[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 22nd 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 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 2886)
---------------------------------------
Vector Time (GMT): 2015/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4640706
39 A = 6784826
91 meter
Y = -4628821
47 meter E =
0016707
Z = 1725134
24 I = 51
96860
XDOT = 2379
325808 Wp = 109
54437
YDOT = -4530
757850 meter/sec RA = 56
80662 deg
ZDOT = -5716
828134 TA = 51
60275
MA = 51
45283
Ha = 220
408 n
mi
Hp = 211
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15225414
67 X = -4596980
90
Y = -15186422
14 feet Y = -4680472
55 meter
Z = 5659889
24 Z = 1702696
54
XDOT = 7806
187033 XDOT = 2457
583032
YDOT = -14864
691110 feet/sec YDOT = -4503
712626 meter/sec
ZDOT = -18755
997814 ZDOT = -5705
080204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15314550
01 X = -4667874
84
Y = 15132021
19 feet Y = 4612240
06 meter
Z = 5564306
62 Z = 1696000
66
XDOT = -13695
376289 XDOT = -4174
350693
YDOT = -6934
204593 feet/sec YDOT = -2113
545560 meter/sec
ZDOT = -18704
545263 ZDOT = -5701
145396
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 15173
53549965
00016717 00000-0 10270-3 0 9000
2 25544 51
6447 57
3298 0003174 82
9925 277
1590 15
55259280 28871
Satellite: ISS
Catalog Number: 25544
Epoch time: 15173
53549965 = yrday
fracday
Element set: 900
Inclination: 51
6447 deg
RA of node: 57
3298 deg
Eccentricity:
0003174
Arg of perigee: 82
9925 deg
Mean anomaly: 277
1590 deg
Mean motion: 15
55259280 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2887
Checksum: 345
Coasting Arc #2 (Orbit 2902)
---------------------------------------
Vector Time (GMT): 2015/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3969529
95 A = 6785773
44 meter
Y = 5485017
99 meter E =
0015323
Z = 340438
03 I = 51
95461
XDOT = -4018
048828 Wp = 55
00200
YDOT = 2522
354447 meter/sec RA = 51
85153 deg
ZDOT = 6028
794651 TA = 308
65403
MA = 308
79105
Ha = 220
207 n
mi
Hp = 211
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13023392
21 X = 3906246
42
Y = 17995465
83 feet Y = 5529054
00 meter
Z = 1116922
66 Z = 359567
88
XDOT = -13182
574895 XDOT = -4075
241283
YDOT = 8275
441099 feet/sec YDOT = 2477
101740 meter/sec
ZDOT = 19779
510009 ZDOT = 6009
137104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17881178
36 X = 5450183
16
Y = -13172740
10 feet Y = -4015051
18 meter
Z = 1198094
40 Z = 365179
17
XDOT = 7432
666338 XDOT = 2265
476700
YDOT = 11931
448617 feet/sec YDOT = 3636
705539 meter/sec
ZDOT = 19694
438390 ZDOT = 6002
864821
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 15174
56355214
00016717 00000-0 10270-3 0 9017
2 25544 51
6449 52
1952 0002981 83
3441 276
8051 15
55334085 29030
Satellite: ISS
Catalog Number: 25544
Epoch time: 15174
56355214 = yrday
fracday
Element set: 901
Inclination: 51
6449 deg
RA of node: 52
1952 deg
Eccentricity:
0002981
Arg of perigee: 83
3441 deg
Mean anomaly: 276
8051 deg
Mean motion: 15
55334085 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2903
Checksum: 301
Coasting Arc #3 (Orbit 2917)
---------------------------------------
Vector Time (GMT): 2015/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2761194
47 A = 6783355
15 meter
Y = -5709226
22 meter E =
0007764
Z = -2406926
59 I = 51
92609
XDOT = 5439
579914 Wp = 117
67130
YDOT = -365
978180 meter/sec RA = 46
89377 deg
ZDOT = -5388
884703 TA = 89
12013
MA = 89
03117
Ha = 220
134 n
mi
Hp = 211
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9059036
96 X = -2685455
38
Y = -18731057
17 feet Y = -5739680
04 meter
Z = -7896740
78 Z = -2420156
40
XDOT = 17846
390793 XDOT = 5469
445237
YDOT = -1200
715814 feet/sec YDOT = -304
