[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 4th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18567 75 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 708)
---------------------------------------
Vector Time (GMT): 2015/033/13:42:43
548
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1328966
58 A = 6781170
57 meter
Y = -5094116
90 meter E =
0008653
Z = -4282418
61 I = 51
85217
XDOT = 6641
266440 Wp = 26
51185
YDOT = 1292
320541 meter/sec RA = 35
66775 deg
ZDOT = -3593
511337 TA = 206
84877
MA = 206
89358
Ha = 220
640 n
mi
Hp = 215
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4360126
56 X = -1251102
31
Y = -16712981
96 feet Y = -5108542
96 meter
Z = -14049929
81 Z = -4288685
13
XDOT = 21788
931891 XDOT = 6643
777329
YDOT = 4239
896789 feet/sec YDOT = 1366
601501 meter/sec
ZDOT = -11789
735358 ZDOT = -3561
244050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2515586
29 X = 766750
70
Y = -17066926
78 feet Y = -5201999
28 meter
Z = -14075753
39 Z = -4290289
63
XDOT = 17285
172588 XDOT = 5268
520605
YDOT = 12170
331392 feet/sec YDOT = 3709
517008 meter/sec
ZDOT = -11651
876961 ZDOT = -3551
492098
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
59389726
00016717 00000-0 10270-3 0 9008
2 25544 51
6430 36
1343 0006223 320
6762 39
3938 15
54254475 7093
Satellite: ISS
Catalog Number: 25544
Epoch time: 15033
59389726 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 36
1343 deg
Eccentricity:
0006223
Arg of perigee: 320
6762 deg
Mean anomaly: 39
3938 deg
Mean motion: 15
54254475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 709
Checksum: 305
Coasting Arc #2 (Orbit 724)
---------------------------------------
Vector Time (GMT): 2015/034/13:42:43
548
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -287573
10 A = 6777872
24 meter
Y = 4475806
46 meter E =
0002156
Z = 5080663
78 I = 51
81555
XDOT = -7018
041715 Wp = 15
76386
YDOT = -2506
700657 meter/sec RA = 30
68580 deg
ZDOT = 1812
888717 TA = 56
74566
MA = 56
72500
Ha = 220
752 n
mi
Hp = 215
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -943481
29 X = -362280
59
Y = 14684404
39 feet Y = 4472173
06 meter
Z = 16668844
43 Z = 5079085
26
XDOT = -23025
071243 XDOT = -6998
295720
YDOT = -8224
083520 feet/sec YDOT = -2585
070508 meter/sec
ZDOT = 5947
797629 ZDOT = 1778
845323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6412491
79 X = -1954527
50
Y = 13253538
84 feet Y = 4039678
64 meter
Z = 16661210
07 Z = 5078336
83
XDOT = -17411
393457 XDOT = -5306
992726
YDOT = -15711
089818 feet/sec YDOT = -4788
740177 meter/sec
ZDOT = 5802
579173 ZDOT = 1768
626132
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
62263056
00016717 00000-0 10270-3 0 9011
2 25544 51
6431 31
0050 0006359 323
7064 36
3657 15
54302650 7254
Satellite: ISS
Catalog Number: 25544
Epoch time: 15034
62263056 = yrday
fracday
Element set: 901
Inclination: 51
6431 deg
RA of node: 31
0050 deg
Eccentricity:
0006359
Arg of perigee: 323
7064 deg
Mean anomaly: 36
3657 deg
Mean motion: 15
54302650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 725
Checksum: 269
Coasting Arc #3 (Orbit 739)
---------------------------------------
Vector Time (GMT): 2015/035/13:42:43
548
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1992765
11 A = 6776822
91 meter
Y = -3696843
59 meter E =
0012509
Z = -5328373
02 I = 51
78481
XDOT = 6840
728377 Wp = 66
43566
YDOT = 3443
734518 meter/sec RA = 25
69471 deg
ZDOT = 174
297444 TA = 205
19322
MA = 205
25429
Ha = 220
851 n
mi
Hp = 215
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6537943
29 X = 2059838
58
Y = -12128751
94 feet Y = -3674184
42 meter
Z = -17481538
79 Z = -5318529
71
XDOT = 22443
334569 XDOT = 6800
864662
YDOT = 11298
341595 feet/sec YDOT = 3520
