[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 24th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 27986 17 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 132 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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 3620)
---------------------------------------
Vector Time (GMT): 2014/328/13:11:16
604
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1798964
71 A = 6788485
39 meter
Y = -4722037
77 meter E =
0016800
Z = -4550085
78 I = 51
78818
XDOT = 6960
062347 Wp = 65
82349
YDOT = 382
880813 meter/sec RA = 24
00011 deg
ZDOT = -3151
635110 TA = 172
56590
MA = 172
54096
Ha = 227
713 n
mi
Hp = 216
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5902115
21 X = -1723924
85
Y = -15492249
90 feet Y = -4741735
08 meter
Z = -14928102
95 Z = -4558643
09
XDOT = 22834
850219 XDOT = 6970
573484
YDOT = 1256
170646 feet/sec YDOT = 460
771723 meter/sec
ZDOT = -10340
010205 ZDOT = -3117
797970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16244954
08 X = 4951462
00
Y = -3143821
40 feet Y = -958236
76 meter
Z = -14963652
05 Z = -4560921
15
XDOT = -5284
169845 XDOT = -1610
614969
YDOT = 21185
421831 feet/sec YDOT = 6457
316574 meter/sec
ZDOT = -10195
785693 ZDOT = -3107
675479
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 14328
57122376
00016717 00000-0 10270-3 0 9008
2 25544 51
6463 24
4416 0006991 61
3984 298
7870 15
51409505 36212
Satellite: ISS
Catalog Number: 25544
Epoch time: 14328
57122376 = yrday
fracday
Element set: 900
Inclination: 51
6463 deg
RA of node: 24
4416 deg
Eccentricity:
0006991
Arg of perigee: 61
3984 deg
Mean anomaly: 298
7870 deg
Mean motion: 15
51409505 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3621
Checksum: 314
Coasting Arc #2 (Orbit 3636)
---------------------------------------
Vector Time (GMT): 2014/329/13:11:16
604
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1224280
69 A = 6786827
06 meter
Y = 4514447
17 meter E =
0012111
Z = 4907169
75 I = 51
75310
XDOT = -7286
154407 Wp = 91
52416
YDOT = -567
649017 meter/sec RA = 19
04002 deg
ZDOT = 2334
741960 TA = 335
64885
MA = 335
70603
Ha = 227
697 n
mi
Hp = 216
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4016668
92 X = 1149870
34
Y = 14811178
38 feet Y = 4527721
49 meter
Z = 16099638
30 Z = 4912936
77
XDOT = -23904
706061 XDOT = -7290
606865
YDOT = -1862
365540 feet/sec YDOT = -649
152567 meter/sec
ZDOT = 7659
914567 ZDOT = 2299
335547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15231811
47 X = -4642656
14
Y = 1653258
34 feet Y = 503913
14 meter
Z = 16123326
08 Z = 4914389
79
XDOT = 5547
169794 XDOT = 1690
777353
YDOT = -22293
208916 feet/sec YDOT = -6794
970078 meter/sec
ZDOT = 7509
034634 ZDOT = 2288
753756
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 14329
60184007
00016717 00000-0 10270-3 0 9013
2 25544 51
6451 19
3245 0007158 64
9126 295
2767 15
51470324 36376
Satellite: ISS
Catalog Number: 25544
Epoch time: 14329
60184007 = yrday
fracday
Element set: 901
Inclination: 51
6451 deg
RA of node: 19
3245 deg
Eccentricity:
0007158
Arg of perigee: 64
9126 deg
Mean anomaly: 295
2767 deg
Mean motion: 15
51470324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3637
Checksum: 303
Coasting Arc #3 (Orbit 3651)
---------------------------------------
Vector Time (GMT): 2014/330/13:11:16
604
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -571210
98 A = 6785661
62 meter
Y = -4361834
85 meter E =
0020882
Z = -5185150
32 I = 51
72061
XDOT = 7480
133572 Wp = 75
12019
YDOT = 715
612507 meter/sec RA = 14
07546 deg
ZDOT = -1425
599882 TA = 181
14165
MA = 181
14643
Ha = 227
669 n
mi
Hp = 216
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1874051
78 X = -497205
46
Y = -14310481
78 feet Y = -4367808
41 meter
