[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 11th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 78 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 651 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
165/09:20:13
000 0
0 0
0 0
0
N/A 0
0 0
0 219
5
000/00:00:00
000 0
0 0
0 216
7
167/11:41:08
000 0
0 0
0 0
0
N/A 0
0 0
0 219
7
000/00:00:00
000 0
0 0
0 216
6
167/16:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
6
000/00:00:00
000 0
0 0
0 216
4
Coasting Arc #1 (Orbit 2054)
---------------------------------------
Vector Time (GMT): 2017/160/11:33:58
253
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -781215
87 A = 6789216
72 meter
Y = -6648818
49 meter E =
0008596
Z = -1096439
47 I = 52
02438
XDOT = 4861
620917 Wp = 171
31357
YDOT = 402
141180 meter/sec RA = 75
95343 deg
ZDOT = -5916
788963 TA = 20
51827
MA = 20
48376
Ha = 219
675 n
mi
Hp = 216
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2563044
21 X = -701482
96
Y = -21813708
95 feet Y = -6657108
61 meter
Z = -3597242
35 Z = -1100041
68
XDOT = 15950
199858 XDOT = 4885
503875
YDOT = 1319
360826 feet/sec YDOT = 456
641486 meter/sec
ZDOT = -19412
037281 ZDOT = -5893
114418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21424035
00 X = -6530045
87
Y = -4828229
40 feet Y = -1471644
32 meter
Z = -3611948
47 Z = -1100921
89
XDOT = 6215
485948 XDOT = 1894
480117
YDOT = -13170
766264 feet/sec YDOT = -4014
449557 meter/sec
ZDOT = -19307
553902 ZDOT = -5884
942429
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 17160
51196400
00016717 00000-0 10270-3 0 9008
2 25544 51
6417 76
5897 0004697 256
9367 103
1262 15
53990213 20557
Satellite: ISS
Catalog Number: 25544
Epoch time: 17160
51196400 = yrday
fracday
Element set: 900
Inclination: 51
6417 deg
RA of node: 76
5897 deg
Eccentricity:
0004697
Arg of perigee: 256
9367 deg
Mean anomaly: 103
1262 deg
Mean motion: 15
53990213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2055
Checksum: 309
Coasting Arc #2 (Orbit 2070)
---------------------------------------
Vector Time (GMT): 2017/161/11:33:58
253
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -47605
34 A = 6786720
60 meter
Y = 6239885
85 meter E =
0008935
Z = 2657750
66 I = 52
00741
XDOT = -5113
513341 Wp = 75
52674
YDOT = -2276
863889 meter/sec RA = 71
00595 deg
ZDOT = 5241
535420 TA = 314
28957
MA = 314
36283
Ha = 219
581 n
mi
Hp = 216
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -156185
50 X = -130287
98
Y = 20472066
45 feet Y = 6238890
80 meter
Z = 8719654
41 Z = 2657319
50
XDOT = -16776
618573 XDOT = -5113
133781
YDOT = -7470
025882 feet/sec YDOT = -2334
045303 meter/sec
ZDOT = 17196
638516 ZDOT = 5216
695973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19364156
81 X = 5902194
99
Y = 6649244
04 feet Y = 2026689
58 meter
Z = 8716608
09 Z = 2656822
15
XDOT = -11921
909584 XDOT = -3633
798041
YDOT = 12265
474846 feet/sec YDOT = 3738
516733 meter/sec
ZDOT = 17087
350118 ZDOT = 5208
224316
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 17161
54088048
00016717 00000-0 10270-3 0 9011
2 25544 51
6418 71
4617 0004644 261
8240 98
2386 15
53997071 20717
Satellite: ISS
Catalog Number: 25544
Epoch time: 17161
54088048 = yrday
fracday
Element set: 901
Inclination: 51
6418 deg
RA of node: 71
4617 deg
Eccentricity:
0004644
Arg of perigee: 261
8240 deg
Mean anomaly: 98
2386 deg
Mean motion: 15
53997071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2071
Checksum: 312
Coasting Arc #3 (Orbit 2085)
---------------------------------------
Vector Time (GMT): 2017/162/11:33:58
