[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 20th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5432 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 98 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 869 ET - UTC (sec) : 68 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 67)
---------------------------------------
Vector Time (GMT): 2016/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6491853
94 A = 6787922
71 meter
Y = -1947462
21 meter E =
0013342
Z = 248335
37 I = 51
55900
XDOT = 1589
178239 Wp = 53
67445
YDOT = -4504
711873 meter/sec RA = 195
03189 deg
ZDOT = 6000
245657 TA = 309
00502
MA = 309
12375
Ha = 220
779 n
mi
Hp = 213
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21298733
40 X = -6470800
77
Y = -6389311
70 feet Y = -2019940
74 meter
Z = 814748
59 Z = 216849
99
XDOT = 5213
839368 XDOT = 1610
285773
YDOT = -14779
238429 feet/sec YDOT = -4486
822919 meter/sec
ZDOT = 19685
845331 ZDOT = 6008
016669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16778109
24 X = -5113967
70
Y = 14599941
54 feet Y = 4450062
18 meter
Z = 678174
75 Z = 206707
66
XDOT = -8712
972467 XDOT = -2655
714008
YDOT = -10968
610464 feet/sec YDOT = -3343
232469 meter/sec
ZDOT = 19720
387288 ZDOT = 6010
774046
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 16141
56388740
00016717 00000-0 10270-3 0 9001
2 25544 51
6408 195
8427 0001546 107
3899 252
7423 15
54606860 685
Satellite: ISS
Catalog Number: 25544
Epoch time: 16141
56388740 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 195
8427 deg
Eccentricity:
0001546
Arg of perigee: 107
3899 deg
Mean anomaly: 252
7423 deg
Mean motion: 15
54606860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 68
Checksum: 320
Coasting Arc #2 (Orbit 82)
---------------------------------------
Vector Time (GMT): 2016/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5839038
01 A = 6785929
33 meter
Y = 2734407
01 meter E =
0008031
Z = -2109830
79 I = 51
58475
XDOT = -3754
489734 Wp = 134
01328
YDOT = 3776
212953 meter/sec RA = 190
05320 deg
ZDOT = -5515
126527 TA = 69
37272
MA = 69
28661
Ha = 220
761 n
mi
Hp = 213
280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19156948
84 X = 5818276
05
Y = 8971151
60 feet Y = 2799587
07 meter
Z = -6922017
03 Z = -2081515
91
XDOT = -12317
879705 XDOT = -3769
646637
YDOT = 12389
150109 feet/sec YDOT = 3734
143386 meter/sec
ZDOT = -18094
247135 ZDOT = -5533
401797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17638351
30 X = 5376169
48
Y = -11749129
06 feet Y = -3581134
54 meter
Z = -6799345
50 Z = -2072440
51
XDOT = 3391
886443 XDOT = 1033
846988
YDOT = 15573
949275 feet/sec YDOT = 4746
939739 meter/sec
ZDOT = -18174
351439 ZDOT = -5539
542319
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 16142
52808866
00016717 00000-0 10270-3 0 9015
2 25544 51
6414 191
0322 0001665 111
3987 248
7344 15
54670054 839
Satellite: ISS
Catalog Number: 25544
Epoch time: 16142
52808866 = yrday
fracday
Element set: 901
Inclination: 51
6414 deg
RA of node: 191
0322 deg
Eccentricity:
0001665
Arg of perigee: 111
3987 deg
Mean anomaly: 248
7344 deg
Mean motion: 15
54670054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 83
Checksum: 298
Coasting Arc #3 (Orbit 98)
---------------------------------------
Vector Time (GMT): 2016/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4623114
72 A = 6782137
86 meter
Y = -3329458
30 meter E =
0013521
Z = 3669380
69 I = 51
60273
XDOT = 5590
236651 Wp = 96
92047
YDOT = -2959
359377 meter/sec RA = 185
06817 deg
ZDOT = 4342
689099 TA = 306
78100
MA = 306
90502
Ha = 220
813 n
mi
Hp = 213
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15167699
22 X = -4603364
86
Y = -10923419
63 feet Y = -3381046
93 meter
Z = 12038650
