Date:
November 16th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18298 65 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
329/05:06:03
718 -2
0 2
6 2
6
N/A 0
5 0
1 189
8
000/00:06:07
437 1
6 0
1 189
0
Coasting Arc #1 (Orbit 729)
---------------------------------------
Vector Time (GMT): 2010/319/16:22:11
858
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4444962
03 A = 6729529
33 meter
Y = 3412326
58 meter E =
0008925
Z = -3735843
00 I = 51
67260
XDOT = -5748
222359 Wp = 162
64601
YDOT = -2813
095874 meter/sec RA = 174
29171 deg
ZDOT = 4264
088278 TA = 152
35479
MA = 152
30731
Ha = 192
762 n
mi
Hp = 186
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14583208
75 X = -4464640
56
Y = 11195297
17 feet Y = 3362510
31 meter
Z = -12256702
76 Z = -3757484
82
XDOT = -18858
997242 XDOT = -5737
053115
YDOT = -9229
317173 feet/sec YDOT = -2877
313503 meter/sec
ZDOT = 13989
790939 ZDOT = 4236
190045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16878049
74 X = -5144429
56
Y = -7141326
67 feet Y = -2176676
37 meter
Z = -12343593
84 Z = -3762327
40
XDOT = -1784
679927 XDOT = -543
970442
YDOT = -19801
738781 feet/sec YDOT = -6035
569980 meter/sec
ZDOT = 13877
770776 ZDOT = 4229
944532
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 10319
69011883
00016717 00000-0 10270-3 0 9007
2 25544 51
6420 175
3248 0007758 204
0678 156
0123 15
72774731 7306
Satellite: ISS
Catalog Number: 25544
Epoch time: 10319
69011883 = yrday
fracday
Element set: 900
Inclination: 51
6420 deg
RA of node: 175
3248 deg
Eccentricity:
0007758
Arg of perigee: 204
0678 deg
Mean anomaly: 156
0123 deg
Mean motion: 15
72774731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 730
Checksum: 297
Coasting Arc #2 (Orbit 745)
---------------------------------------
Vector Time (GMT): 2010/320/16:22:11
858
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5502651
59 A = 6730400
85 meter
Y = 1733844
73 meter E =
0006692
Z = -3460535
31 I = 51
70588
XDOT = -4279
520723 Wp = 169
25804
YDOT = 4484
632325 meter/sec RA = 169
22073 deg
ZDOT = -4565
837416 TA = 51
69138
MA = 51
63123
Ha = 192
581 n
mi
Hp = 186
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18053318
87 X = 5499665
46
Y = 5688466
95 feet Y = 1795361
99 meter
Z = -11353462
31 Z = -3433810
11
XDOT = -14040
422321 XDOT = -4307
170157
YDOT = 14713
360647 feet/sec YDOT = 4436
621553 meter/sec
ZDOT = -14979
781548 ZDOT = -4586
694939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4263817
20 X = 1299611
48
Y = 18507461
76 feet Y = 5641074
35 meter
Z = -11246146
32 Z = -3427825
40
XDOT = -18400
210012 XDOT = -5608
384012
YDOT = -4898
505756 feet/sec YDOT = -1493
064555 meter/sec
ZDOT = -15063
530646 ZDOT = -4591
364141
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 10320
70672592
00016717 00000-0 10270-3 0 9012
2 25544 51
6420 170
1137 0007678 208
7297 151
3444 15
72829876 7467
Satellite: ISS
Catalog Number: 25544
Epoch time: 10320
70672592 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 170
1137 deg
Eccentricity:
0007678
Arg of perigee: 208
7297 deg
Mean anomaly: 151
3444 deg
Mean motion: 15
72829876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 746
Checksum: 313
Coasting Arc #3 (Orbit 761)
---------------------------------------
Vector Time (GMT): 2010/321/16:22:11
858
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2968080
27 A = 6727644
50 meter
Y = -4311095
47 meter E =
0006564
Z = 4219813
98 I = 51
72646
XDOT = 6708
493317 Wp = 124
02010
YDOT = 1063
