Date:
November 4th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15607 67 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 506)
---------------------------------------
Vector Time (GMT): 2010/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3120572
50 A = 6726120
30 meter
Y = 3108147
23 meter E =
0018008
Z = -5097836
15 I = 51
31095
XDOT = -3981
916594 Wp = 102
36975
YDOT = -6405
909663 meter/sec RA = 247
15355 deg
ZDOT = -1476
396293 TA = 153
42952
MA = 153
33710
Ha = 195
180 n
mi
Hp = 184
702
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10238098
75 X = -3130331
68
Y = 10197333
43 feet Y = 3073196
32 meter
Z = -16725184
22 Z = -5113019
98
XDOT = -13064
030821 XDOT = -3902
816393
YDOT = -21016
763985 feet/sec YDOT = -6449
995641 meter/sec
ZDOT = -4843
819858 ZDOT = -1495
548330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1240310
73 X = 378046
71
Y = -14325694
95 feet Y = -4366471
82 meter
Z = -16786070
29 Z = -5116394
22
XDOT = 22435
013370 XDOT = 6838
192075
YDOT = 7676
730043 feet/sec YDOT = 2339
867317 meter/sec
ZDOT = -4920
613980 ZDOT = -1499
803141
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 10305
51847466
00016717 00000-0 10270-3 0 9007
2 25544 51
6435 247
9294 0007674 148
6083 211
5539 15
72150500 5071
Satellite: ISS
Catalog Number: 25544
Epoch time: 10305
51847466 = yrday
fracday
Element set: 900
Inclination: 51
6435 deg
RA of node: 247
9294 deg
Eccentricity:
0007674
Arg of perigee: 148
6083 deg
Mean anomaly: 211
5539 deg
Mean motion: 15
72150500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 507
Checksum: 302
Coasting Arc #2 (Orbit 522)
---------------------------------------
Vector Time (GMT): 2010/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4257271
92 A = 6735822
60 meter
Y = 4868513
34 meter E =
0020674
Z = 1840170
71 I = 51
35759
XDOT = -2704
978919 Wp = 127
04261
YDOT = 4507
029313 meter/sec RA = 241
98090 deg
ZDOT = -5634
980883 TA = 32
44665
MA = 32
31971
Ha = 195
020 n
mi
Hp = 184
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13967427
57 X = 4193575
49
Y = 15972812
79 feet Y = 4915764
66 meter
Z = 6037305
47 Z = 1860697
99
XDOT = -8874
602754 XDOT = -2727
802031
YDOT = 14786
841577 feet/sec YDOT = 4476
652712 meter/sec
ZDOT = -18487
470089 ZDOT = -5648
177610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20986848
41 X = -6396791
40
Y = -2961630
30 feet Y = -902704
92 meter
Z = 6119622
41 Z = 1865260
91
XDOT = -3264
461322 XDOT = -995
007811
YDOT = -15385
777519 feet/sec YDOT = -4689
584988 meter/sec
ZDOT = -18540
386237 ZDOT = -5651
109725
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 10306
53548594
00016717 00000-0 10270-3 0 9011
2 25544 51
6441 242
7211 0007686 152
2129 207
9445 15
72192205 5236
Satellite: ISS
Catalog Number: 25544
Epoch time: 10306
53548594 = yrday
fracday
Element set: 901
Inclination: 51
6441 deg
RA of node: 242
7211 deg
Eccentricity:
0007686
Arg of perigee: 152
2129 deg
Mean anomaly: 207
9445 deg
Mean motion: 15
72192205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 523
Checksum: 291
Coasting Arc #3 (Orbit 538)
---------------------------------------
Vector Time (GMT): 2010/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1472593
75 A = 6727545
82 meter
Y = -4596787
51 meter E =
0014629
Z = 4682408
76 I = 51
34596
XDOT = 5573
332308 Wp = 137
40817
YDOT = 4567
320756 meter/sec RA = 236
87705 deg
ZDOT = 2715
447848 TA = 285
66736
MA = 285
82872
Ha = 194
845 n
mi
Hp = 184
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4831344
32 X = 1501139
55
Y = -15081323
86 feet Y = -4580160
27 meter
Z = 15362233
46 Z = 4689632
35
XDOT = 18285
210984 XDOT = 5508
653954
YDOT = 14984
648151 feet/sec YDOT = 4629
283595 meter/sec
