Date:
December 8th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14531 28 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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
There are no maneuvers
Coasting Arc #1 (Orbit 1058)
---------------------------------------
Vector Time (GMT): 2010/340/14:14:16
929
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2845686
28 A = 6735319
02 meter
Y = 6081944
45 meter E =
0014211
Z = -387128
04 I = 51
98201
XDOT = -4157
684331 Wp = 6
35490
YDOT = 2328
413659 meter/sec RA = 67
50890 deg
ZDOT = 6052
967499 TA = 349
45535
MA = 349
48512
Ha = 191
852 n
mi
Hp = 187
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9336241
09 X = 2779345
97
Y = 19953885
98 feet Y = 6113395
75 meter
Z = -1270105
11 Z = -373463
80
XDOT = -13640
696623 XDOT = -4212
816600
YDOT = 7639
152426 feet/sec YDOT = 2281
610784 meter/sec
ZDOT = 19858
817255 ZDOT = 6032
635679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16077632
79 X = -4900462
47
Y = 15065485
31 feet Y = 4591959
92 meter
Z = -1215321
69 Z = -370430
05
XDOT = -10427
807199 XDOT = -3178
395634
YDOT = -9542
600567 feet/sec YDOT = -2908
584653 meter/sec
ZDOT = 19776
975494 ZDOT = 6028
022131
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 10340
59396444
00016717 00000-0 10270-3 0 9009
2 25544 51
6459 68
1884 0008289 312
7697 47
2767 15
72876251 10591
Satellite: ISS
Catalog Number: 25544
Epoch time: 10340
59396444 = yrday
fracday
Element set: 900
Inclination: 51
6459 deg
RA of node: 68
1884 deg
Eccentricity:
0008289
Arg of perigee: 312
7697 deg
Mean anomaly: 47
2767 deg
Mean motion: 15
72876251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1059
Checksum: 344
Coasting Arc #2 (Orbit 1074)
---------------------------------------
Vector Time (GMT): 2010/341/14:14:16
929
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3219030
01 A = 6723307
33 meter
Y = -2716744
71 meter E =
0011668
Z = -5248740
34 I = 51
92973
XDOT = 4099
487644 Wp = 49
96408
YDOT = 6456
671384 meter/sec RA = 62
41446 deg
ZDOT = -821
631859 TA = 212
20237
MA = 212
27367
Ha = 191
856 n
mi
Hp = 187
115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10561122
09 X = 3274667
48
Y = -8913204
44 feet Y = -2680435
74 meter
Z = -17220276
69 Z = -5232967
44
XDOT = 13449
762613 XDOT = 4030
974615
YDOT = 21183
305064 feet/sec YDOT = 6502
131361 meter/sec
ZDOT = -2695
642581 ZDOT = -801
881927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11903964
75 X = 3628328
46
Y = 7173695
98 feet Y = 2186542
53 meter
Z = -17156752
36 Z = -5229378
12
XDOT = -15110
990761 XDOT = -4605
829984
YDOT = 18769
267056 feet/sec YDOT = 5720
872599 meter/sec
ZDOT = -2616
395698 ZDOT = -797
477409
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 10341
61047937
00016717 00000-0 10270-3 0 9014
2 25544 51
6461 62
9769 0008175 316
1481 43
9032 15
72949360 10759
Satellite: ISS
Catalog Number: 25544
Epoch time: 10341
61047937 = yrday
fracday
Element set: 901
Inclination: 51
6461 deg
RA of node: 62
9769 deg
Eccentricity:
0008175
Arg of perigee: 316
1481 deg
Mean anomaly: 43
9032 deg
Mean motion: 15
72949360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1075
Checksum: 307
Coasting Arc #3 (Orbit 1090)
---------------------------------------
Vector Time (GMT): 2010/342/14:14:16
929
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4245443
68 A = 6734486
18 meter
Y = -5123809
03 meter E =
0006329
Z = 1026728
88 I = 51
95323
XDOT = 3106
990247 Wp = 101
25282
YDOT = -3771
494144 meter/sec RA = 57
29150 deg
ZDOT = -5944
665058 TA = 67
58173
MA = 67
51470
Ha = 191
934 n
mi
Hp = 186
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13928621
00 X = -4192820
43
Y = -16810397
07 feet Y = -5170990
04 meter
Z = 3368533
08 Z = 1006231
62
XDOT = 10193
