[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 4th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 0 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
317/02:00:25
005 0
4 1
0 1
0
N/A 0
8 0
0 226
9
000/00:02:04
610 -0
3 -0
0 219
0
Coasting Arc #1 (Orbit 3293)
---------------------------------------
Vector Time (GMT): 2014/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930906
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2872755
70 A = 6797440
18 meter
Y = 5901925
10 meter E =
0010719
Z = -1744817
39 I = 51
93825
XDOT = -5057
195270 Wp = 21
43426
YDOT = -781
030886 meter/sec RA = 127
96793 deg
ZDOT = 5705
290573 TA = 319
52248
MA = 319
60217
Ha = 226
406 n
mi
Hp = 219
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9425051
53 X = -2930062
96
Y = 19363271
32 feet Y = 5869479
52 meter
Z = -5724466
50 Z = -1758912
76
XDOT = -16591
847998 XDOT = -5075
800751
YDOT = -2562
437290 feet/sec YDOT = -837
687307 meter/sec
ZDOT = 18718
144926 ZDOT = 5680
677819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5920722
04 X = -1804636
08
Y = -20688414
50 feet Y = -6305828
74 meter
Z = -5785494
35 Z = -1763418
68
XDOT = 12648
609600 XDOT = 3855
296206
YDOT = -8806
225384 feet/sec YDOT = -2684
137497 meter/sec
ZDOT = 18613
358277 ZDOT = 5673
351603
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 14307
50346251
00016717 00000-0 10270-3 0 9008
2 25544 51
6412 128
9759 0004217 349
4527 10
6535 15
50891029 32948
Satellite: ISS
Catalog Number: 25544
Epoch time: 14307
50346251 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 128
9759 deg
Eccentricity:
0004217
Arg of perigee: 349
4527 deg
Mean anomaly: 10
6535 deg
Mean motion: 15
50891029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3294
Checksum: 300
Coasting Arc #2 (Orbit 3309)
---------------------------------------
Vector Time (GMT): 2014/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930906
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2899325
27 A = 6797998
45 meter
Y = -6044753
13 meter E =
0011236
Z = 1104647
99 I = 51
95930
XDOT = 4738
084476 Wp = 105
19954
YDOT = 1185
310411 meter/sec RA = 123
03172 deg
ZDOT = -5902
609011 TA = 62
88718
MA = 62
77262
Ha = 226
428 n
mi
Hp = 219
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9512222
00 X = 2961337
46
Y = -19831867
22 feet Y = -6011984
19 meter
Z = 3624173
21 Z = 1118883
89
XDOT = 15544
896576 XDOT = 4753
151570
YDOT = 3888
813684 feet/sec YDOT = 1238
378574 meter/sec
ZDOT = -19365
515128 ZDOT = -5879
555007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6520719
25 X = 1987515
23
Y = 20995589
53 feet Y = 6399455
69 meter
Z = 3685837
34 Z = 1123443
22
XDOT = -12601
904641 XDOT = -3841
060535
YDOT = 7322
976099 feet/sec YDOT = 2232
043115 meter/sec
ZDOT = -19267
434245 ZDOT = -5872
713958
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 14308
53443307
00016717 00000-0 10270-3 0 9013
2 25544 51
6412 123
8608 0004515 352
3851 7
7230 15
50968018 33100
Satellite: ISS
Catalog Number: 25544
Epoch time: 14308
53443307 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 123
8608 deg
Eccentricity:
0004515
Arg of perigee: 352
3851 deg
Mean anomaly: 7
7230 deg
Mean motion: 15
50968018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3310
Checksum: 277
Coasting Arc #3 (Orbit 3324)
---------------------------------------
Vector Time (GMT): 2014/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930906
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2857875
43 A = 6798488
17 meter
Y = 6141511