ZDOT = 8908
949632 ZDOT = 2742
366485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6533100
91 X = 1991289
16
Y = 14395002
72 feet Y = 4387596
83 meter
Z = 15391196
29 Z = 4691236
63
XDOT = -22528
730749 XDOT = -6866
757132
YDOT = 529
124514 feet/sec YDOT = 161
277152 meter/sec
ZDOT = 9016
901778 ZDOT = 2748
351662
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 10307
55246606
00016717 00000-0 10270-3 0 9024
2 25544 51
6444 237
5130 0007707 157
3284 202
8220 15
72269752 5397
Satellite: ISS
Catalog Number: 25544
Epoch time: 10307
55246606 = yrday
fracday
Element set: 902
Inclination: 51
6444 deg
RA of node: 237
5130 deg
Eccentricity:
0007707
Arg of perigee: 157
3284 deg
Mean anomaly: 202
8220 deg
Mean motion: 15
72269752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 539
Checksum: 295
Coasting Arc #4 (Orbit 553)
---------------------------------------
Vector Time (GMT): 2010/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5299466
66 A = 6733451
90 meter
Y = -3029272
41 meter E =
0008474
Z = -2855018
47 I = 51
38391
XDOT = 580
868277 Wp = 127
97690
YDOT = -5769
077705 meter/sec RA = 231
69016 deg
ZDOT = 5048
043040 TA = 199
18776
MA = 199
21969
Ha = 194
741 n
mi
Hp = 184
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17386701
63 X = -5251329
31
Y = -9938557
76 feet Y = -3088265
15 meter
Z = -9366858
50 Z = -2880647
05
XDOT = 1905
735816 XDOT = 620
812778
YDOT = -18927
420291 feet/sec YDOT = -5762
358621 meter/sec
ZDOT = 16561
820999 ZDOT = 5050
962154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19465485
15 X = 5933079
87
Y = -4497905
59 feet Y = -1370961
62 meter
Z = -9469640
70 Z = -2886346
49
XDOT = 11217
363278 XDOT = 3419
052327
YDOT = 13686
716236 feet/sec YDOT = 4171
711109 meter/sec
ZDOT = 16573
521609 ZDOT = 5051
609386
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 10308
50586073
00016717 00000-0 10270-3 0 9036
2 25544 51
6445 232
6294 0007603 160
4343 199
7112 15
72283274 5547
Satellite: ISS
Catalog Number: 25544
Epoch time: 10308
50586073 = yrday
fracday
Element set: 903
Inclination: 51
6445 deg
RA of node: 232
6294 deg
Eccentricity:
0007603
Arg of perigee: 160
4343 deg
Mean anomaly: 199
7112 deg
Mean motion: 15
72283274 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 554
Checksum: 297
Coasting Arc #5 (Orbit 569)
---------------------------------------
Vector Time (GMT): 2010/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 490395
64 A = 6729541
93 meter
Y = 5303855
24 meter E =
0010494
Z = -4117615
19 I = 51
39188
XDOT = -6307
355673 Wp = 116
97432
YDOT = -2315
843873 meter/sec RA = 226
59862 deg
ZDOT = -3746
213408 TA = 114
53164
MA = 114
42221
Ha = 194
554 n
mi
Hp = 185
075
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1608909
59 X = 451053
78
Y = 17401099
86 feet Y = 5309119
17 meter
Z = -13509236
19 Z = -4115328
32
XDOT = -20693
424123 XDOT = -6262
791672
YDOT = -7597
912968 feet/sec YDOT = -2386
127337 meter/sec
ZDOT = -12290
726405 ZDOT = -3776
747296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13268875
95 X = -4044353
39
Y = -11382952
80 feet Y = -3469524
01 meter
Z = -13500060
94 Z = -4114818
57
XDOT = 19307
180284 XDOT = 5884
828551
YDOT = -7830
853130 feet/sec YDOT = -2386
844034 meter/sec
ZDOT = -12413
187203 ZDOT = -3783
539460
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 10309
52278540
00016717 00000-0 10270-3 0 9047
2 25544 51
6455 227
4204 0007590 163
8409 196
2997 15
72345785 5703
Satellite: ISS
Catalog Number: 25544
Epoch time: 10309
52278540 = yrday
fracday
Element set: 904
Inclination: 51
6455 deg
RA of node: 227
4204 deg
Eccentricity:
0007590
Arg of perigee: 163
8409 deg
Mean anomaly: 196
2997 deg
Mean motion: 15