065804 meter/sec RA = 164
04918 deg
ZDOT = -3632
067798 TA = 2
89886
MA = 2
89506
Ha = 192
309 n
mi
Hp = 186
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9737796
15 X = 2995567
53
Y = -14144014
00 feet Y = -4277750
95 meter
Z = 13844534
05 Z = 4234300
01
XDOT = 22009
492509 XDOT = 6713
751694
YDOT = 3487
748701 feet/sec YDOT = 1138
113639 meter/sec
ZDOT = -11916
232933 ZDOT = -3599
464337
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17102499
22 X = 5212841
76
Y = 876463
66 feet Y = 267146
12 meter
Z = 13902706
96 Z = 4237545
08
XDOT = 8586
277763 XDOT = 2617
097462
YDOT = 19418
166757 feet/sec YDOT = 5918
657228 meter/sec
ZDOT = -11785
304429 ZDOT = -3592
160790
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 10321
72330093
00016717 00000-0 10270-3 0 9023
2 25544 51
6417 164
9021 0007731 212
1727 147
8965 15
72848672 7624
Satellite: ISS
Catalog Number: 25544
Epoch time: 10321
72330093 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 164
9021 deg
Eccentricity:
0007731
Arg of perigee: 212
1727 deg
Mean anomaly: 147
8965 deg
Mean motion: 15
72848672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 762
Checksum: 301
Coasting Arc #4 (Orbit 777)
---------------------------------------
Vector Time (GMT): 2010/322/16:22:11
858
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6079245
37 A = 6731613
85 meter
Y = -100415
55 meter E =
0009589
Z = 2887289
06 I = 51
77050
XDOT = 2498
360390 Wp = 115
96111
YDOT = -5231
493426 meter/sec RA = 158
97838 deg
ZDOT = 5061
336454 TA = 277
13734
MA = 277
24637
Ha = 192
027 n
mi
Hp = 186
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19945030
74 X = -6091697
00
Y = -329447
33 feet Y = -168467
01 meter
Z = 9472733
14 Z = 2857725
01
XDOT = 8196
720439 XDOT = 2532
086489
YDOT = -17163
692341 feet/sec YDOT = -5203
366792 meter/sec
ZDOT = 16605
434562 ZDOT = 5073
555642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10430868
54 X = -3179328
73
Y = -17068834
47 feet Y = -5202580
75 meter
Z = 9354000
83 Z = 2851099
45
XDOT = 17586
775939 XDOT = 5360
449306
YDOT = -1589
361376 feet/sec YDOT = -484
437347 meter/sec
ZDOT = 16654
514592 ZDOT = 5076
296048
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 10322
73983940
00016717 00000-0 10270-3 0 9031
2 25544 51
6426 159
6904 0007784 216
8996 143
1632 15
72959729 7785
Satellite: ISS
Catalog Number: 25544
Epoch time: 10322
73983940 = yrday
fracday
Element set: 903
Inclination: 51
6426 deg
RA of node: 159
6904 deg
Eccentricity:
0007784
Arg of perigee: 216
8996 deg
Mean anomaly: 143
1632 deg
Mean motion: 15
72959729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 778
Checksum: 350
Coasting Arc #5 (Orbit 792)
---------------------------------------
Vector Time (GMT): 2010/323/16:22:11
858
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1392984
24 A = 6725897
98 meter
Y = 4717815
34 meter E =
0010499
Z = -4595532
35 I = 51
77946
XDOT = -7037
728704 Wp = 152
96080
YDOT = 838
679789 meter/sec RA = 153
81561 deg
ZDOT = 2987
752707 TA = 146
70488
MA = 146
63879
Ha = 191
747 n
mi
Hp = 186
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4570158
28 X = -1423311
27
Y = 15478396
77 feet Y = 4702068
78 meter
Z = -15077205
89 Z = -4602373
14
XDOT = -23089
661101 XDOT = -7061
098304
YDOT = 2751
574112 feet/sec YDOT = 759
848880 meter/sec
ZDOT = 9802
338276 ZDOT = 2953
505672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15391555
69 X = -4691346
17
Y = 4768381
51 feet Y = 1453402
69 meter
Z = -15104694