58 meter E =
0014363
Z = -474773
48 I = 51
97669
XDOT = -4467
017695 Wp = 30
16804
YDOT = -1620
648666 meter/sec RA = 118
09601 deg
ZDOT = 6015
629434 TA = 324
74000
MA = 324
83494
Ha = 226
522 n
mi
Hp = 219
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9376231
74 X = -2924032
48
Y = 20149316
20 feet Y = 6109183
03 meter
Z = -1557655
77 Z = -488818
04
XDOT = -14655
569867 XDOT = -4477
786000
YDOT = -5317
088798 feet/sec YDOT = -1670
661631 meter/sec
ZDOT = 19736
317040 ZDOT = 5993
902646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7189520
70 X = -2191365
91
Y = -21024416
45 feet Y = -6408242
13 meter
Z = -1618536
89 Z = -493330
04
XDOT = 12812
213457 XDOT = 3905
162662
YDOT = -5871
462837 feet/sec YDOT = -1789
621873 meter/sec
ZDOT = 19643
962725 ZDOT = 5987
479839
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 14309
50095381
00016717 00000-0 10270-3 0 9027
2 25544 51
6408 119
0644 0004205 357
8708 2
2424 15
50947999 33255
Satellite: ISS
Catalog Number: 25544
Epoch time: 14309
50095381 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 119
0644 deg
Eccentricity:
0004205
Arg of perigee: 357
8708 deg
Mean anomaly: 2
2424 deg
Mean motion: 15
50947999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3325
Checksum: 306
Coasting Arc #4 (Orbit 3340)
---------------------------------------
Vector Time (GMT): 2014/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930906
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2821041
97 A = 6798359
19 meter
Y = -6179181
96 meter E =
0009104
Z = -208739
70 I = 51
99093
XDOT = 4218
568975 Wp = 115
68491
YDOT = 2122
643505 meter/sec RA = 113
16239 deg
ZDOT = -6030
964371 TA = 66
54924
MA = 66
45356
Ha = 226
552 n
mi
Hp = 219
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9255387
03 X = 2890943
37
Y = -20272906
71 feet Y = -6147244
41 meter
Z = -684841
54 Z = -194865
08
XDOT = 13840
449393 XDOT = 4223
816857
YDOT = 6964
053495 feet/sec YDOT = 2169
847403 meter/sec
ZDOT = -19786
628513 ZDOT = -6010
457911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7713040
08 X = 2350934
62
Y = 20910302
63 feet Y = 6373460
24 meter
Z = -624659
82 Z = -190396
31
XDOT = -13290
609782 XDOT = -4050
977862
YDOT = 4336
297709 feet/sec YDOT = 1321
703542 meter/sec
ZDOT = -19699
558732 ZDOT = -6004
425502
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 14310
53188740
00016717 00000-0 10270-3 0 9035
2 25544 51
6409 113
9488 0004505 1
2862 358
8300 15
51020534 33418
Satellite: ISS
Catalog Number: 25544
Epoch time: 14310
53188740 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 113
9488 deg
Eccentricity:
0004505
Arg of perigee: 1
2862 deg
Mean anomaly: 358
8300 deg
Mean motion: 15
51020534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3341
Checksum: 277
Coasting Arc #5 (Orbit 3356)
---------------------------------------
Vector Time (GMT): 2014/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930906
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2735066
83 A = 6798102
21 meter
Y = 6153493
40 meter E =
0016486
Z = 861325
94 I = 52
00215
XDOT = -4036
094618 Wp = 43
31745
YDOT = -2636
360958 meter/sec RA = 108
22905 deg
ZDOT = 5962
729353 TA = 325
94756
MA = 326
05324
Ha = 226
616 n
mi
Hp = 219
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8973316
36 X = -2807857
50
Y = 20188626
65 feet Y = 6122501
13 meter
Z = 2825872
52 Z = 847862
10
XDOT = -13241
780243 XDOT = -4035
280066
YDOT = -8649
478209 feet/sec YDOT = -2681
490535 meter/sec
ZDOT = 19562
760343 ZDOT = 5943
