[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 19th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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
080/00:30:36
758 1
9 4
6 4
6
N/A 3
0 -0
4 228
4
000/00:11:13
516 -3
0 0
1 214
0
Coasting Arc #1 (Orbit 2062)
---------------------------------------
Vector Time (GMT): 2013/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 838469
99 A = 6780855
38 meter
Y = -4146695
62 meter E =
0013051
Z = 5291445
12 I = 51
51541
XDOT = 7397
765474 Wp = 39
58507
YDOT = 1999
648306 meter/sec RA = 197
52861 deg
ZDOT = 404
122794 TA = 46
61168
MA = 46
50307
Ha = 226
677 n
mi
Hp = 213
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2750885
79 X = 859072
56
Y = -13604644
43 feet Y = -4137203
68 meter
Z = 17360384
24 Z = 5295568
71
XDOT = 24270
884102 XDOT = 7372
892046
YDOT = 6560
525938 feet/sec YDOT = 2082
235734 meter/sec
ZDOT = 1325
862186 ZDOT = 439
999794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3726424
65 X = 1135814
23
Y = -13347524
99 feet Y = -4068325
62 meter
Z = 17377974
55 Z = 5296806
64
XDOT = 22684
504373 XDOT = 6914
236933
YDOT = 8213
896630 feet/sec YDOT = 2503
595693 meter/sec
ZDOT = 1475
049856 ZDOT = 449
595196
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 13077
54907217
00016717 00000-0 10270-3 0 9000
2 25544 51
6462 198
3567 0012403 27
5933 332
5875 15
52943516 20639
Satellite: ISS
Catalog Number: 25544
Epoch time: 13077
54907217 = yrday
fracday
Element set: 900
Inclination: 51
6462 deg
RA of node: 198
3567 deg
Eccentricity:
0012403
Arg of perigee: 27
5933 deg
Mean anomaly: 332
5875 deg
Mean motion: 15
52943516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2063
Checksum: 313
Coasting Arc #2 (Orbit 2077)
---------------------------------------
Vector Time (GMT): 2013/078/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2076650
96 A = 6781093
92 meter
Y = 3798141
55 meter E =
0022497
Z = -5236339
93 I = 51
54596
XDOT = -7166
264148 Wp = 67
62184
YDOT = -2462
258933 meter/sec RA = 192
53520 deg
ZDOT = 1068
096218 TA = 212
57559
MA = 212
71459
Ha = 226
805 n
mi
Hp = 213
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6813159
33 X = -2093531
64
Y = 12461094
33 feet Y = 3774824
32 meter
Z = -17179592
94 Z = -5246469
38
XDOT = -23511
365316 XDOT = -7143
386529
YDOT = -8078
277340 feet/sec YDOT = -2542
268605 meter/sec
ZDOT = 3504
252685 ZDOT = 1033
339087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7479392
89 X = -2279718
95
Y = 12012173
44 feet Y = 3661310
46 meter
Z = -17222160
05 Z = -5249314
38
XDOT = -22100
398364 XDOT = -6736
201421
YDOT = -9000
403897 feet/sec YDOT = -2743
323108 meter/sec
ZDOT = 3359
757554 ZDOT = 1024
054102
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 13078
51435108
00016717 00000-0 10270-3 0 9014
2 25544 51
6462 193
5549 0012525 31
5348 328
6552 15
52963716 20784
Satellite: ISS
Catalog Number: 25544
Epoch time: 13078
51435108 = yrday
fracday
Element set: 901
Inclination: 51
6462 deg
RA of node: 193
5549 deg
Eccentricity:
0012525
Arg of perigee: 31
5348 deg
Mean anomaly: 328
6552 deg
Mean motion: 15
52963716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2078
Checksum: 312
Coasting Arc #3 (Orbit 2093)
---------------------------------------
Vector Time (GMT): 2013/079/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3330106
60 A = 6782776
41 meter
Y = -3413058
32 meter E =
0019323
Z = 4817414
86 I = 51
58212
XDOT = 6641
471420 Wp = 44
51649
YDOT = 2895
502144 meter/sec RA = 187
54332 deg
ZDOT = -2519