57 Z = 3646970
06
XDOT = 18340
671426 XDOT = 5601
818193
YDOT = -9709
184307 feet/sec YDOT = -2896
781241 meter/sec
ZDOT = 14247
667648 ZDOT = 4369
873421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17122406
60 X = -5218909
53
Y = 7650313
64 feet Y = 2331815
60 meter
Z = 11941741
79 Z = 3639842
90
XDOT = 1384
830772 XDOT = 422
096419
YDOT = -19404
921814 feet/sec YDOT = -5914
620169 meter/sec
ZDOT = 14366
394409 ZDOT = 4378
877016
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 16143
55656586
00016717 00000-0 10270-3 0 9020
2 25544 51
6404 185
9016 0001702 112
7461 247
3872 15
54667896 992
Satellite: ISS
Catalog Number: 25544
Epoch time: 16143
55656586 = yrday
fracday
Element set: 902
Inclination: 51
6404 deg
RA of node: 185
9016 deg
Eccentricity:
0001702
Arg of perigee: 112
7461 deg
Mean anomaly: 247
3872 deg
Mean motion: 15
54667896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 99
Checksum: 326
Coasting Arc #4 (Orbit 113)
---------------------------------------
Vector Time (GMT): 2016/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2928614
68 A = 6778096
09 meter
Y = 3803031
17 meter E =
0012435
Z = -4797300
11 I = 51
62171
XDOT = -6908
441087 Wp = 77
52821
YDOT = 2047
994590 meter/sec RA = 180
07226 deg
ZDOT = -2596
936833 TA = 166
86109
MA = 166
82867
Ha = 220
705 n
mi
Hp = 213
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9608315
87 X = 2909174
12
Y = 12477136
39 feet Y = 3835672
65 meter
Z = -15739173
57 Z = -4783120
27
XDOT = -22665
489131 XDOT = -6918
213839
YDOT = 6719
142356 feet/sec YDOT = 1970
685411 meter/sec
ZDOT = -8520
133967 ZDOT = -2630
520349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15632093
07 X = 4764661
97
Y = -2356698
18 feet Y = -718321
61 meter
Z = -15678134
17 Z = -4778695
29
XDOT = -5385
768616 XDOT = -1641
582274
YDOT = 21863
779811 feet/sec YDOT = 6664
080086 meter/sec
ZDOT = -8666
561283 ZDOT = -2641
567879
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 16144
52075938
00016717 00000-0 10270-3 0 9035
2 25544 51
6408 181
0913 0001653 118
9223 241
2096 15
54667329 1148
Satellite: ISS
Catalog Number: 25544
Epoch time: 16144
52075938 = yrday
fracday
Element set: 903
Inclination: 51
6408 deg
RA of node: 181
0913 deg
Eccentricity:
0001653
Arg of perigee: 118
9223 deg
Mean anomaly: 241
2096 deg
Mean motion: 15
54667329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 114
Checksum: 297
Coasting Arc #5 (Orbit 129)
---------------------------------------
Vector Time (GMT): 2016/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -961334
39 A = 6775820
44 meter
Y = -4118745
32 meter E =
0004562
Z = 5290308
25 I = 51
64599
XDOT = 7577
832195 Wp = 115
21125
YDOT = -1078
685338 meter/sec RA = 175
06872 deg
ZDOT = 534
947116 TA = 329
67490
MA = 329
70129
Ha = 220
720 n
mi
Hp = 213
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3153984
22 X = -940904
43
Y = -13512943
95 feet Y = -4129381
90 meter
Z = 17356654
35 Z = 5285687
48
XDOT = 24861
654184 XDOT = 7586
732550
YDOT = -3538
993890 feet/sec YDOT = -993
895266 meter/sec
ZDOT = 1755
075839 ZDOT = 571
780265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13442565
49 X = -4097293
96
Y = -3538082
39 feet Y = -1078407
51 meter
Z = 17337246
81 Z = 5284392
83
XDOT = 8421
023659 XDOT = 2566
728011
YDOT = -22572
077527 feet/sec YDOT = -6879
969230 meter/sec
ZDOT = 1915
500098 ZDOT = 583
844430
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 16145
54922580
00016717 00000-0 10270-3 0 9043
2 25544 51
6402 175
9601 0001690 116
4903 243
6423 15
54690907 1303
Satellite: ISS
Catalog Number: 25544
Epoch time: 16145
54922580 = yrday
fracday
Element set: 904
Inclination: 51
6402 deg
RA of node: 175
9601 deg
Eccentricity:
0001690
Arg of perigee: 116
