[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 29th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14531 28 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 132 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 186 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 634)
---------------------------------------
Vector Time (GMT): 2015/028/19:29:22
676
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 306385
94 A = 6782781
32 meter
Y = -5518511
41 meter E =
0005357
Z = -3936697
56 I = 51
95825
XDOT = 5627
176359 Wp = 10
32979
YDOT = 3225
865833 meter/sec RA = 59
30719 deg
ZDOT = -4079
834261 TA = 217
11601
MA = 217
15307
Ha = 220
112 n
mi
Hp = 216
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1005203
21 X = 387195
26
Y = -18105352
40 feet Y = -5514633
35 meter
Z = -12915674
41 Z = -3935012
97
XDOT = 18461
864696 XDOT = 5610
503845
YDOT = 10583
549321 feet/sec YDOT = 3288
699384 meter/sec
ZDOT = -13385
283010 ZDOT = -4052
539293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15005679
76 X = -4573731
19
Y = -10191038
87 feet Y = -3106228
65 meter
Z = -12907407
42 Z = -3934177
78
XDOT = 17833
368667 XDOT = 5435
610770
YDOT = -9434
903336 feet/sec YDOT = -2875
758537 meter/sec
ZDOT = -13269
074081 ZDOT = -4044
413780
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 15028
83571020
00016717 00000-0 10270-3 0 9009
2 25544 51
6456 59
8551 0006351 302
3258 57
7280 15
54125802 6356
Satellite: ISS
Catalog Number: 25544
Epoch time: 15028
83571020 = yrday
fracday
Element set: 900
Inclination: 51
6456 deg
RA of node: 59
8551 deg
Eccentricity:
0006351
Arg of perigee: 302
3258 deg
Mean anomaly: 57
7280 deg
Mean motion: 15
54125802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 635
Checksum: 289
Coasting Arc #2 (Orbit 650)
---------------------------------------
Vector Time (GMT): 2015/029/19:29:22
676
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1494882
43 A = 6779237
21 meter
Y = 4466440
34 meter E =
0000821
Z = 4875140
21 I = 51
92938
XDOT = -5647
010650 Wp = 80
54928
YDOT = -4570
401892 meter/sec RA = 54
33657 deg
ZDOT = 2455
465486 TA = 345
44989
MA = 345
45225
Ha = 220
301 n
mi
Hp = 216
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4904469
91 X = -1568397
40
Y = 14653675
64 feet Y = 4449312
48 meter
Z = 15994554
48 Z = 4867699
95
XDOT = -18526
937829 XDOT = -5607
411219
YDOT = -14994
756863 feet/sec YDOT = -4633
329058 meter/sec
ZDOT = 8055
989126 ZDOT = 2428
129887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10237411
13 X = 3120362
91
Y = 11620011
95 feet Y = 3541779
64 meter
Z = 15961846
50 Z = 4865170
81
XDOT = -21390
652704 XDOT = -6519
870944
YDOT = 7937
891466 feet/sec YDOT = 2419
469319 meter/sec
ZDOT = 7939
869298 ZDOT = 2420
072162
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 15029
86454626
00016717 00000-0 10270-3 0 9016
2 25544 51
6454 54
7262 0006344 305
5243 54
5318 15
54144728 6511
Satellite: ISS
Catalog Number: 25544
Epoch time: 15029
86454626 = yrday
fracday
Element set: 901
Inclination: 51
6454 deg
RA of node: 54
7262 deg
Eccentricity:
0006344
Arg of perigee: 305
5243 deg
Mean anomaly: 54
5318 deg
Mean motion: 15
54144728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 651
Checksum: 301
Coasting Arc #3 (Orbit 665)
---------------------------------------
Vector Time (GMT): 2015/030/19:29:22
676
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2742296
16 A = 6777308
03 meter
Y = -3202591
98 meter E =
0011087
Z = -5314997
17 I = 51
90463
XDOT = 5306
623369 Wp = 61
98061
YDOT = 5496
266971 meter/sec RA = 49
35696 deg
ZDOT = -569
675873 TA = 202
57326
MA = 202
62207
Ha = 220
398 n
mi
Hp = 216
414
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8997034
64 X = 2803722
32
Y = -10507191
55 feet Y = -3171582
