[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 3rd 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 129 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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 138)
---------------------------------------
Vector Time (GMT): 2012/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3377239
37 A = 6775913
68 meter
Y = -5846604
06 meter E =
0026311
Z = 530797
18 I = 51
35214
XDOT = 3918
129928 Wp = 85
71700
YDOT = 2827
482398 meter/sec RA = 296
40826 deg
ZDOT = 5961
082460 TA = 280
04226
MA = 280
33904
Ha = 220
060 n
mi
Hp = 201
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11080181
67 X = 3439787
82
Y = -19181771
86 feet Y = -5808487
93 meter
Z = 1741460
57 Z = 547355
63
XDOT = 12854
756983 XDOT = 3857
264080
YDOT = 9276
517054 feet/sec YDOT = 2870
957313 meter/sec
ZDOT = 19557
357151 ZDOT = 5979
968300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16991909
14 X = 5179133
91
Y = -14203632
83 feet Y = -4329267
29 meter
Z = 1809784
63 Z = 551622
35
XDOT = 7731
627470 XDOT = 2356
600053
YDOT = 11853
166896 feet/sec YDOT = 3612
845270 meter/sec
ZDOT = 19634
543130 ZDOT = 5984
608746
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 12062
56305281
00016717 00000-0 10270-3 0 9008
2 25544 51
6429 296
7578 0017310 111
8239 248
4759 15
58710675 1397
Satellite: ISS
Catalog Number: 25544
Epoch time: 12062
56305281 = yrday
fracday
Element set: 900
Inclination: 51
6429 deg
RA of node: 296
7578 deg
Eccentricity:
0017310
Arg of perigee: 111
8239 deg
Mean anomaly: 248
4759 deg
Mean motion: 15
58710675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 139
Checksum: 319
Coasting Arc #2 (Orbit 153)
---------------------------------------
Vector Time (GMT): 2012/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4461793
46 A = 6770758
66 meter
Y = 3710078
81 meter E =
0021752
Z = -3499780
58 I = 51
32167
XDOT = -1506
049092 Wp = 108
42347
YDOT = -6024
156110 meter/sec RA = 291
38621 deg
ZDOT = -4495
860361 TA = 112
99565
MA = 112
76605
Ha = 219
930 n
mi
Hp = 201
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14638430
00 X = -4485947
86
Y = 12172174
57 feet Y = 3660049
04 meter
Z = -11482219
75 Z = -3521514
25
XDOT = -4941
105946 XDOT = -1416
734348
YDOT = -19764
291698 feet/sec YDOT = -6040
498534 meter/sec
ZDOT = -14750
198034 ZDOT = -4502
959286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17753092
94 X = -5411142
73
Y = 6724056
24 feet Y = 2049492
34 meter
Z = -11571585
71 Z = -3527019
32
XDOT = 2385
301801 XDOT = 727
039989
YDOT = -18968
820533 feet/sec YDOT = -5781
696498 meter/sec
ZDOT = -14778
833667 ZDOT = -4504
588502
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 12063
52474767
00016717 00000-0 10270-3 0 9012
2 25544 51
6423 291
9299 0017149 115
6189 244
6740 15
58703396 1541
Satellite: ISS
Catalog Number: 25544
Epoch time: 12063
52474767 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 291
9299 deg
Eccentricity:
0017149
Arg of perigee: 115
6189 deg
Mean anomaly: 244
6740 deg
Mean motion: 15
58703396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 154
Checksum: 327
Coasting Arc #3 (Orbit 169)
---------------------------------------
Vector Time (GMT): 2012/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4388745
13 A = 6764603
19 meter
Y = -388735
39 meter E =
0021703
Z = 5118994
61 I = 51
29106
XDOT = -1009
246452 Wp = 119
99493
YDOT = 7488
546453 meter/sec RA = 286
32983 deg
ZDOT = 1418
748280 TA = 316
24028
MA = 316
41208
Ha = 219
790 n
mi
Hp = 201
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14398770
11 X = 4367899
46
Y = -1275378
59 feet Y = -339773
95 meter
Z = 16794601
75 Z = 5140263
89
XDOT = -3311
176025 XDOT = -1099
801695
YDOT = 24568