981836 meter/sec
ZDOT = -17680
067922 ZDOT = -5362
387796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18491856
75 X = -5636317
94
Y = 9491390
28 feet Y = 2892975
76 meter
Z = -7952478
40 Z = -2423915
41
XDOT = -975
604321 XDOT = -297
364197
YDOT = -16572
876811 feet/sec YDOT = -5051
412852 meter/sec
ZDOT = -17566
018478 ZDOT = -5354
122432
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 15175
52733417
00016717 00000-0 10270-3 0 9020
2 25544 51
6448 47
3819 0002806 88
1401 272
0073 15
55324873 29184
Satellite: ISS
Catalog Number: 25544
Epoch time: 15175
52733417 = yrday
fracday
Element set: 902
Inclination: 51
6448 deg
RA of node: 47
3819 deg
Eccentricity:
0002806
Arg of perigee: 88
1401 deg
Mean anomaly: 272
0073 deg
Mean motion: 15
55324873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2918
Checksum: 308
Coasting Arc #4 (Orbit 2933)
---------------------------------------
Vector Time (GMT): 2015/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1139445
17 A = 6778729
01 meter
Y = 5301316
72 meter E =
0013505
Z = 4058064
96 I = 51
88842
XDOT = -6401
368738 Wp = 98
90756
YDOT = -1626
595488 meter/sec RA = 41
92113 deg
ZDOT = 3909
233809 TA = 310
69119
MA = 310
80846
Ha = 220
132 n
mi
Hp = 211
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3738337
17 X = 1060367
31
Y = 17392771
38 feet Y = 5313616
26 meter
Z = 13313861
43 Z = 4063408
52
XDOT = -21001
865938 XDOT = -6401
693610
YDOT = -5336
599370 feet/sec YDOT = -1698
181913 meter/sec
ZDOT = 12825
570238 ZDOT = 3878
136239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17220271
23 X = 5248738
67
Y = -4400287
78 feet Y = -1341207
71 meter
Z = 13335752
45 Z = 4064737
35
XDOT = -4742
058883 XDOT = -1445
379547
YDOT = 20037
832356 feet/sec YDOT = 6107
531302 meter/sec
ZDOT = 12692
146584 ZDOT = 3868
566279
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 15176
55534762
00016717 00000-0 10270-3 0 9037
2 25544 51
6447 42
2470 0002930 87
3899 272
7590 15
55359044 29347
Satellite: ISS
Catalog Number: 25544
Epoch time: 15176
55534762 = yrday
fracday
Element set: 903
Inclination: 51
6447 deg
RA of node: 42
2470 deg
Eccentricity:
0002930
Arg of perigee: 87
3899 deg
Mean anomaly: 272
7590 deg
Mean motion: 15
55359044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2934
Checksum: 328
Coasting Arc #5 (Orbit 2948)
---------------------------------------
Vector Time (GMT): 2015/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 807288
98 A = 6774589
30 meter
Y = -4403612
52 meter E =
0015969
Z = -5098764
66 I = 51
85006
XDOT = 6687
903661 Wp = 78
95527
YDOT = 3281
212730 meter/sec RA = 36
93126 deg
ZDOT = -1776
696151 TA = 173
89647
MA = 173
87699
Ha = 219
959 n
mi
Hp = 211
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2648585
91 X = 881239
20
Y = -14447547
63 feet Y = -4394170
95 meter
Z = -16728230
53 Z = -5094663
77
XDOT = 21941
941146 XDOT = 6659
345846
YDOT = 10765
133629 feet/sec YDOT = 3355
841729 meter/sec
ZDOT = -5829
055613 ZDOT = -1744
276576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14588962
30 X = -4446715
71
Y = -1878611
79 feet Y = -572600
87 meter
Z = -16709677
83 Z = -5093109
80
XDOT = 9282
565534 XDOT = 2829
325975
YDOT = -21523
924022 feet/sec YDOT = -6560
492042 meter/sec
ZDOT = -5690
296573 ZDOT = -1734
402395
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 15177
51908873
00016717 00000-0 10270-3 0 9043
2 25544 51
6439 37
4329 0002713 91
1310 269
0155 15
55421885 29492
Satellite: ISS
Catalog Number: 25544
Epoch time: 15177
51908873 = yrday
fracday
Element set: 904
Inclination: 51
6439 deg
RA of node: 37
4329 deg
Eccentricity:
0002713
Arg of perigee: 91
1310 deg
Mean anomaly: 269
0155 deg
Mean motion: 15