72345785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 570
Checksum: 324
Coasting Arc #6 (Orbit 585)
---------------------------------------
Vector Time (GMT): 2010/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5545096
78 A = 6730873
91 meter
Y = 988498
64 meter E =
0014700
Z = 3668043
51 I = 51
41801
XDOT = 1762
023788 Wp = 115
46398
YDOT = 6139
495201 meter/sec RA = 221
40855 deg
ZDOT = -4311
056394 TA = 20
26183
MA = 20
20356
Ha = 194
327 n
mi
Hp = 185
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18192574
75 X = 5515811
81
Y = 3243105
77 feet Y = 1050343
40 meter
Z = 12034263
47 Z = 3694911
35
XDOT = 5780
917940 XDOT = 1714
182857
YDOT = 20142
700790 feet/sec YDOT = 6158
931845 meter/sec
ZDOT = -14143
885808 ZDOT = -4302
612235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15140578
63 X = -4614848
37
Y = 10471150
78 feet Y = 3191606
76 meter
Z = 12142029
83 Z = 3700890
69
XDOT = -17593
639171 XDOT = -5362
541219
YDOT = -9050
600861 feet/sec YDOT = -2758
623142 meter/sec
ZDOT = -14110
015449 ZDOT = -4300
732709
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 10310
53968139
00016717 00000-0 10270-3 0 9051
2 25544 51
6450 222
2120 0007631 168
0324 192
1021 15
72365844 5865
Satellite: ISS
Catalog Number: 25544
Epoch time: 10310
53968139 = yrday
fracday
Element set: 905
Inclination: 51
6450 deg
RA of node: 222
2120 deg
Eccentricity:
0007631
Arg of perigee: 168
0324 deg
Mean anomaly: 192
1021 deg
Mean motion: 15
72365844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 586
Checksum: 280
Coasting Arc #7 (Orbit 601)
---------------------------------------
Vector Time (GMT): 2010/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2555600
37 A = 6731774
67 meter
Y = -5225858
02 meter E =
0015532
Z = 3383597
29 I = 51
44498
XDOT = 6168
188767 Wp = 118
88368
YDOT = -20
095206 meter/sec RA = 216
32194 deg
ZDOT = 4604
416249 TA = 281
12745
MA = 281
30205
Ha = 194
279 n
mi
Hp = 185
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8384515
66 X = -2513411
30
Y = -17145203
48 feet Y = -5254200
57 meter
Z = 11101040
97 Z = 3371284
03
XDOT = 20236
839788 XDOT = 6145
586965
YDOT = -65
929153 feet/sec YDOT = 48
754574 meter/sec
ZDOT = 15106
352523 ZDOT = 4634
327279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18182710
83 X = 5542090
26
Y = 5894175
68 feet Y = 1796544
75 meter
Z = 11051648
56 Z = 3368542
48
XDOT = -13568
554645 XDOT = -4135
695456
YDOT = 13163
413107 feet/sec YDOT = 4012
208315 meter/sec
ZDOT = 15226
338580 ZDOT = 4640
987999
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 10311
55654738
00016717 00000-0 10270-3 0 9062
2 25544 51
6451 217
0027 0007557 172
1396 187
9886 15
72414287 6022
Satellite: ISS
Catalog Number: 25544
Epoch time: 10311
55654738 = yrday
fracday
Element set: 906
Inclination: 51
6451 deg
RA of node: 217
0027 deg
Eccentricity:
0007557
Arg of perigee: 172
1396 deg
Mean anomaly: 187
9886 deg
Mean motion: 15
72414287 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 602
Checksum: 318
Coasting Arc #8 (Orbit 616)
---------------------------------------
Vector Time (GMT): 2010/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5074586
70 A = 6728325
72 meter
Y = 960821
52 meter E =
0013892
Z = -4326301
13 I = 51
45955
XDOT = -3989
742400 Wp = 140
56442
YDOT = -5603
104626 meter/sec RA = 211
13532 deg
ZDOT = 3430
912457 TA = 164
25320
MA = 164
20995
Ha = 194
034 n
mi
Hp = 185
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16648906
50 X = -5063936
72
Y = 3152301
57 feet Y = 904134
28 meter
Z = -14193901
36 Z = -4350928
15
XDOT = -13089
706037 XDOT = -3943
458073
YDOT = -18382
889192 feet/sec YDOT = -5647
461761 meter/sec
ZDOT = 11256
274466 ZDOT = 3411
