[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 1st 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10494 81 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 123 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 362 ET - UTC (sec) : 67 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 1767)
---------------------------------------
Vector Time (GMT): 2013/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3424774
17 A = 6793538
33 meter
Y = -5723567
35 meter E =
0016451
Z = 1229695
04 I = 51
34076
XDOT = 3630
570065 Wp = 12
79717
YDOT = 3424
269622 meter/sec RA = 292
41341 deg
ZDOT = 5827
536604 TA =
62859
MA =
62653
Ha = 224
735 n
mi
Hp = 218
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11236135
71 X = 3482548
32
Y = -18778108
10 feet Y = -5684946
17 meter
Z = 4034432
54 Z = 1246473
18
XDOT = 11911
319112 XDOT = 3563
701068
YDOT = 11234
480387 feet/sec YDOT = 3464
495840 meter/sec
ZDOT = 19119
214581 ZDOT = 5845
010487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17730368
29 X = 5404216
26
Y = -12803453
70 feet Y = -3902492
69 meter
Z = 4104917
68 Z = 1251178
91
XDOT = 5446
374494 XDOT = 1660
054946
YDOT = 13694
398924 feet/sec YDOT = 4174
052792 meter/sec
ZDOT = 19191
485771 ZDOT = 5849
564863
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 13058
56194561
00016717 00000-0 10270-3 0 9001
2 25544 51
6481 292
7930 0012008 318
1234 41
8998 15
52456108 17680
Satellite: ISS
Catalog Number: 25544
Epoch time: 13058
56194561 = yrday
fracday
Element set: 900
Inclination: 51
6481 deg
RA of node: 292
7930 deg
Eccentricity:
0012008
Arg of perigee: 318
1234 deg
Mean anomaly: 41
8998 deg
Mean motion: 15
52456108 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1768
Checksum: 315
Coasting Arc #2 (Orbit 1782)
---------------------------------------
Vector Time (GMT): 2013/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3601979
26 A = 6791917
66 meter
Y = 5272625
30 meter E =
0006352
Z = -2320572
84 I = 51
32387
XDOT = -3100
259493 Wp = 326
47437
YDOT = -4488
863449 meter/sec RA = 287
42702 deg
ZDOT = -5374
771453 TA = 239
47047
MA = 239
53318
Ha = 224
989 n
mi
Hp = 218
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11817517
27 X = -3649398
55
Y = 17298639
43 feet Y = 5232080
27 meter
Z = -7613427
96 Z = -2338186
65
XDOT = -10171
455029 XDOT = -3023
724669
YDOT = -14727
242288 feet/sec YDOT = -4523
105264 meter/sec
ZDOT = -17633
764609 ZDOT = -5389
645634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17462346
10 X = -5322523
09
Y = 11525294
13 feet Y = 3512909
65 meter
Z = -7687326
57 Z = -2343097
14
XDOT = -2868
009943 XDOT = -874
169431
YDOT = -16174
570503 feet/sec YDOT = -4930
009089 meter/sec
ZDOT = -17695
096841 ZDOT = -5393
465517
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 13059
52751884
00016717 00000-0 10270-3 0 9016
2 25544 51
6475 287
9922 0012017 321
0278 39
0007 15
52440522 17831
Satellite: ISS
Catalog Number: 25544
Epoch time: 13059
52751884 = yrday
fracday
Element set: 901
Inclination: 51
6475 deg
RA of node: 287
9922 deg
Eccentricity:
0012017
Arg of perigee: 321
0278 deg
Mean anomaly: 39
0007 deg
Mean motion: 15
52440522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1783
Checksum: 301
Coasting Arc #3 (Orbit 1798)
---------------------------------------
Vector Time (GMT): 2013/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3726848
26 A = 6789472
17 meter
Y = -4600343
37 meter E =
0011776
Z = 3307191
99 I = 51
30720
XDOT = 2625
227225 Wp = 28
65591
YDOT = 5485
680683 meter/sec RA = 282
43436 deg
ZDOT = 4675
516270 TA = 10
01249
MA = 9
98904
Ha = 225
115 n
mi
Hp = 217
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12227192
46 X = 3761947
92
Y = -15092990
04 feet Y = -4558470
