[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 31st 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18029 55 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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
092/18:33:27
052 -0
5 1
3 1
3
N/A 1
0 -0
1 220
3
000/00:02:50
103 0
5 -0
0 212
4
Coasting Arc #1 (Orbit 1578)
---------------------------------------
Vector Time (GMT): 2015/089/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904364
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 187286
87 A = 6780373
73 meter
Y = 5817182
76 meter E =
0010250
Z = -3491609
91 I = 51
97163
XDOT = -5411
677706 Wp = 128
23418
YDOT = 2915
405247 meter/sec RA = 116
13717 deg
ZDOT = 4569
834378 TA = 190
99103
MA = 191
01345
Ha = 220
817 n
mi
Hp = 211
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 614458
23 X = 139184
67
Y = 19085245
26 feet Y = 5819007
72 meter
Z = -11455413
09 Z = -3490817
68
XDOT = -17754
848116 XDOT = -5466
074672
YDOT = 9564
977846 feet/sec YDOT = 2854
584760 meter/sec
ZDOT = 14992
894941 ZDOT = 4543
413157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2916743
64 X = 889023
46
Y = 18872541
66 feet Y = 5752350
70 meter
Z = -11452965
23 Z = -3490863
80
XDOT = -15230
631404 XDOT = -4642
296452
YDOT = 11377
608930 feet/sec YDOT = 3467
895202 meter/sec
ZDOT = 14879
117966 ZDOT = 4535
155156
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 15089
50733331
00016717 00000-0 10270-3 0 9005
2 25544 51
6449 117
0916 0006741 153
2641 206
8861 15
55432642 15796
Satellite: ISS
Catalog Number: 25544
Epoch time: 15089
50733331 = yrday
fracday
Element set: 900
Inclination: 51
6449 deg
RA of node: 117
0916 deg
Eccentricity:
0006741
Arg of perigee: 153
2641 deg
Mean anomaly: 206
8861 deg
Mean motion: 15
55432642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1579
Checksum: 305
Coasting Arc #2 (Orbit 1594)
---------------------------------------
Vector Time (GMT): 2015/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904364
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1173152
74 A = 6784392
82 meter
Y = -6477510
93 meter E =
0019564
Z = 1594463
75 I = 51
99698
XDOT = 5036
596303 Wp = 129
74206
YDOT = -517
029125 meter/sec RA = 111
17516 deg
ZDOT = -5771
610687 TA = 32
87556
MA = 32
75402
Ha = 220
724 n
mi
Hp = 211
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3848926
32 X = 1237753
34
Y = -21251676
29 feet Y = -6464030
55 meter
Z = 5231180
28 Z = 1600320
47
XDOT = 16524
266085 XDOT = 5070
039727
YDOT = -1696
289780 feet/sec YDOT = -460
520415 meter/sec
ZDOT = -18935
730600 ZDOT = -5747
062682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 930450
27 X = 283601
24
Y = -21570990
62 feet Y = -6574837
94 meter
Z = 5257361
70 Z = 1602443
85
XDOT = 14692
876815 XDOT = 4478
388853
YDOT = -3983
152709 feet/sec YDOT = -1214
064946 meter/sec
ZDOT = -18830
372194 ZDOT = -5739
497445
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 15090
53530214
00016717 00000-0 10270-3 0 9016
2 25544 51
6436 111
9565 0006708 156
7955 203
3502 15
55454580 15951
Satellite: ISS
Catalog Number: 25544
Epoch time: 15090
53530214 = yrday
fracday
Element set: 901
Inclination: 51
6436 deg
RA of node: 111
9565 deg
Eccentricity:
0006708
Arg of perigee: 156
7955 deg
Mean anomaly: 203
3502 deg
Mean motion: 15
55454580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1595
Checksum: 301
Coasting Arc #3 (Orbit 1610)
---------------------------------------
Vector Time (GMT): 2015/091/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904364
