[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 17th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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 3940)
---------------------------------------
Vector Time (GMT): 2013/198/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4454892
47 A = 6801408
45 meter
Y = 5048111
18 meter E =
0015874
Z = 893947
06 I = 51
43217
XDOT = -4137
762565 Wp = 143
06293
YDOT = -2597
862755 meter/sec RA = 317
50540 deg
ZDOT = -5907
735734 TA = 27
24565
MA = 27
16247
Ha = 228
065 n
mi
Hp = 221
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14615788
95 X = -4515352
99
Y = 16562044
55 feet Y = 4997955
62 meter
Z = 2932897
18 Z = 872159
22
XDOT = -13575
336498 XDOT = -4079
707030
YDOT = -8523
171768 feet/sec YDOT = -2643
808695 meter/sec
ZDOT = -19382
335084 ZDOT = -5927
695805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21157244
86 X = 6448728
23
Y = 6389398
97 feet Y = 1947488
80 meter
Z = 2840961
64 Z = 865925
11
XDOT = -1667
945276 XDOT = -508
389720
YDOT = 14241
770847 feet/sec YDOT = 4340
891754 meter/sec
ZDOT = -19465
423888 ZDOT = -5933
061201
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 13198
53394602
00016717 00000-0 10270-3 0 9001
2 25544 51
6505 317
9495 0005141 196
0011 164
0978 15
49875633 39414
Satellite: ISS
Catalog Number: 25544
Epoch time: 13198
53394602 = yrday
fracday
Element set: 900
Inclination: 51
6505 deg
RA of node: 317
9495 deg
Eccentricity:
0005141
Arg of perigee: 196
0011 deg
Mean anomaly: 164
0978 deg
Mean motion: 15
49875633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3941
Checksum: 319
Coasting Arc #2 (Orbit 3955)
---------------------------------------
Vector Time (GMT): 2013/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4213202
26 A = 6801513
52 meter
Y = -5302790
00 meter E =
0006475
Z = -602448
51 I = 51
41159
XDOT = 4080
655661 Wp = 56
74625
YDOT = 2572
184056 meter/sec RA = 312
53829 deg
ZDOT = 5947
353931 TA = 296
74514
MA = 296
81139
Ha = 227
898 n
mi
Hp = 221
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13822842
05 X = 4275112
59
Y = -17397604
97 feet Y = -5255329
08 meter
Z = -1976537
10 Z = -581831
41
XDOT = 13387
977890 XDOT = 4022
699103
YDOT = 8438
924067 feet/sec YDOT = 2617
491823 meter/sec
ZDOT = 19512
316046 ZDOT = 5967
036844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21671485
30 X = -6605468
72
Y = -4942770
74 feet Y = -1506556
52 meter
Z = -1889460
82 Z = -575907
66
XDOT = 1507
100473 XDOT = 459
364224
YDOT = -14032
553702 feet/sec YDOT = -4277
122368 meter/sec
ZDOT = 19594
251374 ZDOT = 5972
327819
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 13199
50111458
00016717 00000-0 10270-3 0 9016
2 25544 51
6513 313
1593 0004931 199
9186 160
1773 15
49896387 39566
Satellite: ISS
Catalog Number: 25544
Epoch time: 13199
50111458 = yrday
fracday
Element set: 901
Inclination: 51
6513 deg
RA of node: 313
1593 deg
Eccentricity:
0004931
Arg of perigee: 199
9186 deg
Mean anomaly: 160
1773 deg
Mean motion: 15
49896387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3956
Checksum: 336
Coasting Arc #3 (Orbit 3971)
---------------------------------------
Vector Time (GMT): 2013/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3963185
08 A = 6801567
78 meter
Y = 5509706
87 meter E =
0014877
Z = 273273
61 I = 51
39184
XDOT = -4029
796922 Wp = 150
35849
YDOT = -2595
669676 meter/sec RA = 307
57031 deg
ZDOT = -5981
932615 TA = 26
69037
MA = 26
61387
Ha = 227
724 n
mi
Hp = 221
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13002575
72 X = -4025828
74
Y = 18076466
12 feet Y = 5465037
74 meter
Z = 896566
98 Z = 253869
46
XDOT = -13221
118510 XDOT = -3971
413655
YDOT = -8515
976626 feet/sec YDOT = -2640