721960 feet/sec YDOT = 7476
754209 meter/sec
ZDOT = 4654
685957 ZDOT = 1413
625053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13982288
74 X = 4261801
61
Y = 3241889
43 feet Y = 988127
90 meter
Z = 16881811
92 Z = 5145576
27
XDOT = -10589
372122 XDOT = -3227
640623
YDOT = 21287
094783 feet/sec YDOT = 6488
306490 meter/sec
ZDOT = 4633
126112 ZDOT = 1412
176839
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 12064
55053469
00016717 00000-0 10270-3 0 9029
2 25544 51
6421 286
7807 0017219 119
0049 241
2834 15
58742191 1708
Satellite: ISS
Catalog Number: 25544
Epoch time: 12064
55053469 = yrday
fracday
Element set: 902
Inclination: 51
6421 deg
RA of node: 286
7807 deg
Eccentricity:
0017219
Arg of perigee: 119
0049 deg
Mean anomaly: 241
2834 deg
Mean motion: 15
58742191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 170
Checksum: 301
Coasting Arc #4 (Orbit 184)
---------------------------------------
Vector Time (GMT): 2012/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3375015
36 A = 6765474
48 meter
Y = -3235237
64 meter E =
0029062
Z = -4917309
07 I = 51
28550
XDOT = 3126
366947 Wp = 115
74288
YDOT = -6626
463868 meter/sec RA = 281
25507 deg
ZDOT = 2211
801235 TA = 176
00737
MA = 175
98413
Ha = 219
727 n
mi
Hp = 201
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11072885
05 X = -3314700
79
Y = -10614296
71 feet Y = -3272642
34 meter
Z = -16132903
76 Z = -4933557
60
XDOT = 10257
109407 XDOT = 3189
488844
YDOT = -21740
367022 feet/sec YDOT = -6591
149775 meter/sec
ZDOT = 7256
565732 ZDOT = 2227
142553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7353711
25 X = -2241411
19
Y = -13380926
69 feet Y = -4078506
45 meter
Z = -16199271
39 Z = -4937537
92
XDOT = 15197
340828 XDOT = 4632
149484
YDOT = -17222
115655 feet/sec YDOT = -5249
300852 meter/sec
ZDOT = 7319
932587 ZDOT = 2231
115452
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 12065
51218919
00016717 00000-0 10270-3 0 9030
2 25544 51
6408 281
9516 0017045 122
7208 237
5593 15
58792656 1859
Satellite: ISS
Catalog Number: 25544
Epoch time: 12065
51218919 = yrday
fracday
Element set: 903
Inclination: 51
6408 deg
RA of node: 281
9516 deg
Eccentricity:
0017045
Arg of perigee: 122
7208 deg
Mean anomaly: 237
5593 deg
Mean motion: 15
58792656 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 185
Checksum: 323
Coasting Arc #5 (Orbit 200)
---------------------------------------
Vector Time (GMT): 2012/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1649334
37 A = 6772146
16 meter
Y = 5901853
96 meter E =
0029411
Z = 2843258
44 I = 51
30362
XDOT = -4470
756095 Wp = 114
15252
YDOT = 3696
272407 meter/sec RA = 276
20504 deg
ZDOT = -5049
696101 TA = 33
21363
MA = 33
02936
Ha = 219
465 n
mi
Hp = 201
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5411202
02 X = 1569404
45
Y = 19363037
93 feet Y = 5919851
24 meter
Z = 9328275
71 Z = 2851075
86
XDOT = -14667
834958 XDOT = -4487
226509
YDOT = 12126
877975 feet/sec YDOT = 3646
184996 meter/sec
ZDOT = -16567
244425 ZDOT = -5071
454792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -252225
97 X = -76878
48
Y = 20088645
51 feet Y = 6123019
15 meter
Z = 9359902
59 Z = 2852898
31
XDOT = -15903
593094 XDOT = -4847
415175
YDOT = 7605
914317 feet/sec YDOT = 2318
282684 meter/sec
ZDOT = -16656
696777 ZDOT = -5076
961178
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 12066
53793307
00016717 00000-0 10270-3 0 9043
2 25544 51
6408 276
8019 0016869 126
2459 234
0257 15
58856562 2015
Satellite: ISS
Catalog Number: 25544
Epoch time: 12066
53793307 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 276
8019 deg
Eccentricity:
0016869
Arg of perigee: 126
2459 deg
Mean anomaly: 234
0257 deg
Mean motion: 15