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2287139
76 A = 6785209
76 meter
Y = 6363359
93 meter E =
0012373
Z = 535542
13 I = 52
01089
XDOT = -4290
719030 Wp = 81
11702
YDOT = -2057
888854 meter/sec RA = 106
22341 deg
ZDOT = 6011
425989 TA = 284
63237
MA = 284
76953
Ha = 220
528 n
mi
Hp = 211
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7503739
38 X = -2360727
84
Y = 20877165
13 feet Y = 6337372
26 meter
Z = 1757027
98 Z = 524252
00
XDOT = -14077
162171 XDOT = -4296
589549
YDOT = -6751
603851 feet/sec YDOT = -2105
902427 meter/sec
ZDOT = 19722
526210 ZDOT = 5990
568584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4272346
52 X = -1302211
22
Y = 21773391
79 feet Y = 6636529
82 meter
Z = 1707554
03 Z = 520462
47
XDOT = -13471
423991 XDOT = -4106
090032
YDOT = -4213
843966 feet/sec YDOT = -1284
379641 meter/sec
ZDOT = 19633
418070 ZDOT = 5984
265828
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 15091
56324457
00016717 00000-0 10270-3 0 9021
2 25544 51
6437 106
8221 0006674 161
2015 198
9386 15
55506560 16118
Satellite: ISS
Catalog Number: 25544
Epoch time: 15091
56324457 = yrday
fracday
Element set: 902
Inclination: 51
6437 deg
RA of node: 106
8221 deg
Eccentricity:
0006674
Arg of perigee: 161
2015 deg
Mean anomaly: 198
9386 deg
Mean motion: 15
55506560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1611
Checksum: 303
Coasting Arc #4 (Orbit 1625)
---------------------------------------
Vector Time (GMT): 2015/092/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904364
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3169032
87 A = 6782408
32 meter
Y = -5383166
15 meter E =
0011108
Z = -2632510
87 I = 52
00856
XDOT = 3294
158016 Wp = 148
57659
YDOT = 4503
623686 meter/sec RA = 101
26775 deg
ZDOT = -5263
005366 TA = 60
94577
MA = 60
83454
Ha = 220
493 n
mi
Hp = 211
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10397089
47 X = 3241780
96
Y = -17661306
26 feet Y = -5347321
59 meter
Z = -8636846
70 Z = -2616938
80
XDOT = 10807
605041 XDOT = 3269
118358
YDOT = 14775
668261 feet/sec YDOT = 4540
320323 meter/sec
ZDOT = -17267
077972 ZDOT = -5247
064451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7332951
73 X = 2235083
69
Y = -19168036
26 feet Y = -5842417
45 meter
Z = -8569161
81 Z = -2611880
52
XDOT = 11848
025601 XDOT = 3611
278203
YDOT = 12193
365256 feet/sec YDOT = 3716
537730 meter/sec
ZDOT = -17199
465988 ZDOT = -5242
397233
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 15092
52691865
00016717 00000-0 10270-3 0 9039
2 25544 51
6427 102
0071 0006656 164
6553 195
4804 15
55511958 16262
Satellite: ISS
Catalog Number: 25544
Epoch time: 15092
52691865 = yrday
fracday
Element set: 903
Inclination: 51
6427 deg
RA of node: 102
0071 deg
Eccentricity:
0006656
Arg of perigee: 164
6553 deg
Mean anomaly: 195
4804 deg
Mean motion: 15
55511958 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1626
Checksum: 315
Coasting Arc #5 (Orbit 1629)
---------------------------------------
Vector Time (GMT): 2015/092/18:34:52
103
Vector Time (MET): N/A
Weight (LBS) : 904237
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2649286
44 A = 6778042
22 meter
Y = 4506106
05 meter E =
0012208
Z = -4327696
32 I = 51
99561
XDOT = -3789
916008 Wp = 135
10406
YDOT = 5634
091097 meter/sec RA = 99
85879 deg
ZDOT = 3543
953330 TA = 170
86585
MA = 170
84362
Ha = 220
263 n
mi
Hp = 212
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8691884
64 X = 2619723
58
Y = 14783812
50 feet Y = 4535566
16 meter
Z = -14198478
73 Z = -4314899
04
XDOT = -12434
107639 XDOT = -3869
851326
