[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 29th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 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
093/19:42:41
789 -1
0 2
2 2
3
N/A 2
0 -0
2 228
1
000/00:05:23
578 0
2 -0
1 214
6
Coasting Arc #1 (Orbit 2232)
---------------------------------------
Vector Time (GMT): 2013/088/11:45:59
675
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4582169
60 A = 6794106
22 meter
Y = 4819549
67 meter E =
0018855
Z = -1379435
24 I = 51
87059
XDOT = -4324
328360 Wp = 64
31306
YDOT = -2463
905733 meter/sec RA = 142
92415 deg
ZDOT = 5825
764144 TA = 280
72356
MA = 280
93580
Ha = 228
331 n
mi
Hp = 213
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15033364
83 X = -4629021
28
Y = 15812170
83 feet Y = 4768046
85 meter
Z = -4525706
17 Z = -1401809
59
XDOT = -14187
429002 XDOT = -4324
755355
YDOT = -8083
680225 feet/sec YDOT = -2512
264845 meter/sec
ZDOT = 19113
399421 ZDOT = 5804
755942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14235023
86 X = -4338835
27
Y = 16508587
97 feet Y = 5031817
61 meter
Z = -4619463
16 Z = -1408012
37
XDOT = -13469
952933 XDOT = -4105
641654
YDOT = -6353
791943 feet/sec YDOT = -1936
635784 meter/sec
ZDOT = 19026
092700 ZDOT = 5799
153055
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
49301953
00016717 00000-0 10270-3 0 9001
2 25544 51
6441 143
9582 0011801 82
6814 277
5679 15
52196124 22334
Satellite: ISS
Catalog Number: 25544
Epoch time: 13088
49301953 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 143
9582 deg
Eccentricity:
0011801
Arg of perigee: 82
6814 deg
Mean anomaly: 277
5679 deg
Mean motion: 15
52196124 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2233
Checksum: 309
Coasting Arc #2 (Orbit 2248)
---------------------------------------
Vector Time (GMT): 2013/089/11:45:59
675
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4901990
06 A = 6794713
42 meter
Y = -4689433
64 meter E =
0022659
Z = 257880
95 I = 51
89738
XDOT = 3449
418231 Wp = 110
00030
YDOT = 3251
290641 meter/sec RA = 137
97775 deg
ZDOT = -6024
736845 TA = 67
23277
MA = 66
99351
Ha = 228
315 n
mi
Hp = 213
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16082644
55 X = 4952811
25
Y = -15385280
99 feet Y = -4634332
32 meter
Z = 846066
11 Z = 281818
49
XDOT = 11316
988948 XDOT = 3442
072108
YDOT = 10666
964044 feet/sec YDOT = 3289
822615 meter/sec
ZDOT = -19766
196998 ZDOT = -6007
997818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15046298
94 X = 4586111
92
Y = -16394739
36 feet Y = -4997116
56 meter
Z = 946342
58 Z = 288445
22
XDOT = 10910
307623 XDOT = 3325
461764
YDOT = 8804
684022 feet/sec YDOT = 2683
667690 meter/sec
ZDOT = -19696
765864 ZDOT = -6003
574235
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
52310637
00016717 00000-0 10270-3 0 9016
2 25544 51
6444 138
8368 0011942 86
4377 273
8141 15
52266426 22497
Satellite: ISS
Catalog Number: 25544
Epoch time: 13089
52310637 = yrday
fracday
Element set: 901
Inclination: 51
6444 deg
RA of node: 138
8368 deg
Eccentricity:
0011942
Arg of perigee: 86
4377 deg
Mean anomaly: 273
8141 deg
Mean motion: 15
52266426 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2249
Checksum: 317
Coasting Arc #3 (Orbit 2264)
---------------------------------------
Vector Time (GMT): 2013/090/11:45:59
675
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5035864
21 A = 6794619
36 meter
Y = 4479760
08 meter E =
0024103
Z = 796180
21 I = 51
91812
XDOT = -2626
449871 Wp = 70
59128
YDOT = -4037