Z = -17011648
02 Z = -5187745
70
XDOT = 24541
120643 XDOT = 7478
500649
YDOT = 2347
810061 feet/sec YDOT = 799
251161 meter/sec
ZDOT = -4677
164967 ZDOT = -1389
266054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14419890
57 X = 4395182
64
Y = 147903
09 feet Y = 45080
86 meter
Z = -17021839
14 Z = -5188256
57
XDOT = -5575
806658 XDOT = -1699
505869
YDOT = 22989
968539 feet/sec YDOT = 7007
342411 meter/sec
ZDOT = -4522
360604 ZDOT = -1378
415512
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 14330
56801380
00016717 00000-0 10270-3 0 9021
2 25544 51
6463 14
5270 0007113 67
9932 292
1974 15
51497911 36527
Satellite: ISS
Catalog Number: 25544
Epoch time: 14330
56801380 = yrday
fracday
Element set: 902
Inclination: 51
6463 deg
RA of node: 14
5270 deg
Eccentricity:
0007113
Arg of perigee: 67
9932 deg
Mean anomaly: 292
1974 deg
Mean motion: 15
51497911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3652
Checksum: 302
Coasting Arc #4 (Orbit 3667)
---------------------------------------
Vector Time (GMT): 2014/331/13:11:16
604
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -136597
23 A = 6784868
52 meter
Y = 4220911
40 meter E =
0009562
Z = 5302075
91 I = 51
68671
XDOT = -7611
109093 Wp = 80
63989
YDOT = -840
746365 meter/sec RA = 9
10703 deg
ZDOT = 474
014028 TA = 4
84841
MA = 4
83916
Ha = 227
677 n
mi
Hp = 216
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -448153
65 X = -209542
23
Y = 13848134
51 feet Y = 4218975
79 meter
Z = 17395262
17 Z = 5301235
34
XDOT = -24970
830359 XDOT = -7603
444616
YDOT = -2758
354215 feet/sec YDOT = -925
815887 meter/sec
ZDOT = 1555
164134 ZDOT = 437
058681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13692340
16 X = -4173425
28
Y = -2155391
67 feet Y = -656963
38 meter
Z = 17390828
75 Z = 5300724
60
XDOT = 5470
519027 XDOT = 1667
414199
YDOT = -23495
310002 feet/sec YDOT = -7161
370489 meter/sec
ZDOT = 1397
737204 ZDOT = 426
030300
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 14331
59856690
00016717 00000-0 10270-3 0 9030
2 25544 51
6450 9
4091 0007305 71
5848 288
6097 15
51566420 36682
Satellite: ISS
Catalog Number: 25544
Epoch time: 14331
59856690 = yrday
fracday
Element set: 903
Inclination: 51
6450 deg
RA of node: 9
4091 deg
Eccentricity:
0007305
Arg of perigee: 71
5848 deg
Mean anomaly: 288
6097 deg
Mean motion: 15
51566420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3668
Checksum: 326
Coasting Arc #5 (Orbit 3682)
---------------------------------------
Vector Time (GMT): 2014/332/13:11:16
604
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 874280
69 A = 6784872
40 meter
Y = -4150928
00 meter E =
0021620
Z = -5313893
74 I = 51
65675
XDOT = 7572
222719 Wp = 87
31378
YDOT = 949
567673 meter/sec RA = 4
13629 deg
ZDOT = 506
860144 TA = 187
51700
MA = 187
54946
Ha = 227
603 n
mi
Hp = 216
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2868374
97 X = 946445
69
Y = -13618530
19 feet Y = -4140747
59 meter
Z = -17434034
59 Z = -5309471
41
XDOT = 24843
250391 XDOT = 7558
579467
YDOT = 3115
379504 feet/sec YDOT = 1034
168880 meter/sec
ZDOT = 1662
926981 ZDOT = 543
612035
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13260474
15 X = 4041792
52
Y = 4305579
50 feet Y = 1312340
63 meter
Z = -17414342
14 Z = -5307891
48
XDOT = -5232
577476 XDOT = -1594
889615
YDOT = 23437
608573 feet/sec YDOT = 7143
783093 meter/sec
ZDOT = 1819
459341 ZDOT = 554
571207
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 14332
56468139
00016717 00000-0 10270-3 0 9046
2 25544 51
6460 4
6117 0007215 74
4589 285
7359 15
51587131 36831
Satellite: ISS
Catalog Number: 25544
Epoch time: 14332
56468139 = yrday
fracday
Element set: 904
Inclination: 51
6460 deg
RA of node: 4
6117 deg
Eccentricity:
0007215
Arg of perigee: 74
4589 deg