55421885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2949
Checksum: 319
Coasting Arc #6 (Orbit 2964)
---------------------------------------
Vector Time (GMT): 2015/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2808826
41 A = 6773660
65 meter
Y = 3152673
31 meter E =
0005475
Z = 5292049
15 I = 51
82151
XDOT = -6212
186358 Wp = 78
32908
YDOT = -4462
014717 meter/sec RA = 31
93146 deg
ZDOT = -637
373646 TA = 17
74466
MA = 17
72554
Ha = 220
010 n
mi
Hp = 211
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9215309
73 X = -2869578
50
Y = 10343416
36 feet Y = 3120922
94 meter
Z = 17362365
98 Z = 5278257
12
XDOT = -20381
188839 XDOT = -6158
733200
YDOT = -14639
155895 feet/sec YDOT = -4531
184512 meter/sec
ZDOT = -2091
120885 ZDOT = -667
422000
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11036388
77 X = 3363891
30
Y = 8496202
21 feet Y = 2589642
43 meter
Z = 17302387
66 Z = 5273767
76
XDOT = -12398
001270 XDOT = -3778
910787
YDOT = 20635
548861 feet/sec YDOT = 6289
715293 meter/sec
ZDOT = -2219
425280 ZDOT = -676
480825
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 15178
54706052
00016717 00000-0 10270-3 0 9053
2 25544 51
6442 32
2985 0002682 95
8394 264
3065 15
55445739 29655
Satellite: ISS
Catalog Number: 25544
Epoch time: 15178
54706052 = yrday
fracday
Element set: 905
Inclination: 51
6442 deg
RA of node: 32
2985 deg
Eccentricity:
0002682
Arg of perigee: 95
8394 deg
Mean anomaly: 264
3065 deg
Mean motion: 15
55445739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2965
Checksum: 332
Coasting Arc #7 (Orbit 2979)
---------------------------------------
Vector Time (GMT): 2015/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4622410
75 A = 6776361
23 meter
Y = -1753081
80 meter E =
0012844
Z = -4646989
18 I = 51
80201
XDOT = 4898
322450 Wp = 107
29497
YDOT = 5094
990530 meter/sec RA = 26
93137 deg
ZDOT = 2953
331361 TA = 192
06994
MA = 192
10074
Ha = 219
828 n
mi
Hp = 211
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15165389
60 X = 4664244
00
Y = -5751580
72 feet Y = -1701156
52 meter
Z = -15246027
50 Z = -4624432
92
XDOT = 16070
611713 XDOT = 4826
638758
YDOT = 16715
848194 feet/sec YDOT = 5149
365616 meter/sec
ZDOT = 9689
407351 ZDOT = 2976
953057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7171088
11 X = -2185747
65
Y = -14649404
96 feet Y = -4465138
63 meter
Z = -15148647
02 Z = -4617307
61
XDOT = 14059
034789 XDOT = 4285
193804
YDOT = -16995
388057 feet/sec YDOT = -5180
194280 meter/sec
ZDOT = 9789
928973 ZDOT = 2983
970351
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 15179
51076451
00016717 00000-0 10270-3 0 9065
2 25544 51
6429 27
4834 0002611 98
9233 261
2216 15
55482947 29800
Satellite: ISS
Catalog Number: 25544
Epoch time: 15179
51076451 = yrday
fracday
Element set: 906
Inclination: 51
6429 deg
RA of node: 27
4834 deg
Eccentricity:
0002611
Arg of perigee: 98
9233 deg
Mean anomaly: 261
2216 deg
Mean motion: 15
55482947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2980
Checksum: 319
Coasting Arc #8 (Orbit 2995)
---------------------------------------
Vector Time (GMT): 2015/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5960198
87 A = 6780945
30 meter
Y = 317586
28 meter E =
0015283
Z = 3203610
66 I = 51
78957
XDOT = -2875
561566 Wp = 94
53187
YDOT = -5242
239541 meter/sec RA = 21
94435 deg
ZDOT = -4811
646573 TA = 48
46355
MA = 48
33256
Ha = 219
728 n
mi
Hp = 211
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19554458
25 X = -5978869
19
Y = 1041949
74 feet Y = 250830
61 meter
Z = 10510533
67 Z = 3174611
80
XDOT = -9434
257107 XDOT = -2793
354648
YDOT = -17198
948625 feet/sec YDOT = -5273
935651 meter/sec
ZDOT = -15786
242039 ZDOT = -4825
