Date:
January 6th 2011
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
013/09:06:04
487 -3
8 5
1 5
1
N/A -3
0 -0
0 193
9
000/00:12:04
973 -1
6 0
2 187
0
Coasting Arc #1 (Orbit 1498)
---------------------------------------
Vector Time (GMT): 2011/003/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4364221
27 A = 6725197
08 meter
Y = -666213
34 meter E =
0009275
Z = 5066671
90 I = 51
29765
XDOT = -657
432852 Wp = 112
21853
YDOT = 7518
335282 meter/sec RA = 284
46346 deg
ZDOT = 1549
143002 TA = 322
81857
MA = 322
88276
Ha = 194
004 n
mi
Hp = 184
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14318311
24 X = 4346733
98
Y = -2185739
30 feet Y = -617508
51 meter
Z = 16622939
30 Z = 5087830
43
XDOT = -2156
931930 XDOT = -748
980781
YDOT = 24666
454337 feet/sec YDOT = 7510
471373 meter/sec
ZDOT = 5082
490164 ZDOT = 1545
727970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5089193
75 X = 1551186
25
Y = 13455604
91 feet Y = 4101268
38 meter
Z = 16708094
07 Z = 5092627
07
XDOT = -23602
158225 XDOT = -7193
937827
YDOT = 2609
962985 feet/sec YDOT = 795
516718 meter/sec
ZDOT = 5068
512851 ZDOT = 1544
882717
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 11003
55030533
00016717 00000-0 10270-3 0 9006
2 25544 51
6457 284
9048 0004724 98
9693 261
2004 15
72487024 14994
Satellite: ISS
Catalog Number: 25544
Epoch time: 11003
55030533 = yrday
fracday
Element set: 900
Inclination: 51
6457 deg
RA of node: 284
9048 deg
Eccentricity:
0004724
Arg of perigee: 98
9693 deg
Mean anomaly: 261
2004 deg
Mean motion: 15
72487024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1499
Checksum: 304
Coasting Arc #2 (Orbit 1513)
---------------------------------------
Vector Time (GMT): 2011/004/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -420239
42 A = 6735018
62 meter
Y = -6469232
52 meter E =
0010379
Z = -1822314
23 I = 51
32437
XDOT = 4881
787681 Wp = 62
40886
YDOT = -1896
615937 meter/sec RA = 279
28647 deg
ZDOT = 5636
493421 TA = 277
31010
MA = 277
42806
Ha = 194
128 n
mi
Hp = 184
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1378738
25 X = -339015
70
Y = -21224516
14 feet Y = -6473477
50 meter
Z = -5978721
24 Z = -1824159
31
XDOT = 16016
363782 XDOT = 4875
252583
YDOT = -6222
493230 feet/sec YDOT = -1842
062150 meter/sec
ZDOT = 18492
432484 ZDOT = 5660
192607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20382159
36 X = 6212482
17
Y = -6071414
07 feet Y = -1850567
01 meter
Z = -5985952
15 Z = -1824518
22
XDOT = 9189
415480 XDOT = 2800
933838
YDOT = 12617
850877 feet/sec YDOT = 3845
920947 meter/sec
ZDOT = 18587
852803 ZDOT = 5665
577534
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 11004
50357383
00016717 00000-0 10270-3 0 9018
2 25544 51
6458 280
0210 0004759 101
3995 258
7702 15
72492273 15141
Satellite: ISS
Catalog Number: 25544
Epoch time: 11004
50357383 = yrday
fracday
Element set: 901
Inclination: 51
6458 deg
RA of node: 280
0210 deg
Eccentricity:
0004759
Arg of perigee: 101
3995 deg
Mean anomaly: 258
7702 deg
Mean motion: 15
72492273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1514
Checksum: 293
Coasting Arc #3 (Orbit 1529)
---------------------------------------
Vector Time (GMT): 2011/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4010993
61 A = 6726409
88 meter
Y = 2580915
78 meter E =
0015844
Z = -4757419
86 I = 51
29262
XDOT = -1535
096581 Wp = 81
18080
YDOT = -7085
070819 meter/sec RA = 274
17565 deg
ZDOT = -2554
294575 TA = 163
63985
MA = 163