009114 meter/sec
ZDOT = 571
842008 ZDOT = 207
430565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10514603
14 X = 3204851
04
Y = -8988377
30 feet Y = -2739657
40 meter
Z = -17438684
55 Z = -5315311
05
XDOT = 16326
094207 XDOT = 4976
193514
YDOT = 17748
172144 feet/sec YDOT = 5409
642869 meter/sec
ZDOT = 712
974989 ZDOT = 217
314777
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
58704859
00016717 00000-0 10270-3 0 9029
2 25544 51
6435 26
1953 0006313 328
0067 32
0702 15
54315967 7402
Satellite: ISS
Catalog Number: 25544
Epoch time: 15035
58704859 = yrday
fracday
Element set: 902
Inclination: 51
6435 deg
RA of node: 26
1953 deg
Eccentricity:
0006313
Arg of perigee: 328
0067 deg
Mean anomaly: 32
0702 deg
Mean motion: 15
54315967 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 740
Checksum: 295
Coasting Arc #4 (Orbit 755)
---------------------------------------
Vector Time (GMT): 2015/036/13:42:43
548
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3668429
75 A = 6778301
89 meter
Y = 2797750
67 meter E =
0009320
Z = 4966928
46 I = 51
76177
XDOT = -6090
146396 Wp = 14
50369
YDOT = -4125
167780 meter/sec RA = 20
70282 deg
ZDOT = -2164
709198 TA = 96
61494
MA = 96
50884
Ha = 220
988 n
mi
Hp = 215
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12035530
68 X = -3723569
13
Y = 9178972
01 feet Y = 2756419
91 meter
Z = 16295697
04 Z = 4948974
25
XDOT = -19980
795264 XDOT = -6033
050066
YDOT = -13534
015026 feet/sec YDOT = -4192
952656 meter/sec
ZDOT = -7102
064299 ZDOT = -2194
154321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14527659
89 X = -4428030
73
Y = 4535506
35 feet Y = 1382422
34 meter
Z = 16218309
04 Z = 4943340
60
XDOT = -13854
267057 XDOT = -4222
780599
YDOT = -18418
647821 feet/sec YDOT = -5614
003856 meter/sec
ZDOT = -7227
272842 ZDOT = -2202
872762
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
61573905
00016717 00000-0 10270-3 0 9031
2 25544 51
6441 21
0657 0006343 331
7000 28
3807 15
54355761 7562
Satellite: ISS
Catalog Number: 25544
Epoch time: 15036
61573905 = yrday
fracday
Element set: 903
Inclination: 51
6441 deg
RA of node: 21
0657 deg
Eccentricity:
0006343
Arg of perigee: 331
7000 deg
Mean anomaly: 28
3807 deg
Mean motion: 15
54355761 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 756
Checksum: 287
Coasting Arc #5 (Orbit 770)
---------------------------------------
Vector Time (GMT): 2015/037/13:42:43
548
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5098022
72 A = 6781742
93 meter
Y = -1887350
93 meter E =
0005414
Z = -4055374
39 I = 51
74386
XDOT = 4782
716209 Wp = 47
30305
YDOT = 4544
089915 meter/sec RA = 15
71616 deg
ZDOT = 3904
460329 TA = 263
10292
MA = 263
16451
Ha = 221
100 n
mi
Hp = 215
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16725796
34 X = 5138447
72
Y = -6192096
21 feet Y = -1830115
79 meter
Z = -13305034
08 Z = -4030511
37
XDOT = 15691
326144 XDOT = 4712
581650
YDOT = 14908
431479 feet/sec YDOT = 4597
181512 meter/sec
ZDOT = 12809
909217 ZDOT = 3927
522666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17908626
29 X = 5458549
29
Y = -452986
83 feet Y = -138070
39 meter
Z = -13198263
45 Z = -4022830
70
XDOT = 9947
020705 XDOT = 3031
851911
YDOT = 17834
675399 feet/sec YDOT = 5436
009062 meter/sec
ZDOT = 12907
713152 ZDOT = 3934
270969
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
58011520
00016717 00000-0 10270-3 0 9049
2 25544 51
6443 16
2565 0006404 335
1475 24
9369 15
54376209 7712
Satellite: ISS
Catalog Number: 25544
Epoch time: 15037
58011520 = yrday
fracday
Element set: 904
Inclination: 51
6443 deg
RA of node: 16
2565 deg
Eccentricity:
0006404
Arg of perigee: 335
1475 deg
Mean anomaly: 24
9369 deg
Mean motion: 15