124052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8198613
81 X = -2498937
49
Y = -20523418
07 feet Y = -6255537
83 meter
Z = 2767426
66 Z = 843511
65
XDOT = 14021
796665 XDOT = 4273
843623
YDOT = -2949
525388 feet/sec YDOT = -899
015338 meter/sec
ZDOT = 19479
618998 ZDOT = 5937
387871
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 14311
56280391
00016717 00000-0 10270-3 0 9045
2 25544 51
6416 108
8330 0004209 6
4133 353
7071 15
51014299 33571
Satellite: ISS
Catalog Number: 25544
Epoch time: 14311
56280391 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 108
8330 deg
Eccentricity:
0004209
Arg of perigee: 6
4133 deg
Mean anomaly: 353
7071 deg
Mean motion: 15
51014299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3357
Checksum: 280
Coasting Arc #6 (Orbit 3371)
---------------------------------------
Vector Time (GMT): 2014/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930906
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2672017
12 A = 6797266
63 meter
Y = -6055490
00 meter E =
0006133
Z = -1546305
52 I = 52
00909
XDOT = 3885
590651 Wp = 109
91725
YDOT = 3185
103115 meter/sec RA = 103
29626 deg
ZDOT = -5779
498228 TA = 86
86063
MA = 86
79046
Ha = 226
659 n
mi
Hp = 219
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8766460
35 X = 2747044
07
Y = -19867093
19 feet Y = -6025190
27 meter
Z = -5073180
85 Z = -1533142
68
XDOT = 12748
000823 XDOT = 3877
760959
YDOT = 10449
813369 feet/sec YDOT = 3228
510543 meter/sec
ZDOT = -18961
608359 ZDOT = -5760
641105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8448295
45 X = 2575040
45
Y = 20018872
93 feet Y = 6101752
47 meter
Z = -5016015
67 Z = -1528881
58
XDOT = -14966
165514 XDOT = -4561
687249
YDOT = 1602
014367 feet/sec YDOT = 488
293979 meter/sec
ZDOT = -18881
751658 ZDOT = -5755
157905
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 14312
52926903
00016717 00000-0 10270-3 0 9059
2 25544 51
6419 104
0371 0004466 9
8979 350
2263 15
51061479 33721
Satellite: ISS
Catalog Number: 25544
Epoch time: 14312
52926903 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 104
0371 deg
Eccentricity:
0004466
Arg of perigee: 9
8979 deg
Mean anomaly: 350
2263 deg
Mean motion: 15
51061479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3372
Checksum: 304
Coasting Arc #7 (Orbit 3387)
---------------------------------------
Vector Time (GMT): 2014/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930906
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2584939
94 A = 6796225
55 meter
Y = 5884938
81 meter E =
0016579
Z = 2178875
18 I = 52
01322
XDOT = -3807
812716 Wp = 58
17038
YDOT = -3723
725910 meter/sec RA = 98
36308 deg
ZDOT = 5517
791424 TA = 325
86711
MA = 325
97360
Ha = 226
686 n
mi
Hp = 218
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8480774
07 X = -2661139
08
Y = 19307542
01 feet Y = 5855606
25 meter
Z = 7148540
61 Z = 2166132
63
XDOT = -12492
823873 XDOT = -3792
694394
YDOT = -12216
948525 feet/sec YDOT = -3766
222892 meter/sec
ZDOT = 18102
990237 ZDOT = 5499
329860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8560601
36 X = -2609271
30
Y = -19292725
44 feet Y = -5880422
71 meter
Z = 7093179
10 Z = 2162000
99
XDOT = 16111
498963 XDOT = 4910
784884
YDOT = -494
989620 feet/sec YDOT = -150
872836 meter/sec
ZDOT = 18024
915215 ZDOT = 5493
994158
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 14313
56014623
00016717 00000-0 10270-3 0 9062
2 25544 51
6430 98
9218 0004253 13
7837 346
3429 15
51083155 33888
Satellite: ISS
Catalog Number: 25544