641867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9044695
61 X = 2756823
22
Y = -14230320
19 feet Y = -4337401
59 meter
Z = -14292704
33 Z = -4356416
28
XDOT = 21368
032898 XDOT = 6512
976427
YDOT = 2338
618435 feet/sec YDOT = 712
810899 meter/sec
ZDOT = 11178
964354 ZDOT = 3407
348335
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 10312
50983224
00016717 00000-0 10270-3 0 9074
2 25544 51
6453 212
1188 0007507 176
4046 183
7172 15
72467859 6173
Satellite: ISS
Catalog Number: 25544
Epoch time: 10312
50983224 = yrday
fracday
Element set: 907
Inclination: 51
6453 deg
RA of node: 212
1188 deg
Eccentricity:
0007507
Arg of perigee: 176
4046 deg
Mean anomaly: 183
7172 deg
Mean motion: 15
72467859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 617
Checksum: 311
Coasting Arc #9 (Orbit 632)
---------------------------------------
Vector Time (GMT): 2010/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4339791
35 A = 6733580
75 meter
Y = 4430778
65 meter E =
0011390
Z = -2609173
52 I = 51
50382
XDOT = -5251
221687 Wp = 160
64979
YDOT = 2069
490553 meter/sec RA = 206
04679 deg
ZDOT = -5237
017377 TA = 49
05072
MA = 48
95219
Ha = 193
931 n
mi
Hp = 185
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14238160
60 X = 4302598
16
Y = 14536675
37 feet Y = 4479101
03 meter
Z = -8560280
57 Z = -2588180
42
XDOT = -17228
417607 XDOT = -5248
531844
YDOT = 6789
667169 feet/sec YDOT = 2010
783646 meter/sec
ZDOT = -17181
815541 ZDOT = -5262
521636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20367063
94 X = -6207881
09
Y = 811095
79 feet Y = 247222
00 meter
Z = -8476047
51 Z = -2583499
28
XDOT = 6541
925284 XDOT = 1993
978827
YDOT = -15759
067023 feet/sec YDOT = -4803
363629 meter/sec
ZDOT = -17284
152286 ZDOT = -5268
209617
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 10313
52664189
00016717 00000-0 10270-3 0 9084
2 25544 51
6453 206
9092 0007592 181
4740 178
6402 15
72488107 6335
Satellite: ISS
Catalog Number: 25544
Epoch time: 10313
52664189 = yrday
fracday
Element set: 908
Inclination: 51
6453 deg
RA of node: 206
9092 deg
Eccentricity:
0007592
Arg of perigee: 181
4740 deg
Mean anomaly: 178
6402 deg
Mean motion: 15
72488107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 633
Checksum: 313
Coasting Arc #10 (Orbit 648)
---------------------------------------
Vector Time (GMT): 2010/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3960358
54 A = 6726109
30 meter
Y = -2564519
09 meter E =
0006578
Z = 4787578
82 I = 51
50732
XDOT = 5841
156604 Wp = 125
33474
YDOT = 4355
172928 meter/sec RA = 200
87159 deg
ZDOT = -2500
335267 TA = 349
15909
MA = 349
17326
Ha = 193
463 n
mi
Hp = 185
649
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12993302
31 X = 3965483
57
Y = -8413776
53 feet Y = -2520203
63 meter
Z = 15707279
59 Z = 4806830
82
XDOT = 19163
899619 XDOT = 5804
168484
YDOT = 14288
625093 feet/sec YDOT = 4420
285604 meter/sec
ZDOT = -8203
199695 ZDOT = -2472
048046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2177805
50 X = -663795
12
Y = 15246037
64 feet Y = 4646992
27 meter
Z = 15784539
01 Z = 4811127
49
XDOT = -22297
610911 XDOT = -6796
311806
YDOT = 5185
815306 feet/sec YDOT = 1580
636505 meter/sec
ZDOT = -8089
682159 ZDOT = -2465
735122
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 10314
54342128
00016717 00000-0 10270-3 0 9094
2 25544 51
6449 201
6994 0007404 185
6739 174
4341 15
72593836 6498
Satellite: ISS
Catalog Number: 25544
Epoch time: 10314
54342128 = yrday
fracday
Element set: 909
Inclination: 51
6449 deg
RA of node: 201
6994 deg
Eccentricity:
0007404
Arg of perigee: 185
6739 deg
Mean anomaly: 174
4341 deg
Mean motion: 15
72593836 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 649