577315 meter/sec RA = 133
03356 deg
ZDOT = 5966
343088 TA = 297
97982
MA = 298
22353
Ha = 228
411 n
mi
Hp = 213
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16521864
20 X = -5089451
23
Y = 14697375
58 feet Y = 4423146
30 meter
Z = 2612139
79 Z = 771585
76
XDOT = -8616
961519 XDOT = -2610
088756
YDOT = -13246
644735 feet/sec YDOT = -4066
856062 meter/sec
ZDOT = 19574
616430 ZDOT = 5953
623921
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15277416
44 X = -4656556
53
Y = 16003529
00 feet Y = 4877875
64 meter
Z = 2509128
62 Z = 764782
40
XDOT = -8626
735737 XDOT = -2629
429053
YDOT = -11370
524650 feet/sec YDOT = -3465
735913 meter/sec
ZDOT = 19522
026790 ZDOT = 5950
313766
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
55318062
00016717 00000-0 10270-3 0 9022
2 25544 51
6437 133
7163 0012044 89
3902 270
8630 15
52227397 22658
Satellite: ISS
Catalog Number: 25544
Epoch time: 13090
55318062 = yrday
fracday
Element set: 902
Inclination: 51
6437 deg
RA of node: 133
7163 deg
Eccentricity:
0012044
Arg of perigee: 89
3902 deg
Mean anomaly: 270
8630 deg
Mean motion: 15
52227397 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2265
Checksum: 294
Coasting Arc #4 (Orbit 2279)
---------------------------------------
Vector Time (GMT): 2013/091/11:45:59
675
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5091102
35 A = 6793149
96 meter
Y = -4072263
35 meter E =
0017649
Z = -1908854
63 I = 51
93521
XDOT = 1795
917465 Wp = 110
98811
YDOT = 4865
244785 meter/sec RA = 128
08911 deg
ZDOT = -5637
514515 TA = 89
92230
MA = 89
72006
Ha = 228
319 n
mi
Hp = 213
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16703091
71 X = 5145533
64
Y = -13360444
05 feet Y = -4015027
19 meter
Z = -6262646
44 Z = -1883989
97
XDOT = 5892
117667 XDOT = 1768
765443
YDOT = 15962
089188 feet/sec YDOT = 4885
175753 meter/sec
ZDOT = -18495
782530 ZDOT = -5628
856272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15335069
03 X = 4674129
04
Y = -14954049
21 feet Y = -4557994
20 meter
Z = -6158534
62 Z = -1877121
35
XDOT = 6467
653409 XDOT = 1971
340759
YDOT = 14168
821728 feet/sec YDOT = 4318
656863 meter/sec
ZDOT = -18460
215264 ZDOT = -5626
673613
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
51885806
00016717 00000-0 10270-3 0 9035
2 25544 51
6448 128
9149 0012039 93
4945 266
7584 15
52300512 22807
Satellite: ISS
Catalog Number: 25544
Epoch time: 13091
51885806 = yrday
fracday
Element set: 903
Inclination: 51
6448 deg
RA of node: 128
9149 deg
Eccentricity:
0012039
Arg of perigee: 93
4945 deg
Mean anomaly: 266
7584 deg
Mean motion: 15
52300512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2280
Checksum: 316
Coasting Arc #5 (Orbit 2295)
---------------------------------------
Vector Time (GMT): 2013/092/11:45:59
675
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5006622
48 A = 6791284
40 meter
Y = 3566633
62 meter E =
0025294
Z = 2864124
65 I = 51
94606
XDOT = -1080
338441 Wp = 88
31397
YDOT = -5636
039346 meter/sec RA = 123
14356 deg
ZDOT = 5091
974363 TA = 304
12137
MA = 304
36106
Ha = 228
412 n
mi
Hp = 213
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16425926
78 X = -5060046
39
Y = 11701553
87 feet Y = 3510347
85 meter
Z = 9396734
42 Z = 2839672
96
XDOT = -3544
417457 XDOT = -1041
970206
YDOT = -18490
942737 feet/sec YDOT = -5647
905581 meter/sec
ZDOT = 16705
952636 ZDOT = 5086
819656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15012220
97 X = -4575724
95
Y = 13538231
16 feet Y = 4126452
86 meter
Z = 9294383
78 Z = 2832928