70 Z = -4603910
94
XDOT = -14678
830454 XDOT = -4474
107522
YDOT = -16698
525245 feet/sec YDOT = -5089
710495 meter/sec
ZDOT = 9664
783756 ZDOT = 2945
826089
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 10323
69281681
00016717 00000-0 10270-3 0 9041
2 25544 51
6424 154
8050 0007642 221
3168 138
7418 15
72977192 7930
Satellite: ISS
Catalog Number: 25544
Epoch time: 10323
69281681 = yrday
fracday
Element set: 904
Inclination: 51
6424 deg
RA of node: 154
8050 deg
Eccentricity:
0007642
Arg of perigee: 221
3168 deg
Mean anomaly: 138
7418 deg
Mean motion: 15
72977192 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 793
Checksum: 315
Coasting Arc #6 (Orbit 808)
---------------------------------------
Vector Time (GMT): 2010/324/16:22:11
858
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6110732
15 A = 6732624
91 meter
Y = -1555848
04 meter E =
0009576
Z = -2341794
79 I = 51
82927
XDOT = -698
945228 Wp = 188
26083
YDOT = 5417
110074 meter/sec RA = 148
74142 deg
ZDOT = -5429
426573 TA = 18
02409
MA = 17
99016
Ha = 191
591 n
mi
Hp = 186
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20048333
83 X = 6139052
12
Y = -5104488
31 feet Y = -1487355
65 meter
Z = -7683053
77 Z = -2312039
29
XDOT = -2293
127387 XDOT = -733
092460
YDOT = 17772
670847 feet/sec YDOT = 5409
103486 meter/sec
ZDOT = -17813
079309 ZDOT = -5432
904732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15550700
29 X = 4739853
45
Y = 13710931
87 feet Y = 4179092
03 meter
Z = -7563522
55 Z = -2305361
67
XDOT = -14907
927062 XDOT = -4543
936169
YDOT = 7086
192071 feet/sec YDOT = 2159
871343 meter/sec
ZDOT = -17827
074670 ZDOT = -5433
692359
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 10324
70929207
00016717 00000-0 10270-3 0 9058
2 25544 51
6424 149
5922 0007589 225
4377 134
6166 15
73031097 8095
Satellite: ISS
Catalog Number: 25544
Epoch time: 10324
70929207 = yrday
fracday
Element set: 905
Inclination: 51
6424 deg
RA of node: 149
5922 deg
Eccentricity:
0007589
Arg of perigee: 225
4377 deg
Mean anomaly: 134
6166 deg
Mean motion: 15
73031097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 809
Checksum: 317
Coasting Arc #7 (Orbit 824)
---------------------------------------
Vector Time (GMT): 2010/325/16:22:11
858
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -156027
15 A = 6724549
79 meter
Y = -4638117
38 meter E =
0001276
Z = 4865999
09 I = 51
82855
XDOT = 6807
408367 Wp = 176
52764
YDOT = -2709
920052 meter/sec RA = 143
58818 deg
ZDOT = -2365
947755 TA = 296
47430
MA = 296
48738
Ha = 191
264 n
mi
Hp = 187
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -511900
09 X = -127790
06
Y = -15216920
55 feet Y = -4639704
73 meter
Z = 15964563
95 Z = 4865309
26
XDOT = 22334
016953 XDOT = 6848
698912
YDOT = -8890
813820 feet/sec YDOT = -2633
564436 meter/sec
ZDOT = -7762
295784 ZDOT = -2332
776396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12063268
25 X = 3676884
16
Y = -9294182
78 feet Y = -2832866
91 meter
Z = 15961821
34 Z = 4865163
14
XDOT = 19517
556931 XDOT = 5948
951353
YDOT = 12237
347553 feet/sec YDOT = 3729
943534 meter/sec
ZDOT = -7629
018180 ZDOT = -2325
324741
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 10325
72573418
00016717 00000-0 10270-3 0 9061
2 25544 51
6429 144
3803 0007420 229
6419 130
4096 15
73064366 8257
Satellite: ISS
Catalog Number: 25544
Epoch time: 10325
72573418 = yrday
fracday
Element set: 906
Inclination: 51
6429 deg
RA of node: 144
3803 deg
Eccentricity:
0007420