Checksum: 326
Coasting Arc #11 (Orbit 664)
---------------------------------------
Vector Time (GMT): 2010/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5727659
68 A = 6734892
58 meter
Y = -3070382
82 meter E =
0011636
Z = 1761201
14 I = 51
56544
XDOT = 3706
037864 Wp = 96
64476
YDOT = -3636
513345 meter/sec RA = 195
77479 deg
ZDOT = 5679
461714 TA = 282
86261
MA = 282
99258
Ha = 193
446 n
mi
Hp = 185
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18791534
37 X = -5701456
09
Y = -10073434
45 feet Y = -3134286
53 meter
Z = 5778218
97 Z = 1733439
30
XDOT = 12158
916878 XDOT = 3718
836440
YDOT = -11930
818061 feet/sec YDOT = -3594
998938 meter/sec
ZDOT = 18633
404575 ZDOT = 5697
496775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19852692
04 X = 6051100
53
Y = -7857590
13 feet Y = -2394993
47 meter
Z = 5666794
18 Z = 1727238
87
XDOT = 746
197141 XDOT = 227
440889
YDOT = 15456
185479 feet/sec YDOT = 4711
045334 meter/sec
ZDOT = 18705
787810 ZDOT = 5701
524124
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 10315
56017427
00016717 00000-0 10270-3 0 9100
2 25544 51
6448 196
4887 0007378 189
5195 170
5828 15
72592677 6655
Satellite: ISS
Catalog Number: 25544
Epoch time: 10315
56017427 = yrday
fracday
Element set: 910
Inclination: 51
6448 deg
RA of node: 196
4887 deg
Eccentricity:
0007378
Arg of perigee: 189
5195 deg
Mean anomaly: 170
5828 deg
Mean motion: 15
72592677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 665
Checksum: 349
Coasting Arc #12 (Orbit 679)
---------------------------------------
Vector Time (GMT): 2010/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2451635
90 A = 6724693
17 meter
Y = 3655788
89 meter E =
0015414
Z = -5096267
06 I = 51
56138
XDOT = -7076
074806 Wp = 130
56348
YDOT = -2576
846427 meter/sec RA = 190
61521 deg
ZDOT = 1548
779490 TA = 154
37788
MA = 154
30141
Ha = 193
173 n
mi
Hp = 185
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8043424
85 X = -2467576
36
Y = 11994058
04 feet Y = 3628284
28 meter
Z = -16720036
28 Z = -5108215
83
XDOT = -23215
468524 XDOT = -7054
257894
YDOT = -8454
220562 feet/sec YDOT = -2655
853421 meter/sec
ZDOT = 5081
297538 ZDOT = 1514
456420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4256563
59 X = -1297400
58
Y = -13741532
43 feet Y = -4188419
08 meter
Z = -16767995
64 Z = -5110885
07
XDOT = 20256
629295 XDOT = 6174
220609
YDOT = -12334
037032 feet/sec YDOT = -3759
414487 meter/sec
ZDOT = 4943
521913 ZDOT = 1506
785479
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 10316
51335240
00016717 00000-0 10270-3 0 9113
2 25544 51
6447 191
6036 0007402 194
0380 166
0577 15
72655747 6808
Satellite: ISS
Catalog Number: 25544
Epoch time: 10316
51335240 = yrday
fracday
Element set: 911
Inclination: 51
6447 deg
RA of node: 191
6036 deg
Eccentricity:
0007402
Arg of perigee: 194
0380 deg
Mean anomaly: 166
0577 deg
Mean motion: 15
72655747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 680
Checksum: 295
Coasting Arc #13 (Orbit 695)
---------------------------------------
Vector Time (GMT): 2010/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6513817
13 A = 6735685
90 meter
Y = 1382635
74 meter E =
0015596
Z = -948361
59 I = 51
62834
XDOT = -1825
803792 Wp = 165
72247
YDOT = 4550
411089 meter/sec RA = 185
50909 deg
ZDOT = -5941
860635 TA = 24
63811
MA = 24
56368
Ha = 193
166 n
mi
Hp = 186
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21370791
10 X = 6502479
14
Y = 4536206
49 feet Y = 1455413
78 meter
Z = -3111422
54 Z = -916744
59
XDOT = -5990
169920 XDOT = -1847
686799
YDOT = 14929
170239 feet/sec YDOT = 4529
871615 meter/sec
ZDOT = -19494
293421 ZDOT = -5950
783563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16812538
