[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 12th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20451 43 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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
322/05:00:33
880 -0
2 9
8 9
8
N/A 9
7 -0
8 219
3
000/00:03:07
760 -1
6 0
2 203
0
Coasting Arc #1 (Orbit 2390)
---------------------------------------
Vector Time (GMT): 2011/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4427410
85 A = 6771975
48 meter
Y = 5006305
37 meter E =
0031364
Z = -1012488
66 I = 51
88155
XDOT = -4177
741526 Wp = 43
04018
YDOT = -2519
759140 meter/sec RA = 138
31527 deg
ZDOT = 5939
335939 TA = 305
98414
MA = 306
27456
Ha = 219
399 n
mi
Hp = 198
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14525626
16 X = -4478144
68
Y = 16424886
38 feet Y = 4956511
71 meter
Z = -3321813
18 Z = -1034120
64
XDOT = -13706
501069 XDOT = -4178
107524
YDOT = -8266
926313 feet/sec YDOT = -2566
479440 meter/sec
ZDOT = 19486
010299 ZDOT = 5919
038992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3066106
71 X = -934549
32
Y = -21697318
89 feet Y = -6613342
80 meter
Z = -3410350
93 Z = -1039474
96
XDOT = 13681
855006 XDOT = 4170
229406
YDOT = -4917
909317 feet/sec YDOT = -1498
978760 meter/sec
ZDOT = 19403
316975 ZDOT = 5914
131014
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 11315
50201068
00016717 00000-0 10270-3 0 9000
2 25544 51
6355 139
3132 0021738 44
6354 315
6548 15
59958472 23918
Satellite: ISS
Catalog Number: 25544
Epoch time: 11315
50201068 = yrday
fracday
Element set: 900
Inclination: 51
6355 deg
RA of node: 139
3132 deg
Eccentricity:
0021738
Arg of perigee: 44
6354 deg
Mean anomaly: 315
6548 deg
Mean motion: 15
59958472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2391
Checksum: 302
Coasting Arc #2 (Orbit 2406)
---------------------------------------
Vector Time (GMT): 2011/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5548236
63 A = 6769397
19 meter
Y = -2907253
32 meter E =
0023315
Z = -2602079
66 I = 51
89558
XDOT = 446
939147 Wp = 61
23797
YDOT = 5543
319085 meter/sec RA = 133
33283 deg
ZDOT = -5265
219674 TA = 147
94039
MA = 147
79837
Ha = 219
434 n
mi
Hp = 198
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18202876
08 X = 5592974
47
Y = -9538232
67 feet Y = -2844959
27 meter
Z = -8537006
77 Z = -2575017
18
XDOT = 1466
335785 XDOT = 410
497509
YDOT = 18186
742406 feet/sec YDOT = 5548
113530 meter/sec
ZDOT = -17274
342763 ZDOT = -5263
136646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4258508
36 X = -1297993
35
Y = 20151027
69 feet Y = 6142033
24 meter
Z = -8426402
22 Z = -2568367
40
XDOT = -13558
254508 XDOT = -4132
555974
YDOT = -10050
905767 feet/sec YDOT = -3063
516078 meter/sec
ZDOT = -17266
143458 ZDOT = -5262
720526
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 11316
52697417
00016717 00000-0 10270-3 0 9011
2 25544 51
6355 134
1572 0021892 48
4256 311
8772 15
60033974 24071
Satellite: ISS
Catalog Number: 25544
Epoch time: 11316
52697417 = yrday
fracday
Element set: 901
Inclination: 51
6355 deg
RA of node: 134
1572 deg
Eccentricity:
0021892
Arg of perigee: 48
4256 deg
Mean anomaly: 311
8772 deg
Mean motion: 15
60033974 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2407
Checksum: 306
Coasting Arc #3 (Orbit 2422)
---------------------------------------
Vector Time (GMT): 2011/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4552846
06 A = 6761757
81 meter
Y = -502473
92 meter E =
0024656
Z = 4951313
53 I = 51
88986