18
XDOT = -4783
871399 XDOT = -1458
124002
YDOT = -16846
005235 feet/sec YDOT = -5134
662396 meter/sec
ZDOT = 16685
082244 ZDOT = 5085
613068
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
54890288
00016717 00000-0 10270-3 0 9040
2 25544 51
6439 123
7944 0012185 96
6628 263
5911 15
52291149 22969
Satellite: ISS
Catalog Number: 25544
Epoch time: 13092
54890288 = yrday
fracday
Element set: 904
Inclination: 51
6439 deg
RA of node: 123
7944 deg
Eccentricity:
0012185
Arg of perigee: 96
6628 deg
Mean anomaly: 263
5911 deg
Mean motion: 15
52291149 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2296
Checksum: 333
Coasting Arc #6 (Orbit 2310)
---------------------------------------
Vector Time (GMT): 2013/093/11:45:59
675
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4880138
80 A = 6788601
43 meter
Y = -2849705
87 meter E =
0017615
Z = -3775712
36 I = 51
95489
XDOT = 402
922102 Wp = 93
36992
YDOT = 6333
813072 meter/sec RA = 118
19468 deg
ZDOT = -4277
842984 TA = 131
49360
MA = 131
34227
Ha = 228
249 n
mi
Hp = 213
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16010954
06 X = 4929983
45
Y = -9349428
72 feet Y = -2794854
62 meter
Z = -12387507
76 Z = -3751883
91
XDOT = 1321
922908 XDOT = 352
846650
YDOT = 20780
226613 feet/sec YDOT = 6338
038549 meter/sec
ZDOT = -14034
917925 ZDOT = -4276
007651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14697569
33 X = 4479819
13
Y = -11410683
38 feet Y = -3477976
29 meter
Z = -12287822
28 Z = -3745328
23
XDOT = 3332
904444 XDOT = 1015
869275
YDOT = 19334
439424 feet/sec YDOT = 5893
137137 meter/sec
ZDOT = -14027
971966 ZDOT = -4275
725855
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 13093
51455436
00016717 00000-0 10270-3 0 9051
2 25544 51
6452 118
9932 0012086 100
4828 259
7686 15
52342121 23114
Satellite: ISS
Catalog Number: 25544
Epoch time: 13093
51455436 = yrday
fracday
Element set: 905
Inclination: 51
6452 deg
RA of node: 118
9932 deg
Eccentricity:
0012086
Arg of perigee: 100
4828 deg
Mean anomaly: 259
7686 deg
Mean motion: 15
52342121 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2311
Checksum: 299
Coasting Arc #7 (Orbit 2315)
---------------------------------------
Vector Time (GMT): 2013/093/19:45:23
578
Vector Time (MET): N/A
Weight (LBS) : 903996
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2745781
93 A = 6784710
59 meter
Y = 3507940
76 meter E =
0023494
Z = -5138420
38 I = 51
94316
XDOT = -4462
566982 Wp = 102
40511
YDOT = 5973
829430 meter/sec RA = 116
50776 deg
ZDOT = 1695
271052 TA = 183
93847
MA = 183
95700
Ha = 228
140 n
mi
Hp = 214
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9008470
90 X = 2731312
28
Y = 11508991
99 feet Y = 3538564
57 meter
Z = -16858334
60 Z = -5125117
05
XDOT = -14640
967788 XDOT = -4537
271090
YDOT = 19599
177920 feet/sec YDOT = 5923
508615 meter/sec
ZDOT = 5561
912901 ZDOT = 1673
410532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3499040
35 X = 1066507
50
Y = -14255539
30 feet Y = -4345088
38 meter
Z = -16803249
86 Z = -5121630
56
XDOT = 23441
314791 XDOT = 7144
912748
YDOT = -687
626002 feet/sec YDOT = -209
588405 meter/sec
ZDOT = 5470
080229 ZDOT = 1667
280454
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 13093
83643680
00016717 00000-0 10270-3 0 9067
2 25544 51
6457 117
3931 0010085 101
7329 258
4955 15
51923786 23169
Satellite: ISS
Catalog Number: 25544
Epoch time: 13093
83643680 = yrday
fracday
Element set: 906
Inclination: 51
6457 deg
RA of node: 117
3931 deg
Eccentricity:
0010085