77 meter
Z = 10850367
42 Z = 3325382
38
XDOT = 8612
950212 XDOT = 2540
977777
YDOT = 17997
640037 feet/sec YDOT = 5514
567099 meter/sec
ZDOT = 15339
620307 ZDOT = 4688
064054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16821164
48 X = 5127090
93
Y = -9627635
28 feet Y = -2934503
23 meter
Z = 10926578
67 Z = 3330421
18
XDOT = 676
768511 XDOT = 206
279042
YDOT = 18638
247610 feet/sec YDOT = 5680
937872 meter/sec
ZDOT = 15391
160883 ZDOT = 4691
225837
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 13060
55745324
00016717 00000-0 10270-3 0 9024
2 25544 51
6470 282
8694 0012163 325
6584 34
3780 15
52463623 17998
Satellite: ISS
Catalog Number: 25544
Epoch time: 13060
55745324 = yrday
fracday
Element set: 902
Inclination: 51
6470 deg
RA of node: 282
8694 deg
Eccentricity:
0012163
Arg of perigee: 325
6584 deg
Mean anomaly: 34
3780 deg
Mean motion: 15
52463623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1799
Checksum: 316
Coasting Arc #4 (Orbit 1813)
---------------------------------------
Vector Time (GMT): 2013/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3834519
94 A = 6786812
16 meter
Y = 3789474
25 meter E =
0012934
Z = -4132517
08 I = 51
29194
XDOT = -2196
586953 Wp = 3
78190
YDOT = -6311
551724 meter/sec RA = 277
43759 deg
ZDOT = -3737
433417 TA = 227
44411
MA = 227
55336
Ha = 225
312 n
mi
Hp = 217
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12580446
01 X = -3856535
08
Y = 12432658
30 feet Y = 3746470
74 meter
Z = -13558126
91 Z = -4151198
61
XDOT = -7206
650109 XDOT = -2107
691203
YDOT = -20707
190697 feet/sec YDOT = -6335
618657 meter/sec
ZDOT = -12261
920659 ZDOT = -3747
887669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16042470
80 X = -4889745
10
Y = 7304269
54 feet Y = 2226341
36 meter
Z = -13636282
36 Z = -4156338
86
XDOT = 1055
950872 XDOT = 321
853826
YDOT = -20725
363229 feet/sec YDOT = -6317
090712 meter/sec
ZDOT = -12304
660376 ZDOT = -3750
460483
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 13061
52300615
00016717 00000-0 10270-3 0 9033
2 25544 51
6461 278
0680 0012157 328
5679 31
4745 15
52487061 18149
Satellite: ISS
Catalog Number: 25544
Epoch time: 13061
52300615 = yrday
fracday
Element set: 903
Inclination: 51
6461 deg
RA of node: 278
0680 deg
Eccentricity:
0012157
Arg of perigee: 328
5679 deg
Mean anomaly: 31
4745 deg
Mean motion: 15
52487061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1814
Checksum: 296
Coasting Arc #5 (Orbit 1829)
---------------------------------------
Vector Time (GMT): 2013/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3939565
34 A = 6784433
90 meter
Y = -2792423
12 meter E =
0007336
Z = 4761653
28 I = 51
28102
XDOT = 1799
253626 Wp = 7
74695
YDOT = 6981
342573 meter/sec RA = 272
43452 deg
ZDOT = 2612
191027 TA = 56
40003
MA = 56
33003
Ha = 225
445 n
mi
Hp = 217
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12925083
15 X = 3947367
29
Y = -9161493
18 feet Y = -2748324
44 meter
Z = 15622222
05 Z = 4780810
41
XDOT = 5903
063077 XDOT = 1708
363778
YDOT = 22904
667233 feet/sec YDOT = 7000
954963 meter/sec
ZDOT = 8570
180534 ZDOT = 2620
710303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15141748
66 X = 4615204
99
Y = -4383116
57 feet Y = -1335973
93 meter
Z = 15702238
37 Z = 4786042
26
XDOT = -2403
720156 XDOT = -732
653903
YDOT = 22444
347149 feet/sec YDOT = 6841
037011 meter/sec
ZDOT = 8604
799192 ZDOT = 2622
742794
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 13062
55292132
00016717 00000-0 10270-3 0 9042
2 25544 51
6462 272
9454 0012183 333
0994 26
9525 15
52473949 18305
Satellite: ISS
Catalog Number: 25544
Epoch time: 13062
55292132 = yrday
fracday
Element set: 904
Inclination: 51
6462 deg
RA of node: 272
9454 deg
Eccentricity:
0012183