XDOT = 3109
473556 Wp = 66
44642
YDOT = -6694
397369 meter/sec RA = 128
31528 deg
ZDOT = 2180
967831 TA = 2
45130
MA = 2
43924
Ha = 219
577 n
mi
Hp = 198
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14937158
99 X = -4570941
97
Y = -1648536
49 feet Y = -553488
11 meter
Z = 16244466
96 Z = 4929151
38
XDOT = 10201
684896 XDOT = 3173
505569
YDOT = -21963
245961 feet/sec YDOT = -6659
267436 meter/sec
ZDOT = 7155
406269 ZDOT = 2196
229092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10655817
00 X = 3247893
02
Y = -10734045
16 feet Y = -3271736
96 meter
Z = 16154037
78 Z = 4923750
72
XDOT = 10068
146051 XDOT = 3068
770916
YDOT = 20852
022674 feet/sec YDOT = 6355
696511 meter/sec
ZDOT = 7218
072452 ZDOT = 2200
068483
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 11317
55190816
00016717 00000-0 10270-3 0 9027
2 25544 51
6352 129
0006 0021781 52
2293 308
0831 15
60043869 24230
Satellite: ISS
Catalog Number: 25544
Epoch time: 11317
55190816 = yrday
fracday
Element set: 902
Inclination: 51
6352 deg
RA of node: 129
0006 deg
Eccentricity:
0021781
Arg of perigee: 52
2293 deg
Mean anomaly: 308
0831 deg
Mean motion: 15
60043869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2423
Checksum: 281
Coasting Arc #4 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2011/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2122808
71 A = 6761224
03 meter
Y = 3987331
67 meter E =
0032014
Z = -5054686
15 I = 51
90752
XDOT = -5248
613592 Wp = 74
02376
YDOT = 5228
496790 meter/sec RA = 123
27128 deg
ZDOT = 1938
925762 TA = 214
63804
MA = 214
84697
Ha = 219
410 n
mi
Hp = 197
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6964595
49 X = 2102618
94
Y = 13081796
81 feet Y = 4010957
64 meter
Z = -16583615
97 Z = -5044422
17
XDOT = -17219
860867 XDOT = -5316
108684
YDOT = 17153
860859 feet/sec YDOT = 5169
426070 meter/sec
ZDOT = 6361
304995 ZDOT = 1913
263964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14676365
44 X = -4473356
19
Y = -2371412
85 feet Y = -722806
64 meter
Z = -16541947
15 Z = -5041985
49
XDOT = -3254
871563 XDOT = -992
084853
YDOT = -23067
008804 feet/sec YDOT = -7030
824284 meter/sec
ZDOT = 6256
250659 ZDOT = 1906
905201
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 11318
51275497
00016717 00000-0 10270-3 0 9034
2 25544 51
6361 124
1670 0021793 56
1801 304
1425 15
60099831 24386
Satellite: ISS
Catalog Number: 25544
Epoch time: 11318
51275497 = yrday
fracday
Element set: 903
Inclination: 51
6361 deg
RA of node: 124
1670 deg
Eccentricity:
0021793
Arg of perigee: 56
1801 deg
Mean anomaly: 304
1425 deg
Mean motion: 15
60099831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 294
Coasting Arc #5 (Orbit 2453)
---------------------------------------
Vector Time (GMT): 2011/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 887028
39 A = 6768745
51 meter
Y = -6131842
60 meter E =
0033056
Z = 2710057
95 I = 51
94874
XDOT = 5443
412045 Wp = 75
56891
YDOT = -1536
253720 meter/sec RA = 118
25285 deg
ZDOT = -5196
849523 TA = 73
83943
MA = 73
47586
Ha = 219
329 n
mi
Hp = 197
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2910198
13 X = 942364
80
Y = -20117593
82 feet Y = -6121614
05 meter
Z = 8891266
24 Z = 2714501
26
XDOT = 17858
963401 XDOT = 5485
431835
YDOT = -5040
202493 feet/sec YDOT = -1475
146911 meter/sec
ZDOT = -17050
031243 ZDOT = -5170
303116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14455968
24 X = 4406179
12
Y = 14278742
63 feet Y = 4352160
75 meter
Z = 8909766
60 Z = 2715696
86