Arg of perigee: 101
7329 deg
Mean anomaly: 258
4955 deg
Mean motion: 15
51923786 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2316
Checksum: 320
Coasting Arc #8 (Orbit 2331)
---------------------------------------
Vector Time (GMT): 2013/094/19:45:23
578
Vector Time (MET): N/A
Weight (LBS) : 903996
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2324788
52 A = 6786080
63 meter
Y = -4234687
96 meter E =
0016539
Z = 4752071
51 I = 51
96078
XDOT = 4510
604341 Wp = 86
77341
YDOT = -5569
081310 meter/sec RA = 111
55428 deg
ZDOT = -2746
966373 TA = 30
30305
MA = 30
20753
Ha = 228
117 n
mi
Hp = 214
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7627258
91 X = -2300346
71
Y = -13893333
20 feet Y = -4260548
14 meter
Z = 15590785
79 Z = 4740837
69
XDOT = 14798
570673 XDOT = 4585
887716
YDOT = -18271
264141 feet/sec YDOT = -5518
220195 meter/sec
ZDOT = -9012
356866 ZDOT = -2724
871034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5981787
21 X = -1823248
74
Y = 14726229
00 feet Y = 4488554
60 meter
Z = 15544413
43 Z = 4737937
21
XDOT = -22473
683881 XDOT = -6849
978847
YDOT = 318
026052 feet/sec YDOT = 96
934341 meter/sec
ZDOT = -8919
578379 ZDOT = -2718
687490
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 13094
86672505
00016717 00000-0 10270-3 0 9070
2 25544 51
6454 112
2741 0010019 105
1332 255
0929 15
51970658 23320
Satellite: ISS
Catalog Number: 25544
Epoch time: 13094
86672505 = yrday
fracday
Element set: 907
Inclination: 51
6454 deg
RA of node: 112
2741 deg
Eccentricity:
0010019
Arg of perigee: 105
1332 deg
Mean anomaly: 255
0929 deg
Mean motion: 15
51970658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2332
Checksum: 294
Coasting Arc #9 (Orbit 2346)
---------------------------------------
Vector Time (GMT): 2013/095/19:45:23
578
Vector Time (MET): N/A
Weight (LBS) : 903996
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1993335
55 A = 6788073
19 meter
Y = 4925314
83 meter E =
0018021
Z = -4243074
71 I = 51
97827
XDOT = -4488
953338 Wp = 109
39992
YDOT = 4981
912557 meter/sec RA = 106
60390 deg
ZDOT = 3681
022077 TA = 198
21649
MA = 198
28113
Ha = 228
008 n
mi
Hp = 214
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6539814
80 X = 1958723
11
Y = 16159169
39 feet Y = 4947411
59 meter
Z = -13920848
79 Z = -4233475
89
XDOT = -14727
537199 XDOT = -4562
209863
YDOT = 16344
857469 feet/sec YDOT = 4931
305037 meter/sec
ZDOT = 12076
844086 ZDOT = 3659
036776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8171077
89 X = 2490544
54
Y = -15434339
91 feet Y = -4704386
80 meter
Z = -13881376
08 Z = -4231043
43
XDOT = 20907
518459 XDOT = 6372
611626
YDOT = 310
375825 feet/sec YDOT = 94
602551 meter/sec
ZDOT = 11984
581384 ZDOT = 3652
900406
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 13095
83260777
00016717 00000-0 10270-3 0 9083
2 25544 51
6459 107
4747 0010005 108
7569 251
4669 15
51967711 23476
Satellite: ISS
Catalog Number: 25544
Epoch time: 13095
83260777 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node: 107
4747 deg
Eccentricity:
0010005
Arg of perigee: 108
7569 deg
Mean anomaly: 251
4669 deg
Mean motion: 15
51967711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2347
Checksum: 333
Coasting Arc #10 (Orbit 2362)
---------------------------------------
Vector Time (GMT): 2013/096/19:45:23
578
Vector Time (MET): N/A
Weight (LBS) : 903996
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1674859
63 A = 6790295
53 meter
Y = -5538903
41 meter E =
0021740
Z = 3531145
87 I = 51
99334
