[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 20th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24487 9 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 3542)
---------------------------------------
Vector Time (GMT): 2014/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3847198
48 A = 6786120
80 meter
Y = 1866158
63 meter E =
0009970
Z = 5264070
70 I = 51
90409
XDOT = -4381
427929 Wp = 48
24165
YDOT = -6215
467450 meter/sec RA = 48
95508 deg
ZDOT = -991
011946 TA = 51
25392
MA = 51
16486
Ha = 227
708 n
mi
Hp = 217
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12622042
27 X = -3893352
15
Y = 6122567
67 feet Y = 1822878
78 meter
Z = 17270573
16 Z = 5245268
96
XDOT = -14374
763545 XDOT = -4306
785349
YDOT = -20391
953576 feet/sec YDOT = -6264
046083 meter/sec
ZDOT = -3251
351528 ZDOT = -1012
115420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1648696
86 X = 502522
80
Y = -14030649
20 feet Y = -4276541
88 meter
Z = 17190030
97 Z = 5239521
44
XDOT = 23885
681220 XDOT = 7280
355636
YDOT = -1316
571867 feet/sec YDOT = -401
291105 meter/sec
ZDOT = -3340
165754 ZDOT = -1018
082522
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 14323
54660827
00016717 00000-0 10270-3 0 9008
2 25544 51
6470 49
3791 0006394 43
5284 316
6371 15
51236630 35430
Satellite: ISS
Catalog Number: 25544
Epoch time: 14323
54660827 = yrday
fracday
Element set: 900
Inclination: 51
6470 deg
RA of node: 49
3791 deg
Eccentricity:
0006394
Arg of perigee: 43
5284 deg
Mean anomaly: 316
6371 deg
Mean motion: 15
51236630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3543
Checksum: 302
Coasting Arc #2 (Orbit 3557)
---------------------------------------
Vector Time (GMT): 2014/324/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4243384
92 A = 6786833
80 meter
Y = -1468307
16 meter E =
0017630
Z = -5103857
31 I = 51
88499
XDOT = 4267
715055 Wp = 85
22727
YDOT = 6088
901984 meter/sec RA = 44
00508 deg
ZDOT = 1803
309040 TA = 202
16616
MA = 202
24248
Ha = 227
678 n
mi
Hp = 217
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13921866
53 X = 4284282
03
Y = -4817280
71 feet Y = -1420626
19 meter
Z = -16744938
68 Z = -5083143
68
XDOT = 14001
689813 XDOT = 4190
550223
YDOT = 19976
712546 feet/sec YDOT = 6136
194880 meter/sec
ZDOT = 5916
368241 ZDOT = 1823
854126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3196799
64 X = -974384
53
Y = 14483268
74 feet Y = 4414500
31 meter
Z = -16656318
05 Z = -5076845
74
XDOT = -23271
041457 XDOT = -7093
013436
YDOT = 1741
241289 feet/sec YDOT = 530
730345 meter/sec
ZDOT = 6002
810515 ZDOT = 1829
656645
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 14324
51294879
00016717 00000-0 10270-3 0 9017
2 25544 51
6467 44
5843 0006581 47
2587 312
9117 15
51257249 35588
Satellite: ISS
Catalog Number: 25544
Epoch time: 14324
51294879 = yrday
fracday
Element set: 901
Inclination: 51
6467 deg
RA of node: 44
5843 deg
Eccentricity:
0006581
Arg of perigee: 47
2587 deg
Mean anomaly: 312
9117 deg
Mean motion: 15
51257249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3558
Checksum: 329
Coasting Arc #3 (Orbit 3573)
---------------------------------------
Vector Time (GMT): 2014/325/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4670593
10 A = 6787855
07 meter
Y = 1065373
77 meter E =
0014038
Z = 4802179
89 I = 51
86627
XDOT = -4066
319301 Wp = 55
72634
YDOT = -5949
463667 meter/sec RA = 39
05244 deg
ZDOT = -2621
821654 TA = 60
10751
MA = 59
96812
Ha = 227
712 n
mi
Hp = 217
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15323468
19 X = -4705487
28
Y = 3495320
76 feet Y = 1012948
94 meter
Z = 15755183
37 Z = 4779405
48
XDOT = -13340
942589 XDOT = -3986
752494
YDOT = -19519