416565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3228374
26 X = 984008
47
Y = 19381631
77 feet Y = 5907521
36 meter
Z = 10385748
14 Z = 3165576
03
XDOT = -14636
730988 XDOT = -4461
275605
YDOT = 10961
297914 feet/sec YDOT = 3341
003604 meter/sec
ZDOT = -15844
354584 ZDOT = -4829
359277
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 15180
53869379
00016717 00000-0 10270-3 0 9079
2 25544 51
6432 22
3486 0002404 99
4509 260
6917 15
55549143 29963
Satellite: ISS
Catalog Number: 25544
Epoch time: 15180
53869379 = yrday
fracday
Element set: 907
Inclination: 51
6432 deg
RA of node: 22
3486 deg
Eccentricity:
0002404
Arg of perigee: 99
4509 deg
Mean anomaly: 260
6917 deg
Mean motion: 15
55549143 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2996
Checksum: 336
Coasting Arc #9 (Orbit 3010)
---------------------------------------
Vector Time (GMT): 2015/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6592155
71 A = 6784630
47 meter
Y = 976516
88 meter E =
0010328
Z = -1256699
24 I = 51
77034
XDOT = 377
456230 Wp = 50
31292
YDOT = 4937
549130 meter/sec RA = 16
96928 deg
ZDOT = 5855
089435 TA = 296
04214
MA = 296
14845
Ha = 219
716 n
mi
Hp = 211
608
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21627807
45 X = 6586850
69
Y = 3203795
54 feet Y = 1050205
20 meter
Z = -4123029
00 Z = -1224688
61
XDOT = 1238
373457 XDOT = 293
773528
YDOT = 16199
308170 feet/sec YDOT = 4941
301338 meter/sec
ZDOT = 19209
611006 ZDOT = 5856
720508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 387905
17 X = 118233
49
Y = -21885852
06 feet Y = -6670807
71 meter
Z = -3985566
23 Z = -1214800
59
XDOT = 14326
507926 XDOT = 4366
719616
YDOT = -3221
643684 feet/sec YDOT = -981
956995 meter/sec
ZDOT = 19215
576548 ZDOT = 5856
907732
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 15181
50236074
00016717 00000-0 10270-3 0 9088
2 25544 51
6416 17
5334 0002479 105
9476 254
1950 15
55528636 30119
Satellite: ISS
Catalog Number: 25544
Epoch time: 15181
50236074 = yrday
fracday
Element set: 908
Inclination: 51
6416 deg
RA of node: 17
5334 deg
Eccentricity:
0002479
Arg of perigee: 105
9476 deg
Mean anomaly: 254
1950 deg
Mean motion: 15
55528636 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3011
Checksum: 301
Coasting Arc #10 (Orbit 3026)
---------------------------------------
Vector Time (GMT): 2015/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6369217
10 A = 6784687
20 meter
Y = -2120991
08 meter E =
0011903
Z = -951469
21 I = 51
74041
XDOT = 2305
290656 Wp = 134
17422
YDOT = -4288
198097 meter/sec RA = 12
00061 deg
ZDOT = -5926
648573 TA = 56
12082
MA = 56
00764
Ha = 219
563 n
mi
Hp = 211
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20896381
57 X = -6340404
44
Y = -6958632
16 feet Y = -2192054
60 meter
Z = -3121618
14 Z = -982339
80
XDOT = 7563
289553 XDOT = 2381
860256
YDOT = -14068
891393 feet/sec YDOT = -4261
989824 meter/sec
ZDOT = -19444
385083 ZDOT = -5915
264634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3840141
90 X = -1170475
25
Y = 21667742
22 feet Y = 6604327
83 meter
Z = -3253933
23 Z = -991798
85
XDOT = -13461
260291 XDOT = -4102
992137
YDOT = -5272
759639 feet/sec YDOT = -1607
137138 meter/sec
ZDOT = -19394
512209 ZDOT = -5911
447321
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 15182
53024999
00016717 00000-0 10270-3 0 9094
2 25544 51
6415 12
3979 0002476 107
2193 252
9231 15
55581957 30274
Satellite: ISS
Catalog Number: 25544
Epoch time: 15182
53024999 = yrday
fracday
Element set: 909
Inclination: 51
6415 deg
RA of node: 12
3979 deg
Eccentricity:
0002476
Arg of perigee: 107
2193 deg
Mean anomaly: 252
9231 deg
Mean motion: 15
55581957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3027