XDOT = 4495
054630 Wp = 99
01551
YDOT = -4261
191308 meter/sec RA = 101
65735 deg
ZDOT = -4531
607139 TA = 39
60113
MA = 39
44253
Ha = 228
020 n
mi
Hp = 214
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5494946
28 X = -1629951
28
Y = -18172255
29 feet Y = -5557381
24 meter
Z = 11585124
24 Z = 3523119
29
XDOT = 14747
554559 XDOT = 4564
383404
YDOT = -13980
286444 feet/sec YDOT = -4210
537668 meter/sec
ZDOT = -14867
477490 ZDOT = -4509
601693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10120607
72 X = -3084761
23
Y = 16085969
95 feet Y = 4903003
64 meter
Z = 11552284
23 Z = 3521136
23
XDOT = -19106
638736 XDOT = -5823
703487
YDOT = -1361
974703 feet/sec YDOT = -415
129889 meter/sec
ZDOT = -14775
205293 ZDOT = -4503
482573
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 13096
86286824
00016717 00000-0 10270-3 0 9099
2 25544 51
6455 102
3551 0010065 112
2733 247
9487 15
51991732 23634
Satellite: ISS
Catalog Number: 25544
Epoch time: 13096
86286824 = yrday
fracday
Element set: 909
Inclination: 51
6455 deg
RA of node: 102
3551 deg
Eccentricity:
0010065
Arg of perigee: 112
2733 deg
Mean anomaly: 247
9487 deg
Mean motion: 15
51991732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2363
Checksum: 317
Coasting Arc #11 (Orbit 2377)
---------------------------------------
Vector Time (GMT): 2013/097/19:45:23
578
Vector Time (MET): N/A
Weight (LBS) : 903996
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1445122
86 A = 6792318
54 meter
Y = 6049691
64 meter E =
0013083
Z = -2742873
95 I = 52
00575
XDOT = -4479
542112 Wp = 97
60267
YDOT = 3411
929749 meter/sec RA = 96
71422 deg
ZDOT = 5184
717381 TA = 231
60024
MA = 231
71780
Ha = 227
849 n
mi
Hp = 214
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4741216
73 X = 1390690
69
Y = 19848069
68 feet Y = 6065547
23 meter
Z = -8998930
30 Z = -2735986
61
XDOT = -14696
660471 XDOT = -4542
548147
YDOT = 11193
995240 feet/sec YDOT = 3361
485038 meter/sec
ZDOT = 17010
227628 ZDOT = 5162
802644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11605044
19 X = 3537217
47
Y = -16800342
14 feet Y = -5120744
28 meter
Z = -8970908
88 Z = -2734333
03
XDOT = 16984
864297 XDOT = 5176
986638
YDOT = 2732
751222 feet/sec YDOT = 832
942573 meter/sec
ZDOT = 16918
425443 ZDOT = 5156
736075
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 13097
82872264
00016717 00000-0 10270-3 0 9107
2 25544 51
6457 97
5551 0009906 115
9602 244
2571 15
52013968 23785
Satellite: ISS
Catalog Number: 25544
Epoch time: 13097
82872264 = yrday
fracday
Element set: 910
Inclination: 51
6457 deg
RA of node: 97
5551 deg
Eccentricity:
0009906
Arg of perigee: 115
9602 deg
Mean anomaly: 244
2571 deg
Mean motion: 15
52013968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2378
Checksum: 326
Coasting Arc #12 (Orbit 2393)
---------------------------------------
Vector Time (GMT): 2013/098/19:45:23
578
Vector Time (MET): N/A
Weight (LBS) : 903996
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1198178
85 A = 6794165
81 meter
Y = -6431571
90 meter E =
0023967
Z = 1788740
81 I = 52
01424
XDOT = 4525
280350 Wp = 116
85086
YDOT = -2440
416190 meter/sec RA = 91
77484 deg
ZDOT = -5695
490100 TA = 43
59978
MA = 43
41063
Ha = 227
897 n
mi
Hp = 214
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3931032
96 X = -1134859
86
Y = -21100957
68 feet Y = -6444616
44 meter
Z = 5868572
22 Z = 1783074
71
XDOT = 14846
720307 XDOT = 4579
900635
YDOT = -8006
614795 feet/sec YDOT = -2389
506945 meter/sec
ZDOT = -18685
991142 ZDOT = -5673