Epoch time: 14313
56014623 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 98
9218 deg
Eccentricity:
0004253
Arg of perigee: 13
7837 deg
Mean anomaly: 346
3429 deg
Mean motion: 15
51083155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3388
Checksum: 304
Coasting Arc #8 (Orbit 3402)
---------------------------------------
Vector Time (GMT): 2014/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930906
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2542101
37 A = 6794836
15 meter
Y = -5640090
94 meter E =
0005717
Z = -2817426
01 I = 52
01278
XDOT = 3760
934620 Wp = 70
77457
YDOT = 4256
093732 meter/sec RA = 93
42904 deg
ZDOT = -5133
348954 TA = 140
95182
MA = 140
91054
Ha = 226
731 n
mi
Hp = 218
857
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8340227
61 X = 2618667
65
Y = -18504235
36 feet Y = -5611235
35 meter
Z = -9243523
65 Z = -2804890
74
XDOT = 12339
024345 XDOT = 3737
999094
YDOT = 13963
562114 feet/sec YDOT = 4298
022801 meter/sec
ZDOT = -16841
696043 ZDOT = -5115
134147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8371463
23 X = 2551621
99
Y = 18517245
74 feet Y = 5644056
50 meter
Z = -9189073
20 Z = -2800829
51
XDOT = -17352
542228 XDOT = -5289
054871
YDOT = -463
604257 feet/sec YDOT = -141
306578 meter/sec
ZDOT = -16764
769104 ZDOT = -5109
901623
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 14314
52657627
00016717 00000-0 10270-3 0 9077
2 25544 51
6433 94
1262 0004447 17
2221 342
9080 15
51099061 34035
Satellite: ISS
Catalog Number: 25544
Epoch time: 14314
52657627 = yrday
fracday
Element set: 907
Inclination: 51
6433 deg
RA of node: 94
1262 deg
Eccentricity:
0004447
Arg of perigee: 17
2221 deg
Mean anomaly: 342
9080 deg
Mean motion: 15
51099061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3403
Checksum: 286
Coasting Arc #9 (Orbit 3418)
---------------------------------------
Vector Time (GMT): 2014/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930906
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2502448
61 A = 6793216
28 meter
Y = 5322967
19 meter E =
0014634
Z = 3382203
28 I = 52
00980
XDOT = -3780
432096 Wp = 73
00994
YDOT = -4757
980028 meter/sec RA = 88
49341 deg
ZDOT = 4678
593141 TA = 326
22513
MA = 326
31827
Ha = 226
758 n
mi
Hp = 218
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8210133
23 X = -2578215
19
Y = 17463803
11 feet Y = 5294559
50 meter
Z = 11096467
44 Z = 3369862
59
XDOT = -12402
992440 XDOT = -3749
673742
YDOT = -15610
170696 feet/sec YDOT = -4800
083362 meter/sec
ZDOT = 15349
715028 ZDOT = 4660
302683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7971635
26 X = -2429754
43
Y = -17607666
38 feet Y = -5366816
71 meter
Z = 11042889
68 Z = 3365872
77
XDOT = 18705
201037 XDOT = 5701
345276
YDOT = 1135
712324 feet/sec YDOT = 346
165116 meter/sec
ZDOT = 15272
557709 ZDOT = 4655
075590
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 14315
55741415
00016717 00000-0 10270-3 0 9081
2 25544 51
6444 89
0107 0004364 20
3578 339
7747 15
51148165 34197
Satellite: ISS
Catalog Number: 25544
Epoch time: 14315
55741415 = yrday
fracday
Element set: 908
Inclination: 51
6444 deg
RA of node: 89
0107 deg
Eccentricity:
0004364
Arg of perigee: 20
3578 deg
Mean anomaly: 339
7747 deg
Mean motion: 15
51148165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3419
Checksum: 312
Coasting Arc #10 (Orbit 3433)
---------------------------------------
Vector Time (GMT): 2014/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930906
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2526460