31 meter
Z = -17437654
76 Z = -5301526
70
XDOT = 17410
181658 XDOT = 5247
535648
YDOT = 18032
371953 feet/sec YDOT = 5555
278716 meter/sec
ZDOT = -1869
015331 ZDOT = -544
041189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4827004
79 X = -1471271
06
Y = -13041351
30 feet Y = -3975003
88 meter
Z = -17379375
45 Z = -5297233
64
XDOT = 23240
899761 XDOT = 7083
826247
YDOT = -6237
976412 feet/sec YDOT = -1901
335210 meter/sec
ZDOT = -1760
360036 ZDOT = -536
557739
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 15030
82906540
00016717 00000-0 10270-3 0 9022
2 25544 51
6460 49
9179 0006363 310
0097 50
0497 15
54176804 6665
Satellite: ISS
Catalog Number: 25544
Epoch time: 15030
82906540 = yrday
fracday
Element set: 902
Inclination: 51
6460 deg
RA of node: 49
9179 deg
Eccentricity:
0006363
Arg of perigee: 310
0097 deg
Mean anomaly: 50
0497 deg
Mean motion: 15
54176804 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 666
Checksum: 301
Coasting Arc #4 (Orbit 681)
---------------------------------------
Vector Time (GMT): 2015/031/19:29:22
676
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3967626
05 A = 6777746
47 meter
Y = 1813874
96 meter E =
0007118
Z = 5189437
71 I = 51
88490
XDOT = -4569
409132 Wp = 351
22361
YDOT = -5997
071471 meter/sec RA = 44
37369 deg
ZDOT = -1390
804016 TA = 112
14493
MA = 112
06937
Ha = 220
546 n
mi
Hp = 216
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13017145
82 X = -4012822
18
Y = 5951033
34 feet Y = 1769253
63 meter
Z = 17025714
29 Z = 5170054
38
XDOT = -14991
499776 XDOT = -4495
252992
YDOT = -19675
431334 feet/sec YDOT = -6047
754931 meter/sec
ZDOT = -4563
005301 ZDOT = -1412
820821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -853131
77 X = -260034
56
Y = 14386218
52 feet Y = 4384919
40 meter
Z = 16942393
96 Z = 5164041
68
XDOT = -23333
329723 XDOT = -7111
998900
YDOT = 4125
308129 feet/sec YDOT = 1257
393918 meter/sec
ZDOT = -4656
072980 ZDOT = -1419
171044
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 15031
85786828
00016717 00000-0 10270-3 0 9032
2 25544 51
6456 44
7888 0006506 313
2851 46
7758 15
54222138 6824
Satellite: ISS
Catalog Number: 25544
Epoch time: 15031
85786828 = yrday
fracday
Element set: 903
Inclination: 51
6456 deg
RA of node: 44
7888 deg
Eccentricity:
0006506
Arg of perigee: 313
2851 deg
Mean anomaly: 46
7758 deg
Mean motion: 15
54222138 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 682
Checksum: 330
Coasting Arc #5 (Orbit 696)
---------------------------------------
Vector Time (GMT): 2015/032/19:29:22
676
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5033660
92 A = 6780532
00 meter
Y = -459789
84 meter E =
0004741
Z = -4522672
39 I = 51
87128
XDOT = 3425
763900 Wp = 72
18347
YDOT = 6063
910071 meter/sec RA = 39
39328 deg
ZDOT = 3200
510094 TA = 229
85659
MA = 229
89813
Ha = 220
733 n
mi
Hp = 216
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16514635
57 X = 5060397
24
Y = -1508496
85 feet Y = -403350
68 meter
Z = -14838164
01 Z = -4498155
46
XDOT = 11239
382874 XDOT = 3342
154697
YDOT = 19894
718081 feet/sec YDOT = 6101
751708 meter/sec
ZDOT = 10500
361200 ZDOT = 3216
948334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6141816
46 X = 1872025
66
Y = -15504602
41 feet Y = -4725802
81 meter
Z = -14733134
66 Z = -4490659
44
XDOT = 21665
557817 XDOT = 6603
662023
YDOT = -1448
189463 feet/sec YDOT = -441
408148 meter/sec
ZDOT = 10569
534187 ZDOT = 3221
594020
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 15032
82235751
00016717 00000-0 10270-3 0 9045
2 25544 51
6460 39
9800 0006478 317
2385 42
8263 15
54213354 6977
Satellite: ISS
Catalog Number: 25544
Epoch time: 15032
82235751 = yrday
fracday
Element set: 904
Inclination: 51
6460 deg
RA of node: 39
9800 deg