406229 meter/sec
ZDOT = -19625
763174 ZDOT = -6001
367398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21989423
21 X = 6702376
19
Y = 3525795
82 feet Y = 1074662
57 meter
Z = 814534
05 Z = 248269
98
XDOT = -1485
585725 XDOT = -452
806529
YDOT = 13923
931670 feet/sec YDOT = 4244
014373 meter/sec
ZDOT = -19706
661097 ZDOT = -6006
590302
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 13200
53274655
00016717 00000-0 10270-3 0 9022
2 25544 51
6512 308
0500 0004993 203
7744 156
3176 15
49920157 39723
Satellite: ISS
Catalog Number: 25544
Epoch time: 13200
53274655 = yrday
fracday
Element set: 902
Inclination: 51
6512 deg
RA of node: 308
0500 deg
Eccentricity:
0004993
Arg of perigee: 203
7744 deg
Mean anomaly: 156
3176 deg
Mean motion: 15
49920157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3972
Checksum: 299
Coasting Arc #4 (Orbit 3987)
---------------------------------------
Vector Time (GMT): 2013/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3687568
97 A = 6801528
38 meter
Y = -5711510
15 meter E =
0007806
Z = 36743
57 I = 51
37467
XDOT = 3996
175815 Wp = 56
86483
YDOT = 2624
503864 meter/sec RA = 302
60040 deg
ZDOT = 5983
121147 TA = 303
53154
MA = 303
60608
Ha = 227
565 n
mi
Hp = 221
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12098323
38 X = 3750983
76
Y = -18738550
35 feet Y = -5669918
85 meter
Z = 120549
78 Z = 54810
54
XDOT = 13110
813042 XDOT = 3937
466997
YDOT = 8610
576980 feet/sec YDOT = 2668
862596 meter/sec
ZDOT = 19629
662555 ZDOT = 6002
391725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22211345
69 X = -6770018
17
Y = -2033356
11 feet Y = -619766
94 meter
Z = 197017
09 Z = 60050
81
XDOT = 1462
034754 XDOT = 445
628193
YDOT = -13881
510516 feet/sec YDOT = -4231
084405 meter/sec
ZDOT = 19709
875665 ZDOT = 6007
570103
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 13201
56436324
00016717 00000-0 10270-3 0 9030
2 25544 51
6519 302
9403 0004763 208
2894 151
7998 15
49939891 39889
Satellite: ISS
Catalog Number: 25544
Epoch time: 13201
56436324 = yrday
fracday
Element set: 903
Inclination: 51
6519 deg
RA of node: 302
9403 deg
Eccentricity:
0004763
Arg of perigee: 208
2894 deg
Mean anomaly: 151
7998 deg
Mean motion: 15
49939891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3988
Checksum: 343
Coasting Arc #5 (Orbit 4002)
---------------------------------------
Vector Time (GMT): 2013/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3412142
29 A = 6801403
54 meter
Y = 5861752
33 meter E =
0013408
Z = -380930
71 I = 51
35819
XDOT = -3976
511000 Wp = 157
76560
YDOT = -2697
513288 meter/sec RA = 297
63025 deg
ZDOT = -5971
387401 TA = 26
35139
MA = 26
28325
Ha = 227
384 n
mi
Hp = 222
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11194692
55 X = -3475585
65
Y = 19231470
90 feet Y = 5823240
91 meter
Z = -1249772
67 Z = -397659
70
XDOT = -13046
295932 XDOT = -3917
044402
YDOT = -8850
109213 feet/sec YDOT = -2741
647931 meter/sec
ZDOT = -19591
166013 ZDOT = -5990
560486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22239817
32 X = 6778696
32
Y = 615572
49 feet Y = 187626
49 meter
Z = -1320659
84 Z = -402537
12
XDOT = -1539
615874 XDOT = -469
274918
YDOT = 13963
060138 feet/sec YDOT = 4255
940730 meter/sec
ZDOT = -19670
968451 ZDOT = -5995
711184
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 13202
53148992
00016717 00000-0 10270-3 0 9040
2 25544 51
6513 298
1507 0004840 211
6728 148
4132 15
49961321 40039
Satellite: ISS
Catalog Number: 25544
Epoch time: 13202
53148992 = yrday
fracday
Element set: 904
Inclination: 51
6513 deg
RA of node: 298
1507 deg
Eccentricity:
0004840
Arg of perigee: 211
6728 deg
Mean anomaly: 148
4132 deg
Mean motion: 15
49961321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4003