YDOT = 18484
550843 feet/sec YDOT = 5591
263365 meter/sec
ZDOT = 11627
143472 ZDOT = 3525
347607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11194001
75 X = 3411931
73
Y = -13051376
16 feet Y = -3978059
45 meter
Z = -14144351
31 Z = -4311198
28
XDOT = 20564
763049 XDOT = 6268
139777
YDOT = 5116
476201 feet/sec YDOT = 1559
501946 meter/sec
ZDOT = 11546
403150 ZDOT = 3519
343680
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 15092
78389499
00016717 00000-0 10270-3 0 9045
2 25544 51
6447 100
7236 0005711 173
3984 186
7246 15
55303848 16303
Satellite: ISS
Catalog Number: 25544
Epoch time: 15092
78389499 = yrday
fracday
Element set: 904
Inclination: 51
6447 deg
RA of node: 100
7236 deg
Eccentricity:
0005711
Arg of perigee: 173
3984 deg
Mean anomaly: 186
7246 deg
Mean motion: 15
55303848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1630
Checksum: 332
Coasting Arc #6 (Orbit 1645)
---------------------------------------
Vector Time (GMT): 2015/093/18:34:52
103
Vector Time (MET): N/A
Weight (LBS) : 904237
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1653641
85 A = 6782655
93 meter
Y = -5959709
38 meter E =
0015912
Z = 2760753
21 I = 52
01539
XDOT = 4366
247116 Wp = 121
50594
YDOT = -3615
803973 meter/sec RA = 94
89095 deg
ZDOT = -5176
475210 TA = 27
35259
MA = 27
26890
Ha = 220
244 n
mi
Hp = 212
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5425334
15 X = -1600286
86
Y = -19552852
31 feet Y = -5977902
76 meter
Z = 9057589
26 Z = 2752850
55
XDOT = 14324
957731 XDOT = 4431
500931
YDOT = -11862
873927 feet/sec YDOT = -3566
613648 meter/sec
ZDOT = -16983
186386 ZDOT = -5155
105668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16569066
52 X = -5050251
48
Y = 11739202
74 feet Y = 3578108
99 meter
Z = 9024708
35 Z = 2750731
10
XDOT = -15171
191289 XDOT = -4624
179105
YDOT = -8393
091423 feet/sec YDOT = -2558
214266 meter/sec
ZDOT = -16890
924021 ZDOT = -5148
353642
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 15093
81193962
00016717 00000-0 10270-3 0 9059
2 25544 51
6444 95
5894 0005788 176
7350 183
3842 15
55319269 16465
Satellite: ISS
Catalog Number: 25544
Epoch time: 15093
81193962 = yrday
fracday
Element set: 905
Inclination: 51
6444 deg
RA of node: 95
5894 deg
Eccentricity:
0005788
Arg of perigee: 176
7350 deg
Mean anomaly: 183
3842 deg
Mean motion: 15
55319269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1646
Checksum: 348
Coasting Arc #7 (Orbit 1660)
---------------------------------------
Vector Time (GMT): 2015/094/18:34:52
103
Vector Time (MET): N/A
Weight (LBS) : 904237
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 611802
45 A = 6785421
85 meter
Y = 6712392
92 meter E =
0006876
Z = -774250
48 I = 52
02774
XDOT = -4665
931025 Wp = 70
82132
YDOT = 1109
779265 meter/sec RA = 89
93603 deg
ZDOT = 5979
667626 TA = 280
85499
MA = 280
93236
Ha = 219
942 n
mi
Hp = 212
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2007225
89 X = 540458
47
Y = 22022286
47 feet Y = 6718835
48 meter
Z = -2540191
87 Z = -771452
65
XDOT = -15308
172655 XDOT = -4707
041337
YDOT = 3641
008088 feet/sec YDOT = 1057
372740 meter/sec
ZDOT = 19618
332107 ZDOT = 5956
901209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19895522
58 X = 6064155
28
Y = -9655735
17 feet Y = -2943068
08 meter
Z = -2529346
08 Z = -770944
68
XDOT = 8144
382217 XDOT = 2482
407700
YDOT = 11707
094225 feet/sec YDOT = 3568
322320 meter/sec
ZDOT = 19520
501550 ZDOT = 5949
848872
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 15094
77570613
00016717 00000-0 10270-3 0 9068
2 25544 51