54376209 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 771
Checksum: 295
Coasting Arc #6 (Orbit 786)
---------------------------------------
Vector Time (GMT): 2015/038/13:42:43
548
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6171781
33 A = 6785563
01 meter
Y = 956064
17 meter E =
0011370
Z = 2648107
83 I = 51
72741
XDOT = -2985
347264 Wp = 74
75197
YDOT = -4756
993836 meter/sec RA = 10
73853 deg
ZDOT = -5218
708939 TA = 75
43057
MA = 75
30449
Ha = 221
083 n
mi
Hp = 214
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20248626
42 X = -6194876
86
Y = 3136693
46 feet Y = 886918
37 meter
Z = 8688017
82 Z = 2618070
87
XDOT = -9794
446404 XDOT = -2906
581473
YDOT = -15606
935158 feet/sec YDOT = -4789
937958 meter/sec
ZDOT = -17121
748486 ZDOT = -5233
019217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20290940
78 X = -6184678
75
Y = -3216135
99 feet Y = -980278
25 meter
Z = 8559296
86 Z = 2608873
68
XDOT = -4688
030797 XDOT = -1428
911787
YDOT = -16341
843519 feet/sec YDOT = -4980
993905 meter/sec
ZDOT = -17182
052438 ZDOT = -5237
089583
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
60876113
00016717 00000-0 10270-3 0 9051
2 25544 51
6452 11
1265 0006389 339
3293 20
7601 15
54432076 7874
Satellite: ISS
Catalog Number: 25544
Epoch time: 15038
60876113 = yrday
fracday
Element set: 905
Inclination: 51
6452 deg
RA of node: 11
1265 deg
Eccentricity:
0006389
Arg of perigee: 339
3293 deg
Mean anomaly: 20
7601 deg
Mean motion: 15
54432076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 787
Checksum: 299
Coasting Arc #7 (Orbit 801)
---------------------------------------
Vector Time (GMT): 2015/039/13:42:43
548
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6711828
95 A = 6788031
15 meter
Y = -76519
41 meter E =
0014537
Z = -950757
09 I = 51
70465
XDOT = 888
859544 Wp = 17
08203
YDOT = 4792
636962 meter/sec RA = 5
76854 deg
ZDOT = 5925
665313 TA = 332
62420
MA = 332
70072
Ha = 221
176 n
mi
Hp = 214
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22020436
18 X = 6716804
12
Y = -251047
92 feet Y = -1435
63 meter
Z = -3119281
80 Z = -918140
71
XDOT = 2916
205852 XDOT = 806
416838
YDOT = 15723
874546 feet/sec YDOT = 4802
116302 meter/sec
ZDOT = 19441
159162 ZDOT = 5929
782512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21171153
32 X = 6452967
53
Y = 6131572
13 feet Y = 1868903
18 meter
Z = -2979705
32 Z = -908214
18
XDOT = -1425
769110 XDOT = -434
574425
YDOT = 14317
701768 feet/sec YDOT = 4364
035499 meter/sec
ZDOT = 19457
836746 ZDOT = 5930
748640
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
57309518
00016717 00000-0 10270-3 0 9069
2 25544 51
6451 6
3173 0006392 342
5548 17
5384 15
54455118 8022
Satellite: ISS
Catalog Number: 25544
Epoch time: 15039
57309518 = yrday
fracday
Element set: 906
Inclination: 51
6451 deg
RA of node: 6
3173 deg
Eccentricity:
0006392
Arg of perigee: 342
5548 deg
Mean anomaly: 17
5384 deg
Mean motion: 15
54455118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 802
Checksum: 305
Coasting Arc #8 (Orbit 817)
---------------------------------------
Vector Time (GMT): 2015/040/13:42:43
548
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6679905
94 A = 6787885
60 meter
Y = -802281
70 meter E =
0004959
Z = -896791
11 I = 51
67420
XDOT = 1352
308765 Wp = 107
66487
YDOT = -4666
505166 meter/sec RA =
80033 deg
ZDOT = -5926
672795 TA = 82
03113
MA = 81
97486
Ha = 221
170 n
mi
Hp = 214
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21915701
91 X = -6666081
95
Y = -2632157
81 feet Y = -876903
54 meter
Z = -2942228
04 Z = -929206
77
XDOT = 4436
708548 XDOT = 1433
179440
YDOT = -15310
056320 feet/sec YDOT = -4650
931072 meter/sec
ZDOT = -19444
464551 ZDOT = -5919