237751 feet/sec YDOT = -5994
490933 meter/sec
ZDOT = -8601
777081 ZDOT = -2641
382663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4793753
58 X = 1461136
09
Y = -15069948
67 feet Y = -4593320
36 meter
Z = 15657851
74 Z = 4772513
21
XDOT = 22461
294386 XDOT = 6846
202529
YDOT = -1923
057131 feet/sec YDOT = -586
147814 meter/sec
ZDOT = -8684
035821 ZDOT = -2646
894118
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 14325
54368053
00016717 00000-0 10270-3 0 9028
2 25544 51
6470 39
4678 0006583 49
7735 310
3991 15
51323001 35745
Satellite: ISS
Catalog Number: 25544
Epoch time: 14325
54368053 = yrday
fracday
Element set: 902
Inclination: 51
6470 deg
RA of node: 39
4678 deg
Eccentricity:
0006583
Arg of perigee: 49
7735 deg
Mean anomaly: 310
3991 deg
Mean motion: 15
51323001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3574
Checksum: 307
Coasting Arc #4 (Orbit 3588)
---------------------------------------
Vector Time (GMT): 2014/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5097989
29 A = 6789238
33 meter
Y = -752870
63 meter E =
0013902
Z = -4431568
37 I = 51
84535
XDOT = 3768
339376 Wp = 86
25592
YDOT = 5747
523671 meter/sec RA = 34
10106 deg
ZDOT = 3368
585330 TA = 217
73009
MA = 217
82766
Ha = 227
693 n
mi
Hp = 217
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16725686
66 X = 5127556
83
Y = -2470048
00 feet Y = -695696
09 meter
Z = -14539266
30 Z = -4406730
66
XDOT = 12363
318163 XDOT = 3687
425248
YDOT = 18856
704956 feet/sec YDOT = 5789
211112 meter/sec
ZDOT = 11051
789141 ZDOT = 3386
695566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6112154
67 X = -1862984
74
Y = 15860782
17 feet Y = 4834366
41 meter
Z = -14433196
11 Z = -4399238
18
XDOT = -21308
230630 XDOT = -6494
748696
YDOT = 1884
832143 feet/sec YDOT = 574
496837 meter/sec
ZDOT = 11127
888679 ZDOT = 3391
780469
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 14326
50996601
00016717 00000-0 10270-3 0 9032
2 25544 51
6461 34
6724 0006780 54
3831 305
7951 15
51356013 35891
Satellite: ISS
Catalog Number: 25544
Epoch time: 14326
50996601 = yrday
fracday
Element set: 903
Inclination: 51
6461 deg
RA of node: 34
6724 deg
Eccentricity:
0006780
Arg of perigee: 54
3831 deg
Mean anomaly: 305
7951 deg
Mean motion: 15
51356013 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3589
Checksum: 307
Coasting Arc #5 (Orbit 3604)
---------------------------------------
Vector Time (GMT): 2014/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5525542
46 A = 6790887
79 meter
Y = 441003
41 meter E =
0017618
Z = 3913040
64 I = 51
82525
XDOT = -3353
792482 Wp = 71
48881
YDOT = -5551
868148 meter/sec RA = 29
14800 deg
ZDOT = -4089
602509 TA = 61
32174
MA = 61
14473
Ha = 227
693 n
mi
Hp = 216
808
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18128420
15 X = -5549071
89
Y = 1446861
59 feet Y = 379081
42 meter
Z = 12838059
83 Z = 3886140
63
XDOT = -11003
256174 XDOT = -3271
594536
YDOT = -18214
790513 feet/sec YDOT = -5588
912589 meter/sec
ZDOT = -13417
331066 ZDOT = -4105
695787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7401292
05 X = 2255913
82
Y = -16699953
51 feet Y = -5090145
83 meter
Z = 12723255
67 Z = 3878048
33
XDOT = 19999
744180 XDOT = 6095
922026
YDOT = -1461
814118 feet/sec YDOT = -445
560943 meter/sec
ZDOT = -13484
858644 ZDOT = -4110
184915
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 14327
54063949
00016717 00000-0 10270-3 0 9048
2 25544 51
6465 29
5554 0006786 56
1823 303
9973 15
51408657 36051
Satellite: ISS
Catalog Number: 25544
Epoch time: 14327
54063949 = yrday
fracday
Element set: 904
Inclination: 51
6465 deg
RA of node: 29
5554 deg
Eccentricity:
0006786
Arg of perigee: 56
1823 deg
Mean anomaly: 303
9973 deg
Mean motion: 15