964780 TA = 70
37704
MA = 70
16858
Ha = 226
849 n
mi
Hp = 213
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10925546
59 X = 3344623
10
Y = -11197697
89 feet Y = -3375737
39 meter
Z = 15805166
88 Z = 4833627
66
XDOT = 21789
604396 XDOT = 6620
840915
YDOT = 9499
678951 feet/sec YDOT = 2969
655691 meter/sec
ZDOT = -8267
600985 ZDOT = -2487
751685
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11330144
26 X = 3453427
97
Y = -10688025
01 feet Y = -3257710
02 meter
Z = 15873035
59 Z = 4838101
25
XDOT = 20601
993575 XDOT = 6279
487642
YDOT = 9664
893663 feet/sec YDOT = 2945
859589 meter/sec
ZDOT = -8133
727387 ZDOT = -2479
160108
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 13079
54396249
00016717 00000-0 10270-3 0 9021
2 25544 51
6465 188
4307 0012636 35
2859 324
9127 15
52968314 20947
Satellite: ISS
Catalog Number: 25544
Epoch time: 13079
54396249 = yrday
fracday
Element set: 902
Inclination: 51
6465 deg
RA of node: 188
4307 deg
Eccentricity:
0012636
Arg of perigee: 35
2859 deg
Mean anomaly: 324
9127 deg
Mean motion: 15
52968314 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2094
Checksum: 332
Coasting Arc #4 (Orbit 2101)
---------------------------------------
Vector Time (GMT): 2013/080/00:36:13
516
Vector Time (MET): N/A
Weight (LBS) : 906812
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6760162
72 A = 6795069
82 meter
Y = 58850
84 meter E =
0019966
Z = 661913
74 I = 51
62935
XDOT = 556
942487 Wp = 92
61176
YDOT = 4783
683078 meter/sec RA = 184
94486 deg
ZDOT = -5958
741880 TA = 80
24853
MA = 80
02310
Ha = 228
350 n
mi
Hp = 214
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22179011
54 X = 6755786
83
Y = 193080
17 feet Y = 134422
82 meter
Z = 2171633
01 Z = 694743
12
XDOT = 1827
239130 XDOT = 532
354668
YDOT = 15694
498286 feet/sec YDOT = 4789
773151 meter/sec
ZDOT = -19549
678085 ZDOT = -5956
096472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22025957
65 X = -6713511
89
Y = 2488062
12 feet Y = 758361
33 meter
Z = 2308367
22 Z = 703590
33
XDOT = -3649
435934 XDOT = -1112
348073
YDOT = -13736
346388 feet/sec YDOT = -4186
838379 meter/sec
ZDOT = -19539
140048 ZDOT = -5955
529887
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 13080
05878634
00016717 00000-0 10270-3 0 9033
2 25544 51
6454 185
8725 0011935 52
5506 307
6729 15
52083349 21024
Satellite: ISS
Catalog Number: 25544
Epoch time: 13080
05878634 = yrday
fracday
Element set: 903
Inclination: 51
6454 deg
RA of node: 185
8725 deg
Eccentricity:
0011935
Arg of perigee: 52
5506 deg
Mean anomaly: 307
6729 deg
Mean motion: 15
52083349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2102
Checksum: 311
Coasting Arc #5 (Orbit 2117)
---------------------------------------
Vector Time (GMT): 2013/081/00:36:13
516
Vector Time (MET): N/A
Weight (LBS) : 906812
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6769782
38 A = 6795175
62 meter
Y = -271767
14 meter E =
0024620
Z = 346082
54 I = 51
66053
XDOT = 511
684847 Wp = 52
23599
YDOT = -4748
255239 meter/sec RA = 179
98358 deg
ZDOT = 6003
639654 TA = 311
49316
MA = 311
70422
Ha = 228
357 n
mi
Hp = 213
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22210572
13 X = -6767921
44
Y = -891624
48 feet Y = -347460
67 meter
Z = 1135441
41 Z = 313200
39
XDOT = 1678
756061 XDOT = 535
579020
YDOT = -15578
265221 feet/sec YDOT = -4742
399062 meter/sec
ZDOT = 19696
980492 ZDOT = 6006
183859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22127701
43 X = 6744523
39
Y = -2182103
57 feet Y = -665105
17 meter
Z = 998493
