[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 20th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 219 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
057/09:19:29
121 0
1 2
7 2
7
N/A 2
6 -0
2 222
6
000/00:05:58
241 0
7 0
2 211
3
062/07:21:36
413 -0
6 1
4 1
4
N/A -1
2 -0
1 222
7
000/00:03:12
826 -0
1 0
1 211
4
Coasting Arc #1 (Orbit 989)
---------------------------------------
Vector Time (GMT): 2015/051/15:18:42
285
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4375359
34 A = 6775537
85 meter
Y = -905097
55 meter E =
0017755
Z = -5109185
74 I = 51
33270
XDOT = 3251
633642 Wp = 61
40379
YDOT = -6748
411060 meter/sec RA = 305
47448 deg
ZDOT = -1584
986541 TA = 193
19872
MA = 193
24523
Ha = 221
138 n
mi
Hp = 211
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14354853
49 X = -4340095
08
Y = -2969480
15 feet Y = -953829
16 meter
Z = -16762420
40 Z = -5130354
22
XDOT = 10668
089376 XDOT = 3334
553430
YDOT = -22140
456233 feet/sec YDOT = -6711
585745 meter/sec
ZDOT = -5200
087078 ZDOT = -1568
988757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14436670
24 X = -4400297
09
Y = 1850472
43 feet Y = 564024
00 meter
Z = -16852794
22 Z = -5136731
68
XDOT = 3009
257489 XDOT = 917
221683
YDOT = -23369
913696 feet/sec YDOT = -7123
149695 meter/sec
ZDOT = -5130
417485 ZDOT = -1563
751250
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 15051
65677429
00016717 00000-0 10270-3 0 9005
2 25544 51
6431 306
0317 0006083 22
4293 337
7125 15
55033731 9900
Satellite: ISS
Catalog Number: 25544
Epoch time: 15051
65677429 = yrday
fracday
Element set: 900
Inclination: 51
6431 deg
RA of node: 306
0317 deg
Eccentricity:
0006083
Arg of perigee: 22
4293 deg
Mean anomaly: 337
7125 deg
Mean motion: 15
55033731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 990
Checksum: 289
Coasting Arc #2 (Orbit 1005)
---------------------------------------
Vector Time (GMT): 2015/052/15:18:42
285
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3227687
07 A = 6774846
38 meter
Y = 2805871
44 meter E =
0008698
Z = 5250333
80 I = 51
31291
XDOT = -4337
878457 Wp = 38
06062
YDOT = 6292
628938 meter/sec RA = 300
44223 deg
ZDOT = -688
801135 TA = 58
58501
MA = 58
49998
Ha = 221
088 n
mi
Hp = 212
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10589524
50 X = 3170567
46
Y = 9205614
97 feet Y = 2841646
85 meter
Z = 17225504
61 Z = 5265873
96
XDOT = -14231
884700 XDOT = -4404
575827
YDOT = 20645
108065 feet/sec YDOT = 6243
746937 meter/sec
ZDOT = -2259
846242 ZDOT = -710
036220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13003153
82 X = 3963361
29
Y = 5052020
99 feet Y = 1539856
00 meter
Z = 17291456
26 Z = 5270435
87
XDOT = -5901
675336 XDOT = -1798
830642
YDOT = 23321
715688 feet/sec YDOT = 7108
458942 meter/sec
ZDOT = -2351
818850 ZDOT = -716
834386
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 15052
68499857
00016717 00000-0 10270-3 0 9017
2 25544 51
6431 300
8984 0006025 26
2678 333
8779 15
55045521 10068
Satellite: ISS
Catalog Number: 25544
Epoch time: 15052
68499857 = yrday
fracday
Element set: 901
Inclination: 51
6431 deg
RA of node: 300
8984 deg
Eccentricity:
0006025
Arg of perigee: 26
2678 deg
Mean anomaly: 333
8779 deg
Mean motion: 15
55045521 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1006
Checksum: 319
Coasting Arc #3 (Orbit 1020)
---------------------------------------
Vector Time (GMT): 2015/053/15:18:42
285
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1978284
74 A = 6777296
48 meter
Y = -4523005