4903 deg
Mean anomaly: 243
6423 deg
Mean motion: 15
54690907 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 130
Checksum: 290
Coasting Arc #6 (Orbit 144)
---------------------------------------
Vector Time (GMT): 2016/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1085450
82 A = 6776572
29 meter
Y = 4307064
53 meter E =
0015067
Z = -5131409
15 I = 51
68170
XDOT = -7487
866103 Wp = 103
98634
YDOT = 24
171223 meter/sec RA = 170
06506 deg
ZDOT = 1604
602518 TA = 181
50125
MA = 181
50578
Ha = 220
636 n
mi
Hp = 213
280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3561190
36 X = -1108606
44
Y = 14130789
16 feet Y = 4294797
34 meter
Z = -16835331
84 Z = -5136737
85
XDOT = -24566
489838 XDOT = -7495
374406
YDOT = 79
301914 feet/sec YDOT = -59
605219 meter/sec
ZDOT = 5264
443958 ZDOT = 1568
209803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10963870
53 X = 3341787
74
Y = 9557669
58 feet Y = 2913177
69 meter
Z = -16859245
90 Z = -5138698
15
XDOT = -10533
253626 XDOT = -3210
535705
YDOT = 21087
560153 feet/sec YDOT = 6427
488334 meter/sec
ZDOT = 5106
089525 ZDOT = 1556
336087
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 16146
51340802
00016717 00000-0 10270-3 0 9053
2 25544 51
6415 171
1499 0001510 119
3543 240
7760 15
54673833 1450
Satellite: ISS
Catalog Number: 25544
Epoch time: 16146
51340802 = yrday
fracday
Element set: 905
Inclination: 51
6415 deg
RA of node: 171
1499 deg
Eccentricity:
0001510
Arg of perigee: 119
3543 deg
Mean anomaly: 240
7760 deg
Mean motion: 15
54673833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 145
Checksum: 287
Coasting Arc #7 (Orbit 160)
---------------------------------------
Vector Time (GMT): 2016/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2992304
70 A = 6779699
65 meter
Y = -4303324
64 meter E =
0010911
Z = 4292285
23 I = 51
72235
XDOT = 6709
797307 Wp = 78
94143
YDOT = 1112
372323 meter/sec RA = 165
07012 deg
ZDOT = -3552
709199 TA = 47
24625
MA = 47
15449
Ha = 220
537 n
mi
Hp = 213
202
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9817272
65 X = 3019352
98
Y = -14118519
16 feet Y = -4269711
86 meter
Z = 14082300
63 Z = 4306886
47
XDOT = 22013
770691 XDOT = 6714
117414
YDOT = 3649
515494 feet/sec YDOT = 1187
430227 meter/sec
ZDOT = -11655
870074 ZDOT = -3520
103910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8330068
90 X = -2539005
00
Y = -14983561
28 feet Y = -4566989
48 meter
Z = 14146570
61 Z = 4311874
72
XDOT = 11984
710822 XDOT = 3652
939859
YDOT = -17563
742097 feet/sec YDOT = -5353
428591 meter/sec
ZDOT = -11514
166634 ZDOT = -3509
517990
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 16147
54186450
00016717 00000-0 10270-3 0 9065
2 25544 51
6397 166
0190 0001620 119
6951 240
4364 15
54723278 1612
Satellite: ISS
Catalog Number: 25544
Epoch time: 16147
54186450 = yrday
fracday
Element set: 906
Inclination: 51
6397 deg
RA of node: 166
0190 deg
Eccentricity:
0001620
Arg of perigee: 119
6951 deg
Mean anomaly: 240
4364 deg
Mean motion: 15
54723278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 161
Checksum: 301
Coasting Arc #8 (Orbit 175)
---------------------------------------
Vector Time (GMT): 2016/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4545477
17 A = 6783888
80 meter
Y = 4099780
37 meter E =
0005606
Z = -2928020
14 I = 51
76849
XDOT = -5305
134736 Wp = 81
59215
YDOT = -2294
628505 meter/sec RA = 160
08934 deg
ZDOT = 5031
844854 TA = 245
08643
MA = 245
14470
Ha = 220
556 n
mi
Hp = 213
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14912982
85 X = -4576761
00
Y = 13450723
01 feet Y = 4048775
14 meter
Z = -9606365
28 Z = -2950176
66
XDOT = -17405
297690 XDOT = -5303
523954
YDOT = -7528
308742 feet/sec YDOT = -2353
945458 meter/sec
ZDOT = 16508