51408657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3605
Checksum: 333
Coasting Arc #6 (Orbit 3619)
---------------------------------------
Vector Time (GMT): 2014/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5910489
07 A = 6792538
48 meter
Y = -229385
22 meter E =
0011375
Z = -3344557
76 I = 51
80229
XDOT = 2854
542567 Wp = 70
17115
YDOT = 5333
172619 meter/sec RA = 24
19588 deg
ZDOT = 4695
507045 TA = 251
05042
MA = 251
17374
Ha = 227
700 n
mi
Hp = 216
672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19391368
35 X = 5928861
90
Y = -752576
17 feet Y = -163187
35 meter
Z = -10972958
53 Z = -3315800
33
XDOT = 9365
297136 XDOT = 2771
883974
YDOT = 17497
285495 feet/sec YDOT = 5364
631479 meter/sec
ZDOT = 15405
206840 ZDOT = 4709
173833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8306142
09 X = -2531712
11
Y = 17614678
64 feet Y = 5368954
05 meter
Z = -10850274
49 Z = -3307163
66
XDOT = -18516
379690 XDOT = -5643
792530
YDOT = 758
972148 feet/sec YDOT = 231
334711 meter/sec
ZDOT = 15462
423620 ZDOT = 4712
946719
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
50687084
00016717 00000-0 10270-3 0 9058
2 25544 51
6454 24
7589 0006938 61
0478 299
1368 15
51437909 36207
Satellite: ISS
Catalog Number: 25544
Epoch time: 14328
50687084 = yrday
fracday
Element set: 905
Inclination: 51
6454 deg
RA of node: 24
7589 deg
Eccentricity:
0006938
Arg of perigee: 61
0478 deg
Mean anomaly: 299
1368 deg
Mean motion: 15
51437909 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3620
Checksum: 339
Coasting Arc #7 (Orbit 3635)
---------------------------------------
Vector Time (GMT): 2014/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6256230
71 A = 6794163
39 meter
Y = 12302
53 meter E =
0019494
Z = 2633034
90 I = 51
77965
XDOT = -2226
595339 Wp = 89
31452
YDOT = -5141
917497 meter/sec RA = 19
24295 deg
ZDOT = -5232
786208 TA = 61
09797
MA = 60
90254
Ha = 227
665 n
mi
Hp = 216
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20525691
31 X = -6268693
90
Y = 40362
62 feet Y = -57728
56 meter
Z = 8638565
93 Z = 2602612
34
XDOT = -7305
102817 XDOT = -2143
512216
YDOT = -16869
808062 feet/sec YDOT = -5166
351838 meter/sec
ZDOT = -17167
933753 ZDOT = -5243
401369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9138778
54 X = 2785499
70
Y = -18439444
11 feet Y = -5620342
56 meter
Z = 8508823
77 Z = 2593489
48
XDOT = 16965
662687 XDOT = 5171
133987
YDOT = 414
061112 feet/sec YDOT = 126
205827 meter/sec
ZDOT = -17212
170950 ZDOT = -5246
269706
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
53748707
00016717 00000-0 10270-3 0 9063
2 25544 51
6458 19
6413 0007027 62
9580 297
2288 15
51492759 36365
Satellite: ISS
Catalog Number: 25544
Epoch time: 14329
53748707 = yrday
fracday
Element set: 906
Inclination: 51
6458 deg
RA of node: 19
6413 deg
Eccentricity:
0007027
Arg of perigee: 62
9580 deg
Mean anomaly: 297
2288 deg
Mean motion: 15
51492759 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3636
Checksum: 342
Coasting Arc #8 (Orbit 3650)
---------------------------------------
Vector Time (GMT): 2014/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6519652
33 A = 6795507
48 meter
Y = 112268
95 meter E =
0013866
Z = -1903617
18 I = 51
75400
XDOT = 1545
943576 Wp = 52
51702
YDOT = 4968
284477 meter/sec RA = 14
29023 deg
ZDOT = 5623
996464 TA = 286
57733
MA = 286
72957
Ha = 227
716 n
mi
Hp = 216
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21389935
46 X = 6527159
59
Y = 368336
46 feet Y = 185218
02 meter
Z = -6245463
20 Z = -1871927
11
XDOT = 5071
993360 XDOT = 1462
952356
YDOT = 16300
145923 feet/sec YDOT = 4985
107862 meter/sec
ZDOT = 18451
431968 ZDOT = 5631