Arg of perigee: 333
0994 deg
Mean anomaly: 26
9525 deg
Mean motion: 15
52473949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1830
Checksum: 311
Coasting Arc #6 (Orbit 1844)
---------------------------------------
Vector Time (GMT): 2013/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4060861
48 A = 6782652
39 meter
Y = 1741282
66 meter E =
0016190
Z = -5156399
20 I = 51
27391
XDOT = -1426
749474 Wp = 32
54526
YDOT = -7398
451566 meter/sec RA = 267
42798 deg
ZDOT = -1363
395505 TA = 224
19687
MA = 224
32632
Ha = 225
566 n
mi
Hp = 216
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13323036
37 X = -4054982
85
Y = 5712869
63 feet Y = 1695904
11 meter
Z = -16917320
22 Z = -5176112
19
XDOT = -4680
936595 XDOT = -1337
289415
YDOT = -24273
135058 feet/sec YDOT = -7413
906259 meter/sec
ZDOT = -4473
082366 ZDOT = -1370
108735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14345587
42 X = -4372535
05
Y = 1247424
24 feet Y = 380214
91 meter
Z = -16999528
08 Z = -5181456
16
XDOT = 3337
204874 XDOT = 1017
180046
YDOT = -23455
235942 feet/sec YDOT = -7149
155915 meter/sec
ZDOT = -4500
148065 ZDOT = -1371
645130
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 13063
51845446
00016717 00000-0 10270-3 0 9052
2 25544 51
6449 268
1434 0012170 336
1243 23
9343 15
52527037 18451
Satellite: ISS
Catalog Number: 25544
Epoch time: 13063
51845446 = yrday
fracday
Element set: 905
Inclination: 51
6449 deg
RA of node: 268
1434 deg
Eccentricity:
0012170
Arg of perigee: 336
1243 deg
Mean anomaly: 23
9343 deg
Mean motion: 15
52527037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1845
Checksum: 297
Coasting Arc #7 (Orbit 1860)
---------------------------------------
Vector Time (GMT): 2013/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4204102
85 A = 6782059
33 meter
Y = -577268
45 meter E =
0011487
Z = 5291929
87 I = 51
27443
XDOT = 1028
938693 Wp = 351
12619
YDOT = 7595
608214 meter/sec RA = 262
41903 deg
ZDOT = 22
295119 TA = 98
72526
MA = 98
59513
Ha = 225
689 n
mi
Hp = 216
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13792988
34 X = 4184539
06
Y = -1893925
37 feet Y = -530364
63 meter
Z = 17361974
63 Z = 5312305
30
XDOT = 3375
783115 XDOT = 943
818210
YDOT = 24919
974457 feet/sec YDOT = 7606
638520 meter/sec
ZDOT = 73
146715 ZDOT = 27
086387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13624886
34 X = 4152865
36
Y = 2289761
90 feet Y = 697919
43 meter
Z = 17446807
91 Z = 5317787
05
XDOT = -4070
253224 XDOT = -1240
613183
YDOT = 23794
434705 feet/sec YDOT = 7252
543698 meter/sec
ZDOT = 92
205067 ZDOT = 28
104105
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 13064
54834851
00016717 00000-0 10270-3 0 9065
2 25544 51
6451 263
0214 0012142 339
9877 20
0797 15
52511589 18611
Satellite: ISS
Catalog Number: 25544
Epoch time: 13064
54834851 = yrday
fracday
Element set: 906
Inclination: 51
6451 deg
RA of node: 263
0214 deg
Eccentricity:
0012142
Arg of perigee: 339
9877 deg
Mean anomaly: 20
0797 deg
Mean motion: 15
52511589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1861
Checksum: 310
Coasting Arc #8 (Orbit 1875)
---------------------------------------
Vector Time (GMT): 2013/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4365890
97 A = 6782466
72 meter
Y = -529988
12 meter E =
0013878
Z = -5170581
75 I = 51
27998
XDOT = -612
665255 Wp = 48
49199
YDOT = -7523
878372 meter/sec RA = 257
40977 deg
ZDOT = 1299
819627 TA = 234
00556
MA = 234
13431
Ha = 225
771 n
mi
Hp = 216
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14323789
29 X = -4334523
16
Y = -1738806
18 feet Y = -578635
19 meter
Z = -16963850
88 Z = -5191714
29
XDOT = -2010
056611 XDOT = -534
800183
YDOT = -24684
640327 feet/sec YDOT = -7530
294133 meter/sec
ZDOT = 4264