58856562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 201
Checksum: 322
Coasting Arc #6 (Orbit 216)
---------------------------------------
Vector Time (GMT): 2012/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 326602
97 A = 6775606
18 meter
Y = -6764695
37 meter E =
0022376
Z = 233086
39 I = 51
31117
XDOT = 4780
241912 Wp = 96
35468
YDOT = 453
979576 meter/sec RA = 271
18476 deg
ZDOT = 5979
546553 TA = 266
17093
MA = 266
42680
Ha = 219
498 n
mi
Hp = 201
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1071532
04 X = 401090
62
Y = -22193882
46 feet Y = -6760626
58 meter
Z = 764719
12 Z = 234854
80
XDOT = 15683
208373 XDOT = 4745
763369
YDOT = 1489
434303 feet/sec YDOT = 507
243202 meter/sec
ZDOT = 19617
934886 ZDOT = 6002
684529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6845214
88 X = 2086421
50
Y = -21138774
20 feet Y = -6443098
38 meter
Z = 772433
41 Z = 235437
70
XDOT = 13087
890913 XDOT = 3989
189150
YDOT = 5017
569625 feet/sec YDOT = 1529
355222 meter/sec
ZDOT = 19712
749030 ZDOT = 6008
445904
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 12067
56365669
00016717 00000-0 10270-3 0 9054
2 25544 51
6390 271
6510 0016938 130
4857 229
7778 15
58851511 2175
Satellite: ISS
Catalog Number: 25544
Epoch time: 12067
56365669 = yrday
fracday
Element set: 905
Inclination: 51
6390 deg
RA of node: 271
6510 deg
Eccentricity:
0016938
Arg of perigee: 130
4857 deg
Mean anomaly: 229
7778 deg
Mean motion: 15
58851511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 217
Checksum: 333
Coasting Arc #7 (Orbit 231)
---------------------------------------
Vector Time (GMT): 2012/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2289807
36 A = 6770838
12 meter
Y = 5447854
48 meter E =
0020727
Z = -3306406
62 I = 51
29503
XDOT = -4060
542923 Wp = 125
47397
YDOT = -4526
102852 meter/sec RA = 266
16119 deg
ZDOT = -4677
950696 TA = 93
25902
MA = 93
02186
Ha = 219
328 n
mi
Hp = 201
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7512491
34 X = -2334494
61
Y = 17873538
31 feet Y = 5421998
10 meter
Z = -10847790
74 Z = -3317639
57
XDOT = -13321
991217 XDOT = -3986
905200
YDOT = -14849
418806 feet/sec YDOT = -4571
099288 meter/sec
ZDOT = -15347
607271 ZDOT = -4697
496864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11604766
26 X = -3537132
76
Y = 15499071
81 feet Y = 4724117
09 meter
Z = -10894201
89 Z = -3320552
74
XDOT = -8049
578725 XDOT = -2453
511595
YDOT = -16796
208936 feet/sec YDOT = -5119
484484 meter/sec
ZDOT = -15427
425553 ZDOT = -4702
279309
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 12068
52525176
00016717 00000-0 10270-3 0 9063
2 25544 51
6381 266
8218 0016885 133
9359 226
3193 15
58881497 2329
Satellite: ISS
Catalog Number: 25544
Epoch time: 12068
52525176 = yrday
fracday
Element set: 906
Inclination: 51
6381 deg
RA of node: 266
8218 deg
Eccentricity:
0016885
Arg of perigee: 133
9359 deg
Mean anomaly: 226
3193 deg
Mean motion: 15
58881497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 232
Checksum: 336
Coasting Arc #8 (Orbit 247)
---------------------------------------
Vector Time (GMT): 2012/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3729395
13 A = 6764467
45 meter
Y = -2459670
64 meter E =
0021859
Z = 5069609
87 I = 51
27657
XDOT = 2437
443070 Wp = 134
60681
YDOT = 7102
386073 meter/sec RA = 261
10313 deg
ZDOT = 1633
386654 TA = 299
47456
MA = 299
69245
Ha = 219
235 n
mi
Hp = 202
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12235548
34 X = 3731995
64
Y = -8069785
56 feet Y = -2417950
98 meter
Z = 16632578
32 Z = 5087733
63
XDOT = 7996
860467 XDOT = 2349
907035
YDOT = 23301
791579 feet/sec YDOT = 7129
153856 meter/sec
ZDOT = 5358
880099 ZDOT = 1645
013932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13657985