XDOT = -5610
273012 XDOT = -1710
011214
YDOT = 16375
448781 feet/sec YDOT = 4991
236789 meter/sec
ZDOT = -16941
564884 ZDOT = -5163
788977
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 11319
53762769
00016717 00000-0 10270-3 0 9041
2 25544 51
6359 119
0100 0021699 59
6437 300
6861 15
60148201 24541
Satellite: ISS
Catalog Number: 25544
Epoch time: 11319
53762769 = yrday
fracday
Element set: 904
Inclination: 51
6359 deg
RA of node: 119
0100 deg
Eccentricity:
0021699
Arg of perigee: 59
6437 deg
Mean anomaly: 300
6861 deg
Mean motion: 15
60148201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2454
Checksum: 306
Coasting Arc #6 (Orbit 2469)
---------------------------------------
Vector Time (GMT): 2011/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3240696
42 A = 6771444
87 meter
Y = 5868449
63 meter E =
0035087
Z = 841620
01 I = 51
97293
XDOT = -3806
209827 Wp = 60
01074
YDOT = -2983
302467 meter/sec RA = 113
27407 deg
ZDOT = 5978
252713 TA = 309
08793
MA = 309
39948
Ha = 219
318 n
mi
Hp = 197
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10632206
10 X = -3310166
20
Y = 19253443
66 feet Y = 5831821
71 meter
Z = 2761220
51 Z = 825708
07
XDOT = -12487
565049 XDOT = -3801
608614
YDOT = -9787
737752 feet/sec YDOT = -3025
840378 meter/sec
ZDOT = 19613
690002 ZDOT = 5959
773008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9463334
15 X = -2884424
25
Y = -19863047
47 feet Y = -6054256
87 meter
Z = 2695902
43 Z = 821711
06
XDOT = 13845
646079 XDOT = 4220
152925
YDOT = -3868
124393 feet/sec YDOT = -1179
004315 meter/sec
ZDOT = 19538
417773 ZDOT = 5955
309737
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 11320
56247032
00016717 00000-0 10270-3 0 9058
2 25544 51
6371 113
8544 0021775 63
7744 296
5647 15
60206758 24706
Satellite: ISS
Catalog Number: 25544
Epoch time: 11320
56247032 = yrday
fracday
Element set: 905
Inclination: 51
6371 deg
RA of node: 113
8544 deg
Eccentricity:
0021775
Arg of perigee: 63
7744 deg
Mean anomaly: 296
5647 deg
Mean motion: 15
60206758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2470
Checksum: 308
Coasting Arc #7 (Orbit 2484)
---------------------------------------
Vector Time (GMT): 2011/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 871019
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4408641
93 A = 6764555
62 meter
Y = -3131835
14 meter E =
0029106
Z = -4094889
86 I = 51
96182
XDOT = 1040
600718 Wp = 68
16774
YDOT = 6518
389606 meter/sec RA = 108
28198 deg
ZDOT = -3876
549799 TA = 161
87061
MA = 161
76661
Ha = 219
299 n
mi
Hp = 197
467
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14464048
33 X = 4463227
47
Y = -10275049
66 feet Y = -3082229
68 meter
Z = -13434678
01 Z = -4073339
99
XDOT = 3414
044351 XDOT = 986
465196
YDOT = 21385
792669 feet/sec YDOT = 6529
723663 meter/sec
ZDOT = -12718
339234 ZDOT = -3871
625826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 200968
97 X = 61255
34
Y = 17807487
26 feet Y = 5427722
12 meter
Z = -13346494
74 Z = -4068011
60
XDOT = -18287
534356 XDOT = -5574
040472
YDOT = -9282
576320 feet/sec YDOT = -2829
329262 meter/sec
ZDOT = -12698
630102 ZDOT = -3870
542455
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 11321
52323143
00016717 00000-0 10270-3 0 9064
2 25544 51
6376 109
0203 0021857 66
9966 293
3492 15
60251450 24850
Satellite: ISS
Catalog Number: 25544
Epoch time: 11321
52323143 = yrday
fracday
Element set: 906
Inclination: 51
6376 deg
RA of node: 109
0203 deg
Eccentricity:
0021857
Arg of perigee: 66