58865
Ha = 194
030 n
mi
Hp = 184
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13159427
84 X = -4016445
57
Y = 8467571
45 feet Y = 2536032
51 meter
Z = -15608332
87 Z = -4776917
81
XDOT = -5036
406106 XDOT = -1443
347849
YDOT = -23244
983003 feet/sec YDOT = -7101
723897 meter/sec
ZDOT = -8380
231545 ZDOT = -2561
529911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11367591
17 X = -3464841
79
Y = -10639096
23 feet Y = -3242796
53 meter
Z = -15686869
18 Z = -4781357
73
XDOT = 20581
382495 XDOT = 6273
205384
YDOT = -9615
162309 feet/sec YDOT = -2930
701472 meter/sec
ZDOT = -8409
148770 ZDOT = -2563
108545
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 11005
52036762
00016717 00000-0 10270-3 0 9027
2 25544 51
6462 274
8113 0004786 104
7463 255
4230 15
72550303 15303
Satellite: ISS
Catalog Number: 25544
Epoch time: 11005
52036762 = yrday
fracday
Element set: 902
Inclination: 51
6462 deg
RA of node: 274
8113 deg
Eccentricity:
0004786
Arg of perigee: 104
7463 deg
Mean anomaly: 255
4230 deg
Mean motion: 15
72550303 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1530
Checksum: 274
Coasting Arc #4 (Orbit 1545)
---------------------------------------
Vector Time (GMT): 2011/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2209345
49 A = 6733270
54 meter
Y = 5780839
89 meter E =
0018469
Z = 2630754
64 I = 51
31386
XDOT = -4094
562493 Wp = 104
07839
YDOT = 3943
078028 meter/sec RA = 268
98491 deg
ZDOT = -5199
816838 TA = 45
84335
MA = 45
69166
Ha = 193
984 n
mi
Hp = 184
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7248508
82 X = 2131759
39
Y = 18966010
13 feet Y = 5805112
06 meter
Z = 8631084
79 Z = 2641299
53
XDOT = -13433
603979 XDOT = -4113
091189
YDOT = 12936
607702 feet/sec YDOT = 3897
187071 meter/sec
ZDOT = -17059
766528 ZDOT = -5219
752416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16470199
94 X = -5020116
94
Y = 11842769
90 feet Y = 3609676
26 meter
Z = 8673370
75 Z = 2643643
40
XDOT = -15071
718421 XDOT = -4593
859775
YDOT = -8345
499782 feet/sec YDOT = -2543
708334 meter/sec
ZDOT = -17140
099510 ZDOT = -5224
302331
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 11006
53713742
00016717 00000-0 10270-3 0 9030
2 25544 51
6454 269
6016 0004796 109
5203 250
6478 15
72551468 15465
Satellite: ISS
Catalog Number: 25544
Epoch time: 11006
53713742 = yrday
fracday
Element set: 903
Inclination: 51
6454 deg
RA of node: 269
6016 deg
Eccentricity:
0004796
Arg of perigee: 109
5203 deg
Mean anomaly: 250
6478 deg
Mean motion: 15
72551468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1546
Checksum: 309
Coasting Arc #5 (Orbit 1561)
---------------------------------------
Vector Time (GMT): 2011/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3004901
48 A = 6728088
91 meter
Y = -4214398
87 meter E =
0014409
Z = 4289706
26 I = 51
29879
XDOT = 3424
287661 Wp = 109
80074
YDOT = 5973
078011 meter/sec RA = 263
88334 deg
ZDOT = 3455
306720 TA = 305
04981
MA = 305
18490
Ha = 193
828 n
mi
Hp = 184
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9858600
65 X = 3030966
17
Y = -13826767
95 feet Y = -4180650
85 meter
Z = 14073839
43 Z = 4304366
75
XDOT = 11234
539571 XDOT = 3340
456181
YDOT = 19596
712634 feet/sec YDOT = 6010
901467 meter/sec
ZDOT = 11336
308136 ZDOT = 3471
738397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15977356
78 X = 4869898
35
Y = 5606104
08 feet Y = 1708740
52 meter
Z = 14132945
29 Z = 4307721
72
XDOT = -15372
701633 XDOT = -4685
599458