500090 ZDOT = 1297
032988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13146352
55 X = -4007008
26
Y = -5690262
30 feet Y = -1734391
95 meter
Z = -17051714
07 Z = -5197362
45
XDOT = 4612
925683 XDOT = 1406
019748
YDOT = -23293
854579 feet/sec YDOT = -7099
966876 meter/sec
ZDOT = 4253
760415 ZDOT = 1296
546174
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 13065
51386283
00016717 00000-0 10270-3 0 9075
2 25544 51
6438 258
2188 0012107 343
6523 16
4236 15
52561672 18764
Satellite: ISS
Catalog Number: 25544
Epoch time: 13065
51386283 = yrday
fracday
Element set: 907
Inclination: 51
6438 deg
RA of node: 258
2188 deg
Eccentricity:
0012107
Arg of perigee: 343
6523 deg
Mean anomaly: 16
4236 deg
Mean motion: 15
52561672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1876
Checksum: 313
Coasting Arc #9 (Orbit 1891)
---------------------------------------
Vector Time (GMT): 2013/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4534842
32 A = 6784163
93 meter
Y = 1657162
65 meter E =
0015836
Z = 4769073
60 I = 51
29322
XDOT = 108
191339 Wp = 13
74132
YDOT = 7210
328373 meter/sec RA = 252
40352 deg
ZDOT = -2591
435926 TA = 102
02971
MA = 101
85219
Ha = 225
936 n
mi
Hp = 216
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14878091
60 X = 4492808
11
Y = 5436885
35 feet Y = 1707639
45 meter
Z = 15646566
91 Z = 4791000
80
XDOT = 354
958462 XDOT = 40
144124
YDOT = 23655
932981 feet/sec YDOT = 7211
157563 meter/sec
ZDOT = -8502
086371 ZDOT = -2591
076188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12799722
48 X = 3901355
41
Y = 9177519
26 feet Y = 2797307
87 meter
Z = 15737618
40 Z = 4796826
09
XDOT = -5236
847597 XDOT = -1596
191148
YDOT = 21976
433204 feet/sec YDOT = 6698
416841 meter/sec
ZDOT = -8501
394750 ZDOT = -2591
225120
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 13066
54373469
00016717 00000-0 10270-3 0 9082
2 25544 51
6437 253
0968 0012144 346
9919 13
0918 15
52559617 18922
Satellite: ISS
Catalog Number: 25544
Epoch time: 13066
54373469 = yrday
fracday
Element set: 908
Inclination: 51
6437 deg
RA of node: 253
0968 deg
Eccentricity:
0012144
Arg of perigee: 346
9919 deg
Mean anomaly: 13
0918 deg
Mean motion: 15
52559617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1892
Checksum: 338
Coasting Arc #10 (Orbit 1906)
---------------------------------------
Vector Time (GMT): 2013/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4687819
75 A = 6786429
74 meter
Y = -2623661
26 meter E =
0010796
Z = -4145184
88 I = 51
31067
XDOT = 453
788867 Wp = 30
56924
YDOT = -6681
340140 meter/sec RA = 247
40095 deg
ZDOT = 3729
121958 TA = 277
92671
MA = 278
04923
Ha = 225
984 n
mi
Hp = 215
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15379986
05 X = -4637997
23
Y = -8607812
55 feet Y = -2675805
25 meter
Z = -13599687
92 Z = -4167836
14
XDOT = 1488
808619 XDOT = 510
352615
YDOT = -21920
407284 feet/sec YDOT = -6675
948956 meter/sec
ZDOT = 12234
652094 ZDOT = 3731
464421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12662312
23 X = -3859472
77
Y = -12154816
07 feet Y = -3704787
94 meter
Z = -13693656
00 Z = -4173826
35
XDOT = 5954
508356 XDOT = 1814
934147
YDOT = -19949
287474 feet/sec YDOT = -6080
542822 meter/sec
ZDOT = 12245
131987 ZDOT = 3732
316230
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 13067
50922977
00016717 00000-0 10270-3 0 9094
2 25544 51
6431 248
2939 0012062 351
1591 8
9346 15
52588237 19078
Satellite: ISS
Catalog Number: 25544
Epoch time: 13067
50922977 = yrday
fracday
Element set: 909
Inclination: 51
6431 deg
RA of node: 248
2939 deg
Eccentricity:
0012062
Arg of perigee: 351
1591 deg
Mean anomaly: 8
9346 deg
Mean motion: 15
52588237 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1907