305214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9554804
86 X = -2912304
52
Y = 19184375
33 feet Y = 5847397
60 meter
Z = -6110341
10 Z = -1862431
97
XDOT = -15448
538081 XDOT = -4708
714407
YDOT = -1846
454054 feet/sec YDOT = -562
799196 meter/sec
ZDOT = 18481
601585 ZDOT = 5633
192163
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
50366498
00016717 00000-0 10270-3 0 9076
2 25544 51
6454 14
8441 0007125 67
0204 293
1699 15
51500371 36515
Satellite: ISS
Catalog Number: 25544
Epoch time: 14330
50366498 = yrday
fracday
Element set: 907
Inclination: 51
6454 deg
RA of node: 14
8441 deg
Eccentricity:
0007125
Arg of perigee: 67
0204 deg
Mean anomaly: 293
1699 deg
Mean motion: 15
51500371 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3651
Checksum: 295
Coasting Arc #9 (Orbit 3666)
---------------------------------------
Vector Time (GMT): 2014/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6703632
37 A = 6796358
63 meter
Y = -261632
60 meter E =
0018766
Z = 1051224
33 I = 51
72735
XDOT = -748
935918 Wp = 105
38692
YDOT = -4838
403683 meter/sec RA = 9
33661 deg
ZDOT = -5897
254626 TA = 63
24058
MA = 63
04869
Ha = 227
640 n
mi
Hp = 216
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21993544
52 X = -6705315
04
Y = -858374
66 feet Y = -336606
41 meter
Z = 3448898
72 Z = 1018654
72
XDOT = -2457
138837 XDOT = -666
128951
YDOT = -15874
027832 feet/sec YDOT = -4846
315510 meter/sec
ZDOT = -19347
948249 ZDOT = -5900
691954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9912568
08 X = 3021350
75
Y = -19675675
83 feet Y = -5997145
99 meter
Z = 3310058
16 Z = 1008905
73
XDOT = 13979
333689 XDOT = 4260
900908
YDOT = 3737
865099 feet/sec YDOT = 1139
301282 meter/sec
ZDOT = -19361
633609 ZDOT = -5901
425924
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
53422514
00016717 00000-0 10270-3 0 9083
2 25544 51
6459 9
7260 0007264 70
3468 289
8467 15
51566675 36676
Satellite: ISS
Catalog Number: 25544
Epoch time: 14331
53422514 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node: 9
7260 deg
Eccentricity:
0007264
Arg of perigee: 70
3468 deg
Mean anomaly: 289
8467 deg
Mean motion: 15
51566675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3667
Checksum: 333
Coasting Arc #10 (Orbit 3681)
---------------------------------------
Vector Time (GMT): 2014/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6777616
52 A = 6796774
04 meter
Y = 342672
10 meter E =
0018510
Z = -223096
69 I = 51
69769
XDOT = -54
598628 Wp = 54
78502
YDOT = 4757
182064 meter/sec RA = 4
38223 deg
ZDOT = 6010
811742 TA = 302
81534
MA = 302
99347
Ha = 227
708 n
mi
Hp = 216
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22236274
66 X = 6774364
69
Y = 1124252
30 feet Y = 418445
63 meter
Z = -731944
52 Z = -190179
68
XDOT = -179
129356 XDOT = -136
989246
YDOT = 15607
552705 feet/sec YDOT = 4756
110671 meter/sec
ZDOT = 19720
510963 ZDOT = 6010
346514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9906690
00 X = -3019559
11
Y = 19943897
53 feet Y = 6078899
97 meter
Z = -591643
25 Z = -180332
86
XDOT = -12736
894707 XDOT = -3882
205507
YDOT = -5785
497145 feet/sec YDOT = -1763
419530 meter/sec
ZDOT = 19717
571027 ZDOT = 6009
915649
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
50035005
00016717 00000-0 10270-3 0 9097
2 25544 51
6458 4
9287 0007361 73
2509 286
9450 15
51566025 36823
Satellite: ISS
Catalog Number: 25544
Epoch time: 14332
50035005 = yrday
fracday
Element set: 909
Inclination: 51
6458 deg
RA of node: 4
9287 deg
Eccentricity:
0007361
Arg of perigee: 73
2509 deg
Mean anomaly: 286
9450 deg
Mean motion: 15
51566025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3682
Checksum: 304
Coasting Arc #11 (Orbit 3697)
---------------------------------------