6451 90
7755 0005709 181
3950 178
7188 15
55384329 16614
Satellite: ISS
Catalog Number: 25544
Epoch time: 15094
77570613 = yrday
fracday
Element set: 906
Inclination: 51
6451 deg
RA of node: 90
7755 deg
Eccentricity:
0005709
Arg of perigee: 181
3950 deg
Mean anomaly: 178
7188 deg
Mean motion: 15
55384329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1661
Checksum: 336
Coasting Arc #8 (Orbit 1676)
---------------------------------------
Vector Time (GMT): 2015/095/18:34:52
103
Vector Time (MET): N/A
Weight (LBS) : 904237
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 500560
65 A = 6784882
91 meter
Y = -6616571
41 meter E =
0013528
Z = -1379652
17 I = 52
02542
XDOT = 4717
441593 Wp = 159
63813
YDOT = 1569
455592 meter/sec RA = 84
98610 deg
ZDOT = -5844
723789 TA = 35
32756
MA = 35
23799
Ha = 219
901 n
mi
Hp = 212
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1642259
34 X = 581213
43
Y = -21707911
43 feet Y = -6610523
02 meter
Z = -4526417
87 Z = -1377023
79
XDOT = 15477
170582 XDOT = 4727
932797
YDOT = 5149
132519 feet/sec YDOT = 1622
267038 meter/sec
ZDOT = -19175
602982 ZDOT = -5821
781801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20796229
38 X = -6338690
71
Y = 6446673
71 feet Y = 1964946
15 meter
Z = -4513993
25 Z = -1375865
14
XDOT = -493
146819 XDOT = -150
311150
YDOT = -14881
134299 feet/sec YDOT = -4535
769734 meter/sec
ZDOT = -19077
483166 ZDOT = -5814
816869
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 15095
80369955
00016717 00000-0 10270-3 0 9079
2 25544 51
6455 85
6409 0005853 185
8835 174
2251 15
55382345 16773
Satellite: ISS
Catalog Number: 25544
Epoch time: 15095
80369955 = yrday
fracday
Element set: 907
Inclination: 51
6455 deg
RA of node: 85
6409 deg
Eccentricity:
0005853
Arg of perigee: 185
8835 deg
Mean anomaly: 174
2251 deg
Mean motion: 15
55382345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1677
Checksum: 346
Coasting Arc #9 (Orbit 1692)
---------------------------------------
Vector Time (GMT): 2015/096/18:34:52
103
Vector Time (MET): N/A
Weight (LBS) : 904237
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1604357
20 A = 6780956
53 meter
Y = 5706401
86 meter E =
0012861
Z = 3288410
96 I = 52
00937
XDOT = -4479
607490 Wp = 112
99453
YDOT = -4013
246723 meter/sec RA = 80
02754 deg
ZDOT = 4759
059528 TA = 284
99628
MA = 285
13860
Ha = 219
647 n
mi
Hp = 212
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5263639
10 X = -1684022
39
Y = 18721790
87 feet Y = 5688015
81 meter
Z = 10788749
88 Z = 3280423
08
XDOT = -14696
874966 XDOT = -4457
515534
YDOT = -13166
819957 feet/sec YDOT = -4063
216584 meter/sec
ZDOT = 15613
712363 ZDOT = 4737
352254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19333677
13 X = 5892904
79
Y = -2275956
96 feet Y = -693711
68 meter
Z = 10753484
22 Z = 3277661
99
XDOT = -6631
224804 XDOT = -2021
197320
YDOT = 17310
215639 feet/sec YDOT = 5276
153727 meter/sec
ZDOT = 15521
322680 ZDOT = 4730
899153
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 15096
83166593
00016717 00000-0 10270-3 0 9087
2 25544 51
6457 80
5059 0005610 188
9212 171
1843 15
55441598 16931
Satellite: ISS
Catalog Number: 25544
Epoch time: 15096
83166593 = yrday
fracday
Element set: 908
Inclination: 51
6457 deg
RA of node: 80
5059 deg
Eccentricity:
0005610
Arg of perigee: 188
9212 deg
Mean anomaly: 171
1843 deg
Mean motion: 15
55441598 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1693
Checksum: 332
Coasting Arc #10 (Orbit 1707)
---------------------------------------
Vector Time (GMT): 2015/097/18:34:52