03 X = 4162953
84
Y = -5080084
68 feet Y = -1548409
81 meter
Z = 16707032
29 Z = 5092303
44
XDOT = 2053
779058 XDOT = 625
991857
YDOT = 23509
928320 feet/sec YDOT = 7165
826152 meter/sec
ZDOT = 5406
073684 ZDOT = 1647
771259
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 12069
55093294
00016717 00000-0 10270-3 0 9079
2 25544 51
6379 261
6705 0016883 137
5560 222
6904 15
58875051 2487
Satellite: ISS
Catalog Number: 25544
Epoch time: 12069
55093294 = yrday
fracday
Element set: 907
Inclination: 51
6379 deg
RA of node: 261
6705 deg
Eccentricity:
0016883
Arg of perigee: 137
5560 deg
Mean anomaly: 222
6904 deg
Mean motion: 15
58875051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 248
Checksum: 330
Coasting Arc #9 (Orbit 262)
---------------------------------------
Vector Time (GMT): 2012/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4429630
15 A = 6764793
90 meter
Y = -1322055
65 meter E =
0028187
Z = -4964018
94 I = 51
28363
XDOT = -126
238518 Wp = 126
10305
YDOT = -7369
813027 meter/sec RA = 256
02535 deg
ZDOT = 2067
379296 TA = 164
19099
MA = 164
10281
Ha = 219
151 n
mi
Hp = 201
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14532907
32 X = -4390403
42
Y = -4337452
90 feet Y = -1371371
80 meter
Z = -16286151
36 Z = -4985442
37
XDOT = -414
168366 XDOT = -53
861236
YDOT = -24179
176598 feet/sec YDOT = -7370
819759 meter/sec
ZDOT = 6782
740471 ZDOT = 2066
942770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13186592
15 X = -4019273
29
Y = -7298446
73 feet Y = -2224566
56 meter
Z = -16373884
14 Z = -4990759
89
XDOT = 4146
449098 XDOT = 1263
837685
YDOT = -22764
606928 feet/sec YDOT = -6938
652192 meter/sec
ZDOT = 6781
431009 ZDOT = 2066
980171
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 12070
51248585
00016717 00000-0 10270-3 0 9083
2 25544 51
6375 256
8401 0016936 141
3658 218
8712 15
58948551 2639
Satellite: ISS
Catalog Number: 25544
Epoch time: 12070
51248585 = yrday
fracday
Element set: 908
Inclination: 51
6375 deg
RA of node: 256
8401 deg
Eccentricity:
0016936
Arg of perigee: 141
3658 deg
Mean anomaly: 218
8712 deg
Mean motion: 15
58948551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 263
Checksum: 326
Coasting Arc #10 (Orbit 278)
---------------------------------------
Vector Time (GMT): 2012/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4043676
23 A = 6771513
05 meter
Y = 4554497
88 meter E =
0027429
Z = 2919801
82 I = 51
31553
XDOT = -2390
996825 Wp = 124
58684
YDOT = 5337
325800 meter/sec RA = 250
97281 deg
ZDOT = -4996
115905 TA = 21
78557
MA = 21
66914
Ha = 218
824 n
mi
Hp = 202
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13266654
31 X = 3978262
65
Y = 14942578
35 feet Y = 4599351
32 meter
Z = 9579402
30 Z = 2939286
45
XDOT = -7844
477772 XDOT = -2426
232181
YDOT = 17510
911418 feet/sec YDOT = 5310
390668 meter/sec
ZDOT = -16391
456381 ZDOT = -5007
817390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10039605
96 X = 3060071
90
Y = 17232530
06 feet Y = 5252475
16 meter
Z = 9658981
97 Z = 2944057
70
XDOT = -9754
981271 XDOT = -2973
318291
YDOT = 14930
798998 feet/sec YDOT = 4550
907535 meter/sec
ZDOT = -16439
769650 ZDOT = -5010
841789
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 12071
53812036
00016717 00000-0 10270-3 0 9095
2 25544 51
6380 251
6892 0016711 145
5124 214
7119 15
58995888 2795
Satellite: ISS
Catalog Number: 25544
Epoch time: 12071
53812036 = yrday
fracday
Element set: 909
Inclination: 51
6380 deg
RA of node: 251
6892 deg
Eccentricity:
0016711
Arg of perigee: 145
5124 deg
Mean anomaly: 214
7119 deg
Mean motion: 15
58995888 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 279
Checksum: 324
Coasting Arc #11 (Orbit 294)
---------------------------------------
