[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 14th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16953 16 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 1786)
---------------------------------------
Vector Time (GMT): 2013/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3897425
49 A = 6791252
84 meter
Y = -2719002
67 meter E =
0007925
Z = 4846516
65 I = 51
99112
XDOT = 1719
016381 Wp = 67
60116
YDOT = -7021
166809 meter/sec RA = 87
75102 deg
ZDOT = -2550
386705 TA = 47
41080
MA = 47
34397
Ha = 227
854 n
mi
Hp = 220
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12786829
03 X = -3890274
88
Y = -8920612
43 feet Y = -2762546
01 meter
Z = 15900645
17 Z = 4827600
38
XDOT = 5639
817523 XDOT = 1809
790201
YDOT = -23035
324175 feet/sec YDOT = -7001
436218 meter/sec
ZDOT = -8367
410448 ZDOT = -2541
814967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14966025
22 X = 4561644
49
Y = -4648572
07 feet Y = -1416884
77 meter
Z = 15821495
07 Z = 4822391
70
XDOT = 14291
878465 XDOT = 4356
164556
YDOT = 17589
971604 feet/sec YDOT = 5361
423345 meter/sec
ZDOT = -8330
298123 ZDOT = -2539
074868
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 13317
54390251
00016717 00000-0 10270-3 0 9001
2 25544 51
6474 88
3639 0001143 118
1986 241
9280 15
50094742 17875
Satellite: ISS
Catalog Number: 25544
Epoch time: 13317
54390251 = yrday
fracday
Element set: 900
Inclination: 51
6474 deg
RA of node: 88
3639 deg
Eccentricity:
0001143
Arg of perigee: 118
1986 deg
Mean anomaly: 241
9280 deg
Mean motion: 15
50094742 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1787
Checksum: 310
Coasting Arc #2 (Orbit 1801)
---------------------------------------
Vector Time (GMT): 2013/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4043412
93 A = 6791783
64 meter
Y = 2821814
04 meter E =
0011368
Z = -4681907
17 I = 51
99211
XDOT = -1437
305008 Wp = 110
49192
YDOT = 6920
689134 meter/sec RA = 82
81876 deg
ZDOT = 2931
738281 TA = 188
59209
MA = 188
61157
Ha = 227
578 n
mi
Hp = 220
729
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13265790
45 X = 4034302
24
Y = 9257920
07 feet Y = 2866979
00 meter
Z = -15360587
82 Z = -4662286
37
XDOT = -4715
567611 XDOT = -1528
828787
YDOT = 22705
673011 feet/sec YDOT = 6904
104609 meter/sec
ZDOT = 9618
563914 ZDOT = 2924
533331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15439697
33 X = -4706019
75
Y = 5081462
60 feet Y = 1548829
80 meter
Z = -15278495
43 Z = -4656885
41
XDOT = -14868
940268 XDOT = -4532
052994
YDOT = -16371
107574 feet/sec YDOT = -4989
913589 meter/sec
ZDOT = 9587
199785 ZDOT = 2922
178495
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 13318
51091492
00016717 00000-0 10270-3 0 9015
2 25544 51
6482 83
5731 0000958 119
6458 240
4788 15
50152048 18026
Satellite: ISS
Catalog Number: 25544
Epoch time: 13318
51091492 = yrday
fracday
Element set: 901
Inclination: 51
6482 deg
RA of node: 83
5731 deg
Eccentricity:
0000958
Arg of perigee: 119
6458 deg
Mean anomaly: 240
4788 deg
Mean motion: 15
50152048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1802
Checksum: 305
Coasting Arc #3 (Orbit 1817)
---------------------------------------
Vector Time (GMT): 2013/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4195634
66 A = 6792606
01 meter
Y = -2924605
76 meter E =
0009979
Z = 4463482
40 I = 51
99070
XDOT = 1196
649790 Wp = 74
18871
YDOT = -6802
842451 meter/sec RA = 77
88548 deg
ZDOT = -3323
776567 TA = 49
24402
MA = 49
15744
Ha = 227
739 n
mi
Hp = 220
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13765205
57 X = -4184302
18
Y = -9595163
27 feet Y = -2971460
61 meter
Z = 14643971
14 Z = 4443127
43
XDOT = 3926
016373 XDOT = 1288
778160
YDOT = -22319