373568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12797521
01 X = -3900684
40
Y = 17239339
40 feet Y = 5254550
65 meter
Z = 5845699
99 Z = 1781769
36
XDOT = -14780
673712 XDOT = -4505
149347
YDOT = -4613
866609 feet/sec YDOT = -1406
306543 meter/sec
ZDOT = -18593
455968 ZDOT = -5667
285379
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 13098
85895444
00016717 00000-0 10270-3 0 9117
2 25544 51
6455 92
4352 0010057 120
0678 240
1472 15
52007700 23945
Satellite: ISS
Catalog Number: 25544
Epoch time: 13098
85895444 = yrday
fracday
Element set: 911
Inclination: 51
6455 deg
RA of node: 92
4352 deg
Eccentricity:
0010057
Arg of perigee: 120
0678 deg
Mean anomaly: 240
1472 deg
Mean motion: 15
52007700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2394
Checksum: 296
Coasting Arc #13 (Orbit 2408)
---------------------------------------
Vector Time (GMT): 2013/099/19:45:23
578
Vector Time (MET): N/A
Weight (LBS) : 903996
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1015139
56 A = 6795032
36 meter
Y = 6667566
03 meter E =
0014915
Z = -826980
21 I = 52
01764
XDOT = -4586
410242 Wp = 80
52759
YDOT = 1426
597732 meter/sec RA = 86
83699 deg
ZDOT = 5965
929707 TA = 270
58985
MA = 270
76075
Ha = 227
665 n
mi
Hp = 214
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3330510
38 X = 944523
26
Y = 21875216
64 feet Y = 6678523
03 meter
Z = -2713189
68 Z = -822220
98
XDOT = -15047
277697 XDOT = -4631
003090
YDOT = 4680
438752 feet/sec YDOT = 1375
060946 meter/sec
ZDOT = 19573
260192 ZDOT = 5943
540615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13487271
89 X = 4110920
47
Y = -17544625
97 feet Y = -5347602
00 meter
Z = -2694141
28 Z = -821174
26
XDOT = 12591
242449 XDOT = 3837
810699
YDOT = 6735
732238 feet/sec YDOT = 2053
051186 meter/sec
ZDOT = 19479
705266 ZDOT = 5937
414165
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 13099
82478037
00016717 00000-0 10270-3 0 9121
2 25544 51
6454 87
6349 0009836 123
4980 236
7112 15
52067695 24090
Satellite: ISS
Catalog Number: 25544
Epoch time: 13099
82478037 = yrday
fracday
Element set: 912
Inclination: 51
6454 deg
RA of node: 87
6349 deg
Eccentricity:
0009836
Arg of perigee: 123
4980 deg
Mean anomaly: 236
7112 deg
Mean motion: 15
52067695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2409
Checksum: 335
Coasting Arc #14 (Orbit 2424)
---------------------------------------
Vector Time (GMT): 2013/100/19:45:23
578
Vector Time (MET): N/A
Weight (LBS) : 903996
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -768687
67 A = 6795390
49 meter
Y = -6738017
76 meter E =
0021459
Z = -241074
79 I = 52
01587
XDOT = 4715
523222 Wp = 132
54524
YDOT = -334
572485 meter/sec RA = 81
90114 deg
ZDOT = -6039
175244 TA = 50
03809
MA = 49
84981
Ha = 227
694 n
mi
Hp = 214
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2521941
17 X = -692113
49
Y = -22106357
48 feet Y = -6746185
58 meter
Z = -790927
79 Z = -244622
39
XDOT = 15470
876714 XDOT = 4748
251105
YDOT = -1097
678757 feet/sec YDOT = -281
658145 meter/sec
ZDOT = -19813
567073 ZDOT = -6016
187810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13932160
00 X = -4246522
37
Y = 17347156
83 feet Y = 5287413
40 meter
Z = -804899
17 Z = -245333
27
XDOT = -10490
485524 XDOT = -3197
499988
YDOT = -9287
153122 feet/sec YDOT = -2830
724271 meter/sec
ZDOT = -19717
647039 ZDOT = -6009
938818
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 13100
85498211
00016717 00000-0 10270-3 0 9134
2 25544 51
6454 82
5149 0009919 128
1814 232