Checksum: 293
Coasting Arc #6 (Orbit 4018)
---------------------------------------
Vector Time (GMT): 2013/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3115516
60 A = 6801180
95 meter
Y = -6000366
98 meter E =
0008871
Z = 704538
59 I = 51
34472
XDOT = 3981
992538 Wp = 61
13736
YDOT = 2769
765765 meter/sec RA = 292
65804 deg
ZDOT = 5928
037328 TA = 306
48958
MA = 306
57128
Ha = 227
229 n
mi
Hp = 222
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10221511
17 X = 3178960
08
Y = -19686243
36 feet Y = -5965172
64 meter
Z = 2311478
31 Z = 719826
65
XDOT = 13064
279980 XDOT = 3921
928299
YDOT = 9087
158022 feet/sec YDOT = 2813
958489 meter/sec
ZDOT = 19448
941364 ZDOT = 5947
235456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22158785
13 X = -6753997
71
Y = 843568
12 feet Y = 257119
56 meter
Z = 2376349
04 Z = 724311
19
XDOT = 1574
521805 XDOT = 479
914246
YDOT = -14127
348543 feet/sec YDOT = -4306
015836 meter/sec
ZDOT = 19528
846979 ZDOT = 5952
392559
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 13203
56307747
00016717 00000-0 10270-3 0 9050
2 25544 51
6518 293
0409 0004633 216
5486 143
5349 15
49984211 40190
Satellite: ISS
Catalog Number: 25544
Epoch time: 13203
56307747 = yrday
fracday
Element set: 905
Inclination: 51
6518 deg
RA of node: 293
0409 deg
Eccentricity:
0004633
Arg of perigee: 216
5486 deg
Mean anomaly: 143
5349 deg
Mean motion: 15
49984211 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4019
Checksum: 314
Coasting Arc #7 (Orbit 4033)
---------------------------------------
Vector Time (GMT): 2013/204/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2828991
76 A = 6800860
17 meter
Y = 6085639
62 meter E =
0011420
Z = -1057806
59 I = 51
33163
XDOT = -4007
706500 Wp = 165
03085
YDOT = -2877
958768 meter/sec RA = 287
68564 deg
ZDOT = -5863
953874 TA = 26
47198
MA = 26
41369
Ha = 227
036 n
mi
Hp = 222
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9281469
04 X = -2891694
04
Y = 19966009
24 feet Y = 6053653
53 meter
Z = -3470494
07 Z = -1071701
10
XDOT = -13148
643373 XDOT = -3946
741859
YDOT = -9442
121943 feet/sec YDOT = -2922
434169 meter/sec
ZDOT = -19238
693812 ZDOT = -5883
274626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21900024
29 X = 6675127
40
Y = -2182392
80 feet Y = -665193
33 meter
Z = -3529535
26 Z = -1075802
35
XDOT = -1663
157853 XDOT = -506
930514
YDOT = 14424
196155 feet/sec YDOT = 4396
494988 meter/sec
ZDOT = -19319
105627 ZDOT = -5888
463395
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 13204
53017750
00016717 00000-0 10270-3 0 9061
2 25544 51
6505 288
2511 0004670 219
9165 140
1642 15
50002930 40345
Satellite: ISS
Catalog Number: 25544
Epoch time: 13204
53017750 = yrday
fracday
Element set: 906
Inclination: 51
6505 deg
RA of node: 288
2511 deg
Eccentricity:
0004670
Arg of perigee: 219
9165 deg
Mean anomaly: 140
1642 deg
Mean motion: 15
50002930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4034
Checksum: 270
Coasting Arc #8 (Orbit 4049)
---------------------------------------
Vector Time (GMT): 2013/205/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2527863
67 A = 6800443
64 meter
Y = -6154161
68 meter E =
0009545
Z = 1388821
21 I = 51
32221
XDOT = 4063
774997 Wp = 67
97709
YDOT = 2977
906716 meter/sec RA = 282
71116 deg
ZDOT = 5770
569484 TA = 307
19700
MA = 307
28408
Ha = 226
890 n
mi
Hp = 222
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8293515
99 X = 2589746
61
Y = -20190819
17 feet Y = -6125547
57 meter
Z = 4556500
04 Z = 1401251
07
XDOT = 13332
595134 XDOT = 4002
142146
YDOT = 9770
035159 feet/sec YDOT = 3023
005529 meter/sec
ZDOT = 18932
314581 ZDOT = 5790
160932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21530171