Arg of perigee: 229
6419 deg
Mean anomaly: 130
4096 deg
Mean motion: 15
73064366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 825
Checksum: 302
Coasting Arc #8 (Orbit 840)
---------------------------------------
Vector Time (GMT): 2010/326/16:22:11
858
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5678542
10 A = 6733254
49 meter
Y = 3128620
92 meter E =
0007000
Z = 1807933
90 I = 51
88276
XDOT = -986
193345 Wp = 77
61937
YDOT = -5088
119006 meter/sec RA = 138
50940 deg
ZDOT = 5690
489669 TA = 302
34380
MA = 302
41155
Ha = 190
901 n
mi
Hp = 187
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18630387
47 X = -5721887
70
Y = 10264504
33 feet Y = 3064877
49 meter
Z = 5931541
66 Z = 1780241
92
XDOT = -3235
542471 XDOT = -956
867785
YDOT = -16693
303824 feet/sec YDOT = -5098
983860 meter/sec
ZDOT = 18669
585529 ZDOT = 5685
769309
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19325020
07 X = -5890266
12
Y = -8961183
31 feet Y = -2731368
67 meter
Z = 5820254
80 Z = 1774013
66
XDOT = 10815
214576 XDOT = 3296
477403
YDOT = -11172
965615 feet/sec YDOT = -3405
519919 meter/sec
ZDOT = 18650
659492 ZDOT = 5684
721013
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 10326
74213998
00016717 00000-0 10270-3 0 9079
2 25544 51
6434 139
1673 0007408 234
3201 125
7273 15
73142056 8413
Satellite: ISS
Catalog Number: 25544
Epoch time: 10326
74213998 = yrday
fracday
Element set: 907
Inclination: 51
6434 deg
RA of node: 139
1673 deg
Eccentricity:
0007408
Arg of perigee: 234
3201 deg
Mean anomaly: 125
7273 deg
Mean motion: 15
73142056 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 841
Checksum: 296
Coasting Arc #9 (Orbit 855)
---------------------------------------
Vector Time (GMT): 2010/327/16:22:11
858
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1516432
02 A = 6723357
12 meter
Y = 4173557
75 meter E =
0009677
Z = -5055922
34 I = 51
87258
XDOT = -6067
503997 Wp = 135
62762
YDOT = 4378
146800 meter/sec RA = 133
36713 deg
ZDOT = 1789
513794 TA = 151
59836
MA = 151
54558
Ha = 190
567 n
mi
Hp = 187
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4975170
68 X = 1494211
05
Y = 13692774
77 feet Y = 4190391
75 meter
Z = -16587671
71 Z = -5048608
86
XDOT = -19906
509177 XDOT = -6124
703596
YDOT = 14363
998689 feet/sec YDOT = 4309
976295 meter/sec
ZDOT = 5871
108249 ZDOT = 1759
898855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7817090
10 X = -2382649
06
Y = 12333302
02 feet Y = 3759190
46 meter
Z = -16558321
79 Z = -5046976
48
XDOT = -22611
067513 XDOT = -6891
853378
YDOT = -6587
979007 feet/sec YDOT = -2008
016001 meter/sec
ZDOT = 5752
063319 ZDOT = 1753
228900
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 10327
69499046
00016717 00000-0 10270-3 0 9085
2 25544 51
6437 134
2813 0007347 238
7757 121
2686 15
73215238 8562
Satellite: ISS
Catalog Number: 25544
Epoch time: 10327
69499046 = yrday
fracday
Element set: 908
Inclination: 51
6437 deg
RA of node: 134
2813 deg
Eccentricity:
0007347
Arg of perigee: 238
7757 deg
Mean anomaly: 121
2686 deg
Mean motion: 15
73215238 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 856
Checksum: 331
Coasting Arc #10 (Orbit 871)
---------------------------------------
Vector Time (GMT): 2010/328/16:22:11
858
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4852538
92 A = 6733616
71 meter
Y = -4463785
74 meter E =
0010526
Z = -1332137
97 I = 51
92738
XDOT = 2408
629757 Wp = 186
60540
YDOT = 4368
025392 meter/sec RA = 128
28324 deg
ZDOT = -5868