Mean anomaly: 285
7359 deg
Mean motion: 15
51587131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3683
Checksum: 321
Coasting Arc #6 (Orbit 3698)
---------------------------------------
Vector Time (GMT): 2014/333/13:11:16
604
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1637717
36 A = 6785327
31 meter
Y = 4098482
07 meter E =
0011928
Z = 5145119
75 I = 51
62645
XDOT = -7445
407737 Wp = 68
38985
YDOT = -1080
633700 meter/sec RA = 359
16250 deg
ZDOT = -1502
004019 TA = 36
11169
MA = 36
03119
Ha = 227
608 n
mi
Hp = 215
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5373088
45 X = -1708419
34
Y = 13446463
48 feet Y = 4079772
67 meter
Z = 16880314
13 Z = 5136992
21
XDOT = -24427
190739 XDOT = -7425
474171
YDOT = -3545
386154 feet/sec YDOT = -1163
781604 meter/sec
ZDOT = -4927
834708 ZDOT = -1538
124623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12957493
02 X = -3949443
87
Y = -6555714
78 feet Y = -1998181
87 meter
Z = 16844834
31 Z = 5134305
50
XDOT = 5041
224819 XDOT = 1536
565325
YDOT = -23081
266416 feet/sec YDOT = -7035
170004 meter/sec
ZDOT = -5081
641612 ZDOT = -1548
884363
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 14333
59517190
00016717 00000-0 10270-3 0 9053
2 25544 51
6448 359
4933 0007348 78
0935 282
1039 15
51662523 36998
Satellite: ISS
Catalog Number: 25544
Epoch time: 14333
59517190 = yrday
fracday
Element set: 905
Inclination: 51
6448 deg
RA of node: 359
4933 deg
Eccentricity:
0007348
Arg of perigee: 78
0935 deg
Mean anomaly: 282
1039 deg
Mean motion: 15
51662523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3699
Checksum: 335
Coasting Arc #7 (Orbit 3713)
---------------------------------------
Vector Time (GMT): 2014/334/13:11:16
604
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2370453
98 A = 6786562
88 meter
Y = -4116263
03 meter E =
0018443
Z = -4863874
92 I = 51
59971
XDOT = 7143
014586 Wp = 97
01835
YDOT = 1225
102284 meter/sec RA = 354
18882 deg
ZDOT = 2450
218232 TA = 197
07242
MA = 197
13455
Ha = 227
525 n
mi
Hp = 215
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7777079
99 X = 2439934
20
Y = -13504799
98 feet Y = -4089366
56 meter
Z = -15957594
89 Z = -4852190
74
XDOT = 23435
087225 XDOT = 7116
881823
YDOT = 4019
364448 feet/sec YDOT = 1304
833972 meter/sec
ZDOT = 8038
773728 ZDOT = 2484
854884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12972470
59 X = 3954009
03
Y = 8728769
97 feet Y = 2660529
09 meter
Z = -15906948
55 Z = -4848437
92
XDOT = -4876
974241 XDOT = -1486
501749
YDOT = 22131
463710 feet/sec YDOT = 6745
670139 meter/sec
ZDOT = 8186
215604 ZDOT = 2495
158516
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 14334
56122790
00016717 00000-0 10270-3 0 9060
2 25544 51
6451 354
6958 0007309 80
9581 279
2398 15
51677244 37141
Satellite: ISS
Catalog Number: 25544
Epoch time: 14334
56122790 = yrday
fracday
Element set: 906
Inclination: 51
6451 deg
RA of node: 354
6958 deg
Eccentricity:
0007309
Arg of perigee: 80
9581 deg
Mean anomaly: 279
2398 deg
Mean motion: 15
51677244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3714
Checksum: 335
Coasting Arc #8 (Orbit 3729)
---------------------------------------
Vector Time (GMT): 2014/335/13:11:16
604
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3091593
36 A = 6788115
72 meter
Y = 4137127
75 meter E =
0016712
Z = 4393334
78 I = 51
57350
XDOT = -6738
726683 Wp = 76
30616
YDOT = -1439
371796 meter/sec RA = 349
21327 deg
ZDOT = -3371
952376 TA = 47
89424
MA = 47
75228
Ha = 227
475 n
mi
Hp = 215
724
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10143022
83 X = -3158967
61
Y = 13573253
78 feet Y = 4102178
79 meter
Z = 14413828
02 Z = 4378152
45
XDOT = -22108
683344 XDOT = -6705
750365
YDOT = -4722
348413 feet/sec YDOT = -1514
544189 meter/sec