537555 XDOT = 3177
811033
YDOT = -12373
668451 feet/sec YDOT = -3736
353144 meter/sec
ZDOT = -19503
494284 ZDOT = -5929
399746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11019967
13 X = 3358885
98
Y = -18860113
89 feet Y = -5748562
71 meter
Z = 3286240
46 Z = 1001646
09
XDOT = 13780
617641 XDOT = 4200
332257
YDOT = 4647
096059 feet/sec YDOT = 1416
434879 meter/sec
ZDOT = -19441
973338 ZDOT = -5925
913474
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 10342
62696560
00016717 00000-0 10270-3 0 9029
2 25544 51
6463 57
7651 0008253 321
6083 38
4492 15
73034922 10916
Satellite: ISS
Catalog Number: 25544
Epoch time: 10342
62696560 = yrday
fracday
Element set: 902
Inclination: 51
6463 deg
RA of node: 57
7651 deg
Eccentricity:
0008253
Arg of perigee: 321
6083 deg
Mean anomaly: 38
4492 deg
Mean motion: 15
73034922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1091
Checksum: 299
Coasting Arc #4 (Orbit 1106)
---------------------------------------
Vector Time (GMT): 2010/343/14:14:16
929
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2144850
69 A = 6723503
86 meter
Y = 3789326
98 meter E =
0004112
Z = 5122898
48 I = 51
89837
XDOT = -5508
136533 Wp = 348
63935
YDOT = -5162
196999 meter/sec RA = 52
20574 deg
ZDOT = 1516
403242 TA = 86
89083
MA = 86
84378
Ha = 192
133 n
mi
Hp = 186
304
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7036911
70 X = -2211950
34
Y = 12432175
15 feet Y = 3764966
21 meter
Z = 16807409
72 Z = 5112316
25
XDOT = -18071
314085 XDOT = -5457
368912
YDOT = -16936
341860 feet/sec YDOT = -5223
508613 meter/sec
ZDOT = 4975
076253 ZDOT = 1489
767447
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14164812
20 X = -4317434
76
Y = -2206425
88 feet Y = -672518
61 meter
Z = 16764722
09 Z = 5109887
29
XDOT = 9162
296759 XDOT = 2792
668052
YDOT = -21935
394758 feet/sec YDOT = -6685
908322 meter/sec
ZDOT = 4868
091933 ZDOT = 1483
794421
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 10343
64342550
00016717 00000-0 10270-3 0 9030
2 25544 51
6456 52
5531 0008158 326
0476 34
0164 15
73058226 11076
Satellite: ISS
Catalog Number: 25544
Epoch time: 10343
64342550 = yrday
fracday
Element set: 903
Inclination: 51
6456 deg
RA of node: 52
5531 deg
Eccentricity:
0008158
Arg of perigee: 326
0476 deg
Mean anomaly: 34
0164 deg
Mean motion: 15
73058226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1107
Checksum: 280
Coasting Arc #5 (Orbit 1121)
---------------------------------------
Vector Time (GMT): 2010/344/14:14:16
929
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5288509
32 A = 6733625
90 meter
Y = 3828124
93 meter E =
0013542
Z = -1613746
42 I = 51
91394
XDOT = -1716
855963 Wp = 3
15273
YDOT = 4800
003240 meter/sec RA = 47
06895 deg
ZDOT = 5775
630455 TA = 339
09693
MA = 339
15225
Ha = 192
220 n
mi
Hp = 186
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17350752
35 X = 5253148
73
Y = 12559464
98 feet Y = 3887066
66 meter
Z = -5294443
63 Z = -1588140
39
XDOT = -5632
729538 XDOT = -1798
459833
YDOT = 15748
042127 feet/sec YDOT = 4780
347500 meter/sec
ZDOT = 18948
918816 ZDOT = 5767
092219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5137315
37 X = -1565853
72
Y = 20820076
76 feet Y = 6345959
40 meter
Z = -5191560
02 Z = -1582387
50
XDOT = -15236
197230 XDOT = -4643
992916
YDOT = 943
949206 feet/sec YDOT = 287
715718 meter/sec
ZDOT = 18914
418586 ZDOT = 5765
114785
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 10344
59633203
00016717 00000-0 10270-3 0 9044
2 25544 51
6463 47
6667 0008191 330
0545 30
0148 15
73108475 11225
Satellite: ISS
Catalog Number: 25544
Epoch time: 10344
59633203 = yrday
fracday
Element set: 904
Inclination: 51
6463 deg
RA of node: 47
6667 deg
Eccentricity:
0008191
Arg of perigee: 330
0545 deg
Mean anomaly: 30
0148 deg