9966 deg
Mean anomaly: 293
3492 deg
Mean motion: 15
60251450 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2485
Checksum: 298
Coasting Arc #8 (Orbit 2495)
---------------------------------------
Vector Time (GMT): 2011/322/05:02:07
760
Vector Time (MET): N/A
Weight (LBS) : 870101
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4290265
20 A = 6765136
07 meter
Y = -153160
60 meter E =
0028170
Z = -5252994
97 I = 51
95536
XDOT = -1080
454248 Wp = 73
35461
YDOT = 7497
838116 meter/sec RA = 104
71321 deg
ZDOT = -1098
066432 TA = 186
13266
MA = 186
16721
Ha = 219
257 n
mi
Hp = 203
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14075673
23 X = 4317177
34
Y = -502495
40 feet Y = -105033
66 meter
Z = -17234235
45 Z = -5232087
30
XDOT = -3544
797402 XDOT = -1158
881998
YDOT = 24599
206418 feet/sec YDOT = 7485
317319 meter/sec
ZDOT = -3602
580159 ZDOT = -1103
505703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9797423
42 X = -2986254
66
Y = -10262715
33 feet Y = -3128075
63 meter
Z = -17148851
81 Z = -5226970
03
XDOT = 19976
637140 XDOT = 6088
879000
YDOT = -12996
752911 feet/sec YDOT = -3961
410287 meter/sec
ZDOT = -3625
252269 ZDOT = -1104
976892
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 11322
22777790
00016717 00000-0 10270-3 0 9074
2 25544 51
6401 105
4780 0014196 65
0176 295
2451 15
58479025 24965
Satellite: ISS
Catalog Number: 25544
Epoch time: 11322
22777790 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 105
4780 deg
Eccentricity:
0014196
Arg of perigee: 65
0176 deg
Mean anomaly: 295
2451 deg
Mean motion: 15
58479025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2496
Checksum: 313
Coasting Arc #9 (Orbit 2511)
---------------------------------------
Vector Time (GMT): 2011/323/05:02:07
760
Vector Time (MET): N/A
Weight (LBS) : 870101
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3290459
11 A = 6766460
55 meter
Y = -3340442
09 meter E =
0021050
Z = 4865387
15 I = 51
96711
XDOT = 3068
762775 Wp = 65
19768
YDOT = -6608
806698 meter/sec RA = 99
68977 deg
ZDOT = -2445
162619 TA = 48
71528
MA = 48
53421
Ha = 219
244 n
mi
Hp = 202
794
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10795469
53 X = -3276496
50
Y = -10959455
68 feet Y = -3377159
97 meter
Z = 15962556
27 Z = 4849435
83
XDOT = 10068
119340 XDOT = 3154
313968
YDOT = -21682
436674 feet/sec YDOT = -6574
011562 meter/sec
ZDOT = -8022
187069 ZDOT = -2430
046614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -687904
88 X = -209673
41
Y = 15435260
65 feet Y = 4704667
45 meter
Z = 15897627
16 Z = 4845596
76
XDOT = -21679
712186 XDOT = -6607
976274
YDOT = 7289
496068 feet/sec YDOT = 2221
838402 meter/sec
ZDOT = -7960
045533 ZDOT = -2426
221878
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 11323
25373312
00016717 00000-0 10270-3 0 9081
2 25544 51
6399 100
3291 0014118 68
0709 292
1945 15
58548980 25121
Satellite: ISS
Catalog Number: 25544
Epoch time: 11323
25373312 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 100
3291 deg
Eccentricity:
0014118
Arg of perigee: 68
0709 deg
Mean anomaly: 292
1945 deg
Mean motion: 15
58548980 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2512
Checksum: 306
Coasting Arc #10 (Orbit 2526)
---------------------------------------
Vector Time (GMT): 2011/324/05:02:07
760
Vector Time (MET): N/A
Weight (LBS) : 870101
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1739746
20 A = 6773110
67 meter
Y = 5902182
51 meter E =
0018757
Z = -2836379
08 I = 51
99334
XDOT = -4323