ZDOT = -11062
835879 ZDOT = -3404
608530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13078095
01 X = -3986203
36
Y = -10861090
55 feet Y = -3310460
40 meter
Z = 14348265
10 Z = 4373351
20
XDOT = 4962
889187 XDOT = 1512
688624
YDOT = -20838
119701 feet/sec YDOT = -6351
458885 meter/sec
ZDOT = -11201
781883 ZDOT = -3414
303118
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 14335
59165581
00016717 00000-0 10270-3 0 9070
2 25544 51
6440 349
5768 0007327 84
4443 275
7544 15
51761155 37304
Satellite: ISS
Catalog Number: 25544
Epoch time: 14335
59165581 = yrday
fracday
Element set: 907
Inclination: 51
6440 deg
RA of node: 349
5768 deg
Eccentricity:
0007327
Arg of perigee: 84
4443 deg
Mean anomaly: 275
7544 deg
Mean motion: 15
51761155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3730
Checksum: 328
Coasting Arc #9 (Orbit 3744)
---------------------------------------
Vector Time (GMT): 2014/336/13:11:16
604
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3722395
83 A = 6790081
14 meter
Y = -4207460
65 meter E =
0013330
Z = -3826317
50 I = 51
54936
XDOT = 6190
139777 Wp = 94
27432
YDOT = 1694
076212 meter/sec RA = 344
23943 deg
ZDOT = 4170
798306 TA = 219
76856
MA = 219
86635
Ha = 227
435 n
mi
Hp = 215
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12212584
75 X = 3787755
31
Y = -13804004
77 feet Y = -4165468
87 meter
Z = -12553535
11 Z = -3808075
67
XDOT = 20308
857537 XDOT = 6150
475423
YDOT = 5557
992822 feet/sec YDOT = 1763
076493 meter/sec
ZDOT = 13683
721475 ZDOT = 4200
773326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13432032
78 X = 4094083
59
Y = 12698266
50 feet Y = 3870431
63 meter
Z = -12474916
47 Z = -3802354
54
XDOT = -5234
507036 XDOT = -1595
477745
YDOT = 19067
592158 feet/sec YDOT = 5811
802090 meter/sec
ZDOT = 13811
177848 ZDOT = 4209
647008
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 14336
55765351
00016717 00000-0 10270-3 0 9089
2 25544 51
6438 344
7789 0007414 87
6208 272
5792 15
51773252 37459
Satellite: ISS
Catalog Number: 25544
Epoch time: 14336
55765351 = yrday
fracday
Element set: 908
Inclination: 51
6438 deg
RA of node: 344
7789 deg
Eccentricity:
0007414
Arg of perigee: 87
6208 deg
Mean anomaly: 272
5792 deg
Mean motion: 15
51773252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3745
Checksum: 342
Coasting Arc #10 (Orbit 3760)
---------------------------------------
Vector Time (GMT): 2014/337/13:11:16
604
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4303664
90 A = 6791999
67 meter
Y = 4244685
24 meter E =
0020357
Z = 3077933
58 I = 51
52596
XDOT = -5542
404214 Wp = 93
71555
YDOT = -2055
504221 meter/sec RA = 339
26470 deg
ZDOT = -4888
225022 TA = 50
86280
MA = 50
68204
Ha = 227
301 n
mi
Hp = 215
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14119635
50 X = -4365761
97
Y = 13926132
68 feet Y = 4196211
54 meter
Z = 10098207
29 Z = 3056875
96
XDOT = -18183
740860 XDOT = -5495
261316
YDOT = -6743
780251 feet/sec YDOT = -2117
219185 meter/sec
ZDOT = -16037
483668 ZDOT = -4915
035293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13746429
82 X = -4189911
81
Y = -14358241
82 feet Y = -4376392
11 meter
Z = 10007578
51 Z = 3050309
93
XDOT = 5926
538008 XDOT = 1806
408785
YDOT = -16992
889558 feet/sec YDOT = -5179
432737 meter/sec
ZDOT = -16151
369526 ZDOT = -4922
937432
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 14337
58801866
00016717 00000-0 10270-3 0 9096
2 25544 51
6432 339
6592 0007324 90
7758 269
4233 15
51859336 37614
Satellite: ISS
Catalog Number: 25544
Epoch time: 14337
58801866 = yrday
fracday
Element set: 909
Inclination: 51
6432 deg
RA of node: 339
6592 deg
Eccentricity:
0007324
Arg of perigee: 90
7758 deg
Mean anomaly: 269
4233 deg
Mean motion: 15
51859336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3761