93 X = -6562396
41
Y = 3523962
80 feet Y = 1074103
86 meter
Z = 4609410
11 Z = 1404948
20
XDOT = 1667
312393 XDOT = 508
196817
YDOT = -14804
626491 feet/sec YDOT = -4512
450154 meter/sec
ZDOT = 19013
852835 ZDOT = 5795
422344
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 13205
56173651
00016717 00000-0 10270-3 0 9079
2 25544 51
6507 283
1409 0004514 224
9361 135
1425 15
50027925 40500
Satellite: ISS
Catalog Number: 25544
Epoch time: 13205
56173651 = yrday
fracday
Element set: 907
Inclination: 51
6507 deg
RA of node: 283
1409 deg
Eccentricity:
0004514
Arg of perigee: 224
9361 deg
Mean anomaly: 135
1425 deg
Mean motion: 15
50027925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4050
Checksum: 283
Coasting Arc #9 (Orbit 4064)
---------------------------------------
Vector Time (GMT): 2013/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2247577
89 A = 6799911
15 meter
Y = 6170303
96 meter E =
0008929
Z = -1743965
89 I = 51
31348
XDOT = -4143
788998 Wp = 171
53079
YDOT = -3102
608707 meter/sec RA = 277
73634 deg
ZDOT = -5649
260340 TA = 27
66657
MA = 27
61909
Ha = 226
688 n
mi
Hp = 222
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7373943
20 X = -2307936
98
Y = 20243779
41 feet Y = 6144832
69 meter
Z = -5721672
87 Z = -1755030
63
XDOT = -13595
108260 XDOT = -4081
344943
YDOT = -10179
162424 feet/sec YDOT = -3148
597866 meter/sec
ZDOT = -18534
318700 ZDOT = -5669
238517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21012391
13 X = 6404576
82
Y = -4703493
18 feet Y = -1433624
72 meter
Z = -5768860
73 Z = -1758348
75
XDOT = -1673
772645 XDOT = -510
165902
YDOT = 15307
654409 feet/sec YDOT = 4665
773064 meter/sec
ZDOT = -18617
464460 ZDOT = -5674
603168
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 13206
52881054
00016717 00000-0 10270-3 0 9080
2 25544 51
6493 278
3504 0004472 228
4742 131
6025 15
50047877 40652
Satellite: ISS
Catalog Number: 25544
Epoch time: 13206
52881054 = yrday
fracday
Element set: 908
Inclination: 51
6493 deg
RA of node: 278
3504 deg
Eccentricity:
0004472
Arg of perigee: 228
4742 deg
Mean anomaly: 131
6025 deg
Mean motion: 15
50047877 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4065
Checksum: 306
Coasting Arc #10 (Orbit 4080)
---------------------------------------
Vector Time (GMT): 2013/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1960926
23 A = 6799320
06 meter
Y = -6166607
32 meter E =
0009781
Z = 2074799
65 I = 51
30859
XDOT = 4256
337458 Wp = 76
64674
YDOT = 3211
074157 meter/sec RA = 272
75997 deg
ZDOT = 5501
302489 TA = 306
38120
MA = 306
47140
Ha = 226
562 n
mi
Hp = 222
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6433485
00 X = 2019658
18
Y = -20231651
31 feet Y = -6144350
65 meter
Z = 6807085
47 Z = 2084468
04
XDOT = 13964
361739 XDOT = 4193
390775
YDOT = 10535
020199 feet/sec YDOT = 3258
319152 meter/sec
ZDOT = 18048
892680 ZDOT = 5521
826236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20395020
70 X = -6216402
31
Y = 5847062
80 feet Y = 1782184
74 meter
Z = 6848419
10 Z = 2087398
14
XDOT = 1558
293792 XDOT = 474
967948
YDOT = -15879
926045 feet/sec YDOT = -4840
201458 meter/sec
ZDOT = 18134
312281 ZDOT = 5527
338383
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 13207
56034193
00016717 00000-0 10270-3 0 9090
2 25544 51
6494 273
2396 0004361 233
3344 126
7406 15
50068768 40814
Satellite: ISS
Catalog Number: 25544
Epoch time: 13207
56034193 = yrday
fracday
Element set: 909
Inclination: 51
6494 deg
RA of node: 273
2396 deg
Eccentricity:
0004361
Arg of perigee: 233
3344 deg
Mean anomaly: 126
7406 deg
Mean motion: 15
50068768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4081
Checksum: 308
Coasting Arc #11 (Orbit 4095)