036912 feet/sec YDOT = -6788
945666 meter/sec
ZDOT = -10904
778764 ZDOT = -3317
739351
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15914099
24 X = 4850617
45
Y = -5547644
27 feet Y = -1690921
97 meter
Z = 14558812
52 Z = 4437526
06
XDOT = 15281
565613 XDOT = 4657
821199
YDOT = 15212
529984 feet/sec YDOT = 4636
779139 meter/sec
ZDOT = -10878
327576 ZDOT = -3315
714245
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 13319
54238193
00016717 00000-0 10270-3 0 9021
2 25544 51
6488 78
4618 0001075 118
5681 241
5578 15
50147753 18189
Satellite: ISS
Catalog Number: 25544
Epoch time: 13319
54238193 = yrday
fracday
Element set: 902
Inclination: 51
6488 deg
RA of node: 78
4618 deg
Eccentricity:
0001075
Arg of perigee: 118
5681 deg
Mean anomaly: 241
5578 deg
Mean motion: 15
50147753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1818
Checksum: 324
Coasting Arc #4 (Orbit 1832)
---------------------------------------
Vector Time (GMT): 2013/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4387098
11 A = 6793307
23 meter
Y = 2998167
29 meter E =
0008773
Z = -4241553
86 I = 51
98687
XDOT = -976
962100 Wp = 110
47580
YDOT = 6637
022829 meter/sec RA = 72
95317 deg
ZDOT = 3684
112904 TA = 197
16844
MA = 197
19814
Ha = 227
487 n
mi
Hp = 220
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14393366
51 X = 4373850
74
Y = 9836506
84 feet Y = 3047152
57 meter
Z = -13915859
13 Z = -4220273
34
XDOT = -3205
256232 XDOT = -1069
003035
YDOT = 21775
009282 feet/sec YDOT = 6625
583161 meter/sec
ZDOT = 12086
984593 ZDOT = 3679
143265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16372384
58 X = -4990302
82
Y = 6192005
96 feet Y = 1887323
42 meter
Z = -13826824
91 Z = -4214416
23
XDOT = -15479
034730 XDOT = -4718
009786
YDOT = -14010
449704 feet/sec YDOT = -4270
385070 meter/sec
ZDOT = 12065
032810 ZDOT = 3677
422000
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 13320
50936555
00016717 00000-0 10270-3 0 9037
2 25544 51
6496 73
6708 0000852 118
0172 242
1065 15
50194452 18330
Satellite: ISS
Catalog Number: 25544
Epoch time: 13320
50936555 = yrday
fracday
Element set: 903
Inclination: 51
6496 deg
RA of node: 73
6708 deg
Eccentricity:
0000852
Arg of perigee: 118
0172 deg
Mean anomaly: 242
1065 deg
Mean motion: 15
50194452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1833
Checksum: 291
Coasting Arc #5 (Orbit 1848)
---------------------------------------
Vector Time (GMT): 2013/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4579458
90 A = 6794232
71 meter
Y = -3068362
12 meter E =
0011913
Z = 3962741
48 I = 51
98060
XDOT = 809
943318 Wp = 83
04056
YDOT = -6456
620105 meter/sec RA = 68
02039 deg
ZDOT = -4051
560889 TA = 49
14877
MA = 49
04557
Ha = 227
630 n
mi
Hp = 220
533
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15024471
46 X = -4564057
85
Y = -10066804
85 feet Y = -3119486
53 meter
Z = 13001120
33 Z = 3940531
65
XDOT = 2657
294352 XDOT = 901
764356
YDOT = -21183
136829 feet/sec YDOT = -6447
049303 meter/sec
ZDOT = -13292
522601 ZDOT = -4047
403283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16804914
55 X = 5122137
95
Y = -6861327
43 feet Y = -2091332
60 meter
Z = 12908193
73 Z = 3934417
45
XDOT = 15502
533309 XDOT = 4725
172153
YDOT = 12923
304213 feet/sec YDOT = 3939
023124 meter/sec
ZDOT = -13273
998960 ZDOT = -4045
914883
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 13321
54080161
00016717 00000-0 10270-3 0 9046
2 25544 51
6501 68
5600 0001019 116
6870 243
4385 15
50200932 18493
Satellite: ISS
Catalog Number: 25544
Epoch time: 13321
54080161 = yrday
fracday
Element set: 904
Inclination: 51
6501 deg
RA of node: 68
5600 deg
Eccentricity:
0001019
Arg of perigee: 116
6870 deg
Mean anomaly: 243
4385 deg