Checksum: 344
Coasting Arc #11 (Orbit 3775)
---------------------------------------
Vector Time (GMT): 2014/338/13:11:16
604
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4750431
83 A = 6793724
46 meter
Y = -4293591
80 meter E =
0012210
Z = -2273091
15 I = 51
50269
XDOT = 4812
678805 Wp = 71
78807
YDOT = 2469
034194 meter/sec RA = 334
29193 deg
ZDOT = 5421
841193 TA = 262
90620
MA = 263
04506
Ha = 227
300 n
mi
Hp = 215
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15585406
26 X = 4809132
84
Y = -14086587
27 feet Y = -4240141
04 meter
Z = -7457648
13 Z = -2249871
50
XDOT = 15789
628626 XDOT = 4758
373789
YDOT = 8100
505885 feet/sec YDOT = 2522
548729 meter/sec
ZDOT = 17788
192890 ZDOT = 5445
089150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14158177
40 X = 4315412
47
Y = 15567987
35 feet Y = 4745122
55 meter
Z = -7357793
64 Z = -2242655
50
XDOT = -6895
554913 XDOT = -2101
765137
YDOT = 14681
224897 feet/sec YDOT = 4474
837348 meter/sec
ZDOT = 17886
805453 ZDOT = 5451
898302
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 14338
55395752
00016717 00000-0 10270-3 0 9108
2 25544 51
6428 334
8606 0007513 94
8822 265
3188 15
51885387 37764
Satellite: ISS
Catalog Number: 25544
Epoch time: 14338
55395752 = yrday
fracday
Element set: 910
Inclination: 51
6428 deg
RA of node: 334
8606 deg
Eccentricity:
0007513
Arg of perigee: 94
8822 deg
Mean anomaly: 265
3188 deg
Mean motion: 15
51885387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3776
Checksum: 346
Coasting Arc #12 (Orbit 3791)
---------------------------------------
Vector Time (GMT): 2014/339/13:11:16
604
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5118907
13 A = 6794982
81 meter
Y = 4256563
76 meter E =
0020728
Z = 1317428
80 I = 51
47987
XDOT = -4006
733869 Wp = 112
35307
YDOT = -3000
036944 meter/sec RA = 329
31823 deg
ZDOT = -5809
715147 TA = 53
28085
MA = 53
09063
Ha = 227
122 n
mi
Hp = 215
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16794314
72 X = -5172524
30
Y = 13965104
19 feet Y = 4199020
93 meter
Z = 4322272
96 Z = 1292431
59
XDOT = -13145
452326 XDOT = -3944
666819
YDOT = -9842
640894 feet/sec YDOT = -3044
495362 meter/sec
ZDOT = -19060
745234 ZDOT = -5829
029056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14327990
51 X = -4367171
51
Y = -16513598
15 feet Y = -5033344
72 meter
Z = 4214848
73 Z = 1284685
89
XDOT = 8354
633087 XDOT = 2546
492165
YDOT = -12191
005684 feet/sec YDOT = -3715
818533 meter/sec
ZDOT = -19142
478527 ZDOT = -5834
627455
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 14339
58425982
00016717 00000-0 10270-3 0 9112
2 25544 51
6430 329
7402 0007365 97
6799 262
5190 15
51947914 37928
Satellite: ISS
Catalog Number: 25544
Epoch time: 14339
58425982 = yrday
fracday
Element set: 911
Inclination: 51
6430 deg
RA of node: 329
7402 deg
Eccentricity:
0007365
Arg of perigee: 97
6799 deg
Mean anomaly: 262
5190 deg
Mean motion: 15
51947914 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3792
Checksum: 344
Coasting Arc #13 (Orbit 3806)
---------------------------------------
Vector Time (GMT): 2014/340/13:11:16
604
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5335662
13 A = 6795461
76 meter
Y = -4185934
30 meter E =
0016502
Z = -365377
72 I = 51
45538
XDOT = 3195
833454 Wp = 65
60182
YDOT = 3570
850724 meter/sec RA = 324
34524 deg
ZDOT = 5980
010975 TA = 290
45392
MA = 290
63102
Ha = 227
076 n
mi
Hp = 215
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17505453
18 X = 5383848
57
Y = -13733380
26 feet Y = -4125998
01 meter
Z = -1198745
82 Z = -339340
86
XDOT = 10485
017894 XDOT = 3126
616541
YDOT = 11715
389513 feet/sec YDOT = 3606
201061 meter/sec
ZDOT = 19619
458579 ZDOT = 5995
368257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14405015