838967 Wp = 68
89427
YDOT = 3721
198152 meter/sec RA = 94
69043 deg
ZDOT = 5125
026194 TA = 259
01324
MA = 259
22430
Ha = 219
198 n
mi
Hp = 202
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5707828
75 X = 1687396
35
Y = 19364115
84 feet Y = 5921344
70 meter
Z = -9305705
66 Z = -2828054
46
XDOT = -14185
823382 XDOT = -4390
025597
YDOT = 12208
655355 feet/sec YDOT = 3672
476289 meter/sec
ZDOT = 16814
390400 ZDOT = 5103
859888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10044846
39 X = 3061669
18
Y = -17529229
40 feet Y = -5342909
12 meter
Z = -9272088
58 Z = -2826132
60
XDOT = 17416
576156 XDOT = 5308
572412
YDOT = 1190
935201 feet/sec YDOT = 362
997049 meter/sec
ZDOT = 16727
715259 ZDOT = 5098
607611
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 11324
21554188
00016717 00000-0 10270-3 0 9091
2 25544 51
6398 95
5021 0014127 71
3675 288
9013 15
58544601 25276
Satellite: ISS
Catalog Number: 25544
Epoch time: 11324
21554188 = yrday
fracday
Element set: 909
Inclination: 51
6398 deg
RA of node: 95
5021 deg
Eccentricity:
0014127
Arg of perigee: 71
3675 deg
Mean anomaly: 288
9013 deg
Mean motion: 15
58544601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2527
Checksum: 311
Coasting Arc #11 (Orbit 2542)
---------------------------------------
Vector Time (GMT): 2011/325/05:02:07
760
Vector Time (MET): N/A
Weight (LBS) : 870101
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 180349
76 A = 6776468
59 meter
Y = -6765910
34 meter E =
0022141
Z = -273172
41 I = 52
00598
XDOT = 4719
137137 Wp = 102
96026
YDOT = 352
883596 meter/sec RA = 89
72027 deg
ZDOT = -6039
241588 TA = 79
97298
MA = 79
72321
Ha = 219
183 n
mi
Hp = 202
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 591698
69 X = 257321
15
Y = -22197868
57 feet Y = -6763463
19 meter
Z = -896234
94 Z = -272109
28
XDOT = 15482
733389 XDOT = 4744
178484
YDOT = 1157
754580 feet/sec YDOT = 405
795889 meter/sec
ZDOT = -19813
784738 ZDOT = -6016
254759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16226131
19 X = -4945724
79
Y = 15159706
49 feet Y = 4620678
54 meter
Z = -891447
84 Z = -271713
30
XDOT = -9024
968998 XDOT = -2750
810551
YDOT = -10739
019866 feet/sec YDOT = -3273
253255 meter/sec
ZDOT = -19719
935058 ZDOT = -6010
636206
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 11325
24144296
00016717 00000-0 10270-3 0 9102
2 25544 51
6398 90
3525 0014079 75
8106 284
4612 15
58551017 25435
Satellite: ISS
Catalog Number: 25544
Epoch time: 11325
24144296 = yrday
fracday
Element set: 910
Inclination: 51
6398 deg
RA of node: 90
3525 deg
Eccentricity:
0014079
Arg of perigee: 75
8106 deg
Mean anomaly: 284
4612 deg
Mean motion: 15
58551017 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2543
Checksum: 301
Coasting Arc #12 (Orbit 2558)
---------------------------------------
Vector Time (GMT): 2011/326/05:02:07
760
Vector Time (MET): N/A
Weight (LBS) : 870101
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2011838
33 A = 6771927
71 meter
Y = 5592641
49 meter E =
0026894
Z = 3218519
50 I = 51
98986
XDOT = -4176
417626 Wp = 82
04419
YDOT = -4292
817504 meter/sec RA = 84
74610 deg
ZDOT = 4818
221115 TA = 315
13925
MA = 315
35632
Ha = 219
157 n
mi
Hp = 202
533
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6600519
46 X = -2089862
17
Y = 18348561
31 feet Y = 5569707
57 meter
Z = 10559447
19 Z = 3208556
33
XDOT = -13702
157565 XDOT = -4151
510670
YDOT = -14084
046929 feet/sec YDOT = -4339
381581 meter/sec
ZDOT = 15807
812056 ZDOT = 4797