22 meter E =
0013079
Z = -4653808
78 I = 51
30503
XDOT = 4954
610582 Wp = 82
63413
YDOT = -5097
281478 meter/sec RA = 295
41067 deg
ZDOT = 2856
426870 TA = 215
85883
MA = 215
94670
Ha = 221
136 n
mi
Hp = 211
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6490435
49 X = -1904954
17
Y = -14839255
97 feet Y = -4544718
23 meter
Z = -15268401
51 Z = -4663240
15
XDOT = 16255
284063 XDOT = 4997
366044
YDOT = -16723
364430 feet/sec YDOT = -5041
636393 meter/sec
ZDOT = 9371
479231 ZDOT = 2880
599599
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11298110
21 X = -3443663
99
Y = -11553083
85 feet Y = -3521379
96 meter
Z = -15307916
72 Z = -4665853
02
XDOT = 8264
516424 XDOT = 2519
024606
YDOT = -20600
464318 feet/sec YDOT = -6279
021524 meter/sec
ZDOT = 9475
787697 ZDOT = 2888
220090
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 15053
64893999
00016717 00000-0 10270-3 0 9020
2 25544 51
6419 296
0846 0005994 30
3211 329
8288 15
55094449 10210
Satellite: ISS
Catalog Number: 25544
Epoch time: 15053
64893999 = yrday
fracday
Element set: 902
Inclination: 51
6419 deg
RA of node: 296
0846 deg
Eccentricity:
0005994
Arg of perigee: 30
3211 deg
Mean anomaly: 329
8288 deg
Mean motion: 15
55094449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1021
Checksum: 334
Coasting Arc #4 (Orbit 1036)
---------------------------------------
Vector Time (GMT): 2015/054/15:18:42
285
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 672358
53 A = 6781654
82 meter
Y = 5860867
94 meter E =
0016428
Z = 3336502
82 I = 51
30762
XDOT = -5172
930898 Wp = 72
87529
YDOT = 3248
768835 meter/sec RA = 290
39118 deg
ZDOT = -4640
602591 TA = 68
02070
MA = 67
84621
Ha = 221
101 n
mi
Hp = 211
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2205900
68 X = 590563
61
Y = 19228569
37 feet Y = 5867929
70 meter
Z = 10946531
55 Z = 3339569
70
XDOT = -16971
558065 XDOT = -5186
332827
YDOT = 10658
690402 feet/sec YDOT = 3190
846334 meter/sec
ZDOT = -15225
074117 ZDOT = -4665
764343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9196095
59 X = 2802969
94
Y = 17022677
48 feet Y = 5188512
10 meter
Z = 10958590
61 Z = 3340178
42
XDOT = -10401
240988 XDOT = -3170
298253
YDOT = 15540
087371 feet/sec YDOT = 4736
618631 meter/sec
ZDOT = -15333
271672 ZDOT = -4673
581206
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 15054
67712405
00016717 00000-0 10270-3 0 9037
2 25544 51
6422 290
9510 0005956 32
0695 328
0820 15
55140478 10372
Satellite: ISS
Catalog Number: 25544
Epoch time: 15054
67712405 = yrday
fracday
Element set: 903
Inclination: 51
6422 deg
RA of node: 290
9510 deg
Eccentricity:
0005956
Arg of perigee: 32
0695 deg
Mean anomaly: 328
0820 deg
Mean motion: 15
55140478 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1037
Checksum: 293
Coasting Arc #5 (Orbit 1051)
---------------------------------------
Vector Time (GMT): 2015/055/15:18:42
285
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 513251
67 A = 6785332
74 meter
Y = -6577701
34 meter E =
0014049
Z = -1560940
40 I = 51
30927
XDOT = 5017
148623 Wp = 37
66426
YDOT = -957
525564 meter/sec RA = 285
38416 deg
ZDOT = 5722
861515 TA = 305
18004
MA = 305
31154
Ha = 221
166 n
mi
Hp = 211
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1683896
55 X = 594349
33
Y = -21580384
98 feet Y = -6571508
52 meter
Z = -5121195
55 Z = -1558249
59
XDOT = 16460
461362 XDOT = 4999
683749
YDOT = -3141
488070 feet/sec YDOT = -901
517682 meter/sec
ZDOT = 18775
792373 ZDOT = 5747
191289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6861345