52 X = 4390648
73
Y = 16964603
82 feet Y = 5170811
24 meter
Z = -1086904
37 Z = -331288
45
XDOT = -10067
772641 XDOT = -3068
657101
YDOT = 9758
885272 feet/sec YDOT = 2974
508231 meter/sec
ZDOT = 19684
210550 ZDOT = 5999
747376
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 14340
55013890
00016717 00000-0 10270-3 0 9123
2 25544 51
6428 324
9413 0007499 102
7050 257
4940 15
52003862 38079
Satellite: ISS
Catalog Number: 25544
Epoch time: 14340
55013890 = yrday
fracday
Element set: 912
Inclination: 51
6428 deg
RA of node: 324
9413 deg
Eccentricity:
0007499
Arg of perigee: 102
7050 deg
Mean anomaly: 257
4940 deg
Mean motion: 15
52003862 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3807
Checksum: 296
Coasting Arc #14 (Orbit 3822)
---------------------------------------
Vector Time (GMT): 2014/341/13:11:16
604
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5463979
18 A = 6795204
48 meter
Y = 3972676
68 meter E =
0017063
Z = -680967
36 I = 51
43095
XDOT = -2349
218931 Wp = 125
24750
YDOT = -4230
332413 meter/sec RA = 319
36997 deg
ZDOT = -5944
620079 TA = 62
12246
MA = 61
94973
Ha = 226
918 n
mi
Hp = 215
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17926440
89 X = -5504688
54
Y = 13033716
13 feet Y = 3911347
37 meter
Z = -2234144
89 Z = -707609
31
XDOT = -7707
411190 XDOT = -2272
862494
YDOT = -13879
043349 feet/sec YDOT = -4256
175401 meter/sec
ZDOT = -19503
346716 ZDOT = -5955
847280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14018231
31 X = -4272756
90
Y = -17152261
62 feet Y = -5228009
34 meter
Z = -2348521
80 Z = -715829
44
XDOT = 12182
558375 XDOT = 3713
243793
YDOT = -7328
929229 feet/sec YDOT = -2233
857629 meter/sec
ZDOT = -19550
362246 ZDOT = -5958
950413
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 14341
58037776
00016717 00000-0 10270-3 0 9137
2 25544 51
6439 319
8208 0007361 105
2018 254
9948 15
52034441 38231
Satellite: ISS
Catalog Number: 25544
Epoch time: 14341
58037776 = yrday
fracday
Element set: 913
Inclination: 51
6439 deg
RA of node: 319
8208 deg
Eccentricity:
0007361
Arg of perigee: 105
2018 deg
Mean anomaly: 254
9948 deg
Mean motion: 15
52034441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3823
Checksum: 312
Coasting Arc #15 (Orbit 3838)
---------------------------------------
Vector Time (GMT): 2014/342/13:11:16
604
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5454345
82 A = 6794029
89 meter
Y = -3686891
97 meter E =
0019799
Z = 1651555
32 I = 51
40457
XDOT = 1567
226104 Wp = 79
39018
YDOT = 4892
401490 meter/sec RA = 314
39284 deg
ZDOT = 5691
191243 TA = 298
74886
MA = 298
94763
Ha = 226
811 n
mi
Hp = 215
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17894835
37 X = 5487145
37
Y = -12096102
25 feet Y = -3625714
70 meter
Z = 5418488
58 Z = 1678131
19
XDOT = 5141
817926 XDOT = 1484
755567
YDOT = 16051
185992 feet/sec YDOT = 4909
465573 meter/sec
ZDOT = 18671
887279 ZDOT = 5698
604782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13372024
11 X = 4075792
95
Y = 16925749
17 feet Y = 5158968
35 meter
Z = 5532524
51 Z = 1686313
47
XDOT = -14407
303037 XDOT = -4391
345966
YDOT = 5211
661487 feet/sec YDOT = 1588
514421 meter/sec
ZDOT = 18702
517196 ZDOT = 5700
527241
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 14342
61058279
00016717 00000-0 10270-3 0 9144
2 25544 51
6439 314
7016 0007396 110
2632 249
9315 15
52101772 38399
Satellite: ISS
Catalog Number: 25544
Epoch time: 14342
61058279 = yrday
fracday
Element set: 914
Inclination: 51
6439 deg
RA of node: 314
7016 deg
Eccentricity:
0007396
Arg of perigee: 110
2632 deg
Mean anomaly: 249
9315 deg
Mean motion: 15
52101772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3839
Checksum: 307
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