103
Vector Time (MET): N/A
Weight (LBS) : 904237
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2716321
05 A = 6776033
23 meter
Y = -4064457
81 meter E =
0008876
Z = -4698739
26 I = 51
98734
XDOT = 3910
464797 Wp = 102
33267
YDOT = 5931
310427 meter/sec RA = 75
05319 deg
ZDOT = -2876
433672 TA = 139
25457
MA = 139
18815
Ha = 219
438 n
mi
Hp = 212
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8911814
45 X = 2784393
94
Y = -13334835
33 feet Y = -4033701
94 meter
Z = -15415811
22 Z = -4685378
00
XDOT = 12829
608913 XDOT = 3857
821678
YDOT = 19459
679878 feet/sec YDOT = 5974
745193 meter/sec
ZDOT = -9437
118348 ZDOT = -2857
565531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15827498
33 X = -4824221
49
Y = -2917944
84 feet Y = -889389
59 meter
Z = -15357779
80 Z = -4681051
28
XDOT = 12459
840238 XDOT = 3797
759305
YDOT = -18446
443724 feet/sec YDOT = -5622
476047 meter/sec
ZDOT = -9357
257316 ZDOT = -2852
092030
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 15097
79535859
00016717 00000-0 10270-3 0 9099
2 25544 51
6459 75
6920 0005650 194
4528 165
6465 15
55504441 17083
Satellite: ISS
Catalog Number: 25544
Epoch time: 15097
79535859 = yrday
fracday
Element set: 909
Inclination: 51
6459 deg
RA of node: 75
6920 deg
Eccentricity:
0005650
Arg of perigee: 194
4528 deg
Mean anomaly: 165
6465 deg
Mean motion: 15
55504441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1708
Checksum: 346
Coasting Arc #11 (Orbit 1723)
---------------------------------------
Vector Time (GMT): 2015/098/18:34:52
103
Vector Time (MET): N/A
Weight (LBS) : 904237
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3704915
41 A = 6773324
10 meter
Y = 1975978
05 meter E =
0006532
Z = 5314500
43 I = 51
96994
XDOT = -2992
715001 Wp = 172
02179
YDOT = -7044
090090 meter/sec RA = 70
06498 deg
ZDOT = 526
355544 TA = 272
94376
MA = 273
01851
Ha = 219
360 n
mi
Hp = 212
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12155234
28 X = -3752552
09
Y = 6482867
63 feet Y = 1934281
32 meter
Z = 17436025
03 Z = 5296386
58
XDOT = -9818
618769 XDOT = -2916
280759
YDOT = -23110
531791 feet/sec YDOT = -7077
129175 meter/sec
ZDOT = 1726
888268 ZDOT = 512
003517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10999052
84 X = 3352511
31
Y = 8456575
80 feet Y = 2577564
30 meter
Z = 17357978
69 Z = 5290711
91
XDOT = -16310
376033 XDOT = -4971
402615
YDOT = 17750
075020 feet/sec YDOT = 5410
222866 meter/sec
ZDOT = 1666
610702 ZDOT = 507
982942
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 15098
82327268
00016717 00000-0 10270-3 0 9109
2 25544 51
6463 70
5574 0005707 197
3387 162
7572 15
55540312 17247
Satellite: ISS
Catalog Number: 25544
Epoch time: 15098
82327268 = yrday
fracday
Element set: 910
Inclination: 51
6463 deg
RA of node: 70
5574 deg
Eccentricity:
0005707
Arg of perigee: 197
3387 deg
Mean anomaly: 162
7572 deg
Mean motion: 15
55540312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1724
Checksum: 320
Coasting Arc #12 (Orbit 1738)
---------------------------------------
Vector Time (GMT): 2015/099/18:34:52
103
Vector Time (MET): N/A
Weight (LBS) : 904237
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4508224
10 A = 6774362
60 meter
Y = 310138
52 meter E =
0013413
Z = -5058364
83 I = 51
96156
XDOT = 1683
142789 Wp = 129
29821
YDOT = 7218
301987 meter/sec RA = 65
07155 deg
ZDOT = 1937
814919 TA = 159
46175
MA = 159
40778
Ha = 219
049 n
mi
Hp = 213
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14790761
49 X = 4528992
90
Y = 1017514
82 feet Y = 360668
22 meter
Z = -16595685