94 X = -2091338
24
Y = -20532906
25 feet Y = -6258429
83 meter
Z = -5108508
59 Z = -1557073
42
XDOT = 12313
953190 XDOT = 3753
292932
YDOT = -8780
868922 feet/sec YDOT = -2676
408847 meter/sec
ZDOT = 18880
017932 ZDOT = 5754
629466
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 15055
64103099
00016717 00000-0 10270-3 0 9049
2 25544 51
6416 286
1375 0005934 37
9457 322
2113 15
55148485 10521
Satellite: ISS
Catalog Number: 25544
Epoch time: 15055
64103099 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 286
1375 deg
Eccentricity:
0005934
Arg of perigee: 37
9457 deg
Mean anomaly: 322
2113 deg
Mean motion: 15
55148485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1052
Checksum: 304
Coasting Arc #6 (Orbit 1067)
---------------------------------------
Vector Time (GMT): 2015/056/15:18:42
285
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1615828
60 A = 6786030
35 meter
Y = 6569705
09 meter E =
0011771
Z = -505621
10 I = 51
30505
XDOT = -4562
647077 Wp = 107
46280
YDOT = -1571
504114 meter/sec RA = 280
38574 deg
ZDOT = -5956
501577 TA = 78
01664
MA = 77
88472
Ha = 221
161 n
mi
Hp = 211
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5301274
94 X = -1686716
41
Y = 21554150
57 feet Y = 6551239
45 meter
Z = -1658861
89 Z = -513643
09
XDOT = -14969
314558 XDOT = -4515
800894
YDOT = -5155
853394 feet/sec YDOT = -1622
265141 meter/sec
ZDOT = -19542
328007 ZDOT = -5978
551887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3937553
91 X = 1200166
43
Y = 21841740
48 feet Y = 6657362
50 meter
Z = -1694339
89 Z = -516434
80
XDOT = -14066
535373 XDOT = -4287
479982
YDOT = 1042
110868 feet/sec YDOT = 317
635393 meter/sec
ZDOT = -19636
355859 ZDOT = -5985
161266
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 15056
66917671
00016717 00000-0 10270-3 0 9052
2 25544 51
6417 281
0036 0006138 40
1263 320
0342 15
55223228 10684
Satellite: ISS
Catalog Number: 25544
Epoch time: 15056
66917671 = yrday
fracday
Element set: 905
Inclination: 51
6417 deg
RA of node: 281
0036 deg
Eccentricity:
0006138
Arg of perigee: 40
1263 deg
Mean anomaly: 320
0342 deg
Mean motion: 15
55223228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1068
Checksum: 280
Coasting Arc #7 (Orbit 1079)
---------------------------------------
Vector Time (GMT): 2015/057/09:22:28
241
Vector Time (MET): N/A
Weight (LBS) : 905155
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4275543
20 A = 6775840
67 meter
Y = -469839
31 meter E =
0009687
Z = 5227280
25 I = 51
26595
XDOT = -198
287300 Wp = 68
57692
YDOT = 7627
322032 meter/sec RA = 276
61570 deg
ZDOT = 849
954875 TA = 13
27632
MA = 13
25085
Ha = 222
612 n
mi
Hp = 211
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14027372
71 X = 4255087
43
Y = -1541467
57 feet Y = -422141
39 meter
Z = 17149869
59 Z = 5248000
10
XDOT = -650
548886 XDOT = -287
691790
YDOT = 25024
022416 feet/sec YDOT = 7624
604828 meter/sec
ZDOT = 2788
565863 ZDOT = 848
773930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7422149
47 X = 2262271
16
Y = 11874538
22 feet Y = 3619359
25 meter
Z = 17238572
27 Z = 5254316
83
XDOT = -21973
777795 XDOT = -6697
607472
YDOT = 9706
180077 feet/sec YDOT = 2958
443688 meter/sec
ZDOT = 2782
167012 ZDOT = 848
004505
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 15057
44029550
00016717 00000-0 10270-3 0 9060
2 25544 51
6454 277
1579 0008045 50
1109 310
0750 15
54724240 10807
Satellite: ISS
Catalog Number: 25544
Epoch time: 15057
44029550 = yrday
fracday
Element set: 906
Inclination: 51