73 X = -5124461
81
Y = 13978560
47 feet Y = 4260665
23 meter
Z = -2984496
65 Z = -909674
58
XDOT = -7059
117851 XDOT = -2151
619121
YDOT = -12634
142229 feet/sec YDOT = -3850
886552 meter/sec
ZDOT = -19530
107919 ZDOT = -5952
776894
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 10317
53004991
00016717 00000-0 10270-3 0 9123
2 25544 51
6448 186
3936 0007586 198
1282 161
9611 15
72642793 6965
Satellite: ISS
Catalog Number: 25544
Epoch time: 10317
53004991 = yrday
fracday
Element set: 912
Inclination: 51
6448 deg
RA of node: 186
3936 deg
Eccentricity:
0007586
Arg of perigee: 198
1282 deg
Mean anomaly: 161
9611 deg
Mean motion: 15
72642793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 696
Checksum: 332
Coasting Arc #14 (Orbit 711)
---------------------------------------
Vector Time (GMT): 2010/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 702146
34 A = 6723796
22 meter
Y = -4148999
51 meter E =
0005708
Z = 5244006
70 I = 51
61961
XDOT = 7657
051062 Wp = 182
88540
YDOT = 532
200418 meter/sec RA = 180
36822 deg
ZDOT = -609
797901 TA = 272
88039
MA = 272
94571
Ha = 192
787 n
mi
Hp = 186
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2303629
74 X = 723014
24
Y = -13612203
11 feet Y = -4141031
04 meter
Z = 17204746
39 Z = 5247468
43
XDOT = 25121
558601 XDOT = 7653
493133
YDOT = 1746
064365 feet/sec YDOT = 617
806281 meter/sec
ZDOT = -2000
649282 ZDOT = -572
608057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9493793
84 X = 2893708
36
Y = 9999422
67 feet Y = 3047824
03 meter
Z = 17218638
35 Z = 5248240
97
XDOT = -15889
804589 XDOT = -4843
212439
YDOT = 18242
492133 feet/sec YDOT = 5560
311602 meter/sec
ZDOT = -1851
339034 ZDOT = -564
288138
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 10318
54671695
00016717 00000-0 10270-3 0 9137
2 25544 51
6447 181
1826 0007392 202
6392 157
4445 15
72737849 7124
Satellite: ISS
Catalog Number: 25544
Epoch time: 10318
54671695 = yrday
fracday
Element set: 913
Inclination: 51
6447 deg
RA of node: 181
1826 deg
Eccentricity:
0007392
Arg of perigee: 202
6392 deg
Mean anomaly: 157
4445 deg
Mean motion: 15
72737849 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 712
Checksum: 325
Coasting Arc #15 (Orbit 727)
---------------------------------------
Vector Time (GMT): 2010/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6717744
30 A = 6735624
40 meter
Y = 450161
26 meter E =
0005985
Z = 136460
88 I = 51
68949
XDOT = -192
637838 Wp = 70
71341
YDOT = -4768
678403 meter/sec RA = 175
24879 deg
ZDOT = 6035
373527 TA = 290
76642
MA = 290
83053
Ha = 192
545 n
mi
Hp = 186
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22039843
52 X = -6722941
72
Y = 1476907
02 feet Y = 375010
34 meter
Z = 447706
30 Z = 103812
89
XDOT = -632
013903 XDOT = -168
618533
YDOT = -15645
270351 feet/sec YDOT = -4770
698298 meter/sec
ZDOT = 19801
094249 ZDOT = 6034
496019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11863385
19 X = 3615959
81
Y = -18635885
82 feet Y = -5680218
00 meter
Z = 316621
37 Z = 96506
19
XDOT = 11691
200275 XDOT = 3563
477844
YDOT = 7795
582830 feet/sec YDOT = 2376
093647 meter/sec
ZDOT = 19797
564172 ZDOT = 6034
297560
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
56335635
00016717 00000-0 10270-3 0 9142
2 25544 51
6439 175
9708 0007387 207
2073 152
8703 15
72787135 7282
Satellite: ISS
Catalog Number: 25544
Epoch time: 10319
56335635 = yrday
fracday
Element set: 914
Inclination: 51
6439 deg
RA of node: 175
9708 deg
Eccentricity:
0007387
Arg of perigee: 207
2073 deg
Mean anomaly: 152
8703 deg
Mean motion: 15
72787135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 728
Checksum: 328
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list