49 Z = 304340
82
XDOT = 447
555721 XDOT = 136
414984
YDOT = 14029
189878 feet/sec YDOT = 4276
097075 meter/sec
ZDOT = 19708
053740 ZDOT = 6007
014780
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 13081
08895951
00016717 00000-0 10270-3 0 9049
2 25544 51
6454 180
7528 0012022 55
5163 304
7123 15
52108796 21186
Satellite: ISS
Catalog Number: 25544
Epoch time: 13081
08895951 = yrday
fracday
Element set: 904
Inclination: 51
6454 deg
RA of node: 180
7528 deg
Eccentricity:
0012022
Arg of perigee: 55
5163 deg
Mean anomaly: 304
7123 deg
Mean motion: 15
52108796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2118
Checksum: 299
Coasting Arc #6 (Orbit 2132)
---------------------------------------
Vector Time (GMT): 2013/082/00:36:13
516
Vector Time (MET): N/A
Weight (LBS) : 906812
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6621960
51 A = 6794322
93 meter
Y = 554795
18 meter E =
0015537
Z = -1426618
48 I = 51
68937
XDOT = -1632
494492 Wp = 93
12412
YDOT = 4735
077129 meter/sec RA = 175
02380 deg
ZDOT = -5791
535980 TA = 102
39187
MA = 102
21794
Ha = 228
370 n
mi
Hp = 213
830
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21725592
21 X = 6622194
57
Y = 1820194
15 feet Y = 628847
26 meter
Z = -4680506
81 Z = -1394449
38
XDOT = -5355
953058 XDOT = -1657
188346
YDOT = 15535
029951 feet/sec YDOT = 4716
682817 meter/sec
ZDOT = -19001
102296 ZDOT = -5799
526936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21773253
11 X = -6636487
55
Y = 1573530
29 feet Y = 479612
03 meter
Z = -4546543
64 Z = -1385786
50
XDOT = 2882
708519 XDOT = 878
649557
YDOT = -14570
164126 feet/sec YDOT = -4440
986026 meter/sec
ZDOT = -19034
864927 ZDOT = -5801
826830
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 13082
05472898
00016717 00000-0 10270-3 0 9059
2 25544 51
6463 175
9525 0011923 59
3286 300
9039 15
52130112 21334
Satellite: ISS
Catalog Number: 25544
Epoch time: 13082
05472898 = yrday
fracday
Element set: 905
Inclination: 51
6463 deg
RA of node: 175
9525 deg
Eccentricity:
0011923
Arg of perigee: 59
3286 deg
Mean anomaly: 300
9039 deg
Mean motion: 15
52130112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2133
Checksum: 297
Coasting Arc #7 (Orbit 2148)
---------------------------------------
Vector Time (GMT): 2013/083/00:36:13
516
Vector Time (MET): N/A
Weight (LBS) : 906812
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6294066
44 A = 6792722
16 meter
Y = -809496
05 meter E =
0025776
Z = 2386033
55 I = 51
71478
XDOT = 2668
449759 Wp = 68
46246
YDOT = -4778
963400 meter/sec RA = 170
06407 deg
ZDOT = 5380
301564 TA = 318
17656
MA = 318
37325
Ha = 228
448 n
mi
Hp = 213
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20649824
28 X = -6296137
31
Y = -2655826
95 feet Y = -879891
54 meter
Z = 7828194
06 Z = 2355452
87
XDOT = 8754
756427 XDOT = 2695
554983
YDOT = -15679
013779 feet/sec YDOT = -4748
970856 meter/sec
ZDOT = 17651
908019 ZDOT = 5393
331007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20846015
01 X = 6353865
37
Y = -943221
00 feet Y = -287493
76 meter
Z = 7700861
91 Z = 2347222
71
XDOT = -5889
937228 XDOT = -1795
252867
YDOT = 15410
776237 feet/sec YDOT = 4697
204597 meter/sec
ZDOT = 17706
669225 ZDOT = 5396
992780
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 13083
08486570
00016717 00000-0 10270-3 0 9066
2 25544 51
6464 170
8326 0012101 62
3779 297
8591 15
52163661 21497
Satellite: ISS
Catalog Number: 25544
Epoch time: 13083
08486570 = yrday
fracday
Element set: 906
Inclination: 51
6464 deg
RA of node: 170
8326 deg