6454 deg
RA of node: 277
1579 deg
Eccentricity:
0008045
Arg of perigee: 50
1109 deg
Mean anomaly: 310
0750 deg
Mean motion: 15
54724240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1080
Checksum: 281
Coasting Arc #8 (Orbit 1094)
---------------------------------------
Vector Time (GMT): 2015/058/09:22:28
241
Vector Time (MET): N/A
Weight (LBS) : 905155
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4105932
03 A = 6776136
93 meter
Y = -1579465
65 meter E =
0020394
Z = -5171012
73 I = 51
26467
XDOT = 1243
139642 Wp = 83
02221
YDOT = -7441
879856 meter/sec RA = 271
58310 deg
ZDOT = 1292
840677 TA = 199
44308
MA = 199
52099
Ha = 222
763 n
mi
Hp = 211
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13470905
62 X = -4062846
45
Y = -5181973
92 feet Y = -1625140
34 meter
Z = -16965264
85 Z = -5190853
47
XDOT = 4078
542131 XDOT = 1319
984066
YDOT = -24415
616324 feet/sec YDOT = -7427
548499 meter/sec
ZDOT = 4241
603271 ZDOT = 1299
066713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1368383
51 X = -417083
30
Y = -14267741
14 feet Y = -4348807
50 meter
Z = -17049851
99 Z = -5196794
89
XDOT = 22594
546710 XDOT = 6886
817837
YDOT = -7242
384132 feet/sec YDOT = -2207
478683 meter/sec
ZDOT = 4269
535527 ZDOT = 1301
354429
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 15058
40446296
00016717 00000-0 10270-3 0 9078
2 25544 51
6457 272
3472 0008090 52
8898 307
2994 15
54739682 10953
Satellite: ISS
Catalog Number: 25544
Epoch time: 15058
40446296 = yrday
fracday
Element set: 907
Inclination: 51
6457 deg
RA of node: 272
3472 deg
Eccentricity:
0008090
Arg of perigee: 52
8898 deg
Mean anomaly: 307
2994 deg
Mean motion: 15
54739682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1095
Checksum: 345
Coasting Arc #9 (Orbit 1110)
---------------------------------------
Vector Time (GMT): 2015/059/09:22:28
241
Vector Time (MET): N/A
Weight (LBS) : 905155
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3750324
01 A = 6779063
42 meter
Y = 3523211
32 meter E =
0017231
Z = 4404502
33 I = 51
27476
XDOT = -2257
043894 Wp = 63
01805
YDOT = 6550
688978 meter/sec RA = 266
55535 deg
ZDOT = -3300
465578 TA = 60
51997
MA = 60
34819
Ha = 222
651 n
mi
Hp = 210
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12304212
64 X = 3689252
86
Y = 11559092
27 feet Y = 3564808
78 meter
Z = 14450466
98 Z = 4422571
73
XDOT = -7404
999653 XDOT = -2314
095359
YDOT = 21491
761738 feet/sec YDOT = 6525
129981 meter/sec
ZDOT = -10828
299142 ZDOT = -3311
568762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4568552
10 X = -1392494
68
Y = 16183712
48 feet Y = 4932795
56 meter
Z = 14527148
41 Z = 4427874
84
XDOT = -21259
990340 XDOT = -6480
045056
YDOT = 3813
829822 feet/sec YDOT = 1162
455330 meter/sec
ZDOT = -10876
925510 ZDOT = -3315
286895
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 15059
43288781
00016717 00000-0 10270-3 0 9086
2 25544 51
6454 267
2157 0008106 55
5977 304
5942 15
54793387 11113
Satellite: ISS
Catalog Number: 25544
Epoch time: 15059
43288781 = yrday
fracday
Element set: 908
Inclination: 51
6454 deg
RA of node: 267
2157 deg
Eccentricity:
0008106
Arg of perigee: 55
5977 deg
Mean anomaly: 304
5942 deg
Mean motion: 15
54793387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1111
Checksum: 333
Coasting Arc #10 (Orbit 1125)
---------------------------------------
Vector Time (GMT): 2015/060/09:22:28
241
Vector Time (MET): N/A
Weight (LBS) : 905155
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3266139
49 A = 6783281
90 meter