Vector Time (GMT): 2014/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6741165
89 A = 6796363
60 meter
Y = -478500
94 meter E =
0015368
Z = -690618
26 I = 51
66603
XDOT = 934
490103 Wp = 114
28842
YDOT = -4722
554226 meter/sec RA = 359
42538 deg
ZDOT = -5960
353982 TA = 73
15820
MA = 72
98970
Ha = 227
591 n
mi
Hp = 215
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22116685
98 X = -6731959
33
Y = -1569884
98 feet Y = -553833
55 meter
Z = -2265807
93 Z = -723343
77
XDOT = 3065
912410 XDOT = 1016
183044
YDOT = -15493
944312 feet/sec YDOT = -4711
647302 meter/sec
ZDOT = -19554
967134 ZDOT = -5955
615962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9920932
55 X = 3023900
24
Y = -19812522
56 feet Y = -6038856
88 meter
Z = -2405258
91 Z = -733122
92
XDOT = 11645
411453 XDOT = 3549
521411
YDOT = 8161
178672 feet/sec YDOT = 2487
527259 meter/sec
ZDOT = -19533
815251 ZDOT = -5953
906889
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
53085474
00016717 00000-0 10270-3 0 9108
2 25544 51
6461 359
8104 0007399 77
9578 282
2402 15
51632183 36987
Satellite: ISS
Catalog Number: 25544
Epoch time: 14333
53085474 = yrday
fracday
Element set: 910
Inclination: 51
6461 deg
RA of node: 359
8104 deg
Eccentricity:
0007399
Arg of perigee: 77
9578 deg
Mean anomaly: 282
2402 deg
Mean motion: 15
51632183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3698
Checksum: 329
Coasting Arc #12 (Orbit 3713)
---------------------------------------
Vector Time (GMT): 2014/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6585696
30 A = 6795487
31 meter
Y = 580886
23 meter E =
0021172
Z = 1532489
34 I = 51
63155
XDOT = -1771
191720 Wp = 68
46289
YDOT = 4749
119537 meter/sec RA = 354
46615 deg
ZDOT = 5754
979717 TA = 308
27615
MA = 308
46642
Ha = 227
601 n
mi
Hp = 215
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21606615
16 X = 6571266
81
Y = 1905794
72 feet Y = 654451
07 meter
Z = 5027852
16 Z = 1564447
00
XDOT = -5810
996457 XDOT = -1852
121969
YDOT = 15581
100844 feet/sec YDOT = 4728
860375 meter/sec
ZDOT = 18881
167052 ZDOT = 5746
178887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9697567
16 X = -2955818
47
Y = 19366142
01 feet Y = 5902800
09 meter
Z = 5164000
78 Z = 1573987
44
XDOT = -10903
137115 XDOT = -3323
276193
YDOT = -10532
166242 feet/sec YDOT = -3210
204270 meter/sec
ZDOT = 18842
687875 ZDOT = 5743
251264
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
56133180
00016717 00000-0 10270-3 0 9111
2 25544 51
6457 354
6931 0007511 80
6394 279
5606 15
51655398 37143
Satellite: ISS
Catalog Number: 25544
Epoch time: 14334
56133180 = yrday
fracday
Element set: 911
Inclination: 51
6457 deg
RA of node: 354
6931 deg
Eccentricity:
0007511
Arg of perigee: 80
6394 deg
Mean anomaly: 279
5606 deg
Mean motion: 15
51655398 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3714
Checksum: 318
Coasting Arc #13 (Orbit 3728)
---------------------------------------
Vector Time (GMT): 2014/335/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6308174
12 A = 6793845
83 meter
Y = -771396
06 meter E =
0011851
Z = -2406670
64 I = 51
59547
XDOT = 2621
430481 Wp = 104
21903
YDOT = -4804
051239 meter/sec RA = 349
50226 deg
ZDOT = -5356
281162 TA = 102
64846
MA = 102
51593
Ha = 227
500 n
mi
Hp = 215
703
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20696109
33 X = -6287388
36
Y = -2530826
97 feet Y = -841821
91 meter
Z = -7895901
05 Z = -2437264
80
XDOT = 8600
493705 XDOT = 2700
975117
YDOT = -15761
322961 feet/sec YDOT = -4774
291884 meter/sec
ZDOT = -17573
100925 ZDOT = -5343
353290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9622278
54 X = 2932870
50
Y = -18441022
50 feet Y = -5620823
66 meter
Z = -8026189