392345 TA = 7
96481
MA = 7
94811
Ha = 190
401 n
mi
Hp = 187
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15920403
29 X = 4908564
53
Y = -14644966
33 feet Y = -4409208
32 meter
Z = -4370531
40 Z = -1308428
41
XDOT = 7902
328599 XDOT = 2388
114664
YDOT = 14330
791968 feet/sec YDOT = 4394
846100 meter/sec
ZDOT = -19253
255726 ZDOT = -5856
740387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21375362
83 X = 6515210
59
Y = 3442726
83 feet Y = 1049343
14 meter
Z = -4275198
24 Z = -1303080
42
XDOT = -6030
041340 XDOT = -1837
956600
YDOT = 13612
493085 feet/sec YDOT = 4149
087892 meter/sec
ZDOT = -19206
472508 ZDOT = -5854
132820
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 10328
71133099
00016717 00000-0 10270-3 0 9093
2 25544 51
6437 129
0685 0007389 243
1441 116
8967 15
73235415 8726
Satellite: ISS
Catalog Number: 25544
Epoch time: 10328
71133099 = yrday
fracday
Element set: 909
Inclination: 51
6437 deg
RA of node: 129
0685 deg
Eccentricity:
0007389
Arg of perigee: 243
1441 deg
Mean anomaly: 116
8967 deg
Mean motion: 15
73235415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 872
Checksum: 323
Coasting Arc #11 (Orbit 879)
---------------------------------------
Vector Time (GMT): 2010/329/05:09:07
437
Vector Time (MET): N/A
Weight (LBS) : 829691
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1950317
69 A = 6733112
12 meter
Y = 5974882
84 meter E =
0004800
Z = -2406806
89 I = 51
93158
XDOT = -5473
484207 Wp = 306
99029
YDOT = 389
669081 meter/sec RA = 125
53046 deg
ZDOT = 5398
175618 TA = 25
99360
MA = 25
96950
Ha = 189
819 n
mi
Hp = 188
957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6398680
09 X = -2005293
02
Y = 19602633
98 feet Y = 5952766
09 meter
Z = -7896348
07 Z = -2416414
54
XDOT = -17957
625350 XDOT = -5503
658428
YDOT = 1278
441866 feet/sec YDOT = 328
291990 meter/sec
ZDOT = 17710
549927 ZDOT = 5371
511857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17361495
31 X = 5291783
77
Y = -11098310
37 feet Y = -3382765
00 meter
Z = -7935027
83 Z = -2418596
48
XDOT = 13949
634820 XDOT = 4251
848693
YDOT = 9225
364455 feet/sec YDOT = 2811
891086 meter/sec
ZDOT = 17603
378782 ZDOT = 5365
509853
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 10329
21948822
00016717 00000-0 10270-3 0 9109
2 25544 51
6441 126
4644 0007937 263
6819 96
3440 15
72778692 8807
Satellite: ISS
Catalog Number: 25544
Epoch time: 10329
21948822 = yrday
fracday
Element set: 910
Inclination: 51
6441 deg
RA of node: 126
4644 deg
Eccentricity:
0007937
Arg of perigee: 263
6819 deg
Mean anomaly: 96
3440 deg
Mean motion: 15
72778692 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 880
Checksum: 330
Coasting Arc #12 (Orbit 895)
---------------------------------------
Vector Time (GMT): 2010/330/05:09:07
437
Vector Time (MET): N/A
Weight (LBS) : 829691
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4826229
55 A = 6726689
45 meter
Y = -1203560
84 meter E =
0003536
Z = -4531318
63 I = 51
92778
XDOT = -1221
123378 Wp = 21
79010
YDOT = 6920
642747 meter/sec RA = 120
46887 deg
ZDOT = -3136
351819 TA = 217
01984
MA = 217
04424
Ha = 189
233 n
mi
Hp = 188
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15834086
46 X = 4861341
81
Y = -3948690
42 feet Y = -1149394
30 meter
Z = -14866530
95 Z = -4507787
43
XDOT = -4006
310295 XDOT = -1283
184578
YDOT = 22705
520824 feet/sec YDOT = 6906
640697 meter/sec
ZDOT = -10289
868172 ZDOT = -3142
434197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14922654