Y = -5075414
62 meter E =
0012432
Z = -3099412
67 I = 51
29150
XDOT = 3187
744999 Wp = 64
78688
YDOT = -5002
360143 meter/sec RA = 261
53940 deg
ZDOT = 4852
849118 TA = 259
38135
MA = 259
52139
Ha = 222
710 n
mi
Hp = 210
936
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10715680
73 X = -3194086
77
Y = -16651622
76 feet Y = -5111536
14 meter
Z = -10168676
75 Z = -3115103
15
XDOT = 10458
480969 XDOT = 3219
872797
YDOT = -16411
942726 feet/sec YDOT = -4966
532613 meter/sec
ZDOT = 15921
420991 ZDOT = 4868
412752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9506781
06 X = 2897666
87
Y = -17331234
66 feet Y = -5282560
32 meter
Z = -10234928
42 Z = -3119606
18
XDOT = 18103
412051 XDOT = 5517
919993
YDOT = 527
629592 feet/sec YDOT = 160
821500 meter/sec
ZDOT = 15988
851424 ZDOT = 4873
401914
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 15060
39701897
00016717 00000-0 10270-3 0 9092
2 25544 51
6452 262
4046 0008035 58
6642 301
5297 15
54787110 11262
Satellite: ISS
Catalog Number: 25544
Epoch time: 15060
39701897 = yrday
fracday
Element set: 909
Inclination: 51
6452 deg
RA of node: 262
4046 deg
Eccentricity:
0008035
Arg of perigee: 58
6642 deg
Mean anomaly: 301
5297 deg
Mean motion: 15
54787110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1126
Checksum: 308
Coasting Arc #11 (Orbit 1141)
---------------------------------------
Vector Time (GMT): 2015/061/09:22:28
241
Vector Time (MET): N/A
Weight (LBS) : 905155
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2556613
97 A = 6786652
59 meter
Y = 6140652
61 meter E =
0019426
Z = 1319247
09 I = 51
30796
XDOT = -4065
568115 Wp = 100
02605
YDOT = 2952
606382 meter/sec RA = 256
53619 deg
ZDOT = -5794
930786 TA = 65
54069
MA = 65
33818
Ha = 222
784 n
mi
Hp = 210
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8387841
10 X = 2481349
45
Y = 20146498
08 feet Y = 6168821
65 meter
Z = 4328238
47 Z = 1331482
89
XDOT = -13338
478066 XDOT = -4070
133673
YDOT = 9687
028813 feet/sec YDOT = 2907
116397 meter/sec
ZDOT = -19012
240112 ZDOT = -5814
691522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13377253
99 X = -4077387
02
Y = 17229032
37 feet Y = 5251409
07 meter
Z = 4379546
84 Z = 1334885
88
XDOT = -13698
001278 XDOT = -4175
150790
YDOT = -5723
773708 feet/sec YDOT = -1744
606226 meter/sec
ZDOT = -19097
271711 ZDOT = -5820
848418
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 15061
42540661
00016717 00000-0 10270-3 0 9109
2 25544 51
6449 257
2726 0008052 63
5355 296
6624 15
54790609 11423
Satellite: ISS
Catalog Number: 25544
Epoch time: 15061
42540661 = yrday
fracday
Element set: 910
Inclination: 51
6449 deg
RA of node: 257
2726 deg
Eccentricity:
0008052
Arg of perigee: 63
5355 deg
Mean anomaly: 296
6624 deg
Mean motion: 15
54790609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1142
Checksum: 306
Coasting Arc #12 (Orbit 1155)
---------------------------------------
Vector Time (GMT): 2015/062/07:23:12
826
Vector Time (MET): N/A
Weight (LBS) : 905014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3735754
51 A = 6776177
69 meter
Y = 2132845
22 meter E =
0021304
Z = -5254212
95 I = 51
27830
XDOT = -2934
082116 Wp = 77
49999
YDOT = -7027
188990 meter/sec RA = 251
95484 deg
ZDOT = -764
523494 TA = 185
13293
MA = 185
15481
Ha = 222
721 n
mi
Hp = 211
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12256412
43 X = -3733804
36
Y = 6997523
69 feet Y = 2091079
84 meter
Z = -17238231
45 Z = -5272355
67
XDOT = -9626
253660 XDOT = -2851
570668
YDOT = -23055