YDOT = 14949
802438 feet/sec YDOT = 4556
699783 meter/sec
ZDOT = 11402
295009 ZDOT = 3475
419519
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 11007
55388091
00016717 00000-0 10270-3 0 9049
2 25544 51
6456 264
3914 0004700 112
4349 247
7311 15
72602576 15623
Satellite: ISS
Catalog Number: 25544
Epoch time: 11007
55388091 = yrday
fracday
Element set: 904
Inclination: 51
6456 deg
RA of node: 264
3914 deg
Eccentricity:
0004700
Arg of perigee: 112
4349 deg
Mean anomaly: 247
7311 deg
Mean motion: 15
72602576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1562
Checksum: 296
Coasting Arc #6 (Orbit 1576)
---------------------------------------
Vector Time (GMT): 2011/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3658564
78 A = 6731044
13 meter
Y = -4544765
98 meter E =
0009168
Z = -3366421
37 I = 51
31368
XDOT = 2656
706487 Wp = 102
60606
YDOT = -5549
261895 meter/sec RA = 258
68427 deg
ZDOT = 4613
014131 TA = 217
58305
MA = 217
64716
Ha = 193
730 n
mi
Hp = 184
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12003165
27 X = -3591119
29
Y = -14910649
55 feet Y = -4585300
95 meter
Z = -11044689
55 Z = -3384030
79
XDOT = 8716
228631 XDOT = 2696
153168
YDOT = -18206
239814 feet/sec YDOT = -5519
332718 meter/sec
ZDOT = 15134
560797 ZDOT = 4626
015646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10794431
34 X = 3290142
67
Y = -15758025
27 feet Y = -4803046
10 meter
Z = -11115462
45 Z = -3387992
96
XDOT = 18778
318882 XDOT = 5723
631595
YDOT = 2170
486395 feet/sec YDOT = 661
564253 meter/sec
ZDOT = 15187
014657 ZDOT = 4629
002067
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 11008
50705519
00016717 00000-0 10270-3 0 9054
2 25544 51
6456 259
5067 0004529 116
0265 244
1364 15
72648823 15774
Satellite: ISS
Catalog Number: 25544
Epoch time: 11008
50705519 = yrday
fracday
Element set: 905
Inclination: 51
6456 deg
RA of node: 259
5067 deg
Eccentricity:
0004529
Arg of perigee: 116
0265 deg
Mean anomaly: 244
1364 deg
Mean motion: 15
72648823 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1577
Checksum: 312
Coasting Arc #7 (Orbit 1592)
---------------------------------------
Vector Time (GMT): 2011/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1569852
26 A = 6729757
37 meter
Y = 5354269
95 meter E =
0009727
Z = -3770258
24 I = 51
31642
XDOT = -4773
264283 Wp = 94
75419
YDOT = -4340
579587 meter/sec RA = 253
58707 deg
ZDOT = -4186
800291 TA = 131
07236
MA = 130
98829
Ha = 193
596 n
mi
Hp = 184
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5150433
91 X = -1611293
11
Y = 17566502
45 feet Y = 5336483
39 meter
Z = -12369613
64 Z = -3777984
85
XDOT = -15660
315889 XDOT = -4704
033967
YDOT = -14240
746677 feet/sec YDOT = -4393
569817 meter/sec
ZDOT = -13736
221426 ZDOT = -4209
820476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18276072
55 X = -5570546
91
Y = 566585
24 feet Y = 172695
18 meter
Z = -12400825
49 Z = -3779771
61
XDOT = 8806
909517 XDOT = 2684
346021
YDOT = -17867
734600 feet/sec YDOT = -5446
085506 meter/sec
ZDOT = -13828
787019 ZDOT = -4215
014283
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 11009
52375095
00016717 00000-0 10270-3 0 9060
2 25544 51
6454 254
2959 0004380 121
2404 238
9188 15
72673138 15932
Satellite: ISS
Catalog Number: 25544
Epoch time: 11009
52375095 = yrday
fracday
Element set: 906
Inclination: 51
6454 deg
RA of node: 254
2959 deg
Eccentricity:
0004380
Arg of perigee: 121
2404 deg
Mean anomaly: 238
9188 deg
Mean motion: 15