---------------------------------------
Vector Time (GMT): 2013/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1705931
78 A = 6798576
01 meter
Y = 6114725
19 meter E =
0006037
Z = -2423441
48 I = 51
30534
XDOT = -4392
957620 Wp = 175
52796
YDOT = -3331
111815 meter/sec RA = 267
78325 deg
ZDOT = -5319
392395 TA = 31
66269
MA = 31
62638
Ha = 226
364 n
mi
Hp = 222
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5596889
05 X = -1762408
90
Y = 20061434
34 feet Y = 6095332
64 meter
Z = -7950923
48 Z = -2431865
70
XDOT = -14412
590616 XDOT = -4329
542058
YDOT = -10928
844538 feet/sec YDOT = -3379
881967 meter/sec
ZDOT = -17452
074788 ZDOT = -5340
578760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19673060
39 X = 5996348
81
Y = -6795694
74 feet Y = -2071327
76 meter
Z = -7987034
92 Z = -2434448
24
XDOT = -1396
966693 XDOT = -425
795448
YDOT = 16544
966851 feet/sec YDOT = 5042
905896 meter/sec
ZDOT = -17540
256232 ZDOT = -5346
270099
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 13208
52739051
00016717 00000-0 10270-3 0 9104
2 25544 51
6489 268
4483 0004264 237
1637 122
9104 15
50095312 40964
Satellite: ISS
Catalog Number: 25544
Epoch time: 13208
52739051 = yrday
fracday
Element set: 910
Inclination: 51
6489 deg
RA of node: 268
4483 deg
Eccentricity:
0004264
Arg of perigee: 237
1637 deg
Mean anomaly: 122
9104 deg
Mean motion: 15
50095312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4096
Checksum: 302
Coasting Arc #12 (Orbit 4111)
---------------------------------------
Vector Time (GMT): 2013/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1453699
81 A = 6797844
77 meter
Y = -6042444
89 meter E =
0009553
Z = 2745246
26 I = 51
30500
XDOT = 4561
151589 Wp = 86
77134
YDOT = 3427
358562 meter/sec RA = 262
80584 deg
ZDOT = 5113
594250 TA = 304
40693
MA = 304
49721
Ha = 226
270 n
mi
Hp = 222
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4769356
35 X = 1507824
17
Y = -19824294
27 feet Y = -6025886
15 meter
Z = 9006713
45 Z = 2752439
44
XDOT = 14964
408102 XDOT = 4497
646907
YDOT = 11244
614704 feet/sec YDOT = 3478
009033 meter/sec
ZDOT = 16776
884021 ZDOT = 5135
597546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18875784
36 X = -5753339
07
Y = 7674361
07 feet Y = 2339145
26 meter
Z = 9037656
64 Z = 2754677
74
XDOT = 1085
800109 XDOT = 330
951873
YDOT = -17251
930398 feet/sec YDOT = -5258
388385 meter/sec
ZDOT = 16868
476960 ZDOT = 5141
511777
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 13209
55889522
00016717 00000-0 10270-3 0 9118
2 25544 51
6488 263
3374 0004161 241
7323 118
3408 15
50107233 41126
Satellite: ISS
Catalog Number: 25544
Epoch time: 13209
55889522 = yrday
fracday
Element set: 911
Inclination: 51
6488 deg
RA of node: 263
3374 deg
Eccentricity:
0004161
Arg of perigee: 241
7323 deg
Mean anomaly: 118
3408 deg
Mean motion: 15
50107233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4112
Checksum: 288
Coasting Arc #13 (Orbit 4126)
---------------------------------------
Vector Time (GMT): 2013/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1243054
03 A = 6796922
99 meter
Y = 5929553
22 meter E =
0003009
Z = -3078056
83 I = 51
30759
XDOT = -4749
341177 Wp = 168
41666
YDOT = -3521
452900 meter/sec RA = 257
82820 deg
ZDOT = -4869
441464 TA = 47
05691
MA = 47
03167
Ha = 226
092 n
mi
Hp = 222
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4078261
26 X = -1294314
96
Y = 19453914
75 feet Y = 5915366
10 meter
Z = -10098611
64 Z = -3084219
70
XDOT = -15581
828009 XDOT = -4685
956308
YDOT = -11553
323164 feet/sec YDOT = -3574
208445 meter/sec
ZDOT = -15975
857820 ZDOT = -4892
359327
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18028167
28 X = 5494985
39
Y = -8338706
80 feet Y = -2541637
83 meter