Eccentricity:
0012101
Arg of perigee: 62
3779 deg
Mean anomaly: 297
8591 deg
Mean motion: 15
52163661 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2149
Checksum: 317
Coasting Arc #8 (Orbit 2163)
---------------------------------------
Vector Time (GMT): 2013/084/00:36:13
516
Vector Time (MET): N/A
Weight (LBS) : 906812
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5814412
42 A = 6790387
13 meter
Y = 1167284
88 meter E =
0016095
Z = -3325600
35 I = 51
73790
XDOT = -3647
111989 Wp = 74
44639
YDOT = 4808
747722 meter/sec RA = 165
10303 deg
ZDOT = -4703
457287 TA = 144
08385
MA = 143
97555
Ha = 228
321 n
mi
Hp = 213
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19076156
23 X = 5817082
23
Y = 3829674
81 feet Y = 1232319
75 meter
Z = -10910762
30 Z = -3297348
30
XDOT = -11965
590515 XDOT = -3677
765371
YDOT = 15776
731373 feet/sec YDOT = 4767
791341 meter/sec
ZDOT = -15431
290313 ZDOT = -4721
249684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19521724
77 X = -5950221
71
Y = -144469
51 feet Y = -44034
31 meter
Z = -10793158
49 Z = -3289754
71
XDOT = 8666
476978 XDOT = 2641
542183
YDOT = -16310
085770 feet/sec YDOT = -4971
314143 meter/sec
ZDOT = -15505
904563 ZDOT = -4726
199711
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 13084
05060102
00016717 00000-0 10270-3 0 9074
2 25544 51
6470 166
0324 0011916 65
6729 294
5665 15
52194027 21646
Satellite: ISS
Catalog Number: 25544
Epoch time: 13084
05060102 = yrday
fracday
Element set: 907
Inclination: 51
6470 deg
RA of node: 166
0324 deg
Eccentricity:
0011916
Arg of perigee: 65
6729 deg
Mean anomaly: 294
5665 deg
Mean motion: 15
52194027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2164
Checksum: 294
Coasting Arc #9 (Orbit 2179)
---------------------------------------
Vector Time (GMT): 2013/085/00:36:13
516
Vector Time (MET): N/A
Weight (LBS) : 906812
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5190984
29 A = 6787948
02 meter
Y = -1538600
08 meter E =
0021893
Z = 4073971
66 I = 51
75921
XDOT = 4495
998048 Wp = 84
89063
YDOT = -4869
731793 meter/sec RA = 160
13988 deg
ZDOT = 3873
612606 TA = 325
06325
MA = 325
20672
Ha = 228
478 n
mi
Hp = 213
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17030788
35 X = -5193183
75
Y = -5047900
53 feet Y = -1596660
61 meter
Z = 13366048
75 Z = 4048749
26
XDOT = 14750
649765 XDOT = 4531
301340
YDOT = -15976
810343 feet/sec YDOT = -4819
256723 meter/sec
ZDOT = 12708
702774 ZDOT = 3895
540220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17785160
39 X = 5420916
89
Y = 1418321
47 feet Y = 432304
39 meter
Z = 13261098
94 Z = 4041982
96
XDOT = -10967
922176 XDOT = -3343
022679
YDOT = 17355
757154 feet/sec YDOT = 5290
034781 meter/sec
ZDOT = 12800
561156 ZDOT = 3901
611040
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 13085
08070220
00016717 00000-0 10270-3 0 9081
2 25544 51
6468 160
9122 0012112 69
1837 291
0611 15
52220867 21803
Satellite: ISS
Catalog Number: 25544
Epoch time: 13085
08070220 = yrday
fracday
Element set: 908
Inclination: 51
6468 deg
RA of node: 160
9122 deg
Eccentricity:
0012112
Arg of perigee: 69
1837 deg
Mean anomaly: 291
0611 deg
Mean motion: 15
52220867 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2180
Checksum: 278
Coasting Arc #10 (Orbit 2194)
---------------------------------------
Vector Time (GMT): 2013/086/00:36:13
516
Vector Time (MET): N/A
Weight (LBS) : 906812
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4464832
97 A = 6785502
65 meter
Y = 2024194
77 meter E =
0022545
Z = -4713358