72673138 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1593
Checksum: 316
Coasting Arc #8 (Orbit 1608)
---------------------------------------
Vector Time (GMT): 2011/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4566711
30 A = 6728883
54 meter
Y = 2970047
85 meter E =
0014429
Z = 3937287
75 I = 51
32405
XDOT = -824
857725 Wp = 91
03253
YDOT = 6550
457422 meter/sec RA = 248
38681 deg
ZDOT = -3972
267061 TA = 40
34852
MA = 40
24156
Ha = 193
353 n
mi
Hp = 184
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14982648
63 X = 4514033
89
Y = 9744251
48 feet Y = 3020820
86 meter
Z = 12917610
71 Z = 3959344
71
XDOT = -2706
226133 XDOT = -878
748570
YDOT = 21491
002042 feet/sec YDOT = 6540
932221 meter/sec
ZDOT = -13032
372246 ZDOT = -3976
404776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4397138
06 X = -1340247
68
Y = 17256745
68 feet Y = 5259856
08 meter
Z = 13006335
72 Z = 3964331
13
XDOT = -19926
353976 XDOT = -6073
552692
YDOT = 4787
864280 feet/sec YDOT = 1459
341033 meter/sec
ZDOT = -13049
156021 ZDOT = -3977
382755
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 11010
54042186
00016717 00000-0 10270-3 0 9077
2 25544 51
6454 249
0851 0004340 122
9058 237
2523 15
72755852 16091
Satellite: ISS
Catalog Number: 25544
Epoch time: 11010
54042186 = yrday
fracday
Element set: 907
Inclination: 51
6454 deg
RA of node: 249
0851 deg
Eccentricity:
0004340
Arg of perigee: 122
9058 deg
Mean anomaly: 237
2523 deg
Mean motion: 15
72755852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1609
Checksum: 292
Coasting Arc #9 (Orbit 1624)
---------------------------------------
Vector Time (GMT): 2011/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -166952
75 A = 6731452
46 meter
Y = -5939481
16 meter E =
0016502
Z = 3151191
93 I = 51
34426
XDOT = 5515
251060 Wp = 95
88520
YDOT = 2407
371922 meter/sec RA = 243
28919 deg
ZDOT = 4806
469336 TA = 300
98292
MA = 301
14493
Ha = 193
431 n
mi
Hp = 184
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -547745
25 X = -115831
71
Y = -19486486
74 feet Y = -5941062
44 meter
Z = 10338556
19 Z = 3150504
77
XDOT = 18094
655709 XDOT = 5464
572753
YDOT = 7898
201845 feet/sec YDOT = 2468
763205 meter/sec
ZDOT = 15769
256352 ZDOT = 4833
139163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18119336
66 X = 5522773
81
Y = -7194979
08 feet Y = -2193029
63 meter
Z = 10335901
01 Z = 3150382
63
XDOT = -1836
497581 XDOT = -559
764463
YDOT = 18292
011141 feet/sec YDOT = 5575
404996 meter/sec
ZDOT = 15876
567607 ZDOT = 4839
177806
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 11011
55706996
00016717 00000-0 10270-3 0 9086
2 25544 51
6449 243
8736 0004292 126
7152 233
4405 15
72742072 16257
Satellite: ISS
Catalog Number: 25544
Epoch time: 11011
55706996 = yrday
fracday
Element set: 908
Inclination: 51
6449 deg
RA of node: 243
8736 deg
Eccentricity:
0004292
Arg of perigee: 126
7152 deg
Mean anomaly: 233
4405 deg
Mean motion: 15
72742072 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1625
Checksum: 307
Coasting Arc #10 (Orbit 1639)
---------------------------------------
Vector Time (GMT): 2011/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828621
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4931374
66 A = 6727003
09 meter
Y = -1230210
97 meter E =
0013540
Z = -4420720
97 I = 51
34436
XDOT = -1204
635715 Wp = 117
39749
YDOT = -6859
550792 meter/sec RA = 238
09281 deg
ZDOT = 3254
183488 TA = 185
42073
MA = 185
43540
Ha = 193
246 n
mi