906818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20349640
96 X = -6202570
57
Y = -8501997
28 feet Y = -2591408
77 meter
Z = -3080763
83 Z = -939016
81
XDOT = 7941
282847 XDOT = 2420
503012
YDOT = -12004
874008 feet/sec YDOT = -3659
085598 meter/sec
ZDOT = -19414
600744 ZDOT = -5917
570307
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
60169571
00016717 00000-0 10270-3 0 9079
2 25544 51
6461 1
1870 0006354 346
3309 13
7671 15
54494515 8183
Satellite: ISS
Catalog Number: 25544
Epoch time: 15040
60169571 = yrday
fracday
Element set: 907
Inclination: 51
6461 deg
RA of node: 1
1870 deg
Eccentricity:
0006354
Arg of perigee: 346
3309 deg
Mean anomaly: 13
7671 deg
Mean motion: 15
54494515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 818
Checksum: 296
Coasting Arc #9 (Orbit 833)
---------------------------------------
Vector Time (GMT): 2015/041/13:42:43
548
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6029416
71 A = 6785178
97 meter
Y = 1639894
75 meter E =
0015214
Z = 2620433
43 I = 51
63362
XDOT = -3478
263289 Wp = 52
58506
YDOT = 4407
587774 meter/sec RA = 355
82573 deg
ZDOT = 5233
107165 TA = 336
96975
MA = 337
03788
Ha = 221
160 n
mi
Hp = 214
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19781550
88 X = 5997901
94
Y = 5380232
11 feet Y = 1707143
59 meter
Z = 8597222
54 Z = 2649646
21
XDOT = -11411
624965 XDOT = -3552
711688
YDOT = 14460
589810 feet/sec YDOT = 4368
275685 meter/sec
ZDOT = 17168
986763 ZDOT = 5216
029457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17691570
35 X = 5392390
64
Y = 10252121
45 feet Y = 3124846
62 meter
Z = 8721882
37 Z = 2658429
75
XDOT = -14091
218736 XDOT = -4295
003471
YDOT = 9740
617090 feet/sec YDOT = 2968
940089 meter/sec
ZDOT = 17095
058320 ZDOT = 5210
573776
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
63027256
00016717 00000-0 10270-3 0 9087
2 25544 51
6458 356
0568 0006366 350
3066 9
7963 15
54524973 8342
Satellite: ISS
Catalog Number: 25544
Epoch time: 15041
63027256 = yrday
fracday
Element set: 908
Inclination: 51
6458 deg
RA of node: 356
0568 deg
Eccentricity:
0006366
Arg of perigee: 350
3066 deg
Mean anomaly: 9
7963 deg
Mean motion: 15
54524973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 834
Checksum: 323
Coasting Arc #10 (Orbit 848)
---------------------------------------
Vector Time (GMT): 2015/042/13:42:43
548
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4846826
86 A = 6780940
34 meter
Y = -2476119
16 meter E =
0010725
Z = -4056337
12 I = 51
58925
XDOT = 5277
809700 Wp = 35
40330
YDOT = -3967
992716 meter/sec RA = 350
83826 deg
ZDOT = -3880
749360 TA = 194
29291
MA = 194
32328
Ha = 221
267 n
mi
Hp = 213
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15901662
92 X = -4799074
10
Y = -8123750
53 feet Y = -2530052
79 meter
Z = -13308192
65 Z = -4079765
70
XDOT = 17315
648621 XDOT = 5340
639525
YDOT = -13018
348806 feet/sec YDOT = -3908
621750 meter/sec
ZDOT = -12732
117324 ZDOT = -3854
958170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13412516
50 X = -4088135
03
Y = -11674666
48 feet Y = -3558438
34 meter
Z = -13407936
52 Z = -4086739
05
XDOT = 19155
246138 XDOT = 5838
519023
YDOT = -7499
156038 feet/sec YDOT = -2285
742760 meter/sec
ZDOT = -12621
001714 ZDOT = -3846
881322
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
59454096
00016717 00000-0 10270-3 0 9090
2 25544 51
6465 351
2469 0006372 354
1332 5
9746 15
54582564 8495
Satellite: ISS
Catalog Number: 25544
Epoch time: 15042
59454096 = yrday
fracday
Element set: 909
Inclination: 51
6465 deg
RA of node: 351
2469 deg
Eccentricity:
0006372
Arg of perigee: 354
1332 deg
Mean anomaly: 5
9746 deg
Mean motion: 15
54582564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 849
Checksum: 329