Checksum: 322
Coasting Arc #11 (Orbit 3042)
---------------------------------------
Vector Time (GMT): 2015/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5296906
31 A = 6781189
56 meter
Y = 3010573
26 meter E =
0015280
Z = 2963178
20 I = 51
69708
XDOT = -4734
973136 Wp = 87
54895
YDOT = 3392
456808 meter/sec RA = 7
02221 deg
ZDOT = 4995
826478 TA = 306
32284
MA = 306
46381
Ha = 219
441 n
mi
Hp = 211
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17378301
54 X = 5248453
81
Y = 9877208
86 feet Y = 3069535
40 meter
Z = 9721713
24 Z = 2988792
03
XDOT = -15534
688767 XDOT = -4796
824100
YDOT = 11130
107639 feet/sec YDOT = 3339
160704 meter/sec
ZDOT = 16390
506816 ZDOT = 4972
675370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6926770
83 X = 2111279
75
Y = -18693396
73 feet Y = -5697747
32 meter
Z = 9831230
45 Z = 2996559
04
XDOT = 12166
363885 XDOT = 3708
307712
YDOT = 13112
373293 feet/sec YDOT = 3996
651380 meter/sec
ZDOT = 16290
217348 ZDOT = 4965
258248
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 15183
55811759
00016717 00000-0 10270-3 0 9107
2 25544 51
6407 7
2610 0002450 115
8204 244
3203 15
55618267 30437
Satellite: ISS
Catalog Number: 25544
Epoch time: 15183
55811759 = yrday
fracday
Element set: 910
Inclination: 51
6407 deg
RA of node: 7
2610 deg
Eccentricity:
0002450
Arg of perigee: 115
8204 deg
Mean anomaly: 244
3203 deg
Mean motion: 15
55618267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3043
Checksum: 278
Coasting Arc #12 (Orbit 3057)
---------------------------------------
Vector Time (GMT): 2015/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3467054
92 A = 6776218
73 meter
Y = -3694176
97 meter E =
0011742
Z = -4511204
93 I = 51
64915
XDOT = 6580
002885 Wp = 78
18637
YDOT = -2289
876452 meter/sec RA = 2
02689 deg
ZDOT = -3186
534657 TA = 159
80628
MA = 159
75980
Ha = 219
495 n
mi
Hp = 211
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11374852
09 X = -3403574
62
Y = -12120003
18 feet Y = -3732592
33 meter
Z = -14800541
12 Z = -4527893
28
XDOT = 21587
935976 XDOT = 6620
598577
YDOT = -7512
718018 feet/sec YDOT = -2216
067161 meter/sec
ZDOT = -10454
510030 ZDOT = -3154
472394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9895980
15 X = -3016294
75
Y = 13275729
97 feet Y = 4046442
49 meter
Z = -14871527
33 Z = -4532841
53
XDOT = -10316
064258 XDOT = -3144
336386
YDOT = -19228
865953 feet/sec YDOT = -5860
958343 meter/sec
ZDOT = -10316
133288 ZDOT = -3144
357426
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 15184
52172563
00016717 00000-0 10270-3 0 9119
2 25544 51
6408 2
4460 0002591 114
9437 245
1986 15
55643204 30584
Satellite: ISS
Catalog Number: 25544
Epoch time: 15184
52172563 = yrday
fracday
Element set: 911
Inclination: 51
6408 deg
RA of node: 2
4460 deg
Eccentricity:
0002591
Arg of perigee: 114
9437 deg
Mean anomaly: 245
1986 deg
Mean motion: 15
55643204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3058
Checksum: 297
Coasting Arc #13 (Orbit 3073)
---------------------------------------
Vector Time (GMT): 2015/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1164100
85 A = 6773212
61 meter
Y = 4108033
62 meter E =
0005768
Z = 5253814
72 I = 51
60681
XDOT = -7554
563211 Wp = 118
03832
YDOT = 1061
234117 meter/sec RA = 357
01347 deg
ZDOT = 840
730096 TA = 323
90803
MA = 323
94696
Ha = 219
482 n
mi
Hp = 211
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3819228
51 X = 1092556
64
Y = 13477800
59 feet Y = 4120650
76 meter
Z = 17236924
94 Z = 5259296
29
XDOT = -24785
312372 XDOT = -7569
952605
YDOT = 3481
739230 feet/sec YDOT = 976
667905 meter/sec
ZDOT = 2758
300839 ZDOT = 803
994788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12486639
19 X = 3805927