Checksum: 326
Coasting Arc #11 (Orbit 1922)
---------------------------------------
Vector Time (GMT): 2013/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4795503
35 A = 6789156
29 meter
Y = 3522851
23 meter E =
0016305
Z = 3271719
82 I = 51
33237
XDOT = -1139
455128 Wp = 44
60398
YDOT = 5940
668911 meter/sec RA = 242
40471 deg
ZDOT = -4700
794588 TA = 97
29287
MA = 97
10751
Ha = 226
181 n
mi
Hp = 215
733
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15733278
69 X = 4739860
84
Y = 11557910
85 feet Y = 3576166
84 meter
Z = 10733988
91 Z = 3294879
91
XDOT = -3738
369843 XDOT = -1182
965526
YDOT = 19490
383565 feet/sec YDOT = 5927
682968 meter/sec
ZDOT = -15422
554423 ZDOT = -4706
436237
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12543061
77 X = 3823125
23
Y = 14890360
36 feet Y = 4538581
84 meter
Z = 10829988
42 Z = 3300980
47
XDOT = -6997
343423 XDOT = -2132
790275
YDOT = 17189
721688 feet/sec YDOT = 5239
427171 meter/sec
ZDOT = -15446
670879 ZDOT = -4708
145284
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 13068
53907909
00016717 00000-0 10270-3 0 9108
2 25544 51
6428 243
1714 0012149 354
3628 5
7386 15
52605975 19237
Satellite: ISS
Catalog Number: 25544
Epoch time: 13068
53907909 = yrday
fracday
Element set: 910
Inclination: 51
6428 deg
RA of node: 243
1714 deg
Eccentricity:
0012149
Arg of perigee: 354
3628 deg
Mean anomaly: 5
7386 deg
Mean motion: 15
52605975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1923
Checksum: 319
Coasting Arc #12 (Orbit 1937)
---------------------------------------
Vector Time (GMT): 2013/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4826499
04 A = 6791502
80 meter
Y = -4195208
86 meter E =
0016711
Z = -2260431
17 I = 51
35583
XDOT = 1893
308370 Wp = 13
58637
YDOT = -5086
250366 meter/sec RA = 237
41395 deg
ZDOT = 5421
220336 TA = 321
15556
MA = 321
27556
Ha = 226
221 n
mi
Hp = 215
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15834970
61 X = -4768248
23
Y = -13763808
61 feet Y = -4248856
42 meter
Z = -7416112
76 Z = -2283735
41
XDOT = 6211
641635 XDOT = 1923
708808
YDOT = -16687
173118 feet/sec YDOT = -5064
907488 meter/sec
ZDOT = 17786
155958 ZDOT = 5430
492231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12439742
52 X = -3791633
52
Y = -16852308
88 feet Y = -5136583
75 meter
Z = -7512652
10 Z = -2289856
36
XDOT = 8336
085288 XDOT = 2540
838796
YDOT = -14064
994817 feet/sec YDOT = -4287
010420 meter/sec
ZDOT = 17825
279854 ZDOT = 5433
145300
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 13069
50455406
00016717 00000-0 10270-3 0 9117
2 25544 51
6433 238
3686 0012063 358
8159 1
2963 15
52616920 19380
Satellite: ISS
Catalog Number: 25544
Epoch time: 13069
50455406 = yrday
fracday
Element set: 911
Inclination: 51
6433 deg
RA of node: 238
3686 deg
Eccentricity:
0012063
Arg of perigee: 358
8159 deg
Mean anomaly: 1
2963 deg
Mean motion: 15
52616920 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1938
Checksum: 311
Coasting Arc #13 (Orbit 1953)
---------------------------------------
Vector Time (GMT): 2013/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4741721
37 A = 6793042
57 meter
Y = 4744362
91 meter E =
0012818
Z = 1083252
08 I = 51
37854
XDOT = -2749
384029 Wp = 67
97404
YDOT = 4098
748350 meter/sec RA = 232
42883 deg
ZDOT = -5855
966935 TA = 100
25152
MA = 100
10696
Ha = 226
405 n
mi
Hp = 215
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15556828
65 X = 4683054
40
Y = 15565495
12 feet Y = 4797059
96 meter
Z = 3553976
63 Z = 1106143
44
XDOT = -9020
288808 XDOT = -2766
566419
YDOT = 13447
337105 feet/sec YDOT = 4067
906075 meter/sec
ZDOT = -19212
489943 ZDOT = -5869
365359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12119419
53 X = 3693999
07
Y = 18350384