Coasting Arc #11 (Orbit 864)
---------------------------------------
Vector Time (GMT): 2015/043/13:42:43
548
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3218352
10 A = 6777247
05 meter
Y = 3269431
47 meter E =
0005455
Z = 4983507
98 I = 51
54588
XDOT = -6589
220025 Wp = 56
66011
YDOT = 3349
444666 meter/sec RA = 345
83634 deg
ZDOT = 2059
226568 TA = 13
30580
MA = 13
29142
Ha = 221
175 n
mi
Hp = 213
649
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10558897
98 X = 3157345
58
Y = 10726481
21 feet Y = 3305080
33 meter
Z = 16350091
79 Z = 4998993
61
XDOT = -21618
175935 XDOT = -6636
187431
YDOT = 10988
991687 feet/sec YDOT = 3275
497210 meter/sec
ZDOT = 6755
992677 ZDOT = 2027
103493
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7804497
51 X = 2378810
84
Y = 12786240
18 feet Y = 3897246
01 meter
Z = 16415696
99 Z = 5003504
44
XDOT = -22631
083854 XDOT = -6897
954359
YDOT = 5322
654237 feet/sec YDOT = 1622
345011 meter/sec
ZDOT = 6617
915839 ZDOT = 2017
140748
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 15043
62307040
00016717 00000-0 10270-3 0 9103
2 25544 51
6461 346
1161 0006263 356
8766 3
2347 15
54622988 8653
Satellite: ISS
Catalog Number: 25544
Epoch time: 15043
62307040 = yrday
fracday
Element set: 910
Inclination: 51
6461 deg
RA of node: 346
1161 deg
Eccentricity:
0006263
Arg of perigee: 356
8766 deg
Mean anomaly: 3
2347 deg
Mean motion: 15
54622988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 865
Checksum: 300
Coasting Arc #12 (Orbit 879)
---------------------------------------
Vector Time (GMT): 2015/044/13:42:43
548
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1361900
95 A = 6775844
05 meter
Y = -3997718
74 meter E =
0016211
Z = -5311543
82 I = 51
51154
XDOT = 7240
603199 Wp = 67
10877
YDOT = -2494
899512 meter/sec RA = 340
82399 deg
ZDOT = 27
496344 TA = 203
11752
MA = 203
19053
Ha = 221
322 n
mi
Hp = 213
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4468178
97 X = -1291295
12
Y = -13115875
12 feet Y = -4012553
83 meter
Z = -17426324
87 Z = -5317987
94
XDOT = 23755
259839 XDOT = 7267
830052
YDOT = -8185
365852 feet/sec YDOT = -2413
778135 meter/sec
ZDOT = 90
211103 ZDOT = 62
735586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1564609
44 X = -476892
96
Y = -13733484
17 feet Y = -4185965
98 meter
Z = -17453108
95 Z = -5319707
61
XDOT = 23928
864025 XDOT = 7293
517755
YDOT = -3007
011838 feet/sec YDOT = -916
537208 meter/sec
ZDOT = 241
446218 ZDOT = 73
592807
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 15044
58729631
00016717 00000-0 10270-3 0 9114
2 25544 51
6468 341
3057 0006335
9606 359
1558 15
54648235 8808
Satellite: ISS
Catalog Number: 25544
Epoch time: 15044
58729631 = yrday
fracday
Element set: 911
Inclination: 51
6468 deg
RA of node: 341
3057 deg
Eccentricity:
0006335
Arg of perigee:
9606 deg
Mean anomaly: 359
1558 deg
Mean motion: 15
54648235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 880
Checksum: 316
Coasting Arc #13 (Orbit 895)
---------------------------------------
Vector Time (GMT): 2015/045/13:42:43
548
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -590419
00 A = 6777260
93 meter
Y = 4586284
99 meter E =
0011350
Z = 4952972
85 I = 51
48695
XDOT = -7235
415596 Wp = 30
07066
YDOT = 1387
350884 meter/sec RA = 335
80943 deg
ZDOT = -2135
380794 TA = 80
83515
MA = 80
70676
Ha = 221
361 n
mi
Hp = 213
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1937070
20 X = -665719
35
Y = 15046866
76 feet Y = 4579261
67 meter
Z = 16249910
92 Z = 4949921
71
XDOT = -23738
240144 XDOT = -7240
018811
YDOT = 4551
676130 feet/sec YDOT = 1306
413947 meter/sec
ZDOT = -7005
842500 ZDOT = -2170
539720
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4846659
84 X = -1477261