Eccentricity:
0006478
Arg of perigee: 317
2385 deg
Mean anomaly: 42
8263 deg
Mean motion: 15
54213354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 697
Checksum: 306
Coasting Arc #6 (Orbit 712)
---------------------------------------
Vector Time (GMT): 2015/033/19:29:22
676
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5841131
56 A = 6784360
12 meter
Y = -812151
40 meter E =
0009810
Z = 3351586
49 I = 51
85909
XDOT = -1897
065584 Wp = 61
23255
YDOT = -5762
111800 meter/sec RA = 34
42081 deg
ZDOT = -4687
484765 TA = 79
84750
MA = 79
73686
Ha = 220
787 n
mi
Hp = 215
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19163817
47 X = -5847896
13
Y = -2664538
71 feet Y = -877508
50 meter
Z = 10996018
68 Z = 3323195
69
XDOT = -6223
968450 XDOT = -1809
721813
YDOT = -18904
566273 feet/sec YDOT = -5782
837729 meter/sec
ZDOT = -15378
887024 ZDOT = -4696
487879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10774158
52 X = -3283963
52
Y = 16153123
25 feet Y = 4923471
97 meter
Z = 10874659
10 Z = 3314596
10
XDOT = -18509
014423 XDOT = -5641
547596
YDOT = -1933
478523 feet/sec YDOT = -589
324254 meter/sec
ZDOT = -15416
292303 ZDOT = -4698
885894
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 15033
85112897
00016717 00000-0 10270-3 0 9055
2 25544 51
6458 34
8506 0006419 321
8212 38
2485 15
54236417 7135
Satellite: ISS
Catalog Number: 25544
Epoch time: 15033
85112897 = yrday
fracday
Element set: 905
Inclination: 51
6458 deg
RA of node: 34
8506 deg
Eccentricity:
0006419
Arg of perigee: 321
8212 deg
Mean anomaly: 38
2485 deg
Mean motion: 15
54236417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 713
Checksum: 304
Coasting Arc #7 (Orbit 727)
---------------------------------------
Vector Time (GMT): 2015/034/19:29:22
676
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6252504
33 A = 6787555
97 meter
Y = 1878867
94 meter E =
0011132
Z = -1831178
80 I = 51
84400
XDOT = 102
031196 Wp = 3
82316
YDOT = 5170
180981 meter/sec RA = 29
45611 deg
ZDOT = 5666
013019 TA = 336
09010
MA = 336
14176
Ha = 220
924 n
mi
Hp = 215
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20513465
65 X = 6239924
65
Y = 6164264
90 feet Y = 1948717
12 meter
Z = -6007804
45 Z = -1800836
72
XDOT = 334
748017 XDOT = 16
686754
YDOT = 16962
536028 feet/sec YDOT = 5170
844963 meter/sec
ZDOT = 18589
281559 ZDOT = 5666
301192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14224784
84 X = 4335714
42
Y = -16062227
83 feet Y = -4895767
04 meter
Z = -5878306
09 Z = -1791707
69
XDOT = 14315
473245 XDOT = 4363
356245
YDOT = 5890
348147 feet/sec YDOT = 1795
378115 meter/sec
ZDOT = 18589
500492 ZDOT = 5666
079750
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 15034
81558525
00016717 00000-0 10270-3 0 9065
2 25544 51
6463 30
0411 0006527 324
6544 35
4175 15
54269564 7283
Satellite: ISS
Catalog Number: 25544
Epoch time: 15034
81558525 = yrday
fracday
Element set: 906
Inclination: 51
6463 deg
RA of node: 30
0411 deg
Eccentricity:
0006527
Arg of perigee: 324
6544 deg
Mean anomaly: 35
4175 deg
Mean motion: 15
54269564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 728
Checksum: 302
Coasting Arc #8 (Orbit 743)
---------------------------------------
Vector Time (GMT): 2015/035/19:29:22
676
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6201863
84 A = 6788969
96 meter
Y = -2755209
14 meter E =
0006184
Z = 81948
65 I = 51
82070
XDOT = 1853
465372 Wp = 119
79764
YDOT = -4361
299413 meter/sec RA = 24
49748 deg
ZDOT = -6024
433972 TA = 59
32223
MA = 59
26129
Ha = 220
934 n
mi
Hp = 215
491
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20347322
32 X = -6170991
58
Y = -9039400
05 feet Y = -2824389
79 meter
Z = 268860
40 Z = 51897
06
XDOT = 6080
923135 XDOT = 1931
360424
YDOT = -14308
725107 feet/sec YDOT = -4340