Mean motion: 15
50200932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1849
Checksum: 273
Coasting Arc #6 (Orbit 1863)
---------------------------------------
Vector Time (GMT): 2013/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4802421
43 A = 6795040
40 meter
Y = 3096492
46 meter E =
0006256
Z = -3683468
22 I = 51
97185
XDOT = -671
150593 Wp = 100
79132
YDOT = 6243
307916 meter/sec RA = 63
08757 deg
ZDOT = 4378
546909 TA = 215
75035
MA = 215
79224
Ha = 227
412 n
mi
Hp = 220
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15755975
83 X = 4785332
55
Y = 10159095
99 feet Y = 3150100
79 meter
Z = -12084869
48 Z = -3660179
33
XDOT = -2201
937641 XDOT = -762
185047
YDOT = 20483
293689 feet/sec YDOT = 6235
293506 meter/sec
ZDOT = 14365
311380 ZDOT = 4375
065570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17158386
49 X = -5229876
20
Y = 7706736
00 feet Y = 2349013
13 meter
Z = -11987412
95 Z = -3653763
47
XDOT = -15341
058390 XDOT = -4675
954597
YDOT = -11862
018495 feet/sec YDOT = -3615
543237 meter/sec
ZDOT = 14349
652200 ZDOT = 4373
773991
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 13322
50775663
00016717 00000-0 10270-3 0 9052
2 25544 51
6507 63
7689 0000776 114
1728 245
9504 15
50235600 18644
Satellite: ISS
Catalog Number: 25544
Epoch time: 13322
50775663 = yrday
fracday
Element set: 905
Inclination: 51
6507 deg
RA of node: 63
7689 deg
Eccentricity:
0000776
Arg of perigee: 114
1728 deg
Mean anomaly: 245
9504 deg
Mean motion: 15
50235600 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1864
Checksum: 310
Coasting Arc #7 (Orbit 1879)
---------------------------------------
Vector Time (GMT): 2013/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5018329
81 A = 6795978
06 meter
Y = -3119261
47 meter E =
0013502
Z = 3344969
67 I = 51
96026
XDOT = 595
004877 Wp = 93
00756
YDOT = -6021
070192 meter/sec RA = 58
15442 deg
ZDOT = -4706
458356 TA = 48
27279
MA = 48
15739
Ha = 227
518 n
mi
Hp = 220
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16464336
66 X = -4999325
85
Y = -10233797
46 feet Y = -3175273
53 meter
Z = 10974309
94 Z = 3320636
59
XDOT = 1952
115738 XDOT = 685
152754
YDOT = -19754
167298 feet/sec YDOT = -6013
912187 meter/sec
ZDOT = -15441
136339 ZDOT = -4703
349151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17459771
48 X = 5321738
35
Y = -8554898
31 feet Y = -2607533
00 meter
Z = 10872468
24 Z = 3313928
32
XDOT = 15014
447290 XDOT = 4576
403534
YDOT = 10970
847981 feet/sec YDOT = 3343
914465 meter/sec
ZDOT = -15427
066395 ZDOT = -4702
169837
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 13323
53916198
00016717 00000-0 10270-3 0 9067
2 25544 51
6506 58
6582 0000969 113
1510 246
9743 15
50254645 18804
Satellite: ISS
Catalog Number: 25544
Epoch time: 13323
53916198 = yrday
fracday
Element set: 906
Inclination: 51
6506 deg
RA of node: 58
6582 deg
Eccentricity:
0000969
Arg of perigee: 113
1510 deg
Mean anomaly: 246
9743 deg
Mean motion: 15
50254645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1880
Checksum: 315
Coasting Arc #8 (Orbit 1894)
---------------------------------------
Vector Time (GMT): 2013/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5252940
01 A = 6796812
32 meter
Y = 3090876
10 meter E =
0005120
Z = -3010628
77 I = 51
94652
XDOT = -550
068613 Wp = 73
17217
YDOT = 5784
060035 meter/sec RA = 53
22042 deg
ZDOT = 4986
921279 TA = 252
60364
MA = 252
65963
Ha = 227
352 n
mi
Hp = 220
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17234055
14 X = 5232611
80
Y = 10140669
62 feet Y = 3149504
32 meter
Z = -9877390
98 Z = -2985159
23
XDOT = -1804
687051 XDOT = -638
931894
YDOT = 18976
574917 feet/sec YDOT = 5777
411684 meter/sec
ZDOT = 16361