Mean motion: 15
73108475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1122
Checksum: 283
Coasting Arc #6 (Orbit 1137)
---------------------------------------
Vector Time (GMT): 2010/345/14:14:16
929
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 828164
02 A = 6724057
08 meter
Y = -4485379
02 meter E =
0013859
Z = -4951377
19 I = 51
86065
XDOT = 6470
096255 Wp = 38
45462
YDOT = 3563
950706 meter/sec RA = 41
98958 deg
ZDOT = -2138
918195 TA = 210
79498
MA = 210
87636
Ha = 192
282 n
mi
Hp = 185
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2717073
56 X = 902311
71
Y = -14715810
43 feet Y = -4475703
02 meter
Z = -16244675
81 Z = -4947174
22
XDOT = 21227
349917 XDOT = 6440
153096
YDOT = 11692
751661 feet/sec YDOT = 3636
135965 meter/sec
ZDOT = -7017
448145 ZDOT = -2107
558912
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14647382
93 X = 4464522
32
Y = -3153645
87 feet Y = -961231
26 meter
Z = -16227623
01 Z = -4946179
49
XDOT = -2693
256379 XDOT = -820
904544
YDOT = 23077
413612 feet/sec YDOT = 7033
995669 meter/sec
ZDOT = -6891
414228 ZDOT = -2100
503057
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 10345
61273907
00016717 00000-0 10270-3 0 9050
2 25544 51
6465 42
4543 0008218 334
2060 25
8692 15
73127420 11385
Satellite: ISS
Catalog Number: 25544
Epoch time: 10345
61273907 = yrday
fracday
Element set: 905
Inclination: 51
6465 deg
RA of node: 42
4543 deg
Eccentricity:
0008218
Arg of perigee: 334
2060 deg
Mean anomaly: 25
8692 deg
Mean motion: 15
73127420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1138
Checksum: 289
Coasting Arc #7 (Orbit 1153)
---------------------------------------
Vector Time (GMT): 2010/346/14:14:16
929
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5934249
13 A = 6732631
94 meter
Y = -2380522
55 meter E =
0010612
Z = 2105452
83 I = 51
86529
XDOT = 158
215838 Wp = 74
39658
YDOT = -5327
181980 meter/sec RA = 36
84035 deg
ZDOT = -5551
362678 TA = 82
17261
MA = 82
05216
Ha = 192
409 n
mi
Hp = 185
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19469321
30 X = -5917416
57
Y = -7810113
36 feet Y = -2446788
92 meter
Z = 6907653
65 Z = 2076664
90
XDOT = 519
080833 XDOT = 244
741202
YDOT = -17477
631168 feet/sec YDOT = -5324
928550 meter/sec
ZDOT = -18213
132146 ZDOT = -5550
384254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -786273
35 X = -239656
12
Y = -21000464
40 feet Y = -6400941
55 meter
Z = 6791928
32 Z = 2070179
75
XDOT = 14695
653609 XDOT = 4479
235220
YDOT = -6467
251374 feet/sec YDOT = -1971
218219 meter/sec
ZDOT = -18209
020362 ZDOT = -5550
109406
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 10346
62911900
00016717 00000-0 10270-3 0 9065
2 25544 51
6453 37
2413 0008293 339
3624 20
7202 15
73186751 11546
Satellite: ISS
Catalog Number: 25544
Epoch time: 10346
62911900 = yrday
fracday
Element set: 906
Inclination: 51
6453 deg
RA of node: 37
2413 deg
Eccentricity:
0008293
Arg of perigee: 339
3624 deg
Mean anomaly: 20
7202 deg
Mean motion: 15
73186751 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1154
Checksum: 285
Coasting Arc #8 (Orbit 1169)
---------------------------------------
Vector Time (GMT): 2010/347/14:14:16
929
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 559728
59 A = 6724640
16 meter
Y = 4731603
83 meter E =
0006038
Z = 4740057
88 I = 51
81333
XDOT = -6983
474802 Wp = 43
69383
YDOT = -1850
253800 meter/sec RA = 31
76393 deg
ZDOT = 2673
862041 TA = 20
11165
MA = 20
08787
Ha = 192
546 n
mi
Hp = 185
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1836379
90 X = 483750
85
Y = 15523634
62 feet Y = 4737437
94 meter
Z = 15551370
99 Z = 4742592
80
XDOT = -22911
662737 XDOT = -6975
255094
YDOT = -6070
386484 feet/sec YDOT = -1928
301431 meter/sec
ZDOT = 8772
513259 ZDOT = 2639