137529 meter/sec
ZDOT = -19765
203320 ZDOT = -6015
240999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16494664
02 X = -5027573
59
Y = 14956697
62 feet Y = 4558801
44 meter
Z = 140782
62 Z = 42910
54
XDOT = -9488
972481 XDOT = -2892
238812
YDOT = -10259
134216 feet/sec YDOT = -3126
984109 meter/sec
ZDOT = -19725
002526 ZDOT = -6012
180770
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 15035
84432345
00016717 00000-0 10270-3 0 9071
2 25544 51
6463 24
9118 0006361 327
5989 32
4773 15
54250418 7447
Satellite: ISS
Catalog Number: 25544
Epoch time: 15035
84432345 = yrday
fracday
Element set: 907
Inclination: 51
6463 deg
RA of node: 24
9118 deg
Eccentricity:
0006361
Arg of perigee: 327
5989 deg
Mean anomaly: 32
4773 deg
Mean motion: 15
54250418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 744
Checksum: 312
Coasting Arc #9 (Orbit 759)
---------------------------------------
Vector Time (GMT): 2015/036/19:29:22
676
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5630659
24 A = 6787548
50 meter
Y = 3386868
11 meter E =
0015127
Z = 1662712
87 I = 51
78744
XDOT = -3769
389267 Wp = 38
07668
YDOT = 3446
981206 meter/sec RA = 19
53589 deg
ZDOT = 5727
358862 TA = 340
11610
MA = 340
17499
Ha = 220
986 n
mi
Hp = 215
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18473291
47 X = 5584291
35
Y = 11111772
00 feet Y = 3449574
66 meter
Z = 5455094
70 Z = 1689952
05
XDOT = -12366
762686 XDOT = -3835
474811
YDOT = 11308
993458 feet/sec YDOT = 3404
460316 meter/sec
ZDOT = 18790
547446 ZDOT = 5708
887575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17402842
43 X = 5304386
37
Y = -12672687
34 feet Y = -3862635
10 meter
Z = 5571005
64 Z = 1698042
52
XDOT = 4647
277798 XDOT = 1416
490273
YDOT = 14630
011950 feet/sec YDOT = 4459
227642 meter/sec
ZDOT = 18710
820236 ZDOT = 5703
058008
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 15036
87304156
00016717 00000-0 10270-3 0 9084
2 25544 51
6461 19
7813 0006594 331
7302 28
3493 15
54322013 7605
Satellite: ISS
Catalog Number: 25544
Epoch time: 15036
87304156 = yrday
fracday
Element set: 908
Inclination: 51
6461 deg
RA of node: 19
7813 deg
Eccentricity:
0006594
Arg of perigee: 331
7302 deg
Mean anomaly: 28
3493 deg
Mean motion: 15
54322013 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 760
Checksum: 293
Coasting Arc #10 (Orbit 774)
---------------------------------------
Vector Time (GMT): 2015/037/19:29:22
676
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4567389
77 A = 6784217
15 meter
Y = -3831125
53 meter E =
0005657
Z = -3245920
10 I = 51
74599
XDOT = 5462
552383 Wp = 17
59567
YDOT = -2467
310436 meter/sec RA = 14
56670 deg
ZDOT = -4771
221160 TA = 199
91842
MA = 199
94051
Ha = 221
105 n
mi
Hp = 214
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14984874
56 X = -4508442
61
Y = -12569309
48 feet Y = -3881871
72 meter
Z = -10649344
18 Z = -3267963
68
XDOT = 17921
759786 XDOT = 5512
912788
YDOT = -8094
850512 feet/sec YDOT = -2405
943406 meter/sec
ZDOT = -15653
612729 ZDOT = -4744
563163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17223261
30 X = -5249650
05
Y = 9159221
21 feet Y = 2791730
62 meter
Z = -10742926
73 Z = -3274444
07
XDOT = -130
817831 XDOT = -39
873275
YDOT = -18483
656863 feet/sec YDOT = -5633
818612 meter/sec
ZDOT = -15539
048629 ZDOT = -4736
302022
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 15037
83745015
00016717 00000-0 10270-3 0 9095
2 25544 51
6457 14
9725 0006564 334
3284 25
7542 15
54324557 7751
Satellite: ISS
Catalog Number: 25544
Epoch time: 15037
83745015 = yrday
fracday
Element set: 909
Inclination: 51
6457 deg
RA of node: 14
9725 deg
Eccentricity:
0006564
Arg of perigee: 334
3284 deg
Mean anomaly: 25
7542 deg
Mean motion: 15