677344 ZDOT = 5006
077469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5787410
67 X = 1764002
77
Y = 19182005
71 feet Y = 5846675
34 meter
Z = -9703493
99 Z = -2957624
97
XDOT = -12906
547180 XDOT = -3933
915580
YDOT = 12173
815098 feet/sec YDOT = 3710
578842 meter/sec
ZDOT = 16396
916065 ZDOT = 4997
780017
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 16148
50603819
00016717 00000-0 10270-3 0 9076
2 25544 51
6410 161
2090 0001608 123
6816 236
4490 15
54722874 1767
Satellite: ISS
Catalog Number: 25544
Epoch time: 16148
50603819 = yrday
fracday
Element set: 907
Inclination: 51
6410 deg
RA of node: 161
2090 deg
Eccentricity:
0001608
Arg of perigee: 123
6816 deg
Mean anomaly: 236
4490 deg
Mean motion: 15
54722874 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 176
Checksum: 297
Coasting Arc #9 (Orbit 191)
---------------------------------------
Vector Time (GMT): 2016/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5625068
87 A = 6787010
35 meter
Y = -3605601
10 meter E =
0015298
Z = 1149857
77 I = 51
80777
XDOT = 3457
352287 Wp = 122
46124
YDOT = 3501
040278 meter/sec RA = 155
12175 deg
ZDOT = -5886
130055 TA = 45
07646
MA = 44
95244
Ha = 220
571 n
mi
Hp = 213
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18454950
37 X = 5659384
01
Y = -11829399
93 feet Y = -3542506
05 meter
Z = 3772499
23 Z = 1177266
14
XDOT = 11343
019313 XDOT = 3446
538199
YDOT = 11486
352617 feet/sec YDOT = 3539
642631 meter/sec
ZDOT = -19311
450311 ZDOT = -5869
361069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3162192
55 X = -963836
29
Y = -21670285
29 feet Y = -6605102
96 meter
Z = 3892418
29 Z = 1186409
10
XDOT = 13614
850729 XDOT = 4149
806502
YDOT = -5470
393024 feet/sec YDOT = -1667
375794 meter/sec
ZDOT = -19239
049900 ZDOT = -5864
062409
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 16149
53448439
00016717 00000-0 10270-3 0 9086
2 25544 51
6401 156
0774 0001585 122
3638 237
7669 15
54722198 1929
Satellite: ISS
Catalog Number: 25544
Epoch time: 16149
53448439 = yrday
fracday
Element set: 908
Inclination: 51
6401 deg
RA of node: 156
0774 deg
Eccentricity:
0001585
Arg of perigee: 122
3638 deg
Mean anomaly: 237
7669 deg
Mean motion: 15
54722198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 192
Checksum: 329
Coasting Arc #10 (Orbit 207)
---------------------------------------
Vector Time (GMT): 2016/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6115410
15 A = 6787275
68 meter
Y = 2835661
51 meter E =
0013540
Z = 741714
31 I = 51
83681
XDOT = -1402
226068 Wp = 59
48215
YDOT = -4605
267767 meter/sec RA = 150
16255 deg
ZDOT = 5970
942349 TA = 308
51395
MA = 308
63528
Ha = 220
446 n
mi
Hp = 213
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20063681
60 X = -6150267
67
Y = 9303351
40 feet Y = 2767079
98 meter
Z = 2433445
91 Z = 711922
53
XDOT = -4600
479226 XDOT = -1379
629004
YDOT = -15109
146217 feet/sec YDOT = -4620
822384 meter/sec
ZDOT = 19589
705869 ZDOT = 5964
185275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 561902
08 X = 171267
75
Y = 22122489
76 feet Y = 6742934
88 meter
Z = 2303266
96 Z = 702035
77
XDOT = -14128
604686 XDOT = -4306
398708
YDOT = -1704
515994 feet/sec YDOT = -519
536475 meter/sec
ZDOT = 19561
073096 ZDOT = 5962
215080
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 16150
56292385
00016717 00000-0 10270-3 0 9099
2 25544 51
6392 150
9471 0001560 134
7102 225
4178 15
54764111 2089
Satellite: ISS
Catalog Number: 25544
Epoch time: 16150
56292385 = yrday
fracday
Element set: 909
Inclination: 51
6392 deg
RA of node: 150
9471 deg
Eccentricity:
0001560
Arg of perigee: 134
7102 deg
Mean anomaly: 225
4178 deg
Mean motion: 15
54764111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 208
Checksum: 292