63
Y = -6287944
87 feet Y = -1916565
60 meter
Z = 17259628
84 Z = 5260734
87
XDOT = 7833
339581 XDOT = 2387
601904
YDOT = 22722
634793 feet/sec YDOT = 6925
859085 meter/sec
ZDOT = 2600
092393 ZDOT = 792
508161
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 15185
54955373
00016717 00000-0 10270-3 0 9121
2 25544 51
6407 357
3092 0002555 118
1671 241
9741 15
55620116 30740
Satellite: ISS
Catalog Number: 25544
Epoch time: 15185
54955373 = yrday
fracday
Element set: 912
Inclination: 51
6407 deg
RA of node: 357
3092 deg
Eccentricity:
0002555
Arg of perigee: 118
1671 deg
Mean anomaly: 241
9741 deg
Mean motion: 15
55620116 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3074
Checksum: 305
Coasting Arc #14 (Orbit 3088)
---------------------------------------
Vector Time (GMT): 2015/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1302902
52 A = 6773780
04 meter
Y = -4273230
31 meter E =
0015810
Z = -5106000
23 I = 51
57838
XDOT = 7469
725925 Wp = 105
75198
YDOT = 285
091175 meter/sec RA = 351
99359 deg
ZDOT = 1667
570272 TA = 180
38280
MA = 180
38401
Ha = 219
385 n
mi
Hp = 211
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4274614
56 X = 1375392
63
Y = -14019784
47 feet Y = -4258254
63 meter
Z = -16751969
27 Z = -5099495
39
XDOT = 24506
974819 XDOT = 7457
882495
YDOT = 935
338501 feet/sec YDOT = 368
556174 meter/sec
ZDOT = 5471
031076 ZDOT = 1703
827463
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14633458
31 X = -4460278
09
Y = -1286533
32 feet Y = -392135
36 meter
Z = -16723094
53 Z = -5097199
21
XDOT = -4404
379054 XDOT = -1342
454736
YDOT = -23040
088231 feet/sec YDOT = -7022
618893 meter/sec
ZDOT = 5626
892526 ZDOT = 1715
076842
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 15186
51312054
00016717 00000-0 10270-3 0 9133
2 25544 51
6415 352
4941 0002591 123
5169 236
6233 15
55693262 30895
Satellite: ISS
Catalog Number: 25544
Epoch time: 15186
51312054 = yrday
fracday
Element set: 913
Inclination: 51
6415 deg
RA of node: 352
4941 deg
Eccentricity:
0002591
Arg of perigee: 123
5169 deg
Mean anomaly: 236
6233 deg
Mean motion: 15
55693262 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3089
Checksum: 302
Coasting Arc #15 (Orbit 3104)
---------------------------------------
Vector Time (GMT): 2015/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3565245
60 A = 6777908
79 meter
Y = 4109284
97 meter E =
0012629
Z = 4032257
60 I = 51
56047
XDOT = -6387
150658 Wp = 86
69155
YDOT = -1701
781123 meter/sec RA = 346
98049 deg
ZDOT = -3901
844993 TA = 43
82471
MA = 43
72457
Ha = 219
379 n
mi
Hp = 211
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11697000
01 X = -3630518
58
Y = 13481906
07 feet Y = 4069050
81 meter
Z = 13229191
59 Z = 4014780
31
XDOT = -20955
218694 XDOT = -6348
692777
YDOT = -5583
271400 feet/sec YDOT = -1772
991116 meter/sec
ZDOT = -12801
328716 ZDOT = -3932
778839
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15833695
83 X = 4826110
49
Y = 8359499
51 feet Y = 2547975
45 meter
Z = 13153172
81 Z = 4009087
07
XDOT = -18
126233 XDOT = -5
524876
YDOT = 20443
673705 feet/sec YDOT = 6231
231745 meter/sec
ZDOT = -12933
993576 ZDOT = -3942
281242
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 15187
54090555
00016717 00000-0 10270-3 0 9147
2 25544 51
6411 347
3577 0002500 127
4828 232
6553 15
55706044 31057
Satellite: ISS
Catalog Number: 25544
Epoch time: 15187
54090555 = yrday
fracday
Element set: 914
Inclination: 51
6411 deg
RA of node: 347
3577 deg
Eccentricity:
0002500
Arg of perigee: 127
4828 deg
Mean anomaly: 232
6553 deg
Mean motion: 15
55706044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3105
Checksum: 298
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