ZDOT = 1473
135830
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 10230
55018507
00016717 00000-0 10270-3 0 9149
2 25544 51
6445 271
4718 0006168 243
4603 116
5927 15
71837210 33282
Satellite: ISS
Catalog Number: 25544
Epoch time: 10230
55018507 = yrday
fracday
Element set: 914
Inclination: 51
6445 deg
RA of node: 271
4718 deg
Eccentricity:
0006168
Arg of perigee: 243
4603 deg
Mean anomaly: 116
5927 deg
Mean motion: 15
71837210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3328
Checksum: 295
Coasting Arc #16 (Orbit 3332)
---------------------------------------
Vector Time (GMT): 2010/230/20:43:00
953
Vector Time (MET): N/A
Weight (LBS) : 828329
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2040512
06 A = 6737979
53 meter
Y = -5941206
67 meter E =
0005310
Z = -2427755
78 I = 51
31775
XDOT = 4207
226700 Wp = 310
64649
YDOT = -3623
723300 meter/sec RA = 269
06954 deg
ZDOT = 5327
617897 TA = 21
85064
MA = 21
82800
Ha = 191
889 n
mi
Hp = 191
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6694593
37 X = -1962131
29
Y = -19492147
88 feet Y = -5963586
51 meter
Z = -7965078
01 Z = -2437478
43
XDOT = 13803
237206 XDOT = 4221
554862
YDOT = -11888
855970 feet/sec YDOT = -3576
595772 meter/sec
ZDOT = 17479
061342 ZDOT = 5348
090945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18524658
71 X = 5646315
98
Y = -8998733
75 feet Y = -2742814
05 meter
Z = -8003979
48 Z = -2439612
94
XDOT = 12829
707990 XDOT = 3910
494995
YDOT = 10779
124754 feet/sec YDOT = 3285
477225 meter/sec
ZDOT = 17560
926698 ZDOT = 5352
570458
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 10230
86807075
00016717 00000-0 10270-3 0 9150
2 25544 51
6455 269
8451 0008070 268
5125 91
5112 15
71058506 33336
Satellite: ISS
Catalog Number: 25544
Epoch time: 10230
86807075 = yrday
fracday
Element set: 915
Inclination: 51
6455 deg
RA of node: 269
8451 deg
Eccentricity:
0008070
Arg of perigee: 268
5125 deg
Mean anomaly: 91
5112 deg
Mean motion: 15
71058506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3333
Checksum: 300
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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