290285 ZDOT = 4984
033515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17625087
62 X = -5372126
71
Y = 9554951
21 feet Y = 2912349
13 meter
Z = -9770766
76 Z = -2978129
71
XDOT = -14557
749090 XDOT = -4437
201923
YDOT = -10164
479067 feet/sec YDOT = -3098
133220 meter/sec
ZDOT = 16348
180863 ZDOT = 4982
925527
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 13324
50608868
00016717 00000-0 10270-3 0 9078
2 25544 51
6509 53
8667 0000727 108
3664 251
7566 15
50274230 18951
Satellite: ISS
Catalog Number: 25544
Epoch time: 13324
50608868 = yrday
fracday
Element set: 907
Inclination: 51
6509 deg
RA of node: 53
8667 deg
Eccentricity:
0000727
Arg of perigee: 108
3664 deg
Mean anomaly: 251
7566 deg
Mean motion: 15
50274230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1895
Checksum: 323
Coasting Arc #9 (Orbit 1910)
---------------------------------------
Vector Time (GMT): 2013/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5470398
61 A = 6797641
19 meter
Y = -3057403
23 meter E =
0014517
Z = 2616082
08 I = 51
92984
XDOT = 574
527469 Wp = 103
41575
YDOT = -5546
361689 meter/sec RA = 48
28588 deg
ZDOT = -5259
430081 TA = 47
28744
MA = 47
16530
Ha = 227
396 n
mi
Hp = 220
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17947501
99 X = -5448511
87
Y = -10030850
50 feet Y = -3118454
47 meter
Z = 8582946
45 Z = 2589560
00
XDOT = 1884
932640 XDOT = 662
054658
YDOT = -18196
724701 feet/sec YDOT = -5539
447293 meter/sec
ZDOT = -17255
348035 ZDOT = -5256
426723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17717759
64 X = 5400373
14
Y = -10521682
83 feet Y = -3207008
93 meter
Z = 8471891
35 Z = 2582232
48
XDOT = 13964
667729 XDOT = 4256
430724
YDOT = 9575
943490 feet/sec YDOT = 2918
747576 meter/sec
ZDOT = -17241
784080 ZDOT = -5255
295787
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 13325
53746370
00016717 00000-0 10270-3 0 9084
2 25544 51
6503 48
7557 0000913 107
7547 252
3703 15
50309606 19111
Satellite: ISS
Catalog Number: 25544
Epoch time: 13325
53746370 = yrday
fracday
Element set: 908
Inclination: 51
6503 deg
RA of node: 48
7557 deg
Eccentricity:
0000913
Arg of perigee: 107
7547 deg
Mean anomaly: 252
3703 deg
Mean motion: 15
50309606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1911
Checksum: 299
Coasting Arc #10 (Orbit 1925)
---------------------------------------
Vector Time (GMT): 2013/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5692748
21 A = 6798413
50 meter
Y = 2968510
88 meter E =
0006563
Z = -2231711
27 I = 51
91124
XDOT = -628
178992 Wp = 47
67097
YDOT = 5313
385103 meter/sec RA = 43
34997 deg
ZDOT = 5479
796062 TA = 287
67308
MA = 287
74473
Ha = 227
306 n
mi
Hp = 220
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18676995
44 X = 5669971
74
Y = 9739208
94 feet Y = 3032043
57 meter
Z = -7321887
36 Z = -2204111
27
XDOT = -2060
954699 XDOT = -714
167434
YDOT = 17432
365822 feet/sec YDOT = 5305
879373 meter/sec
ZDOT = 17978
333537 ZDOT = 5476
535760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17631492
54 X = -5374078
93
Y = 11597081
81 feet Y = 3534790
54 meter
Z = -7206285
33 Z = -2196475
77
XDOT = -13315
704474 XDOT = -4058
626724
YDOT = -9112
150970 feet/sec YDOT = -2777
383616 meter/sec
ZDOT = 17963
721864 ZDOT = 5475
342424
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 13326
50436262
00016717 00000-0 10270-3 0 9099
2 25544 51
6503 43
9638 0000716 100
2213 259
9018 15
50309345 19265
Satellite: ISS
Catalog Number: 25544
Epoch time: 13326
50436262 = yrday
fracday
Element set: 909
Inclination: 51
6503 deg
RA of node: 43
9638 deg
Eccentricity:
0000716
Arg of perigee: 100
2213 deg
Mean anomaly: 259
9018 deg
Mean motion: 15
50309345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1926