Hp = 184
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16179050
72 X = -4895776
81
Y = -4036125
23 feet Y = -1285157
30 meter
Z = -14503677
71 Z = -4444591
00
XDOT = -3952
216914 XDOT = -1143
649508
YDOT = -22505
087900 feet/sec YDOT = -6872
680940 meter/sec
ZDOT = 10676
455013 ZDOT = 3248
479175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1955744
92 X = -596111
05
Y = -16475166
01 feet Y = -5021630
60 meter
Z = -14599747
37 Z = -4450003
00
XDOT = 18399
860425 XDOT = 5608
277458
YDOT = -11620
770565 feet/sec YDOT = -3542
010868 meter/sec
ZDOT = 10653
614636 ZDOT = 3247
221741
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 11012
51015307
00016717 00000-0 10270-3 0 9093
2 25544 51
6444 238
9878 0004195 132
2291 227
9228 15
72804843 16405
Satellite: ISS
Catalog Number: 25544
Epoch time: 11012
51015307 = yrday
fracday
Element set: 909
Inclination: 51
6444 deg
RA of node: 238
9878 deg
Eccentricity:
0004195
Arg of perigee: 132
2291 deg
Mean anomaly: 227
9228 deg
Mean motion: 15
72804843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1640
Checksum: 302
Coasting Arc #11 (Orbit 1653)
---------------------------------------
Vector Time (GMT): 2011/013/09:12:06
973
Vector Time (MET): N/A
Weight (LBS) : 828127
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3263820
48 A = 6726310
82 meter
Y = 2659373
02 meter E =
0015010
Z = -5258052
88 I = 51
34812
XDOT = -4680
093797 Wp = 107
07740
YDOT = -6095
501306 meter/sec RA = 233
57221 deg
ZDOT = -182
634061 TA = 161
20700
MA = 161
15153
Ha = 193
941 n
mi
Hp = 187
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10708072
46 X = -3267773
02
Y = 8724977
10 feet Y = 2622853
25 meter
Z = -17250829
65 Z = -5273917
84
XDOT = -15354
638443 XDOT = -4610
697723
YDOT = -19998
363864 feet/sec YDOT = -6147
448911 meter/sec
ZDOT = -599
193114 ZDOT = -205
201645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4514820
17 X = -1376117
19
Y = -12969005
82 feet Y = -3952952
97 meter
Z = -17314746
65 Z = -5277534
78
XDOT = 23129
567784 XDOT = 7049
892260
YDOT = -7151
633655 feet/sec YDOT = -2179
817938 meter/sec
ZDOT = -689
940982 ZDOT = -210
294011
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 11013
39968592
00016717 00000-0 10270-3 0 9105
2 25544 51
6450 234
4284 0004813 187
7416 172
3673 15
71829220 16542
Satellite: ISS
Catalog Number: 25544
Epoch time: 11013
39968592 = yrday
fracday
Element set: 910
Inclination: 51
6450 deg
RA of node: 234
4284 deg
Eccentricity:
0004813
Arg of perigee: 187
7416 deg
Mean anomaly: 172
3673 deg
Mean motion: 15
71829220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1654
Checksum: 311
Coasting Arc #12 (Orbit 1669)
---------------------------------------
Vector Time (GMT): 2011/014/09:12:06
973
Vector Time (MET): N/A
Weight (LBS) : 828127
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4912052
89 A = 6738067
91 meter
Y = 4519761
45 meter E =
0016217
Z = 846139
04 I = 51
40648
XDOT = -2720
674436 Wp = 142
01759
YDOT = 4077
916474 meter/sec RA = 228
42477 deg
ZDOT = -5940
843334 TA = 28
72351
MA = 28
63429
Ha = 193
869 n
mi
Hp = 187
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16115659
09 X = 4857036
63
Y = 14828613
67 feet Y = 4574383
30 meter
Z = 2776046
73 Z = 869868
38
XDOT = -8926
097230 XDOT = -2737
212903
YDOT = 13378
991055 feet/sec YDOT = 4047
400264 meter/sec
ZDOT = -19490
955821 ZDOT = -5954
100125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19309575
45 X = -5885558
60
Y = 10305504