54324557 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 775
Checksum: 320
Coasting Arc #11 (Orbit 790)
---------------------------------------
Vector Time (GMT): 2015/038/19:29:22
676
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3062963
99 A = 6780219
09 meter
Y = 4084688
50 meter E =
0006788
Z = 4454556
70 I = 51
70196
XDOT = -6770
323366 Wp = 64
30834
YDOT = 1490
093207 meter/sec RA = 9
58343 deg
ZDOT = 3287
901331 TA = 352
59113
MA = 352
60115
Ha = 221
232 n
mi
Hp = 214
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10049094
44 X = 2995422
19
Y = 13401208
99 feet Y = 4118563
28 meter
Z = 14614687
32 Z = 4469271
34
XDOT = -22212
347001 XDOT = -6802
453882
YDOT = 4888
757241 feet/sec YDOT = 1414
203662 meter/sec
ZDOT = 10787
077858 ZDOT = 3254
934806
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16071753
16 X = 4898670
36
Y = -4522669
65 feet Y = -1378509
71 meter
Z = 14676852
42 Z = 4473504
62
XDOT = -3706
332223 XDOT = -1129
690062
YDOT = 21387
219235 feet/sec YDOT = 6518
824423 meter/sec
ZDOT = 10645
718449 ZDOT = 3244
814983
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 15038
86613604
00016717 00000-0 10270-3 0 9109
2 25544 51
6457 9
8419 0006614 339
8984 20
1907 15
54337323 7914
Satellite: ISS
Catalog Number: 25544
Epoch time: 15038
86613604 = yrday
fracday
Element set: 910
Inclination: 51
6457 deg
RA of node: 9
8419 deg
Eccentricity:
0006614
Arg of perigee: 339
8984 deg
Mean anomaly: 20
1907 deg
Mean motion: 15
54337323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 791
Checksum: 317
Coasting Arc #12 (Orbit 805)
---------------------------------------
Vector Time (GMT): 2015/039/19:29:22
676
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1274151
91 A = 6777193
15 meter
Y = -4205435
65 meter E =
0014597
Z = -5171453
69 I = 51
65993
XDOT = 7508
140050 Wp = 52
50708
YDOT = -523
060276 meter/sec RA = 4
58787 deg
ZDOT = -1418
587092 TA = 203
79976
MA = 203
86733
Ha = 221
241 n
mi
Hp = 214
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4180288
42 X = -1201910
40
Y = -13797361
05 feet Y = -4219280
55 meter
Z = -16966711
57 Z = -5177467
37
XDOT = 24633
005413 XDOT = 7520
321884
YDOT = -1716
077020 feet/sec YDOT = -439
031368 meter/sec
ZDOT = -4654
157125 ZDOT = -1382
084878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14361119
22 X = -4377269
14
Y = -868581
61 feet Y = -264743
68 meter
Z = -16991618
68 Z = -5179045
37
XDOT = 6719
203475 XDOT = 2048
013219
YDOT = -22725
809221 feet/sec YDOT = -6926
826651 meter/sec
ZDOT = -4497
868739 ZDOT = -1370
950392
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 15039
83050998
00016717 00000-0 10270-3 0 9119
2 25544 51
6446 5
0322 0006580 342
2505 17
8417 15
54399479 8068
Satellite: ISS
Catalog Number: 25544
Epoch time: 15039
83050998 = yrday
fracday
Element set: 911
Inclination: 51
6446 deg
RA of node: 5
0322 deg
Eccentricity:
0006580
Arg of perigee: 342
2505 deg
Mean anomaly: 17
8417 deg
Mean motion: 15
54399479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 806
Checksum: 311
Coasting Arc #13 (Orbit 821)
---------------------------------------
Vector Time (GMT): 2015/040/19:29:22
676
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -680806
24 A = 6776679
14 meter
Y = 4188522
36 meter E =
0007712
Z = 5283367
72 I = 51
62707
XDOT = -7631
231305 Wp = 7
75049
YDOT = -440
730871 meter/sec RA = 359
58517 deg
ZDOT = -626
365408 TA = 88
27309
MA = 88
18477
Ha = 221
367 n
mi
Hp = 214
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2233616
28 X = -753257
02
Y = 13741871
26 feet Y = 4180504
46 meter
Z = 17333883
61 Z = 5279884
23
XDOT = -25036
848113 XDOT = -7622
693166
YDOT = -1445
967424 feet/sec YDOT = -526
020581 meter/sec
ZDOT = -2055
004619 ZDOT = -663
415257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12241125