Vector Time (GMT): 2012/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2608703
51 A = 6775120
36 meter
Y = -6253211
87 meter E =
0018905
Z = 207232
00 I = 51
33854
XDOT = 4497
858633 Wp = 108
63307
YDOT = -1663
112577 meter/sec RA = 245
95302 deg
ZDOT = 5981
134997 TA = 253
61068
MA = 253
81860
Ha = 218
878 n
mi
Hp = 202
335
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8558738
53 X = -2539591
63
Y = -20515786
97 feet Y = -6281997
56 meter
Z = 679895
00 Z = 194727
41
XDOT = 14756
754046 XDOT = 4487
066620
YDOT = -5456
406092 feet/sec YDOT = -1612
874614 meter/sec
ZDOT = 19623
146314 ZDOT = 6002
959287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4770500
76 X = -1454048
63
Y = -21713093
22 feet Y = -6618150
81 meter
Z = 629033
33 Z = 191729
36
XDOT = 13791
703101 XDOT = 4203
711105
YDOT = -2412
291704 feet/sec YDOT = -735
266511 meter/sec
ZDOT = 19712
723501 ZDOT = 6008
438123
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 12072
56373373
00016717 00000-0 10270-3 0 9107
2 25544 51
6377 246
5377 0016900 149
0887 211
1267 15
59021113 2952
Satellite: ISS
Catalog Number: 25544
Epoch time: 12072
56373373 = yrday
fracday
Element set: 910
Inclination: 51
6377 deg
RA of node: 246
5377 deg
Eccentricity:
0016900
Arg of perigee: 149
0887 deg
Mean anomaly: 211
1267 deg
Mean motion: 15
59021113 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 295
Checksum: 303
Coasting Arc #12 (Orbit 309)
---------------------------------------
Vector Time (GMT): 2012/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 230135
52 A = 6770287
46 meter
Y = 5889912
16 meter E =
0019687
Z = -3325165
98 I = 51
33661
XDOT = -5603
865268 Wp = 140
40403
YDOT = -2397
992995 meter/sec RA = 240
93173 deg
ZDOT = -4665
579515 TA = 78
59051
MA = 78
36943
Ha = 218
666 n
mi
Hp = 202
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 755037
78 X = 180409
08
Y = 19323858
78 feet Y = 5892207
44 meter
Z = -10909337
19 Z = -3324169
12
XDOT = -18385
384739 XDOT = -5553
969677
YDOT = -7867
431086 feet/sec YDOT = -2460
380170 meter/sec
ZDOT = -15307
019407 ZDOT = -4692
681409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2304619
64 X = -702448
07
Y = 19202897
92 feet Y = 5853043
29 meter
Z = -10905625
98 Z = -3324034
80
XDOT = -15384
021236 XDOT = -4689
049673
YDOT = -10546
242114 feet/sec YDOT = -3214
494596 meter/sec
ZDOT = -15417
981718 ZDOT = -4699
400828
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 12073
52522375
00016717 00000-0 10270-3 0 9113
2 25544 51
6382 241
7085 0016786 152
0722 208
1338 15
59066972 3100
Satellite: ISS
Catalog Number: 25544
Epoch time: 12073
52522375 = yrday
fracday
Element set: 911
Inclination: 51
6382 deg
RA of node: 241
7085 deg
Eccentricity:
0016786
Arg of perigee: 152
0722 deg
Mean anomaly: 208
1338 deg
Mean motion: 15
59066972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 310
Checksum: 297
Coasting Arc #13 (Orbit 325)
---------------------------------------
Vector Time (GMT): 2012/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2392485
53 A = 6763813
83 meter
Y = -3740772
25 meter E =
0021103
Z = 5097015
73 I = 51
33009
XDOT = 5186
986490 Wp = 149
37006
YDOT = 5450
465996 meter/sec RA = 235
87578 deg
ZDOT = 1544
762473 TA = 285
58662
MA = 285
81945
Ha = 218
519 n
mi
Hp = 202
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7849361
98 X = 2409377
81
Y = -12272874
85 feet Y = -3713923
30 meter
Z = 16722492
55 Z = 5108679
44
XDOT = 17017
672212 XDOT = 5118
148718
YDOT = 17882
106286 feet/sec YDOT = 5508
085264 meter/sec
ZDOT = 5068
118350 ZDOT = 1569
792963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9436418
06 X = 2876220
22
Y = -11026343
35 feet Y = -3360829
45 meter
Z = 16770553
49 Z = 5111664
70