92 X = -4548425
22
Y = -6813857
45 feet Y = -2076863
75 meter
Z = -14771929
78 Z = -4502484
20
XDOT = 16717
376219 XDOT = 5095
456272
YDOT = -14233
551544 feet/sec YDOT = -4338
386511 meter/sec
ZDOT = -10314
397316 ZDOT = -3143
828302
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 10330
23610124
00016717 00000-0 10270-3 0 9115
2 25544 51
6447 121
2537 0007975 268
8555 91
1694 15
72836143 8960
Satellite: ISS
Catalog Number: 25544
Epoch time: 10330
23610124 = yrday
fracday
Element set: 911
Inclination: 51
6447 deg
RA of node: 121
2537 deg
Eccentricity:
0007975
Arg of perigee: 268
8555 deg
Mean anomaly: 91
1694 deg
Mean motion: 15
72836143 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 896
Checksum: 309
Coasting Arc #13 (Orbit 911)
---------------------------------------
Vector Time (GMT): 2010/331/05:09:07
437
Vector Time (MET): N/A
Weight (LBS) : 829691
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 195053
26 A = 6731376
49 meter
Y = -5994402
97 meter E =
0005292
Z = 3050626
41 I = 51
95813
XDOT = 5401
496231 Wp = 100
32182
YDOT = -2349
667250 meter/sec RA = 115
31658 deg
ZDOT = -4956
101253 TA = 44
53240
MA = 44
48988
Ha = 189
170 n
mi
Hp = 188
517
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 639938
52 X = 247249
80
Y = -19666676
43 feet Y = -5991930
14 meter
Z = 10008616
82 Z = 3051700
35
XDOT = 17721
444327 XDOT = 5451
445209
YDOT = -7708
882053 feet/sec YDOT = -2288
984839 meter/sec
ZDOT = -16260
174713 ZDOT = -4929
739433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12428960
26 X = -3788347
09
Y = 15251908
83 feet Y = 4648781
81 meter
Z = 10013007
42 Z = 3051964
66
XDOT = -17718
027091 XDOT = -5400
454657
YDOT = -3819
715837 feet/sec YDOT = -1164
249387 meter/sec
ZDOT = -16154
170726 ZDOT = -4923
791237
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 10331
25268159
00016717 00000-0 10270-3 0 9126
2 25544 51
6445 116
0425 0007901 272
9082 87
1177 15
72860709 9121
Satellite: ISS
Catalog Number: 25544
Epoch time: 10331
25268159 = yrday
fracday
Element set: 912
Inclination: 51
6445 deg
RA of node: 116
0425 deg
Eccentricity:
0007901
Arg of perigee: 272
9082 deg
Mean anomaly: 87
1177 deg
Mean motion: 15
72860709 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 912
Checksum: 301
Coasting Arc #14 (Orbit 927)
---------------------------------------
Vector Time (GMT): 2010/332/05:09:07
437
Vector Time (MET): N/A
Weight (LBS) : 829691
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4488840
08 A = 6728006
04 meter
Y = 2852469
20 meter E =
0002765
Z = 4119632
65 I = 51
95952
XDOT = -724
323590 Wp = 121
37483
YDOT = -6648
787712 meter/sec RA = 110
26087 deg
ZDOT = 3811
167236 TA = 289
66066
MA = 289
69049
Ha = 189
914 n
mi
Hp = 188
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14727165
63 X = -4540415
90
Y = 9358494
75 feet Y = 2801983
71 meter
Z = 13515855
16 Z = 4097700
55
XDOT = -2376
389730 XDOT = -668
435884
YDOT = -21813
607980 feet/sec YDOT = -6656
575239 meter/sec
ZDOT = 12503
829516 ZDOT = 3807
783865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17469889
82 X = 5324822
42
Y = 1284712
99 feet Y = 391580
52 meter
Z = 13427644
40 Z = 4092746
01
XDOT = -10911
544733 XDOT = -3325
838835
YDOT = 17718
271526 feet/sec YDOT = 5400
529161 meter/sec
ZDOT = 12490
313553 ZDOT = 3807
047571
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 10332
26922639
00016717 00000-0 10270-3 0 9139
2 25544 51
6449 110
8303 0007967 278
0396 81
9862 15
72910051 9285
Satellite: ISS