79 X = 3731095
14
Y = 6672917
30 feet Y = 2033905
19 meter
Z = 17318158
17 Z = 5278574
61
XDOT = -8994
955535 XDOT = -2741
662447
YDOT = 22309
916601 feet/sec YDOT = 6800
062580 meter/sec
ZDOT = -2213
436520 ZDOT = -674
655451
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 15040
85915968
00016717 00000-0 10270-3 0 9121
2 25544 51
6450 359
9023 0006497 345
8883 14
2087 15
54409996 8225
Satellite: ISS
Catalog Number: 25544
Epoch time: 15040
85915968 = yrday
fracday
Element set: 912
Inclination: 51
6450 deg
RA of node: 359
9023 deg
Eccentricity:
0006497
Arg of perigee: 345
8883 deg
Mean anomaly: 14
2087 deg
Mean motion: 15
54409996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 822
Checksum: 340
Coasting Arc #14 (Orbit 836)
---------------------------------------
Vector Time (GMT): 2015/041/19:29:22
676
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2550769
64 A = 6778700
20 meter
Y = -4061397
88 meter E =
0009918
Z = -4797602
69 I = 51
60121
XDOT = 7075
670338 Wp = 73
40304
YDOT = 1391
625793 meter/sec RA = 354
58126 deg
ZDOT = 2591
098665 TA = 222
11992
MA = 222
19619
Ha = 221
385 n
mi
Hp = 214
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8368666
81 X = 2619300
31
Y = -13324796
21 feet Y = -4032490
68 meter
Z = -15740166
29 Z = -4785044
92
XDOT = 23214
141530 XDOT = 7046
996506
YDOT = 4565
701420 feet/sec YDOT = 1470
590407 meter/sec
ZDOT = 8500
979873 ZDOT = 2625
400823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10071202
04 X = -3069702
38
Y = -12160142
51 feet Y = -3706411
44 meter
Z = -15685644
28 Z = -4780984
38
XDOT = 10589
198855 XDOT = 3227
587811
YDOT = -19894
050149 feet/sec YDOT = -6063
706486 meter/sec
ZDOT = 8647
460288 ZDOT = 2635
745896
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 15041
82350134
00016717 00000-0 10270-3 0 9138
2 25544 51
6436 355
0916 0006446 349
5537 10
5481 15
54452579 8376
Satellite: ISS
Catalog Number: 25544
Epoch time: 15041
82350134 = yrday
fracday
Element set: 913
Inclination: 51
6436 deg
RA of node: 355
0916 deg
Eccentricity:
0006446
Arg of perigee: 349
5537 deg
Mean anomaly: 10
5481 deg
Mean motion: 15
54452579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 837
Checksum: 308
Coasting Arc #15 (Orbit 852)
---------------------------------------
Vector Time (GMT): 2015/042/19:29:22
676
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4225179
00 A = 6782464
67 meter
Y = 3778132
18 meter E =
0013140
Z = 3722372
25 I = 51
58324
XDOT = -5904
367823 Wp = 54
66116
YDOT = -2367
018121 meter/sec RA = 349
58522 deg
ZDOT = -4281
318367 TA = 80
86265
MA = 80
71400
Ha = 221
424 n
mi
Hp = 214
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13862135
83 X = -4285194
66
Y = 12395446
80 feet Y = 3730548
13 meter
Z = 12212507
38 Z = 3701701
35
XDOT = -19371
285509 XDOT = -5856
663596
YDOT = -7765
807485 feet/sec YDOT = -2432
778134 meter/sec
ZDOT = -14046
320103 ZDOT = -4309
884363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7794753
63 X = 2375840
91
Y = 16947501
54 feet Y = 5165598
47 meter
Z = 12123335
14 Z = 3695192
55
XDOT = -11814
720861 XDOT = -3601
126919
YDOT = 15611
915106 feet/sec YDOT = 4758
511724 meter/sec
ZDOT = -14168
062298 ZDOT = -4318
425388
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 15042
85211351
00016717 00000-0 10270-3 0 9140
2 25544 51
6440 349
9613 0006523 351
9183 8
1864 15
54498732 8534
Satellite: ISS
Catalog Number: 25544
Epoch time: 15042
85211351 = yrday
fracday
Element set: 914
Inclination: 51
6440 deg
RA of node: 349
9613 deg
Eccentricity:
0006523
Arg of perigee: 351
9183 deg
Mean anomaly: 8
1864 deg
Mean motion: 15
54498732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 853
Checksum: 308
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