Coasting Arc #11 (Orbit 222)
---------------------------------------
Vector Time (GMT): 2016/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6032464
64 A = 6784859
22 meter
Y = -1725350
61 meter E =
0006720
Z = -2579717
32 I = 51
85526
XDOT = -673
843454 Wp = 129
97601
YDOT = 5517
328172 meter/sec RA = 145
20026 deg
ZDOT = -5279
088516 TA = 78
93956
MA = 78
86399
Ha = 220
560 n
mi
Hp = 213
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19791550
66 X = 6063840
85
Y = -5660599
12 feet Y = -1657716
01 meter
Z = -8463639
49 Z = -2550336
75
XDOT = -2210
772487 XDOT = -709
845777
YDOT = 18101
470381 feet/sec YDOT = 5509
591769 meter/sec
ZDOT = -17319
844214 ZDOT = -5282
449075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2335561
06 X = 711879
01
Y = -20504801
46 feet Y = -6249863
48 meter
Z = -8335425
90 Z = -2540637
81
XDOT = 14435
899837 XDOT = 4400
062270
YDOT = 8673
329068 feet/sec YDOT = 2643
630700 meter/sec
ZDOT = -17335
418884 ZDOT = -5283
835676
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 16151
52708535
00016717 00000-0 10270-3 0 9107
2 25544 51
6388 146
1358 0001499 130
0774 230
0511 15
54723128 2233
Satellite: ISS
Catalog Number: 25544
Epoch time: 16151
52708535 = yrday
fracday
Element set: 910
Inclination: 51
6388 deg
RA of node: 146
1358 deg
Eccentricity:
0001499
Arg of perigee: 130
0774 deg
Mean anomaly: 230
0511 deg
Mean motion: 15
54723128 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 223
Checksum: 284
Coasting Arc #12 (Orbit 238)
---------------------------------------
Vector Time (GMT): 2016/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5418968
50 A = 6780645
71 meter
Y = 372459
04 meter E =
0011916
Z = 4051193
67 I = 51
86738
XDOT = 2518
851137 Wp = 105
65970
YDOT = -6097
101591 meter/sec RA = 140
23009 deg
ZDOT = 3917
131615 TA = 303
81097
MA = 303
92437
Ha = 220
477 n
mi
Hp = 213
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17778768
06 X = -5442409
86
Y = 1221978
48 feet Y = 311729
25 meter
Z = 13291317
82 Z = 4024812
46
XDOT = 8263
947300 XDOT = 2567
815293
YDOT = -20003
614145 feet/sec YDOT = -6068
660549 meter/sec
ZDOT = 12851
481675 ZDOT = 3929
486318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5389552
81 X = -1642735
70
Y = 17075496
76 feet Y = 5204611
41 meter
Z = 13176383
62 Z = 4016161
73
XDOT = -14384
181637 XDOT = -4384
298563
YDOT = -14531
740147 feet/sec YDOT = -4429
274397 meter/sec
ZDOT = 12906
326893 ZDOT = 3933
848437
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 16152
55551470
00016717 00000-0 10270-3 0 9116
2 25544 51
6388 141
0049 0001328 138
1441 221
9813 15
54759555 2399
Satellite: ISS
Catalog Number: 25544
Epoch time: 16152
55551470 = yrday
fracday
Element set: 911
Inclination: 51
6388 deg
RA of node: 141
0049 deg
Eccentricity:
0001328
Arg of perigee: 138
1441 deg
Mean anomaly: 221
9813 deg
Mean motion: 15
54759555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 239
Checksum: 299
Coasting Arc #13 (Orbit 253)
---------------------------------------
Vector Time (GMT): 2016/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4396950
43 A = 6776980
44 meter
Y = 1197023
45 meter E =
0013438
Z = -5028235
52 I = 51
87826
XDOT = -4003
527095 Wp = 80
12376
YDOT = 6207
271066 meter/sec RA = 135
24761 deg
ZDOT = -2025
543528 TA = 170
24573
MA = 170
21961
Ha = 220
436 n
mi
Hp = 213
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14425690
40 X = 4407663
58
Y = 3927242
29 feet Y = 1246253
29 meter
Z = -16496835
70 Z = -5006849
83
XDOT = -13134
931414 XDOT = -4062
801442
YDOT = 20365
062551 feet/sec YDOT = 6162
169664 meter/sec
ZDOT = -6645
484016 ZDOT = -2045
135530
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8755265
38 X = 2668604
89
Y = -12244434