Checksum: 288
Coasting Arc #11 (Orbit 1941)
---------------------------------------
Vector Time (GMT): 2013/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5886656
32 A = 6799000
48 meter
Y = -2878003
70 meter E =
0014771
Z = 1788026
48 I = 51
89023
XDOT = 753
288591 Wp = 113
76941
YDOT = -5089
636159 meter/sec RA = 38
41319 deg
ZDOT = -5680
984609 TA = 46
68411
MA = 46
56106
Ha = 227
279 n
mi
Hp = 220
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19313176
90 X = -5862722
17
Y = -9442269
34 feet Y = -2943698
27 meter
Z = 5866228
61 Z = 1759487
36
XDOT = 2471
419262 XDOT = 837
743021
YDOT = -16698
281361 feet/sec YDOT = -5080
739999 meter/sec
ZDOT = -18638
400949 ZDOT = -5677
120199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17464124
36 X = 5323065
11
Y = -12591588
67 feet Y = -3837916
23 meter
Z = 5746663
84 Z = 1751583
14
XDOT = 12577
136507 XDOT = 3833
511207
YDOT = 8897
752511 feet/sec YDOT = 2712
034965 meter/sec
ZDOT = -18621
281398 ZDOT = -5675
766570
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 13327
53570786
00016717 00000-0 10270-3 0 9105
2 25544 51
6498 38
8521 0000883 100
2541 259
8710 15
50364725 19420
Satellite: ISS
Catalog Number: 25544
Epoch time: 13327
53570786 = yrday
fracday
Element set: 910
Inclination: 51
6498 deg
RA of node: 38
8521 deg
Eccentricity:
0000883
Arg of perigee: 100
2541 deg
Mean anomaly: 259
8710 deg
Mean motion: 15
50364725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1942
Checksum: 309
Coasting Arc #12 (Orbit 1956)
---------------------------------------
Vector Time (GMT): 2013/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6071428
49 A = 6799613
29 meter
Y = 2733130
87 meter E =
0009290
Z = -1361776
04 I = 51
86717
XDOT = -900
473274 Wp = 41
25777
YDOT = 4889
416975 meter/sec RA = 33
47474 deg
ZDOT = 5827
933230 TA = 303
98382
MA = 304
07206
Ha = 227
281 n
mi
Hp = 220
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19919384
79 X = 6047029
97
Y = 8966964
78 feet Y = 2800889
06 meter
Z = -4467769
15 Z = -1332340
48
XDOT = -2954
308643 XDOT = -983
391707
YDOT = 16041
394276 feet/sec YDOT = 4878
883551 meter/sec
ZDOT = 19120
515847 ZDOT = 5823
357473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17095577
92 X = -5210732
15
Y = 13638790
30 feet Y = 4157103
28 meter
Z = -4344412
97 Z = -1324177
07
XDOT = -11867
398581 XDOT = -3617
183087
YDOT = -8822
725636 feet/sec YDOT = -2689
166774 meter/sec
ZDOT = 19100
434697 ZDOT = 5821
812496
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 13328
50257974
00016717 00000-0 10270-3 0 9115
2 25544 51
6496 34
0598 0000779 90
8767 269
2473 15
50342252 19576
Satellite: ISS
Catalog Number: 25544
Epoch time: 13328
50257974 = yrday
fracday
Element set: 911
Inclination: 51
6496 deg
RA of node: 34
0598 deg
Eccentricity:
0000779
Arg of perigee: 90
8767 deg
Mean anomaly: 269
2473 deg
Mean motion: 15
50342252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1957
Checksum: 335
Coasting Arc #13 (Orbit 1972)
---------------------------------------
Vector Time (GMT): 2013/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6216677
29 A = 6799846
96 meter
Y = -2593931
71 meter E =
0014146
Z = 879261
49 I = 51
84257
XDOT = 1115
466916 Wp = 123
51686
YDOT = -4708
548227 meter/sec RA = 28
53508 deg
ZDOT = -5942
869043 TA = 47
00889
MA = 46
89040
Ha = 227
191 n
mi
Hp = 220
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20395922
87 X = -6191480
59
Y = -8510274
64 feet Y = -2663309
68 meter
Z = 2884716
18 Z = 849122
27
XDOT = 3659
668361 XDOT = 1196
905213
YDOT = -15447
992870 feet/sec YDOT = -4695
618945 meter/sec
ZDOT = -19497
601847 ZDOT = -5937
252390
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16655117