15 Z = -5036414
10
XDOT = 5522
122011 XDOT = 1592
887650
YDOT = 23682
093133 feet/sec YDOT = 7236
619470 meter/sec
ZDOT = 6357
660496 ZDOT = 1945
771691
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5511952
69 X = -1680043
18
Y = -13875677
36 feet Y = -4229306
46 meter
Z = -16501596
38 Z = -5029686
58
XDOT = 17986
147309 XDOT = 5482
177700
YDOT = -14763
616353 feet/sec YDOT = -4499
950264 meter/sec
ZDOT = 6390
463274 ZDOT = 1947
813206
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 15099
78691643
00016717 00000-0 10270-3 0 9117
2 25544 51
6458 65
7424 0005715 202
1311 157
9597 15
55590245 17391
Satellite: ISS
Catalog Number: 25544
Epoch time: 15099
78691643 = yrday
fracday
Element set: 911
Inclination: 51
6458 deg
RA of node: 65
7424 deg
Eccentricity:
0005715
Arg of perigee: 202
1311 deg
Mean anomaly: 157
9597 deg
Mean motion: 15
55590245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1739
Checksum: 332
Coasting Arc #13 (Orbit 1754)
---------------------------------------
Vector Time (GMT): 2015/100/18:34:52
103
Vector Time (MET): N/A
Weight (LBS) : 904237
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4948691
10 A = 6778415
12 meter
Y = -2438426
73 meter E =
0009087
Z = 3928598
70 I = 51
96196
XDOT = -47
691574 Wp = 110
85396
YDOT = -6495
720673 meter/sec RA = 60
08852 deg
ZDOT = -4087
434774 TA = 21
71237
MA = 21
67387
Ha = 218
894 n
mi
Hp = 212
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16235863
18 X = -4940140
03
Y = -8000087
71 feet Y = -2493718
18 meter
Z = 12889103
34 Z = 3904579
66
XDOT = -156
468419 XDOT = 44
804033
YDOT = -21311
419531 feet/sec YDOT = -6495
737066 meter/sec
ZDOT = -13410
219075 ZDOT = -4087
441395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 138906
87 X = 42338
81
Y = 18171924
03 feet Y = 5538802
45 meter
Z = 12786536
80 Z = 3897336
42
XDOT = -17707
624527 XDOT = -5397
283956
YDOT = 9580
872099 feet/sec YDOT = 2920
249816 meter/sec
ZDOT = -13409
044700 ZDOT = -4087
076824
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 15100
81477562
00016717 00000-0 10270-3 0 9127
2 25544 51
6461 60
6077 0005666 207
1069 152
9790 15
55661172 17559
Satellite: ISS
Catalog Number: 25544
Epoch time: 15100
81477562 = yrday
fracday
Element set: 912
Inclination: 51
6461 deg
RA of node: 60
6077 deg
Eccentricity:
0005666
Arg of perigee: 207
1069 deg
Mean anomaly: 152
9790 deg
Mean motion: 15
55661172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1755
Checksum: 310
Coasting Arc #14 (Orbit 1769)
---------------------------------------
Vector Time (GMT): 2015/101/18:34:52
103
Vector Time (MET): N/A
Weight (LBS) : 904237
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4924766
08 A = 6783030
17 meter
Y = 4150330
08 meter E =
0001318
Z = -2129983
99 I = 51
95947
XDOT = -1806
588524 Wp = 95
59518
YDOT = 4983
744926 meter/sec RA = 55
11926 deg
ZDOT = 5536
730842 TA = 240
90866
MA = 240
92185
Ha = 218
672 n
mi
Hp = 213
194
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16157369
02 X = 4888336
79
Y = 13616568
50 feet Y = 4205198
21 meter
Z = -6988136
46 Z = -2106149
08
XDOT = -5927
127702 XDOT = -1889
079152
YDOT = 16350
869179 feet/sec YDOT = 4963
081588 meter/sec
ZDOT = 18165
127435 ZDOT = 5527
754074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4582746
21 X = 1396821
04
Y = -20661016
75 feet Y = -6297477
91 meter
Z = -6886681
81 Z = -2099060
62
XDOT = 15786
750516 XDOT = 4811
801557
YDOT = -2536
892428 feet/sec YDOT = -773
244812 meter/sec
ZDOT = 18125
695387 ZDOT = 5524
711954
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 15101