Z = -10125222
21 Z = -3086167
73
XDOT = -691
813365 XDOT = -210
864714
YDOT = 18003
953810 feet/sec YDOT = 5487
605121 meter/sec
ZDOT = -16071
272426 ZDOT = -4898
523835
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 13210
52591865
00016717 00000-0 10270-3 0 9128
2 25544 51
6493 258
5458 0004083 245
8411 114
2313 15
50141885 41274
Satellite: ISS
Catalog Number: 25544
Epoch time: 13210
52591865 = yrday
fracday
Element set: 912
Inclination: 51
6493 deg
RA of node: 258
5458 deg
Eccentricity:
0004083
Arg of perigee: 245
8411 deg
Mean anomaly: 114
2313 deg
Mean motion: 15
50141885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4127
Checksum: 296
Coasting Arc #14 (Orbit 4142)
---------------------------------------
Vector Time (GMT): 2013/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1044309
41 A = 6796089
91 meter
Y = -5798447
34 meter E =
0008822
Z = 3381088
02 I = 51
31149
XDOT = 4965
050760 Wp = 98
21390
YDOT = 3585
598935 meter/sec RA = 252
85043 deg
ZDOT = 4604
045508 TA = 301
40412
MA = 301
49037
Ha = 226
035 n
mi
Hp = 222
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3426211
97 X = 1092647
02
Y = -19023777
36 feet Y = -5786499
11 meter
Z = 11092808
48 Z = 3386278
25
XDOT = 16289
536615 XDOT = 4902
221777
YDOT = 11763
776034 feet/sec YDOT = 3640
769742 meter/sec
ZDOT = 15105
136182 ZDOT = 4628
012657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17140191
32 X = -5224330
31
Y = 8908243
77 feet Y = 2715232
70 meter
Z = 11115325
80 Z = 3387951
30
XDOT = 134
184066 XDOT = 40
899303
YDOT = -18761
230550 feet/sec YDOT = -5718
423072 meter/sec
ZDOT = 15204
942316 ZDOT = 4634
466418
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 13211
55739718
00016717 00000-0 10270-3 0 9134
2 25544 51
6485 253
4349 0003953 250
2679 109
8045 15
50145778 41434
Satellite: ISS
Catalog Number: 25544
Epoch time: 13211
55739718 = yrday
fracday
Element set: 913
Inclination: 51
6485 deg
RA of node: 253
4349 deg
Eccentricity:
0003953
Arg of perigee: 250
2679 deg
Mean anomaly: 109
8045 deg
Mean motion: 15
50145778 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4143
Checksum: 322
Coasting Arc #15 (Orbit 4157)
---------------------------------------
Vector Time (GMT): 2013/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921602
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -895029
79 A = 6795062
73 meter
Y = 5637510
45 meter E =
0001736
Z = -3687968
11 I = 51
31946
XDOT = -5192
478800 Wp = 91
53509
YDOT = -3634
856287 meter/sec RA = 247
87274 deg
ZDOT = -4297
971045 TA = 132
50560
MA = 132
49093
Ha = 225
882 n
mi
Hp = 222
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2936449
43 X = -940088
15
Y = 18495769
18 feet Y = 5627249
95 meter
Z = -12099632
92 Z = -3692425
14
XDOT = -17035
691601 XDOT = -5130
568950
YDOT = -11925
381519 feet/sec YDOT = -3692
575449 meter/sec
ZDOT = -14100
954873 ZDOT = -4323
045248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16262413
72 X = 4956783
70
Y = -9261735
08 feet Y = -2822976
85 meter
Z = -12119054
95 Z = -3693887
95
XDOT = 525
605037 XDOT = 160
204415
YDOT = 19503
029643 feet/sec YDOT = 5944
523435 meter/sec
ZDOT = -14205
398742 ZDOT = -4329
805537
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 13212
52439545
00016717 00000-0 10270-3 0 9148
2 25544 51
6496 248
6435 0003960 254
4604 105
6110 15
50184559 41583
Satellite: ISS
Catalog Number: 25544
Epoch time: 13212
52439545 = yrday
fracday
Element set: 914
Inclination: 51
6496 deg
RA of node: 248
6435 deg
Eccentricity:
0003960
Arg of perigee: 254
4604 deg
Mean anomaly: 105
6110 deg
Mean motion: 15
50184559 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4158
Checksum: 305
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