58 A = 6791581
57 meter
Y = -4943433
75 meter E =
0009948
Z = -3923806
24 I = 52
00276
XDOT = 3817
094291 Wp = 53
63669
YDOT = 5209
410373 meter/sec RA = 83
55601 deg
ZDOT = -4106
865443 TA = 173
45282
MA = 173
43981
Ha = 226
783 n
mi
Hp = 218
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8288912
65 X = 2600612
28
Y = -16218614
67 feet Y = -4914766
60 meter
Z = -12873380
06 Z = -3911352
80
XDOT = 12523
275233 XDOT = 3778
507859
YDOT = 17091
241380 feet/sec YDOT = 5251
879868 meter/sec
ZDOT = -13473
967989 ZDOT = -4088
415981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7252764
68 X = 2210642
67
Y = 16749160
96 feet Y = 5105144
26 meter
Z = -12819378
33 Z = -3907346
51
XDOT = -19989
450619 XDOT = -6092
784549
YDOT = -1593
441766 feet/sec YDOT = -485
681050 meter/sec
ZDOT = -13396
217569 ZDOT = -4083
167115
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 14316
52380823
00016717 00000-0 10270-3 0 9092
2 25544 51
6445 84
2152 0004501 23
5182 336
6174 15
51144316 34345
Satellite: ISS
Catalog Number: 25544
Epoch time: 14316
52380823 = yrday
fracday
Element set: 909
Inclination: 51
6445 deg
RA of node: 84
2152 deg
Eccentricity:
0004501
Arg of perigee: 23
5182 deg
Mean anomaly: 336
6174 deg
Mean motion: 15
51144316 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3434
Checksum: 281
Coasting Arc #11 (Orbit 3442)
---------------------------------------
Vector Time (GMT): 2014/317/02:01:27
310
Vector Time (MET): N/A
Weight (LBS) : 930815
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3598209
37 A = 6787570
38 meter
Y = -2692198
91 meter E =
0015971
Z = -5101074
23 I = 51
98682
XDOT = 2598
610775 Wp = 61
94696
YDOT = 6958
144702 meter/sec RA = 80
66401 deg
ZDOT = -1836
375267 TA = 190
30053
MA = 190
33329
Ha = 226
924 n
mi
Hp = 219
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11805148
84 X = 3652826
43
Y = -8832673
60 feet Y = -2651656
03 meter
Z = -16735807
83 Z = -5083461
74
XDOT = 8525
625902 XDOT = 2529
530683
YDOT = 22828
558735 feet/sec YDOT = 6986
817801 meter/sec
ZDOT = -6024
853238 ZDOT = -1823
919220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7010592
09 X = -2136828
47
Y = -13067293
00 feet Y = -3982910
91 meter
Z = -16660203
42 Z = -5078030
00
XDOT = 22876
849196 XDOT = 6972
863635
YDOT = -4645
873703 feet/sec YDOT = -1416
062305 meter/sec
ZDOT = -5972
983845 ZDOT = -1820
565476
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 14317
10363666
00016717 00000-0 10270-3 0 9105
2 25544 51
6456 81
3420 0004600 17
1468 342
9838 15
51004369 34439
Satellite: ISS
Catalog Number: 25544
Epoch time: 14317
10363666 = yrday
fracday
Element set: 910
Inclination: 51
6456 deg
RA of node: 81
3420 deg
Eccentricity:
0004600
Arg of perigee: 17
1468 deg
Mean anomaly: 342
9838 deg
Mean motion: 15
51004369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3443
Checksum: 288
Coasting Arc #12 (Orbit 3458)
---------------------------------------
Vector Time (GMT): 2014/318/02:01:27
310
Vector Time (MET): N/A
Weight (LBS) : 930815
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3679076
84 A = 6786717
52 meter
Y = 2204457
34 meter E =
0005162
Z = 5255330
95 I = 51
97819
XDOT = -2689
653966 Wp = 63
98069
YDOT = -7096
292333 meter/sec RA = 75
72079 deg
ZDOT = 1095
123789 TA = 15
58158
MA = 15
56570
Ha = 227
020 n
mi
Hp = 218
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12070462
07 X = -3728983
19
Y = 7232471
59 feet Y = 2163036
54 meter
Z = 17241899
45 Z = 5237337
04
XDOT = -8824
324035 XDOT = -2615
421499