91 feet Y = -3732103
76 meter
Z = -16403917
38 Z = -4999914
02
XDOT = 13614
382086 XDOT = 4149
663660
YDOT = 18743
141448 feet/sec YDOT = 5712
909513 meter/sec
ZDOT = -6731
878959 ZDOT = -2051
876707
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 16153
51966454
00016717 00000-0 10270-3 0 9126
2 25544 51
6380 136
1936 0001354 133
9291 226
1974 15
54736483 2543
Satellite: ISS
Catalog Number: 25544
Epoch time: 16153
51966454 = yrday
fracday
Element set: 912
Inclination: 51
6380 deg
RA of node: 136
1936 deg
Eccentricity:
0001354
Arg of perigee: 133
9291 deg
Mean anomaly: 226
1974 deg
Mean motion: 15
54736483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 254
Checksum: 313
Coasting Arc #14 (Orbit 269)
---------------------------------------
Vector Time (GMT): 2016/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3104608
58 A = 6775561
81 meter
Y = -2800515
96 meter E =
0003315
Z = 5328899
59 I = 51
89568
XDOT = 5027
456560 Wp = 104
69025
YDOT = -5794
658716 meter/sec RA = 130
25934 deg
ZDOT = -117
058786 TA = 346
41626
MA = 346
42518
Ha = 220
475 n
mi
Hp = 213
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10185723
69 X = -3098947
69
Y = -9188044
50 feet Y = -2835202
54 meter
Z = 17483266
36 Z = 5313831
45
XDOT = 16494
280053 XDOT = 5092
448863
YDOT = -19011
347492 feet/sec YDOT = -5738
074946 meter/sec
ZDOT = -384
051136 ZDOT = -92
478866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12092820
06 X = -3685891
56
Y = 6648754
24 feet Y = 2026540
29 meter
Z = 17418137
14 Z = 5309048
20
XDOT = -11943
521658 XDOT = -3640
385401
YDOT = -21006
528203 feet/sec YDOT = -6402
789796 meter/sec
ZDOT = -275
985629 ZDOT = -84
120420
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 16154
54808574
00016717 00000-0 10270-3 0 9139
2 25544 51
6379 131
0621 0001275 141
2451 218
8794 15
54741993 2706
Satellite: ISS
Catalog Number: 25544
Epoch time: 16154
54808574 = yrday
fracday
Element set: 913
Inclination: 51
6379 deg
RA of node: 131
0621 deg
Eccentricity:
0001275
Arg of perigee: 141
2451 deg
Mean anomaly: 218
8794 deg
Mean motion: 15
54741993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 270
Checksum: 309
Coasting Arc #15 (Orbit 284)
---------------------------------------
Vector Time (GMT): 2016/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 924109
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1707356
31 A = 6777188
99 meter
Y = 4310048
84 meter E =
0013327
Z = -4955915
99 I = 51
92231
XDOT = -5542
565604 Wp = 109
50317
YDOT = 4782
660121 meter/sec RA = 125
27256 deg
ZDOT = 2250
498894 TA = 182
41202
MA = 182
41845
Ha = 220
330 n
mi
Hp = 213
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5601562
70 X = 1683107
46
Y = 14140580
20 feet Y = 4329006
57 meter
Z = -16259566
90 Z = -4947680
40
XDOT = -18184
270355 XDOT = -5606
566701
YDOT = 15691
142128 feet/sec YDOT = 4720
321378 meter/sec
ZDOT = 7383
526555 ZDOT = 2223
419100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15218645
47 X = 4638643
14
Y = -930903
74 feet Y = -283739
46 meter
Z = -16224465
38 Z = -4945217
05
XDOT = 9036
828273 XDOT = 2754
425258
YDOT = 21155
100100 feet/sec YDOT = 6448
074511 meter/sec
ZDOT = 7264
729029 ZDOT = 2214
289408
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 16155
51222407
00016717 00000-0 10270-3 0 9143
2 25544 51
6390 126
2512 0001207 141
9778 218
1460 15
54744153 2858
Satellite: ISS
Catalog Number: 25544
Epoch time: 16155
51222407 = yrday
fracday
Element set: 914
Inclination: 51
6390 deg
RA of node: 126
2512 deg
Eccentricity:
0001207
Arg of perigee: 141
9778 deg
Mean anomaly: 218
1460 deg
Mean motion: 15
54744153 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 285
Checksum: 285
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