14 feet Y = 3141117
66 meter
Z = 2871509
55 Z = 875236
11
XDOT = -8971
394083 XDOT = -2734
480916
YDOT = -11321
884970 feet/sec YDOT = -3450
910539 meter/sec
ZDOT = -19544
400577 ZDOT = -5957
133296
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 11014
41692174
00016717 00000-0 10270-3 0 9110
2 25544 51
6448 229
2218 0004913 191
7630 168
3418 15
71817595 16704
Satellite: ISS
Catalog Number: 25544
Epoch time: 11014
41692174 = yrday
fracday
Element set: 911
Inclination: 51
6448 deg
RA of node: 229
2218 deg
Eccentricity:
0004913
Arg of perigee: 191
7630 deg
Mean anomaly: 168
3418 deg
Mean motion: 15
71817595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1670
Checksum: 308
Coasting Arc #13 (Orbit 1685)
---------------------------------------
Vector Time (GMT): 2011/015/09:12:06
973
Vector Time (MET): N/A
Weight (LBS) : 828127
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1335587
88 A = 6727174
65 meter
Y = -4261443
14 meter E =
0008218
Z = 5030424
54 I = 51
39159
XDOT = 6315
139902 Wp = 158
54472
YDOT = 4043
568562 meter/sec RA = 223
31140 deg
ZDOT = 1740
329863 TA = 274
59181
MA = 274
68567
Ha = 193
609 n
mi
Hp = 187
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4381849
99 X = 1358704
18
Y = -13981112
66 feet Y = -4246379
04 meter
Z = 16504017
51 Z = 5036968
50
XDOT = 20718
962934 XDOT = 6261
000464
YDOT = 13266
301058 feet/sec YDOT = 4113
885382 meter/sec
ZDOT = 5709
743645 ZDOT = 1770
877462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11931808
73 X = 3636815
30
Y = 8451699
73 feet Y = 2576078
08 meter
Z = 16530439
40 Z = 5038477
93
XDOT = -18467
913392 XDOT = -5629
020002
YDOT = 14610
347543 feet/sec YDOT = 4453
233931 meter/sec
ZDOT = 5832
681413 ZDOT = 1777
801295
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 11015
43413240
00016717 00000-0 10270-3 0 9129
2 25544 51
6449 224
0148 0004734 196
7780 163
3227 15
71887557 16867
Satellite: ISS
Catalog Number: 25544
Epoch time: 11015
43413240 = yrday
fracday
Element set: 912
Inclination: 51
6449 deg
RA of node: 224
0148 deg
Eccentricity:
0004734
Arg of perigee: 196
7780 deg
Mean anomaly: 163
3227 deg
Mean motion: 15
71887557 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1686
Checksum: 310
Coasting Arc #14 (Orbit 1700)
---------------------------------------
Vector Time (GMT): 2011/016/09:12:06
973
Vector Time (MET): N/A
Weight (LBS) : 828127
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5895332
70 A = 6735994
16 meter
Y = -2446148
08 meter E =
0002405
Z = -2154513
25 I = 51
44467
XDOT = 229
342327 Wp = 84
29661
YDOT = -5383
037760 meter/sec RA = 218
14198 deg
ZDOT = 5489
630404 TA = 251
56250
MA = 251
58865
Ha = 193
398 n
mi
Hp = 187
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19341642
70 X = -5857075
14
Y = -8025420
23 feet Y = -2511859
10 meter
Z = -7068613
04 Z = -2183059
80
XDOT = 752
435455 XDOT = 262
852105
YDOT = -17660
885041 feet/sec YDOT = -5380
286377 meter/sec
ZDOT = 18010
598437 ZDOT = 5490
825319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13399360
82 X = 4084125
18
Y = -16041376
09 feet Y = -4889411
43 meter
Z = -7183535
70 Z = -2189541
68
XDOT = 15500
513028 XDOT = 4724
556371
YDOT = 4887
938240 feet/sec YDOT = 1489
843576 meter/sec
ZDOT = 18015
498403 ZDOT = 5491
123913
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 11016
38774666
00016717 00000-0 10270-3 0 9137
2 25544 51
6447 219
1329 0004655 202
3069 157
7891 15
71928580 17011
Satellite: ISS
Catalog Number: 25544