YDOT = -23281
798994 feet/sec YDOT = -7125
954716 meter/sec
ZDOT = 3592
925816 ZDOT = 1082
238058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5612953
80 X = 1710828
32
Y = 13005916
40 feet Y = 3964203
32 meter
Z = 17164751
23 Z = 5231816
17
XDOT = -23275
131990 XDOT = -7094
260230
YDOT = 5379
808836 feet/sec YDOT = 1639
765733 meter/sec
ZDOT = 3539
257887 ZDOT = 1078
765804
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 14318
13454314
00016717 00000-0 10270-3 0 9111
2 25544 51
6454 76
2270 0004555 19
2088 340
9234 15
51045689 34598
Satellite: ISS
Catalog Number: 25544
Epoch time: 14318
13454314 = yrday
fracday
Element set: 911
Inclination: 51
6454 deg
RA of node: 76
2270 deg
Eccentricity:
0004555
Arg of perigee: 19
2088 deg
Mean anomaly: 340
9234 deg
Mean motion: 15
51045689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3459
Checksum: 303
Coasting Arc #13 (Orbit 3473)
---------------------------------------
Vector Time (GMT): 2014/319/02:01:27
310
Vector Time (MET): N/A
Weight (LBS) : 930815
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3826395
84 A = 6786334
94 meter
Y = -1727340
06 meter E =
0017374
Z = -5346492
34 I = 51
96913
XDOT = 2756
660764 Wp = 73
24987
YDOT = 7129
652951 meter/sec RA = 70
77599 deg
ZDOT = -326
558829 TA = 193
62045
MA = 193
66739
Ha = 226
987 n
mi
Hp = 218
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12553792
14 X = 3871398
87
Y = -5667126
17 feet Y = -1684299
31 meter
Z = -17540985
38 Z = -5327794
65
XDOT = 9044
162612 XDOT = 2678
316783
YDOT = 23391
249839 feet/sec YDOT = 7160
041665 meter/sec
ZDOT = -1071
387234 ZDOT = -313
357626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4226299
67 X = -1288176
14
Y = -13215705
76 feet Y = -4028147
12 meter
Z = -17460919
12 Z = -5322088
15
XDOT = 23288
327206 XDOT = 7098
282132
YDOT = -6087
220130 feet/sec YDOT = -1855
384696 meter/sec
ZDOT = -1016
389838 ZDOT = -309
795623
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 14319
10100169
00016717 00000-0 10270-3 0 9126
2 25544 51
6461 71
4313 0004722 23
2842 336
8523 15
51061655 34743
Satellite: ISS
Catalog Number: 25544
Epoch time: 14319
10100169 = yrday
fracday
Element set: 912
Inclination: 51
6461 deg
RA of node: 71
4313 deg
Eccentricity:
0004722
Arg of perigee: 23
2842 deg
Mean anomaly: 336
8523 deg
Mean motion: 15
51061655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3474
Checksum: 273
Coasting Arc #14 (Orbit 3489)
---------------------------------------
Vector Time (GMT): 2014/320/02:01:27
310
Vector Time (MET): N/A
Weight (LBS) : 930815
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4018072
17 A = 6786215
10 meter
Y = 1225416
38 meter E =
0006938
Z = 5326188
87 I = 51
95799
XDOT = -2797
311705 Wp = 40
78518
YDOT = -7123
420331 meter/sec RA = 65
82999 deg
ZDOT = -465
921263 TA = 53
67221
MA = 53
60817
Ha = 227
065 n
mi
Hp = 218
533
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13182651
46 X = -4057349
74
Y = 4020394
94 feet Y = 1180264
23 meter
Z = 17474372
95 Z = 5306573
90
XDOT = -9177
531840 XDOT = -2715
184726
YDOT = -23370
801611 feet/sec YDOT = -7154
242499 meter/sec
ZDOT = -1528
613066 ZDOT = -479
310730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2754478
42 X = 839565
02
Y = 13611886
73 feet Y = 4148903
08 meter
Z = 17390485
13 Z = 5300619
87
XDOT = -23136
708872 XDOT = -7052
068864
YDOT = 6729
111645 feet/sec YDOT = 2051
033229 meter/sec
ZDOT = -1584
403410 ZDOT = -482
926159
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 14320
13186938