61 I = 51
77967
XDOT = -5185
630769 Wp = 71
69117
YDOT = 4855
529042 meter/sec RA = 155
17398 deg
ZDOT = -2831
188418 TA = 170
21662
MA = 170
17265
Ha = 228
251 n
mi
Hp = 213
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14648402
12 X = 4464762
45
Y = 6641058
96 feet Y = 2074122
24 meter
Z = -15463774
98 Z = -4691669
27
XDOT = -17013
224307 XDOT = -5225
787729
YDOT = 15930
213391 feet/sec YDOT = 4797
315092 meter/sec
ZDOT = -9288
675912 ZDOT = -2856
478097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15851439
93 X = -4831518
89
Y = -3192524
61 feet Y = -973081
50 meter
Z = -15373591
78 Z = -4685870
78
XDOT = 12752
736681 XDOT = 3887
034141
YDOT = -18147
440285 feet/sec YDOT = -5531
339799 meter/sec
ZDOT = -9394
552763 ZDOT = -2863
459682
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 13086
04640362
00016717 00000-0 10270-3 0 9099
2 25544 51
6465 156
1116 0011944 72
0782 288
1671 15
52266771 21957
Satellite: ISS
Catalog Number: 25544
Epoch time: 13086
04640362 = yrday
fracday
Element set: 909
Inclination: 51
6465 deg
RA of node: 156
1116 deg
Eccentricity:
0011944
Arg of perigee: 72
0782 deg
Mean anomaly: 288
1671 deg
Mean motion: 15
52266771 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2195
Checksum: 310
Coasting Arc #11 (Orbit 2210)
---------------------------------------
Vector Time (GMT): 2013/087/00:36:13
516
Vector Time (MET): N/A
Weight (LBS) : 906812
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3650333
26 A = 6783710
78 meter
Y = -2541733
53 meter E =
0015983
Z = 5108102
40 I = 51
80102
XDOT = 5731
988329 Wp = 90
54300
YDOT = -4817
978940 meter/sec RA = 150
20651 deg
ZDOT = 1694
084498 TA = 343
12294
MA = 343
17605
Ha = 228
408 n
mi
Hp = 213
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11976158
99 X = -3646453
72
Y = -8339020
77 feet Y = -2582531
45 meter
Z = 16758866
15 Z = 5090379
06
XDOT = 18805
735988 XDOT = 5777
208515
YDOT = -15807
017520 feet/sec YDOT = -4753
627159 meter/sec
ZDOT = 5558
020008 ZDOT = 1722
040700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13723449
23 X = 4182907
32
Y = 5205406
91 feet Y = 1586608
02 meter
Z = 16685260
75 Z = 5085667
48
XDOT = -14064
158888 XDOT = -4286
755629
YDOT = 18838
160051 feet/sec YDOT = 5741
871184 meter/sec
ZDOT = 5675
018213 ZDOT = 1729
745551
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 13087
07646912
00016717 00000-0 10270-3 0 9102
2 25544 51
6462 150
9911 0012054 76
0199 284
2293 15
52281351 22115
Satellite: ISS
Catalog Number: 25544
Epoch time: 13087
07646912 = yrday
fracday
Element set: 910
Inclination: 51
6462 deg
RA of node: 150
9911 deg
Eccentricity:
0012054
Arg of perigee: 76
0199 deg
Mean anomaly: 284
2293 deg
Mean motion: 15
52281351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2211
Checksum: 291
Coasting Arc #12 (Orbit 2225)
---------------------------------------
Vector Time (GMT): 2013/088/00:36:13
516
Vector Time (MET): N/A
Weight (LBS) : 906812
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2813243
10 A = 6782695
08 meter
Y = 3149454
46 meter E =
0026622
Z = -5330723
88 I = 51
82305
XDOT = -6059
110752 Wp = 83
30175
YDOT = 4640
669561 meter/sec RA = 145
23713 deg
ZDOT = -454
812147 TA = 182
35211
MA = 182
36465
Ha = 228
186 n
mi
Hp = 213
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9229800
18 X = 2803711
63
Y = 10332855
85 feet Y = 3180859
98 meter
Z = -17489251
57 Z = -5317080
78
XDOT = -19878
972283 XDOT = -6108
344003
YDOT = 15225
293836 feet/sec YDOT = 4572
637435 meter/sec
ZDOT = -1492