081989 feet/sec YDOT = -7059
538556 meter/sec
ZDOT = -2508
279181 ZDOT = -778
575138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7149342
69 X = -2179119
65
Y = -12057265
31 feet Y = -3675054
47 meter
Z = -17316202
21 Z = -5277978
43
XDOT = 22052
462766 XDOT = 6721
590651
YDOT = -9380
170448 feet/sec YDOT = -2859
075953 meter/sec
ZDOT = -2567
223403 ZDOT = -782
489693
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 15062
32522854
00016717 00000-0 10270-3 0 9114
2 25544 51
6446 252
7813 0007039 63
7257 296
4619 15
54605082 11561
Satellite: ISS
Catalog Number: 25544
Epoch time: 15062
32522854 = yrday
fracday
Element set: 911
Inclination: 51
6446 deg
RA of node: 252
7813 deg
Eccentricity:
0007039
Arg of perigee: 63
7257 deg
Mean anomaly: 296
4619 deg
Mean motion: 15
54605082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1156
Checksum: 309
Coasting Arc #13 (Orbit 1171)
---------------------------------------
Vector Time (GMT): 2015/063/07:23:12
826
Vector Time (MET): N/A
Weight (LBS) : 905014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4394004
45 A = 6776388
02 meter
Y = -210386
88 meter E =
0011186
Z = 5146875
29 I = 51
29006
XDOT = 1937
454412 Wp = 62
06874
YDOT = 7304
138443 meter/sec RA = 246
92431 deg
ZDOT = -1348
079265 TA = 40
97986
MA = 40
89585
Ha = 222
466 n
mi
Hp = 211
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14416025
09 X = 4371029
35
Y = -690245
68 feet Y = -161378
02 meter
Z = 16886073
79 Z = 5168164
33
XDOT = 6356
477730 XDOT = 1862
182157
YDOT = 23963
708804 feet/sec YDOT = 7325
383267 meter/sec
ZDOT = -4422
832234 ZDOT = -1338
851490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1115824
59 X = 340103
34
Y = 14281726
78 feet Y = 4353070
32 meter
Z = 16977188
29 Z = 5174646
99
XDOT = -22720
499331 XDOT = -6925
208196
YDOT = 7015
923131 feet/sec YDOT = 2138
453370 meter/sec
ZDOT = -4384
552949 ZDOT = -1336
411739
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 15063
35374553
00016717 00000-0 10270-3 0 9120
2 25544 51
6443 247
6500 0006906 66
2551 293
9318 15
54659908 11723
Satellite: ISS
Catalog Number: 25544
Epoch time: 15063
35374553 = yrday
fracday
Element set: 912
Inclination: 51
6443 deg
RA of node: 247
6500 deg
Eccentricity:
0006906
Arg of perigee: 66
2551 deg
Mean anomaly: 293
9318 deg
Mean motion: 15
54659908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1172
Checksum: 317
Coasting Arc #14 (Orbit 1186)
---------------------------------------
Vector Time (GMT): 2015/064/07:23:12
826
Vector Time (MET): N/A
Weight (LBS) : 905014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4883828
68 A = 6779390
94 meter
Y = -1617302
74 meter E =
0015224
Z = -4428754
67 I = 51
31358
XDOT = -692
252958 Wp = 93
26649
YDOT = -6882
334568 meter/sec RA = 241
89986 deg
ZDOT = 3285
647520 TA = 210
03424
MA = 210
12165
Ha = 222
616 n
mi
Hp = 211
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16023059
97 X = -4843867
76
Y = -5306111
35 feet Y = -1671694
12 meter
Z = -14530035
01 Z = -4452381
67
XDOT = -2271
171121 XDOT = -631
201804
YDOT = -22579
837822 feet/sec YDOT = -6889
733948 meter/sec
ZDOT = 10779
683465 ZDOT = 3282
434050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4551856
82 X = 1387405
96
Y = -16162726
89 feet Y = -4926399
16 meter
Z = -14630859
33 Z = -4459485
92
XDOT = 21265
184132 XDOT = 6481
628123
YDOT = -3731
313414 feet/sec YDOT = -1137
304329 meter/sec
ZDOT = 10767
050866 ZDOT = 3281
797104
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 15064
31796391
00016717 00000-0 10270-3 0 9136