Epoch time: 11016
38774666 = yrday
fracday
Element set: 913
Inclination: 51
6447 deg
RA of node: 219
1329 deg
Eccentricity:
0004655
Arg of perigee: 202
3069 deg
Mean anomaly: 157
7891 deg
Mean motion: 15
71928580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1701
Checksum: 322
Coasting Arc #15 (Orbit 1716)
---------------------------------------
Vector Time (GMT): 2011/017/09:12:06
973
Vector Time (MET): N/A
Weight (LBS) : 828127
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 967760
14 A = 6729220
44 meter
Y = 4911249
22 meter E =
0007045
Z = -4502950
80 I = 51
44599
XDOT = -6868
477579 Wp = 95
58150
YDOT = -1502
625001 meter/sec RA = 213
05085 deg
ZDOT = -3119
881420 TA = 143
20066
MA = 143
15228
Ha = 193
172 n
mi
Hp = 187
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3175066
07 X = 934643
85
Y = 16113022
37 feet Y = 4921886
67 meter
Z = -14773460
62 Z = -4498329
35
XDOT = -22534
375259 XDOT = -6836
008899
YDOT = -4929
872050 feet/sec YDOT = -1579
250544 meter/sec
ZDOT = -10235
831429 ZDOT = -3153
169242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16380488
81 X = -4992772
99
Y = -1391938
05 feet Y = -424262
72 meter
Z = -14754923
52 Z = -4497300
69
XDOT = 10940
128343 XDOT = 3334
551119
YDOT = -18990
209940 feet/sec YDOT = -5788
215990 meter/sec
ZDOT = -10369
883488 ZDOT = -3160
740487
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 11017
40491212
00016717 00000-0 10270-3 0 9145
2 25544 51
6440 213
9254 0004644 208
4349 151
6560 15
71960131 17170
Satellite: ISS
Catalog Number: 25544
Epoch time: 11017
40491212 = yrday
fracday
Element set: 914
Inclination: 51
6440 deg
RA of node: 213
9254 deg
Eccentricity:
0004644
Arg of perigee: 208
4349 deg
Mean anomaly: 151
6560 deg
Mean motion: 15
71960131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1717
Checksum: 279
Coasting Arc #16 (Orbit 1732)
---------------------------------------
Vector Time (GMT): 2011/018/09:12:06
973
Vector Time (MET): N/A
Weight (LBS) : 828127
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5879819
57 A = 6733099
32 meter
Y = 172080
63 meter E =
0011125
Z = 3262654
89 I = 51
48599
XDOT = 2464
887473 Wp = 112
23996
YDOT = 5558
637374 meter/sec RA = 207
87039 deg
ZDOT = -4726
615982 TA = 29
45166
MA = 29
38903
Ha = 192
846 n
mi
Hp = 187
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19290746
62 X = 5861609
30
Y = 564569
00 feet Y = 237730
13 meter
Z = 10704248
32 Z = 3291174
20
XDOT = 8086
901158 XDOT = 2425
507078
YDOT = 18236
999260 feet/sec YDOT = 5585
981578 meter/sec
ZDOT = -15507
270282 ZDOT = -4714
736852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5624891
66 X = -1714466
98
Y = 18394008
55 feet Y = 5606493
81 meter
Z = 10819132
07 Z = 3297671
45
XDOT = -18408
087489 XDOT = -5610
785067
YDOT = 3480
459074 feet/sec YDOT = 1060
843926 meter/sec
ZDOT = -15459
498682 ZDOT = -4712
055198
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 11018
42205411
00016717 00000-0 10270-3 0 9153
2 25544 51
6440 208
7180 0004493 212
2552 147
8336 15
72018854 17334
Satellite: ISS
Catalog Number: 25544
Epoch time: 11018
42205411 = yrday
fracday
Element set: 915
Inclination: 51
6440 deg
RA of node: 208
7180 deg
Eccentricity:
0004493
Arg of perigee: 212
2552 deg
Mean anomaly: 147
8336 deg
Mean motion: 15
72018854 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1733
Checksum: 281
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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