77836987
00016717 00000-0 10270-3 0 9134
2 25544 51
6449 55
7923 0005780 210
5129 149
5689 15
55651550 17707
Satellite: ISS
Catalog Number: 25544
Epoch time: 15101
77836987 = yrday
fracday
Element set: 913
Inclination: 51
6449 deg
RA of node: 55
7923 deg
Eccentricity:
0005780
Arg of perigee: 210
5129 deg
Mean anomaly: 149
5689 deg
Mean motion: 15
55651550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1770
Checksum: 335
Coasting Arc #15 (Orbit 1785)
---------------------------------------
Vector Time (GMT): 2015/102/18:34:52
103
Vector Time (MET): N/A
Weight (LBS) : 904237
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4299486
83 A = 6784810
91 meter
Y = -5236507
99 meter E =
0014372
Z = -67934
81 I = 51
94677
XDOT = 3692
276416 Wp = 158
51590
YDOT = -2958
569453 meter/sec RA = 50
16225 deg
ZDOT = -6043
136893 TA = 22
21364
MA = 22
15144
Ha = 218
569 n
mi
Hp = 213
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14105927
94 X = -4240281
41
Y = -17180144
33 feet Y = -5284256
63 meter
Z = -222883
24 Z = -88676
75
XDOT = 12113
767768 XDOT = 3754
440786
YDOT = -9706
592692 feet/sec YDOT = -2916
932858 meter/sec
ZDOT = -19826
564611 ZDOT = -6025
049289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8359701
61 X = -2548037
05
Y = 20596188
78 feet Y = 6277718
34 meter
Z = -310862
98 Z = -94751
04
XDOT = -12872
621269 XDOT = -3923
574963
YDOT = -5508
135154 feet/sec YDOT = -1678
879595 meter/sec
ZDOT = -19748
430443 ZDOT = -6019
321599
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 15102
80617603
00016717 00000-0 10270-3 0 9142
2 25544 51
6447 50
6570 0005868 213
1768 146
9018 15
55684237 17864
Satellite: ISS
Catalog Number: 25544
Epoch time: 15102
80617603 = yrday
fracday
Element set: 914
Inclination: 51
6447 deg
RA of node: 50
6570 deg
Eccentricity:
0005868
Arg of perigee: 213
1768 deg
Mean anomaly: 146
9018 deg
Mean motion: 15
55684237 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1786
Checksum: 320
Coasting Arc #16 (Orbit 1801)
---------------------------------------
Vector Time (GMT): 2015/103/18:34:52
103
Vector Time (MET): N/A
Weight (LBS) : 904237
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3086304
25 A = 6782397
93 meter
Y = 5604012
45 meter E =
0009542
Z = 2244372
32 I = 51
91765
XDOT = -5320
830808 Wp = 92
49291
YDOT = 729
704010 meter/sec RA = 45
20122 deg
ZDOT = 5474
391668 TA = 292
37692
MA = 292
47800
Ha = 218
289 n
mi
Hp = 213
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10125670
13 X = 3012507
13
Y = 18385867
62 feet Y = 5638113
09 meter
Z = 7363426
24 Z = 2259185
28
XDOT = -17456
793990 XDOT = -5355
187668
YDOT = 2394
042028 feet/sec YDOT = 670
011371 meter/sec
ZDOT = 17960
602586 ZDOT = 5448
460551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11036868
60 X = 3364037
55
Y = -17827868
46 feet Y = -5433934
31 meter
Z = 7425901
12 Z = 2263414
66
XDOT = 9439
438704 XDOT = 2877
140917
YDOT = 13306
257871 feet/sec YDOT = 4055
747399 meter/sec
ZDOT = 17849
247246 ZDOT = 5440
450561
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 15103
83395165
00016717 00000-0 10270-3 0 9153
2 25544 51
6438 45
5196 0006005 217
7128 142
3605 15
55766529 18021
Satellite: ISS
Catalog Number: 25544
Epoch time: 15103
83395165 = yrday
fracday
Element set: 915
Inclination: 51
6438 deg
RA of node: 45
5196 deg
Eccentricity:
0006005
Arg of perigee: 217
7128 deg
Mean anomaly: 142
3605 deg
Mean motion: 15
55766529 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1802
Checksum: 308
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