92 Z = -2446382
69
XDOT = 10353
817701 XDOT = 3155
843635
YDOT = 12991
379796 feet/sec YDOT = 3959
772562 meter/sec
ZDOT = -17517
016171 ZDOT = -5339
186529
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
52737620
00016717 00000-0 10270-3 0 9128
2 25544 51
6456 349
8945 0007446 85
0097 275
1905 15
51705920 37296
Satellite: ISS
Catalog Number: 25544
Epoch time: 14335
52737620 = yrday
fracday
Element set: 912
Inclination: 51
6456 deg
RA of node: 349
8945 deg
Eccentricity:
0007446
Arg of perigee: 85
0097 deg
Mean anomaly: 275
1905 deg
Mean motion: 15
51705920 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3729
Checksum: 328
Coasting Arc #14 (Orbit 3744)
---------------------------------------
Vector Time (GMT): 2014/336/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5923373
93 A = 6791921
43 meter
Y = 964604
66 meter E =
0020319
Z = 3161087
38 I = 51
55788
XDOT = -3387
158646 Wp = 86
40833
YDOT = 4909
669615 meter/sec RA = 344
53408 deg
ZDOT = 4823
264522 TA = 310
10467
MA = 310
28258
Ha = 227
408 n
mi
Hp = 215
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19433641
49 X = 5896791
45
Y = 3164713
46 feet Y = 1030694
97 meter
Z = 10371021
59 Z = 3189798
22
XDOT = -11112
725218 XDOT = -3465
238225
YDOT = 16107
839943 feet/sec YDOT = 4871
355529 meter/sec
ZDOT = 15824
358667 ZDOT = 4806
620374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9472809
36 X = -2887312
29
Y = 17187141
12 feet Y = 5238640
61 meter
Z = 10493235
19 Z = 3198338
09
XDOT = -10167
256185 XDOT = -3098
979685
YDOT = -15271
619563 feet/sec YDOT = -4654
789643 meter/sec
ZDOT = 15752
410332 ZDOT = 4801
334669
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
55779695
00016717 00000-0 10270-3 0 9131
2 25544 51
6446 344
7765 0007508 87
9572 272
2439 15
51751895 37457
Satellite: ISS
Catalog Number: 25544
Epoch time: 14336
55779695 = yrday
fracday
Element set: 913
Inclination: 51
6446 deg
RA of node: 344
7765 deg
Eccentricity:
0007508
Arg of perigee: 87
9572 deg
Mean anomaly: 272
2439 deg
Mean motion: 15
51751895 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3745
Checksum: 362
Coasting Arc #15 (Orbit 3759)
---------------------------------------
Vector Time (GMT): 2014/337/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914609
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5430849
54 A = 6789657
36 meter
Y = -1271340
50 meter E =
0013851
Z = -3884875
00 I = 51
52039
XDOT = 4094
410341 Wp = 82
94773
YDOT = -5001
977191 meter/sec RA = 339
55972 deg
ZDOT = -4097
780738 TA = 143
94618
MA = 143
85269
Ha = 227
398 n
mi
Hp = 215
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17817747
82 X = -5397357
67
Y = -4171064
63 feet Y = -1331884
36 meter
Z = -12745652
88 Z = -3911176
47
XDOT = 13433
104792 XDOT = 4169
945359
YDOT = -16410
686321 feet/sec YDOT = -4955
768332 meter/sec
ZDOT = -13444
162525 ZDOT = -4077
707048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9609807
24 X = 2929069
25
Y = -15480864
69 feet Y = -4718567
56 meter
Z = -12857527
69 Z = -3918974
44
XDOT = 10116
363935 XDOT = 3083
467727
YDOT = 17344
297437 feet/sec YDOT = 5286
541859 meter/sec
ZDOT = -13357
575966 ZDOT = -4071
389155
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
52378975
00016717 00000-0 10270-3 0 9146
2 25544 51
6443 339
9774 0007491 91
6825 268
5184 15
51789046 37605
Satellite: ISS
Catalog Number: 25544
Epoch time: 14337
52378975 = yrday
fracday
Element set: 914
Inclination: 51
6443 deg
RA of node: 339
9774 deg
Eccentricity:
0007491
Arg of perigee: 91
6825 deg
Mean anomaly: 268
5184 deg
Mean motion: 15
51789046 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3760
Checksum: 355
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