165835 ZDOT = -484
367215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11670766
18 X = -3557249
53
Y = -7597681
17 feet Y = -2315773
22 meter
Z = -17432713
49 Z = -5313491
07
XDOT = 14756
845906 XDOT = 4497
886632
YDOT = -18952
383468 feet/sec YDOT = -5776
686481 meter/sec
ZDOT = -1615
825285 ZDOT = -492
503547
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 13088
04213758
00016717 00000-0 10270-3 0 9119
2 25544 51
6451 146
1896 0011943 78
9932 281
2563 15
52327668 22269
Satellite: ISS
Catalog Number: 25544
Epoch time: 13088
04213758 = yrday
fracday
Element set: 911
Inclination: 51
6451 deg
RA of node: 146
1896 deg
Eccentricity:
0011943
Arg of perigee: 78
9932 deg
Mean anomaly: 281
2563 deg
Mean motion: 15
52327668 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2226
Checksum: 322
Coasting Arc #13 (Orbit 2241)
---------------------------------------
Vector Time (GMT): 2013/089/00:36:13
516
Vector Time (MET): N/A
Weight (LBS) : 906812
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1946527
99 A = 6782713
88 meter
Y = -3772941
49 meter E =
0014926
Z = 5277448
26 I = 51
84798
XDOT = 6258
058942 Wp = 78
64372
YDOT = -4371
510314 meter/sec RA = 140
26938 deg
ZDOT = -812
245860 TA = 19
11675
MA = 19
06080
Ha = 228
230 n
mi
Hp = 213
113
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6386246
69 X = -1929830
20
Y = -12378416
96 feet Y = -3794614
92 meter
Z = 17314462
78 Z = 5268033
01
XDOT = 20531
689441 XDOT = 6310
422705
YDOT = -14342
225440 feet/sec YDOT = -4301
236054 meter/sec
ZDOT = -2664
848622 ZDOT = -781
716809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9620307
54 X = 2932269
74
Y = 10139173
11 feet Y = 3090419
96 meter
Z = 17275613
62 Z = 5265607
03
XDOT = -15121
858742 XDOT = -4609
142545
YDOT = 18697
851852 feet/sec YDOT = 5699
105244 meter/sec
ZDOT = -2537
139081 ZDOT = -773
319992
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 13089
07216694
00016717 00000-0 10270-3 0 9126
2 25544 51
6450 141
0687 0011919 82
8761 277
3746 15
52351323 22429
Satellite: ISS
Catalog Number: 25544
Epoch time: 13089
07216694 = yrday
fracday
Element set: 912
Inclination: 51
6450 deg
RA of node: 141
0687 deg
Eccentricity:
0011919
Arg of perigee: 82
8761 deg
Mean anomaly: 277
3746 deg
Mean motion: 15
52351323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2242
Checksum: 309
Coasting Arc #14 (Orbit 2256)
---------------------------------------
Vector Time (GMT): 2013/090/00:36:13
516
Vector Time (MET): N/A
Weight (LBS) : 906812
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1143792
42 A = 6783801
61 meter
Y = 4426142
75 meter E =
0024349
Z = -5033786
32 I = 51
87350
XDOT = -6239
538620 Wp = 96
15536
YDOT = 3923
583745 meter/sec RA = 135
30288 deg
ZDOT = 2038
124249 TA = 193
61556
MA = 193
68136
Ha = 228
117 n
mi
Hp = 213
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3752599
80 X = 1118666
36
Y = 14521465
71 feet Y = 4438792
49 meter
Z = -16515046
97 Z = -5028291
18
XDOT = -20470
927232 XDOT = -6292
849992
YDOT = 12872
650083 feet/sec YDOT = 3853
511366 meter/sec
ZDOT = 6686
759347 ZDOT = 2007
683040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7886828
25 X = -2403905
25
Y = -12786455
02 feet Y = -3897311
49 meter
Z = -16492612
18 Z = -5026948
19
XDOT = 14983
040867 XDOT = 4566
830856
YDOT = -17677
255332 feet/sec YDOT = -5388
027425 meter/sec
ZDOT = 6559
443362 ZDOT = 1999
318337
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 13090
03780334
00016717 00000-0 10270-3 0 9132
2 25544 51
6438 136
2664 0011894 86
1953 274