54 X = 5076479
83
Y = -14551234
34 feet Y = -4435216
23 meter
Z = 2758381
85 Z = 840754
79
XDOT = 11127
132951 XDOT = 3391
550123
YDOT = 9004
732047 feet/sec YDOT = 2744
642328 meter/sec
ZDOT = -19473
170590 ZDOT = -5935
422396
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 13329
53389594
00016717 00000-0 10270-3 0 9124
2 25544 51
6498 28
9478 0000927 93
4840 266
6417 15
50415725 19736
Satellite: ISS
Catalog Number: 25544
Epoch time: 13329
53389594 = yrday
fracday
Element set: 912
Inclination: 51
6498 deg
RA of node: 28
9478 deg
Eccentricity:
0000927
Arg of perigee: 93
4840 deg
Mean anomaly: 266
6417 deg
Mean motion: 15
50415725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1973
Checksum: 344
Coasting Arc #14 (Orbit 1987)
---------------------------------------
Vector Time (GMT): 2013/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6340376
01 A = 6800189
79 meter
Y = 2406620
76 meter E =
0011987
Z = -422472
39 I = 51
81556
XDOT = -1340
999079 Wp = 45
05994
YDOT = 4567
206645 meter/sec RA = 23
59358 deg
ZDOT = 6004
140580 TA = 310
40320
MA = 310
50774
Ha = 227
271 n
mi
Hp = 220
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20801758
56 X = 6315045
69
Y = 7895737
41 feet Y = 2477381
26 meter
Z = -1386064
28 Z = -391732
53
XDOT = -4399
603278 XDOT = -1421
137800
YDOT = 14984
273771 feet/sec YDOT = 4551
762639 meter/sec
ZDOT = 19698
623951 ZDOT = 5997
431401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16015677
89 X = -4881578
62
Y = 15456214
51 feet Y = 4711054
18 meter
Z = -1257178
35 Z = -383187
96
XDOT = -10499
636532 XDOT = -3200
289215
YDOT = -9312
870883 feet/sec YDOT = -2838
563045 meter/sec
ZDOT = 19669
619423 ZDOT = 5995
300000
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 13330
50074138
00016717 00000-0 10270-3 0 9139
2 25544 51
6495 24
1554 0000936 84
8247 275
3011 15
50377740 19888
Satellite: ISS
Catalog Number: 25544
Epoch time: 13330
50074138 = yrday
fracday
Element set: 913
Inclination: 51
6495 deg
RA of node: 24
1554 deg
Eccentricity:
0000936
Arg of perigee: 84
8247 deg
Mean anomaly: 275
3011 deg
Mean motion: 15
50377740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1988
Checksum: 301
Coasting Arc #15 (Orbit 2003)
---------------------------------------
Vector Time (GMT): 2013/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6415345
08 A = 6800012
48 meter
Y = -2236063
38 meter E =
0012601
Z = -85182
38 I = 51
78784
XDOT = 1624
531039 Wp = 131
76780
YDOT = -4453
680936 meter/sec RA = 18
65039 deg
ZDOT = -6019
973345 TA = 49
14646
MA = 49
03730
Ha = 227
141 n
mi
Hp = 220
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21047720
09 X = -6389450
32
Y = -7336165
93 feet Y = -2307659
07 meter
Z = -279469
75 Z = -116285
14
XDOT = 5329
826243 XDOT = 1703
456208
YDOT = -14611
814095 feet/sec YDOT = -4435
073105 meter/sec
ZDOT = -19750
568718 ZDOT = -6011
889682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15334170
87 X = 4673855
28
Y = -16174026
64 feet Y = -4929843
32 meter
Z = -409903
33 Z = -124938
54
XDOT = 9904
014765 XDOT = 3018
743700
YDOT = 9856
403865 feet/sec YDOT = 3004
231898 meter/sec
ZDOT = -19715
800676 ZDOT = -6009
376046
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 13331
53202924
00016717 00000-0 10270-3 0 9140
2 25544 51
6502 19
0430 0001036 91
6553 268
4717 15
50458082 20046
Satellite: ISS
Catalog Number: 25544
Epoch time: 13331
53202924 = yrday
fracday
Element set: 914
Inclination: 51
6502 deg
RA of node: 19
0430 deg
Eccentricity:
0001036
Arg of perigee: 91
6553 deg
Mean anomaly: 268
4717 deg
Mean motion: 15
50458082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2004
Checksum: 270
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