0233 15
52038148 24254
Satellite: ISS
Catalog Number: 25544
Epoch time: 13100
85498211 = yrday
fracday
Element set: 913
Inclination: 51
6454 deg
RA of node: 82
5149 deg
Eccentricity:
0009919
Arg of perigee: 128
1814 deg
Mean anomaly: 232
0233 deg
Mean motion: 15
52038148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2425
Checksum: 292
Coasting Arc #15 (Orbit 2440)
---------------------------------------
Vector Time (GMT): 2013/101/19:45:23
578
Vector Time (MET): N/A
Weight (LBS) : 903996
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 548317
19 A = 6794510
53 meter
Y = 6654689
87 meter E =
0019044
Z = 1237975
93 I = 52
00816
XDOT = -4871
865187 Wp = 87
89039
YDOT = -705
486425 meter/sec RA = 76
96346 deg
ZDOT = 5873
022673 TA = 285
48387
MA = 285
69409
Ha = 227
448 n
mi
Hp = 214
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1798940
90 X = 467848
42
Y = 21832972
01 feet Y = 6660371
67 meter
Z = 4061600
83 Z = 1240443
64
XDOT = -15983
809669 XDOT = -4892
144195
YDOT = -2314
588009 feet/sec YDOT = -760
079592 meter/sec
ZDOT = 19268
447089 ZDOT = 5849
306028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13973069
71 X = 4258991
65
Y = -16869831
82 feet Y = -5141924
74 meter
Z = 4071062
94 Z = 1240859
99
XDOT = 8683
276897 XDOT = 2646
662798
YDOT = 11879
209261 feet/sec YDOT = 3620
782983 meter/sec
ZDOT = 19169
614102 ZDOT = 5842
898378
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 13101
88516524
00016717 00000-0 10270-3 0 9147
2 25544 51
6451 77
3943 0009761 131
7748 228
4239 15
52125032 24418
Satellite: ISS
Catalog Number: 25544
Epoch time: 13101
88516524 = yrday
fracday
Element set: 914
Inclination: 51
6451 deg
RA of node: 77
3943 deg
Eccentricity:
0009761
Arg of perigee: 131
7748 deg
Mean anomaly: 228
4239 deg
Mean motion: 15
52125032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2441
Checksum: 299
Coasting Arc #16 (Orbit 2455)
---------------------------------------
Vector Time (GMT): 2013/102/19:45:23
578
Vector Time (MET): N/A
Weight (LBS) : 903996
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -216561
33 A = 6793048
84 meter
Y = -6397407
75 meter E =
0015694
Z = -2262907
34 I = 51
99493
XDOT = 5067
630801 Wp = 135
57835
YDOT = 1753
506090 meter/sec RA = 72
02465 deg
ZDOT = -5476
039698 TA = 69
44577
MA = 69
27745
Ha = 227
424 n
mi
Hp = 214
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -710503
06 X = -134015
29
Y = -20988870
57 feet Y = -6399368
08 meter
Z = -7424236
68 Z = -2263758
48
XDOT = 16626
085304 XDOT = 5074
247613
YDOT = 5752
972736 feet/sec YDOT = 1810
212175 meter/sec
ZDOT = -17966
009507 ZDOT = -5451
405264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13909457
86 X = -4239602
76
Y = 15732890
30 feet Y = 4795384
96 meter
Z = -7426973
63 Z = -2263741
56
XDOT = -7090
311781 XDOT = -2161
127031
YDOT = -14649
017310 feet/sec YDOT = -4465
020476 meter/sec
ZDOT = -17863
482232 ZDOT = -5444
789384
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 13102
85095077
00016717 00000-0 10270-3 0 9151
2 25544 51
6447 72
5943 0009740 135
5645 224
6289 15
52103523 24565
Satellite: ISS
Catalog Number: 25544
Epoch time: 13102
85095077 = yrday
fracday
Element set: 915
Inclination: 51
6447 deg
RA of node: 72
5943 deg
Eccentricity:
0009740
Arg of perigee: 135
5645 deg
Mean anomaly: 224
6289 deg
Mean motion: 15
52103523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2456
Checksum: 310
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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