992046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17602493
35 X = 5365239
97
Y = -8441233
38 feet Y = -2572887
94 meter
Z = 10518378
72 Z = 3206001
83
XDOT = -617
901416 XDOT = -188
336352
YDOT = 18432
017048 feet/sec YDOT = 5618
078796 meter/sec
ZDOT = 15725
491851 ZDOT = 4793
129916
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 11326
26731380
00016717 00000-0 10270-3 0 9112
2 25544 51
6395 85
2027 0014144 78
1602 282
1138 15
58616711 25590
Satellite: ISS
Catalog Number: 25544
Epoch time: 11326
26731380 = yrday
fracday
Element set: 911
Inclination: 51
6395 deg
RA of node: 85
2027 deg
Eccentricity:
0014144
Arg of perigee: 78
1602 deg
Mean anomaly: 282
1138 deg
Mean motion: 15
58616711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2559
Checksum: 296
Coasting Arc #13 (Orbit 2573)
---------------------------------------
Vector Time (GMT): 2011/327/05:02:07
760
Vector Time (MET): N/A
Weight (LBS) : 870101
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3550009
70 A = 6765245
03 meter
Y = -2740743
85 meter E =
0027171
Z = -5089367
71 I = 51
96378
XDOT = 2712
763624 Wp = 78
92850
YDOT = 6918
711985 meter/sec RA = 79
73942 deg
ZDOT = -1836
860428 TA = 173
35237
MA = 173
31625
Ha = 218
975 n
mi
Hp = 202
535
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11647013
47 X = 3605117
24
Y = -8991941
78 feet Y = -2700737
13 meter
Z = -16697400
61 Z = -5071987
58
XDOT = 8900
143123 XDOT = 2644
118955
YDOT = 22699
186301 feet/sec YDOT = 6948
664037 meter/sec
ZDOT = -6026
444975 ZDOT = -1823
847936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14713536
97 X = -4484686
07
Y = -1546448
58 feet Y = -471357
53 meter
Z = -16626227
88 Z = -5067674
26
XDOT = 9003
799201 XDOT = 2744
357997
YDOT = -21554
172025 feet/sec YDOT = -6569
711633 meter/sec
ZDOT = -5973
790662 ZDOT = -1820
811394
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 11327
22904052
00016717 00000-0 10270-3 0 9128
2 25544 51
6390 80
3744 0014017 81
5833 278
6910 15
58679401 25740
Satellite: ISS
Catalog Number: 25544
Epoch time: 11327
22904052 = yrday
fracday
Element set: 912
Inclination: 51
6390 deg
RA of node: 80
3744 deg
Eccentricity:
0014017
Arg of perigee: 81
5833 deg
Mean anomaly: 278
6910 deg
Mean motion: 15
58679401 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2574
Checksum: 302
Coasting Arc #14 (Orbit 2589)
---------------------------------------
Vector Time (GMT): 2011/328/05:02:07
760
Vector Time (MET): N/A
Weight (LBS) : 870101
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4363043
63 A = 6765034
82 meter
Y = -893645
48 meter E =
0018869
Z = 5077623
76 I = 51
95797
XDOT = -578
022452 Wp = 76
77185
YDOT = -7452
766305 meter/sec RA = 74
71363 deg
ZDOT = -1798
543399 TA = 30
56223
MA = 30
45242
Ha = 219
029 n
mi
Hp = 202
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14314447
61 X = -4377393
22
Y = -2931907
74 feet Y = -942516
32 meter
Z = 16658870
60 Z = 5056392
65
XDOT = -1896
399122 XDOT = -485
903972
YDOT = -24451
333021 feet/sec YDOT = -7458
714911 meter/sec
ZDOT = -5900
732937 ZDOT = -1801
128291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8658309
85 X = 2639052
84
Y = 11891697
46 feet Y = 3624589
38 meter
Z = 16572225
71 Z = 5051214
40
XDOT = -14262
904086 XDOT = -4347
333165
YDOT = 18666
994748 feet/sec YDOT = 5689
699999 meter/sec
ZDOT = -5910
744919 ZDOT = -1801
595051
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 11328
25485518
00016717 00000-0 10270-3 0 9134
2 25544 51
6397 75
2250 0013975 85
2619 275
0131 15