955987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13340492
60 X = -4066182
14
Y = 8128621
78 feet Y = 2477603
92 meter
Z = 15561408
29 Z = 4743117
25
XDOT = -3588
640678 XDOT = -1093
817679
YDOT = -22408
451998 feet/sec YDOT = -6830
096169 meter/sec
ZDOT = 8636
186622 ZDOT = 2632
309682
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 10347
64547277
00016717 00000-0 10270-3 0 9071
2 25544 51
6450 32
0281 0008325 343
5866 16
5026 15
73207166 11709
Satellite: ISS
Catalog Number: 25544
Epoch time: 10347
64547277 = yrday
fracday
Element set: 907
Inclination: 51
6450 deg
RA of node: 32
0281 deg
Eccentricity:
0008325
Arg of perigee: 343
5866 deg
Mean anomaly: 16
5026 deg
Mean motion: 15
73207166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1170
Checksum: 294
Coasting Arc #9 (Orbit 1184)
---------------------------------------
Vector Time (GMT): 2010/348/14:14:16
929
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6164503
94 A = 6731482
79 meter
Y = 840819
69 meter E =
0011724
Z = -2553949
14 I = 51
81113
XDOT = 1454
852299 Wp = 10
50783
YDOT = 5393
539230 meter/sec RA = 26
60551 deg
ZDOT = 5302
356560 TA = 320
60058
MA = 320
68579
Ha = 192
650 n
mi
Hp = 184
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20224750
45 X = 6167050
30
Y = 2758594
78 feet Y = 909769
29 meter
Z = -8379098
23 Z = -2523995
49
XDOT = 4773
137465 XDOT = 1368
674501
YDOT = 17695
338680 feet/sec YDOT = 5409
326072 meter/sec
ZDOT = 17396
182941 ZDOT = 5309
215317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6385317
92 X = 1946244
90
Y = 19439193
24 feet Y = 5925066
10 meter
Z = -8258640
58 Z = -2517233
65
XDOT = -12454
880306 XDOT = -3796
247517
YDOT = 11472
130160 feet/sec YDOT = 3496
705273 meter/sec
ZDOT = 17423
585141 ZDOT = 5310
708751
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 10348
59827926
00016717 00000-0 10270-3 0 9089
2 25544 51
6459 27
1421 0008334 347
4541 12
6413 15
73274485 11853
Satellite: ISS
Catalog Number: 25544
Epoch time: 10348
59827926 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node: 27
1421 deg
Eccentricity:
0008334
Arg of perigee: 347
4541 deg
Mean anomaly: 12
6413 deg
Mean motion: 15
73274485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1185
Checksum: 316
Coasting Arc #10 (Orbit 1200)
---------------------------------------
Vector Time (GMT): 2010/349/14:14:16
929
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1940904
69 A = 6725290
28 meter
Y = -4596624
19 meter E =
0014328
Z = -4522304
83 I = 51
76177
XDOT = 7022
171876 Wp = 34
04228
YDOT = 119
921231 meter/sec RA = 21
53026 deg
ZDOT = -3128
833535 TA = 204
71804
MA = 204
78676
Ha = 192
669 n
mi
Hp = 184
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6367797
54 X = -1867391
34
Y = -15080788
04 feet Y = -4617917
19 meter
Z = -14836958
11 Z = -4531555
63
XDOT = 23038
621642 XDOT = 7035
508464
YDOT = 393
442358 feet/sec YDOT = 198
522184 meter/sec
ZDOT = -10265
201885 ZDOT = -3094
687035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10604837
01 X = 3232354
32
Y = -12426414
43 feet Y = -3787571
12 meter
Z = -14874004
03 Z = -4533596
43
XDOT = 9200
495210 XDOT = 2804
310940
YDOT = 20001
415449 feet/sec YDOT = 6096
431429 meter/sec
ZDOT = -10127
857744 ZDOT = -3086
971041
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 10349
61458095
00016717 00000-0 10270-3 0 9091
2 25544 51
6448 21
9284 0008423 350
9892 9
1118 15
73290793 12019
Satellite: ISS
Catalog Number: 25544
Epoch time: 10349
61458095 = yrday
fracday
Element set: 909
Inclination: 51
6448 deg
RA of node: 21
9284 deg
Eccentricity:
0008423
Arg of perigee: 350
9892 deg
Mean anomaly: 9
1118 deg
Mean motion: 15
73290793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1201
Checksum: 314
Coasting Arc #11 (Orbit 1216)