2 25544 51
6446 242
8393 0006924 69
2209 290
9686 15
54651662 11876
Satellite: ISS
Catalog Number: 25544
Epoch time: 15064
31796391 = yrday
fracday
Element set: 913
Inclination: 51
6446 deg
RA of node: 242
8393 deg
Eccentricity:
0006924
Arg of perigee: 69
2209 deg
Mean anomaly: 290
9686 deg
Mean motion: 15
54651662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1187
Checksum: 336
Coasting Arc #15 (Orbit 1202)
---------------------------------------
Vector Time (GMT): 2015/065/07:23:12
826
Vector Time (MET): N/A
Weight (LBS) : 905014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5077306
18 A = 6783547
59 meter
Y = 3243175
75 meter E =
0019626
Z = 3101702
34 I = 51
34355
XDOT = -786
291369 Wp = 87
17647
YDOT = 5895
089773 meter/sec RA = 236
88762 deg
ZDOT = -4849
314456 TA = 56
93902
MA = 56
75068
Ha = 222
583 n
mi
Hp = 211
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16657828
68 X = 5025596
15
Y = 10640340
38 feet Y = 3299664
85 meter
Z = 10176188
77 Z = 3126240
48
XDOT = -2579
696091 XDOT = -828
597363
YDOT = 19340
845712 feet/sec YDOT = 5886
059649 meter/sec
ZDOT = -15909
824332 ZDOT = -4853
237731
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9553448
86 X = -2911891
21
Y = 17242233
13 feet Y = 5255432
66 meter
Z = 10280658
01 Z = 3133544
56
XDOT = -18201
407486 XDOT = -5547
789002
YDOT = -534
779496 feet/sec YDOT = -163
000790 meter/sec
ZDOT = -15927
555645 ZDOT = -4854
718961
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 15065
34644255
00016717 00000-0 10270-3 0 9142
2 25544 51
6447 237
7077 0007029 72
6560 287
5361 15
54684697 12039
Satellite: ISS
Catalog Number: 25544
Epoch time: 15065
34644255 = yrday
fracday
Element set: 914
Inclination: 51
6447 deg
RA of node: 237
7077 deg
Eccentricity:
0007029
Arg of perigee: 72
6560 deg
Mean anomaly: 287
5361 deg
Mean motion: 15
54684697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1203
Checksum: 325
Coasting Arc #16 (Orbit 1217)
---------------------------------------
Vector Time (GMT): 2015/066/07:23:12
826
Vector Time (MET): N/A
Weight (LBS) : 905014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4927221
44 A = 6786715
00 meter
Y = -4440078
02 meter E =
0014511
Z = -1422096
16 I = 51
37276
XDOT = 2365
513265 Wp = 54
68073
YDOT = -4457
907460 meter/sec RA = 231
88804 deg
ZDOT = 5772
499466 TA = 289
75294
MA = 289
90939
Ha = 222
517 n
mi
Hp = 211
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16165424
67 X = -4870297
29
Y = -14567185
09 feet Y = -4494859
36 meter
Z = -4665669
83 Z = -1445892
47
XDOT = 7760
870291 XDOT = 2387
146442
YDOT = -14625
680644 feet/sec YDOT = -4431
332879 meter/sec
ZDOT = 18938
646541 ZDOT = 5784
043810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13206013
03 X = 4025192
77
Y = -17267637
25 feet Y = -5263175
83 meter
Z = -4766784
55 Z = -1452915
93
XDOT = 13938
190776 XDOT = 4248
360549
YDOT = 5462
060889 feet/sec YDOT = 1664
836159 meter/sec
ZDOT = 18988
750368 ZDOT = 5787
771112
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 15066
31062098
00016717 00000-0 10270-3 0 9150
2 25544 51
6449 232
8965 0006882 75
1206 285
0709 15
54717926 12181
Satellite: ISS
Catalog Number: 25544
Epoch time: 15066
31062098 = yrday
fracday
Element set: 915
Inclination: 51
6449 deg
RA of node: 232
8965 deg
Eccentricity:
0006882
Arg of perigee: 75
1206 deg
Mean anomaly: 285
0709 deg
Mean motion: 15
54717926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1218
Checksum: 325
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