58735350 25907
Satellite: ISS
Catalog Number: 25544
Epoch time: 11328
25485518 = yrday
fracday
Element set: 913
Inclination: 51
6397 deg
RA of node: 75
2250 deg
Eccentricity:
0013975
Arg of perigee: 85
2619 deg
Mean anomaly: 275
0131 deg
Mean motion: 15
58735350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2590
Checksum: 315
Coasting Arc #15 (Orbit 2604)
---------------------------------------
Vector Time (GMT): 2011/329/05:02:07
760
Vector Time (MET): N/A
Weight (LBS) : 870101
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4258449
29 A = 6771394
55 meter
Y = 4135754
61 meter E =
0018579
Z = -3272583
93 I = 51
96969
XDOT = -1877
319801 Wp = 86
91956
YDOT = 5692
855736 meter/sec RA = 69
70535 deg
ZDOT = 4775
799004 TA = 235
27970
MA = 235
45483
Ha = 218
870 n
mi
Hp = 202
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13971290
33 X = 4227783
92
Y = 13568748
70 feet Y = 4183204
06 meter
Z = -10736823
91 Z = -3251970
02
XDOT = -6159
185698 XDOT = -1964
039360
YDOT = 18677
348216 feet/sec YDOT = 5671
377041 meter/sec
ZDOT = 15668
631903 ZDOT = 4766
468718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1534397
52 X = -467684
36
Y = -19461442
19 feet Y = -5931847
58 meter
Z = -10652942
08 Z = -3247016
75
XDOT = 15634
796141 XDOT = 4765
485864
YDOT = -9744
478499 feet/sec YDOT = -2970
117046 meter/sec
ZDOT = 15630
093555 ZDOT = 4764
052516
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 11329
21653126
00016717 00000-0 10270-3 0 9144
2 25544 51
6389 70
3966 0013988 88
6879 271
5879 15
58763243 26056
Satellite: ISS
Catalog Number: 25544
Epoch time: 11329
21653126 = yrday
fracday
Element set: 914
Inclination: 51
6389 deg
RA of node: 70
3966 deg
Eccentricity:
0013988
Arg of perigee: 88
6879 deg
Mean anomaly: 271
5879 deg
Mean motion: 15
58763243 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2605
Checksum: 354
Coasting Arc #16 (Orbit 2620)
---------------------------------------
Vector Time (GMT): 2011/330/05:02:07
760
Vector Time (MET): N/A
Weight (LBS) : 870101
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3021461
28 A = 6775757
66 meter
Y = -6054451
47 meter E =
0024836
Z = 188971
13 I = 51
97348
XDOT = 4150
225543 Wp = 110
97670
YDOT = -2279
390631 meter/sec RA = 64
73005 deg
ZDOT = -6043
377303 TA = 66
99235
MA = 66
73057
Ha = 218
798 n
mi
Hp = 202
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9912930
72 X = -2954452
65
Y = -19863685
94 feet Y = -6087864
66 meter
Z = 619984
02 Z = 174454
71
XDOT = 13616
225535 XDOT = 4204
763759
YDOT = -7478
315720 feet/sec YDOT = -2232
674628 meter/sec
ZDOT = -19827
353357 ZDOT = -6023
082988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5351255
46 X = -1631062
67
Y = 21546827
13 feet Y = 6567472
91 meter
Z = 561159
98 Z = 171041
56
XDOT = -13732
349670 XDOT = -4185
620179
YDOT = -2836
985600 feet/sec YDOT = -864
713211 meter/sec
ZDOT = -19744
281785 ZDOT = -6018
057088
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 11330
24229085
00016717 00000-0 10270-3 0 9153
2 25544 51
6392 65
2469 0014035 92
0784 268
1978 15
58805484 26213
Satellite: ISS
Catalog Number: 25544
Epoch time: 11330
24229085 = yrday
fracday
Element set: 915
Inclination: 51
6392 deg
RA of node: 65
2469 deg
Eccentricity:
0014035
Arg of perigee: 92
0784 deg
Mean anomaly: 268
1978 deg
Mean motion: 15
58805484 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2621
Checksum: 320
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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