Catalog Number: 25544
Epoch time: 10332
26922639 = yrday
fracday
Element set: 913
Inclination: 51
6449 deg
RA of node: 110
8303 deg
Eccentricity:
0007967
Arg of perigee: 278
0396 deg
Mean anomaly: 81
9862 deg
Mean motion: 15
72910051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 928
Checksum: 318
Coasting Arc #15 (Orbit 942)
---------------------------------------
Vector Time (GMT): 2010/333/05:09:07
437
Vector Time (MET): N/A
Weight (LBS) : 829691
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1415461
29 A = 6729534
17 meter
Y = 5514286
22 meter E =
0002836
Z = -3585091
62 I = 51
97460
XDOT = -4728
641522 Wp = 290
34342
YDOT = 4118
273243 meter/sec RA = 105
10526 deg
ZDOT = 4465
560120 TA = 27
08881
MA = 27
07402
Ha = 190
198 n
mi
Hp = 188
799
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4643901
88 X = 1371110
24
Y = 18091490
22 feet Y = 5529866
91 meter
Z = -11762111
60 Z = -3578322
76
XDOT = -15513
915754 XDOT = -4796
034504
YDOT = 13511
395154 feet/sec YDOT = 4065
017754 meter/sec
ZDOT = 14650
787796 ZDOT = 4442
424567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6672626
89 X = 2033816
68
Y = -17463720
55 feet Y = -5322942
02 meter
Z = -11734974
54 Z = -3576820
24
XDOT = 19274
331461 XDOT = 5874
816229
YDOT = -2421
932115 feet/sec YDOT = -738
204909 meter/sec
ZDOT = 14557
713591 ZDOT = 4437
191103
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 10333
22220500
00016717 00000-0 10270-3 0 9145
2 25544 51
6446 105
9441 0008191 282
1786 77
8459 15
72975368 9434
Satellite: ISS
Catalog Number: 25544
Epoch time: 10333
22220500 = yrday
fracday
Element set: 914
Inclination: 51
6446 deg
RA of node: 105
9441 deg
Eccentricity:
0008191
Arg of perigee: 282
1786 deg
Mean anomaly: 77
8459 deg
Mean motion: 15
72975368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 943
Checksum: 313
Coasting Arc #16 (Orbit 958)
---------------------------------------
Vector Time (GMT): 2010/334/05:09:07
437
Vector Time (MET): N/A
Weight (LBS) : 829691
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3680280
90 A = 6729168
46 meter
Y = -4263719
91 meter E =
0004097
Z = -3683005
49 I = 51
98007
XDOT = 2422
359819 Wp = 324
26673
YDOT = 5861
323156 meter/sec RA = 100
05255 deg
ZDOT = -4359
264867 TA = 259
73633
MA = 259
78253
Ha = 190
319 n
mi
Hp = 188
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12074412
42 X = 3745576
74
Y = -13988582
37 feet Y = -4222199
58 meter
Z = -12083351
34 Z = -3664967
94
XDOT = 7947
374735 XDOT = 2377
814225
YDOT = 19230
062849 feet/sec YDOT = 5888
162522 meter/sec
ZDOT = -14302
050087 ZDOT = -4347
604863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17935801
37 X = -5466832
26
Y = 4639811
21 feet Y = 1414214
46 meter
Z = -12010763
20 Z = -3660880
62
XDOT = 4620
997931 XDOT = 1408
480169
YDOT = -19086
980898 feet/sec YDOT = -5817
711778 meter/sec
ZDOT = -14255
259573 ZDOT = -4345
003118
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 10334
23868297
00016717 00000-0 10270-3 0 9159
2 25544 51
6442 100
7320 0008292 285
9544 74
0705 15
73012912 9592
Satellite: ISS
Catalog Number: 25544
Epoch time: 10334
23868297 = yrday
fracday
Element set: 915
Inclination: 51
6442 deg
RA of node: 100
7320 deg
Eccentricity:
0008292
Arg of perigee: 285
9544 deg
Mean anomaly: 74
0705 deg
Mean motion: 15
73012912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 959
Checksum: 305
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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