00016717 00000-0 10270-3 0 9130
2 25544 51
6460 66
3159 0004714 25
1084 335
0295 15
51113137 34901
Satellite: ISS
Catalog Number: 25544
Epoch time: 14320
13186938 = yrday
fracday
Element set: 913
Inclination: 51
6460 deg
RA of node: 66
3159 deg
Eccentricity:
0004714
Arg of perigee: 25
1084 deg
Mean anomaly: 335
0295 deg
Mean motion: 15
51113137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3490
Checksum: 285
Coasting Arc #15 (Orbit 3504)
---------------------------------------
Vector Time (GMT): 2014/321/02:01:27
310
Vector Time (MET): N/A
Weight (LBS) : 930815
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4264302
56 A = 6786666
55 meter
Y = -768646
65 meter E =
0016260
Z = -5236950
88 I = 51
94647
XDOT = 2789
801118 Wp = 83
15050
YDOT = 7015
258970 meter/sec RA = 60
88329 deg
ZDOT = 1247
204502 TA = 198
76553
MA = 198
82554
Ha = 227
038 n
mi
Hp = 218
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13990493
97 X = 4298020
69
Y = -2521806
58 feet Y = -720772
09 meter
Z = -17181597
38 Z = -5216153
21
XDOT = 9152
890806 XDOT = 2705
088886
YDOT = 23015
941503 feet/sec YDOT = 7045
982722 meter/sec
ZDOT = 4091
878288 ZDOT = 1260
551213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1432076
28 X = -436496
85
Y = -14250886
74 feet Y = -4343670
28 meter
Z = -17092750
02 Z = -5209870
20
XDOT = 22610
618433 XDOT = 6891
716498
YDOT = -7226
140646 feet/sec YDOT = -2202
527669 meter/sec
ZDOT = 4147
493882 ZDOT = 1264
156135
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 14321
09829197
00016717 00000-0 10270-3 0 9148
2 25544 51
6466 61
5200 0004827 28
8336 331
3082 15
51116651 35050
Satellite: ISS
Catalog Number: 25544
Epoch time: 14321
09829197 = yrday
fracday
Element set: 914
Inclination: 51
6466 deg
RA of node: 61
5200 deg
Eccentricity:
0004827
Arg of perigee: 28
8336 deg
Mean anomaly: 331
3082 deg
Mean motion: 15
51116651 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3505
Checksum: 292
Coasting Arc #16 (Orbit 3520)
---------------------------------------
Vector Time (GMT): 2014/322/02:01:27
310
Vector Time (MET): N/A
Weight (LBS) : 930815
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4546468
34 A = 6787355
79 meter
Y = 303598
97 meter E =
0010635
Z = 5026333
51 I = 51
93354
XDOT = -2721
331249 Wp = 44
86056
YDOT = -6872
203732 meter/sec RA = 55
93594 deg
ZDOT = -2036
469841 TA = 64
91220
MA = 64
80186
Ha = 227
101 n
mi
Hp = 218
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14916234
70 X = -4573942
16
Y = 996059
63 feet Y = 252603
96 meter
Z = 16490595
50 Z = 5004180
21
XDOT = -8928
252129 XDOT = -2634
389689
YDOT = -22546
600171 feet/sec YDOT = -6902
149367 meter/sec
ZDOT = -6681
331499 ZDOT = -2049
478566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 98898
55 X = 30144
28
Y = 15052758
26 feet Y = 4588080
72 meter
Z = 16396055
03 Z = 4997517
57
XDOT = -21939
889478 XDOT = -6687
278313
YDOT = 7516
547343 feet/sec YDOT = 2291
043630 meter/sec
ZDOT = -6735
518739 ZDOT = -2052
986112
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 14322
12912153
00016717 00000-0 10270-3 0 9159
2 25544 51
6468 56
4044 0004876 30
8618 329
2819 15
51176479 35217
Satellite: ISS
Catalog Number: 25544
Epoch time: 14322
12912153 = yrday
fracday
Element set: 915
Inclination: 51
6468 deg
RA of node: 56
4044 deg
Eccentricity:
0004876
Arg of perigee: 30
8618 deg
Mean anomaly: 329
2819 deg
Mean motion: 15
51176479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3521
Checksum: 310
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