01 feet Y = 5593197
05 meter
Z = 3648750
82 Z = 1112139
25
XDOT = -10065
535676 XDOT = -3067
975274
YDOT = 10517
583073 feet/sec YDOT = 3205
759321 meter/sec
ZDOT = -19268
678430 ZDOT = -5873
093185
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 13070
53438043
00016717 00000-0 10270-3 0 9121
2 25544 51
6430 233
2457 0012272 2
0323 358
0876 15
52670573 19548
Satellite: ISS
Catalog Number: 25544
Epoch time: 13070
53438043 = yrday
fracday
Element set: 912
Inclination: 51
6430 deg
RA of node: 233
2457 deg
Eccentricity:
0012272
Arg of perigee: 2
0323 deg
Mean anomaly: 358
0876 deg
Mean motion: 15
52670573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1954
Checksum: 283
Coasting Arc #14 (Orbit 1969)
---------------------------------------
Vector Time (GMT): 2013/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4516181
87 A = 6793605
15 meter
Y = -5055075
83 meter E =
0022874
Z = 114921
94 I = 51
40105
XDOT = 3644
326201 Wp = 26
92573
YDOT = -3109
300216 meter/sec RA = 227
44711 deg
ZDOT = 5997
213385 TA = 334
31709
MA = 334
43051
Ha = 226
447 n
mi
Hp = 215
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14816869
64 X = -4459877
53
Y = -16584894
44 feet Y = -5105263
78 meter
Z = 377040
48 Z = 93120
44
XDOT = 11956
450791 XDOT = 3649
691598
YDOT = -10201
116194 feet/sec YDOT = -3068
516159 meter/sec
ZDOT = 19675
896934 ZDOT = 6014
930548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11543614
74 X = -3518493
77
Y = -19010607
55 feet Y = -5794433
18 meter
Z = 286824
93 Z = 87424
24
XDOT = 12111
193083 XDOT = 3691
491652
YDOT = -7027
026318 feet/sec YDOT = -2141
837622 meter/sec
ZDOT = 19749
955409 ZDOT = 6019
786409
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 13071
56419784
00016717 00000-0 10270-3 0 9137
2 25544 51
6444 228
1231 0012064 6
7610 353
3703 15
52661375 19700
Satellite: ISS
Catalog Number: 25544
Epoch time: 13071
56419784 = yrday
fracday
Element set: 913
Inclination: 51
6444 deg
RA of node: 228
1231 deg
Eccentricity:
0012064
Arg of perigee: 6
7610 deg
Mean anomaly: 353
3703 deg
Mean motion: 15
52661375 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1970
Checksum: 291
Coasting Arc #15 (Orbit 1984)
---------------------------------------
Vector Time (GMT): 2013/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4119330
30 A = 6792722
38 meter
Y = 5234667
83 meter E =
0009118
Z = -1354152
50 I = 51
41988
XDOT = -4552
916170 Wp = 55
98449
YDOT = 2091
627070 meter/sec RA = 222
46675 deg
ZDOT = -5787
589987 TA = 138
77954
MA = 138
71065
Ha = 226
617 n
mi
Hp = 214
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13514863
20 X = 4067067
05
Y = 17174107
07 feet Y = 5280440
36 meter
Z = -4442757
55 Z = -1334268
97
XDOT = -14937
389009 XDOT = -4547
852373
YDOT = 6862
293538 feet/sec YDOT = 2040
740953 meter/sec
ZDOT = -18988
156125 ZDOT = -5809
695557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10512126
70 X = 3204096
22
Y = 19178647
05 feet Y = 5845651
62 meter
Z = -4360535
00 Z = -1329091
07
XDOT = -14352
807159 XDOT = -4374
735622
YDOT = 3546
373477 feet/sec YDOT = 1080
934636 meter/sec
ZDOT = -19080
376842 ZDOT = -5815
698862
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 13072
52963911
00016717 00000-0 10270-3 0 9141
2 25544 51
6443 223
3206 0012291 10
1629 349
9769 15
52701783 19856
Satellite: ISS
Catalog Number: 25544
Epoch time: 13072
52963911 = yrday
fracday
Element set: 914
Inclination: 51
6443 deg
RA of node: 223
3206 deg
Eccentricity:
0012291
Arg of perigee: 10
1629 deg
Mean anomaly: 349
9769 deg
Mean motion: 15
52701783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1985
Checksum: 311
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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