92
Y = 14391782
50 feet Y = 4386615
30 meter
Z = 16235964
10 Z = 4948721
86
XDOT = -23077
032028 XDOT = -7033
879362
YDOT = 345
555867 feet/sec YDOT = 105
325428 meter/sec
ZDOT = -7156
513966 ZDOT = -2181
305457
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 15045
61577918
00016717 00000-0 10270-3 0 9129
2 25544 51
6465 336
1747 0006376 3
6828 356
4370 15
54702155 8965
Satellite: ISS
Catalog Number: 25544
Epoch time: 15045
61577918 = yrday
fracday
Element set: 912
Inclination: 51
6465 deg
RA of node: 336
1747 deg
Eccentricity:
0006376
Arg of perigee: 3
6828 deg
Mean anomaly: 356
4370 deg
Mean motion: 15
54702155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 896
Checksum: 328
Coasting Arc #14 (Orbit 910)
---------------------------------------
Vector Time (GMT): 2015/046/13:42:43
548
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2359566
47 A = 6780942
23 meter
Y = -4954618
17 meter E =
0008475
Z = -3986130
63 I = 51
47168
XDOT = 6561
728201 Wp = 59
16891
YDOT = -53
677795 meter/sec RA = 330
80092 deg
ZDOT = 3961
419321 TA = 252
13369
MA = 252
22615
Ha = 221
423 n
mi
Hp = 213
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7741359
82 X = 2434157
57
Y = -16255308
94 feet Y = -4927815
03 meter
Z = -13077856
38 Z = -3974487
19
XDOT = 21527
979663 XDOT = 6542
598040
YDOT = -176
108251 feet/sec YDOT = 19
592898 meter/sec
ZDOT = 12996
782550 ZDOT = 3993
247844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10504073
58 X = 3201641
63
Y = -14668110
62 feet Y = -4470840
12 meter
Z = -13027087
83 Z = -3970656
37
XDOT = 20085
951600 XDOT = 6122
198048
YDOT = 2750
988046 feet/sec YDOT = 838
501156 meter/sec
ZDOT = 13132
946025 ZDOT = 4002
921948
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 15046
57996137
00016717 00000-0 10270-3 0 9134
2 25544 51
6473 331
3640 0006348 7
3471 352
7774 15
54712311 9117
Satellite: ISS
Catalog Number: 25544
Epoch time: 15046
57996137 = yrday
fracday
Element set: 913
Inclination: 51
6473 deg
RA of node: 331
3640 deg
Eccentricity:
0006348
Arg of perigee: 7
3471 deg
Mean anomaly: 352
7774 deg
Mean motion: 15
54712311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 911
Checksum: 305
Coasting Arc #15 (Orbit 926)
---------------------------------------
Vector Time (GMT): 2015/047/13:42:43
548
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3863511
62 A = 6785072
41 meter
Y = 4999339
47 meter E =
0014728
Z = 2464872
26 I = 51
45834
XDOT = -5331
043939 Wp = 80
05250
YDOT = -1488
752404 meter/sec RA = 325
80320 deg
ZDOT = -5306
908450 TA = 72
25876
MA = 72
09806
Ha = 221
482 n
mi
Hp = 212
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12675563
07 X = -3931101
42
Y = 16402032
38 feet Y = 4955757
36 meter
Z = 8086851
23 Z = 2445940
10
XDOT = -17490
301636 XDOT = -5288
221765
YDOT = -4884
358282 feet/sec YDOT = -1548
128426 meter/sec
ZDOT = -17411
116961 ZDOT = -5332
700951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15116074
95 X = -4607379
64
Y = 14230935
71 feet Y = 4337589
20 meter
Z = 8004903
20 Z = 2439894
49
XDOT = -15374
047532 XDOT = -4686
009688
YDOT = -6419
475320 feet/sec YDOT = -1956
656077 meter/sec
ZDOT = -17521
162293 ZDOT = -5340
450267
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 15047
60839954
00016717 00000-0 10270-3 0 9143
2 25544 51
6471 326
2327 0006257 11
8607 348
2693 15
54725357 9271
Satellite: ISS
Catalog Number: 25544
Epoch time: 15047
60839954 = yrday
fracday
Element set: 914
Inclination: 51
6471 deg
RA of node: 326
2327 deg
Eccentricity:
0006257
Arg of perigee: 11
8607 deg
Mean anomaly: 348
2693 deg
Mean motion: 15
54725357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 927
Checksum: 328
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