---------------------------------------
Vector Time (GMT): 2010/350/14:14:16
929
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6041002
32 A = 6730423
76 meter
Y = 610522
97 meter E =
0014065
Z = 2901779
12 I = 51
75031
XDOT = -2942
745929 Wp = 61
94539
YDOT = -5010
638145 meter/sec RA = 16
36173 deg
ZDOT = -5047
071807 TA = 84
75102
MA = 84
59053
Ha = 192
765 n
mi
Hp = 184
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19819561
41 X = -6061476
82
Y = 2003028
10 feet Y = 542854
10 meter
Z = 9520272
70 Z = 2872381
86
XDOT = -9654
678245 XDOT = -2861
979240
YDOT = -16439
101527 feet/sec YDOT = -5043
093665 meter/sec
ZDOT = -16558
634537 ZDOT = -5061
172114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11071863
73 X = -3374704
07
Y = -16627652
21 feet Y = -5068108
39 meter
Z = 9402007
44 Z = 2865731
87
XDOT = 8844
132991 XDOT = 2695
691736
YDOT = -15330
951537 feet/sec YDOT = -4672
874028 meter/sec
ZDOT = -16615
165041 ZDOT = -5064
302305
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 10350
63085501
00016717 00000-0 10270-3 0 9105
2 25544 51
6444 16
7149 0008614 354
6043 5
5026 15
73364120 12179
Satellite: ISS
Catalog Number: 25544
Epoch time: 10350
63085501 = yrday
fracday
Element set: 910
Inclination: 51
6444 deg
RA of node: 16
7149 deg
Eccentricity:
0008614
Arg of perigee: 354
6043 deg
Mean anomaly: 5
5026 deg
Mean motion: 15
73364120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1217
Checksum: 268
Coasting Arc #12 (Orbit 1232)
---------------------------------------
Vector Time (GMT): 2010/351/14:14:16
929
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3166063
41 A = 6725829
39 meter
Y = 4087055
36 meter E =
0010402
Z = 4291261
45 I = 51
70525
XDOT = -6693
466494 Wp = 58
06777
YDOT = 1494
084024 meter/sec RA = 11
28610 deg
ZDOT = 3514
620871 TA = 356
40023
MA = 356
40770
Ha = 192
735 n
mi
Hp = 184
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10387347
13 X = 3099279
42
Y = 13408974
28 feet Y = 4122086
31 meter
Z = 14078941
78 Z = 4306480
63
XDOT = -21960
191909 XDOT = -6726
749766
YDOT = 4901
850473 feet/sec YDOT = 1419
047173 meter/sec
ZDOT = 11530
908369 ZDOT = 3482
022881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6763320
33 X = -2061460
04
Y = 15499420
47 feet Y = 4724223
36 meter
Z = 14140001
30 Z = 4309872
40
XDOT = -13804
097023 XDOT = -4207
488773
YDOT = -16425
786694 feet/sec YDOT = -5006
579784 meter/sec
ZDOT = 11399
736046 ZDOT = 3474
639547
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 10351
64710328
00016717 00000-0 10270-3 0 9110
2 25544 51
6439 11
5017 0008549 358
0665 2
0463 15
73387183 12334
Satellite: ISS
Catalog Number: 25544
Epoch time: 10351
64710328 = yrday
fracday
Element set: 911
Inclination: 51
6439 deg
RA of node: 11
5017 deg
Eccentricity:
0008549
Arg of perigee: 358
0665 deg
Mean anomaly: 2
0463 deg
Mean motion: 15
73387183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1233
Checksum: 288
Coasting Arc #13 (Orbit 1247)
---------------------------------------
Vector Time (GMT): 2010/352/14:14:16
929
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5568148
21 A = 6729459
29 meter
Y = -1964332
18 meter E =
0010612
Z = -3222108
43 I = 51
68700
XDOT = 4265
440426 Wp = 27
32725
YDOT = 4261
702636 meter/sec RA = 6
11023 deg
ZDOT = 4788
471283 TA = 295
04690
MA = 295
15703
Ha = 193
012 n
mi
Hp = 183
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18268202
78 X = 5605352
51
Y = -6444659
39 feet Y = -1901857
35 meter
Z = -10571221
89 Z = -3194967
92
XDOT = 13994
227118 XDOT = 4194
206440
YDOT = 13981
964028 feet/sec YDOT = 4309
002437 meter/sec
ZDOT = 15710
207622 ZDOT = 4809
020580
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14719157
85 X = 4486399
31
Y = 12684831
90 feet Y = 3866336
76 meter
Z = -10461980