XDOT = 13426
068515 XDOT = 4092
265683
YDOT = 19457
039501 feet/sec YDOT = 5930
505640 meter/sec
ZDOT = 5170
407225 ZDOT = 1575
940122
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 12074
55079058
00016717 00000-0 10270-3 0 9123
2 25544 51
6375 236
5571 0016743 156
1392 204
0543 15
59075935 3264
Satellite: ISS
Catalog Number: 25544
Epoch time: 12074
55079058 = yrday
fracday
Element set: 912
Inclination: 51
6375 deg
RA of node: 236
5571 deg
Eccentricity:
0016743
Arg of perigee: 156
1392 deg
Mean anomaly: 204
0543 deg
Mean motion: 15
59075935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 326
Checksum: 311
Coasting Arc #14 (Orbit 340)
---------------------------------------
Vector Time (GMT): 2012/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4640777
21 A = 6764486
25 meter
Y = 528444
86 meter E =
0026158
Z = -4915091
74 I = 51
35174
XDOT = -3118
797096 Wp = 137
50662
YDOT = -6632
861192 meter/sec RA = 230
80252 deg
ZDOT = 2219
610656 TA = 154
34240
MA = 154
21239
Ha = 218
412 n
mi
Hp = 202
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15225647
02 X = -4622465
34
Y = 1733742
99 feet Y = 476650
96 meter
Z = -16125629
07 Z = -4937591
71
XDOT = -10232
273936 XDOT = -3055
177552
YDOT = -21761
355616 feet/sec YDOT = -6667
381678 meter/sec
ZDOT = 7282
187190 ZDOT = 2204
614721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15224942
60 X = -4640562
51
Y = -204991
28 feet Y = -62481
34 meter
Z = -16217928
54 Z = -4943224
62
XDOT = -7440
488359 XDOT = -2267
860852
YDOT = -21780
897588 feet/sec YDOT = -6638
817585 meter/sec
ZDOT = 7221
104590 ZDOT = 2200
992679
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 12075
51223632
00016717 00000-0 10270-3 0 9130
2 25544 51
6384 231
7278 0016821 159
5768 200
6064 15
59120585 3415
Satellite: ISS
Catalog Number: 25544
Epoch time: 12075
51223632 = yrday
fracday
Element set: 913
Inclination: 51
6384 deg
RA of node: 231
7278 deg
Eccentricity:
0016821
Arg of perigee: 159
5768 deg
Mean anomaly: 200
6064 deg
Mean motion: 15
59120585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 341
Checksum: 299
Coasting Arc #15 (Orbit 356)
---------------------------------------
Vector Time (GMT): 2012/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886586
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5595812
24 A = 6771461
85 meter
Y = 2586091
82 meter E =
0025761
Z = 2760686
10 I = 51
39460
XDOT = -119
815792 Wp = 135
89784
YDOT = 5737
548970 meter/sec RA = 225
75509 deg
ZDOT = -5121
304706 TA = 12
56694
MA = 12
50283
Ha = 218
156 n
mi
Hp = 202
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18358964
06 X = 5553067
56
Y = 8484553
21 feet Y = 2648428
82 meter
Z = 9057369
10 Z = 2787765
90
XDOT = -393
096430 XDOT = -159
087549
YDOT = 18823
979562 feet/sec YDOT = 5735
989214 meter/sec
ZDOT = -16802
180795 ZDOT = -5121
982506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17258218
67 X = 5260305
05
Y = 10448532
90 feet Y = 3184712
83 meter
Z = 9168270
71 Z = 2794488
91
XDOT = -1599
546559 XDOT = -487
541791
YDOT = 17418
102039 feet/sec YDOT = 5309
037502 meter/sec
ZDOT = -16805
309623 ZDOT = -5122
258373
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 12076
53775501
00016717 00000-0 10270-3 0 9141
2 25544 51
6376 226
5757 0016762 163
5168 196
6536 15
59140442 3572
Satellite: ISS
Catalog Number: 25544
Epoch time: 12076
53775501 = yrday
fracday
Element set: 914
Inclination: 51
6376 deg
RA of node: 226
5757 deg
Eccentricity:
0016762
Arg of perigee: 163
5168 deg
Mean anomaly: 196
6536 deg
Mean motion: 15
59140442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 357
Checksum: 327
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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