0559 15
52372444 22577
Satellite: ISS
Catalog Number: 25544
Epoch time: 13090
03780334 = yrday
fracday
Element set: 913
Inclination: 51
6438 deg
RA of node: 136
2664 deg
Eccentricity:
0011894
Arg of perigee: 86
1953 deg
Mean anomaly: 274
0559 deg
Mean motion: 15
52372444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2257
Checksum: 313
Coasting Arc #15 (Orbit 2272)
---------------------------------------
Vector Time (GMT): 2013/091/00:36:13
516
Vector Time (MET): N/A
Weight (LBS) : 906812
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -357444
68 A = 6785667
86 meter
Y = -5042730
79 meter E =
0020310
Z = 4510948
03 I = 51
90174
XDOT = 6127
902768 Wp = 80
52915
YDOT = -3322
953633 meter/sec RA = 130
34148 deg
ZDOT = -3213
566243 TA = 41
68834
MA = 41
53373
Ha = 228
034 n
mi
Hp = 213
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1172718
76 X = -322942
34
Y = -16544392
34 feet Y = -5046534
79 meter
Z = 14799698
27 Z = 4509295
68
XDOT = 20104
667874 XDOT = 6180
216051
YDOT = -10902
078849 feet/sec YDOT = -3254
135250 meter/sec
ZDOT = -10543
196335 ZDOT = -3183
669977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6256976
18 X = 1907126
34
Y = 15366525
63 feet Y = 4683717
01 meter
Z = 14793356
46 Z = 4509015
05
XDOT = -14754
342111 XDOT = -4497
123475
YDOT = 16086
440057 feet/sec YDOT = 4903
146929 meter/sec
ZDOT = -10418
197025 ZDOT = -3175
466453
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 13091
06779694
00016717 00000-0 10270-3 0 9144
2 25544 51
6441 131
1451 0011791 89
7299 270
5204 15
52420294 22730
Satellite: ISS
Catalog Number: 25544
Epoch time: 13091
06779694 = yrday
fracday
Element set: 914
Inclination: 51
6441 deg
RA of node: 131
1451 deg
Eccentricity:
0011791
Arg of perigee: 89
7299 deg
Mean anomaly: 270
5204 deg
Mean motion: 15
52420294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2273
Checksum: 308
Coasting Arc #16 (Orbit 2287)
---------------------------------------
Vector Time (GMT): 2013/092/00:36:13
516
Vector Time (MET): N/A
Weight (LBS) : 906812
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -299714
02 A = 6788087
21 meter
Y = 5606466
29 meter E =
0017991
Z = -3832587
24 I = 51
92775
XDOT = -5857
835232 Wp = 97
54107
YDOT = 2554
023491 meter/sec RA = 125
38455 deg
ZDOT = 4208
842803 TA = 216
71984
MA = 216
84324
Ha = 228
036 n
mi
Hp = 213
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -983313
72 X = -343766
72
Y = 18393918
28 feet Y = 5602868
20 meter
Z = -12574105
12 Z = -3834150
51
XDOT = -19218
619528 XDOT = -5906
404978
YDOT = 8379
342162 feet/sec YDOT = 2488
246132 meter/sec
ZDOT = 13808
539379 ZDOT = 4180
267785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5061293
25 X = -1542682
18
Y = -17706128
07 feet Y = -5396827
84 meter
Z = -12581239
78 Z = -3834761
89
XDOT = 14288
741662 XDOT = 4355
208459
YDOT = -13777
286031 feet/sec YDOT = -4199
316782 meter/sec
ZDOT = 13689
114966 ZDOT = 4172
442242
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 13092
03340150
00016717 00000-0 10270-3 0 9154
2 25544 51
6429 126
3429 0011889 93
6880 266
5632 15
52421648 22885
Satellite: ISS
Catalog Number: 25544
Epoch time: 13092
03340150 = yrday
fracday
Element set: 915
Inclination: 51
6429 deg
RA of node: 126
3429 deg
Eccentricity:
0011889
Arg of perigee: 93
6880 deg
Mean anomaly: 266
5632 deg
Mean motion: 15
52421648 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2288
Checksum: 313
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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