28 Z = -3188811
59
XDOT = -4275
939666 XDOT = -1303
306410
YDOT = 17944
690892 feet/sec YDOT = 5469
541784 meter/sec
ZDOT = 15792
695074 ZDOT = 4813
613459
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 10352
59981157
00016717 00000-0 10270-3 0 9126
2 25544 51
6437 6
6141 0008636 2
8203 357
3007 15
73399493 12487
Satellite: ISS
Catalog Number: 25544
Epoch time: 10352
59981157 = yrday
fracday
Element set: 912
Inclination: 51
6437 deg
RA of node: 6
6141 deg
Eccentricity:
0008636
Arg of perigee: 2
8203 deg
Mean anomaly: 357
3007 deg
Mean motion: 15
73399493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1248
Checksum: 307
Coasting Arc #14 (Orbit 1263)
---------------------------------------
Vector Time (GMT): 2010/353/14:14:16
929
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4208197
30 A = 6726406
72 meter
Y = -3309897
11 meter E =
0013843
Z = -4086740
94 I = 51
64699
XDOT = 6003
220667 Wp = 36
00999
YDOT = -2913
255526 meter/sec RA = 1
03080 deg
ZDOT = -3817
705246 TA = 194
67925
MA = 194
71949
Ha = 192
956 n
mi
Hp = 183
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13806421
57 X = -4151019
82
Y = -10859242
47 feet Y = -3356635
39 meter
Z = -13407942
72 Z = -4107046
16
XDOT = 19695
605862 XDOT = 6053
896942
YDOT = -9557
924954 feet/sec YDOT = -2845
839976 meter/sec
ZDOT = -12525
279678 ZDOT = -3788
418683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2281621
43 X = 695438
21
Y = -17353425
14 feet Y = -5289323
98 meter
Z = -13489484
48 Z = -4111594
87
XDOT = 17080
451110 XDOT = 5206
121498
YDOT = 11901
734171 feet/sec YDOT = 3627
648575 meter/sec
ZDOT = -12407
364368 ZDOT = -3781
764659
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 10353
61600724
00016717 00000-0 10270-3 0 9139
2 25544 51
6437 1
3994 0008632 6
6998 353
4279 15
73453602 12643
Satellite: ISS
Catalog Number: 25544
Epoch time: 10353
61600724 = yrday
fracday
Element set: 913
Inclination: 51
6437 deg
RA of node: 1
3994 deg
Eccentricity:
0008632
Arg of perigee: 6
6998 deg
Mean anomaly: 353
4279 deg
Mean motion: 15
73453602 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1264
Checksum: 306
Coasting Arc #15 (Orbit 1279)
---------------------------------------
Vector Time (GMT): 2010/354/14:14:16
929
Vector Time (MET): N/A
Weight (LBS) : 813307
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4883627
45 A = 6728510
88 meter
Y = 3088921
79 meter E =
0016438
Z = 3443834
24 I = 51
62356
XDOT = -5285
452064 Wp = 57
48500
YDOT = -3240
391745 meter/sec RA = 355
84819 deg
ZDOT = -4564
283931 TA = 81
74386
MA = 81
55749
Ha = 193
027 n
mi
Hp = 183
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16022399
76 X = -4934534
97
Y = 10134257
83 feet Y = 3034024
93 meter
Z = 11298668
77 Z = 3419986
33
XDOT = -17340
721996 XDOT = -5226
652019
YDOT = -10631
206512 feet/sec YDOT = -3299
167343 meter/sec
ZDOT = -14974
684814 ZDOT = -4589
818462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17098401
08 X = -5211592
65
Y = -8320241
95 feet Y = -2536009
75 meter
Z = 11202617
84 Z = 3414557
92
XDOT = -677
421752 XDOT = -206
478150
YDOT = -19017
307142 feet/sec YDOT = -5796
475217 meter/sec
ZDOT = -15077
264919 ZDOT = -4595
550347
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 10354
63217468
00016717 00000-0 10270-3 0 9142
2 25544 51
6435 356
1852 0008729 9
6473 350
4856 15
73509672 12808
Satellite: ISS
Catalog Number: 25544
Epoch time: 10354
63217468 = yrday
fracday
Element set: 914
Inclination: 51
6435 deg
RA of node: 356
1852 deg
Eccentricity:
0008729
Arg of perigee: 9
6473 deg
Mean anomaly: 350
4856 deg
Mean motion: 15
73509672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1280
Checksum: 324
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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