253
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 994400
54 A = 6782976
23 meter
Y = -5409924
21 meter E =
0002511
Z = -3971871
06 I = 51
98448
XDOT = 5198
501056 Wp = 47
83299
YDOT = 3922
176353 meter/sec RA = 66
04980 deg
ZDOT = -4040
727362 TA = 180
16000
MA = 180
16008
Ha = 219
499 n
mi
Hp = 216
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3262468
96 X = 1074115
29
Y = -17749095
17 feet Y = -5398357
85 meter
Z = -13031073
04 Z = -3966847
73
XDOT = 17055
449659 XDOT = 5173
883828
YDOT = 12868
032655 feet/sec YDOT = 3980
172463 meter/sec
ZDOT = -13256
979535 ZDOT = -4015
533774
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15941524
24 X = -4858976
59
Y = -8493859
48 feet Y = -2588928
37 meter
Z = -13007886
20 Z = -3964803
71
XDOT = 16778
045064 XDOT = 5113
948136
YDOT = -11356
431294 feet/sec YDOT = -3461
440259 meter/sec
ZDOT = -13146
431742 ZDOT = -4007
032395
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 17162
50548604
00016717 00000-0 10270-3 0 9028
2 25544 51
6426 66
6548 0004613 266
3535 93
7090 15
54022488 20868
Satellite: ISS
Catalog Number: 25544
Epoch time: 17162
50548604 = yrday
fracday
Element set: 902
Inclination: 51
6426 deg
RA of node: 66
6548 deg
Eccentricity:
0004613
Arg of perigee: 266
3535 deg
Mean anomaly: 93
7090 deg
Mean motion: 15
54022488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2086
Checksum: 310
Coasting Arc #4 (Orbit 2101)
---------------------------------------
Vector Time (GMT): 2017/163/11:33:58
253
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2011716
93 A = 6779605
41 meter
Y = 4254925
59 meter E =
0003870
Z = 4879965
42 I = 51
95846
XDOT = -5066
221505 Wp = 159
96131
YDOT = -5208
462808 meter/sec RA = 61
08270 deg
ZDOT = 2448
736222 TA = 266
09353
MA = 266
13777
Ha = 219
534 n
mi
Hp = 216
553
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6600121
15 X = -2082851
60
Y = 13959729
63 feet Y = 4232030
78 meter
Z = 16010385
24 Z = 4870020
94
XDOT = -16621
461631 XDOT = -5019
497342
YDOT = -17088
132571 feet/sec YDOT = -5264
855825 meter/sec
ZDOT = 8033
911488 ZDOT = 2424
238812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11503112
16 X = 3506148
59
Y = 10370338
18 feet Y = 3160879
08 meter
Z = 15965668
88 Z = 4866335
87
XDOT = -20340
449369 XDOT = -6199
768968
YDOT = 10337
913580 feet/sec YDOT = 3150
996059 meter/sec
ZDOT = 7926
681886 ZDOT = 2416
052639
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 17163
53439734
00016717 00000-0 10270-3 0 9036
2 25544 51
6420 61
5270 0004672 268
8950 91
1667 15
54018274 21020
Satellite: ISS
Catalog Number: 25544
Epoch time: 17163
53439734 = yrday
fracday
Element set: 903
Inclination: 51
6420 deg
RA of node: 61
5270 deg
Eccentricity:
0004672
Arg of perigee: 268
8950 deg
Mean anomaly: 91
1667 deg
Mean motion: 15
54018274 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2102
Checksum: 300
Coasting Arc #5 (Orbit 2116)
---------------------------------------
Vector Time (GMT): 2017/164/11:33:58
253
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3072990
50 A = 6777727
07 meter
Y = -2888453
94 meter E =
0010003
Z = -5314412
64 I = 51
93658
XDOT = 4645
527093 Wp = 81
36595
YDOT = 6061
566412 meter/sec RA = 56
10710 deg
ZDOT = -607
839375 TA = 182
84758
MA = 182
85328
Ha = 219
403 n
mi
Hp = 216
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10081989
83 X = 3130876
33
Y = -9476554
93 feet Y = -2853765
32 meter
Z = -17435737
02 Z = -5299344
81
XDOT = 15241
230621 XDOT = 4580
352383
YDOT = 19887
028910 feet/sec YDOT = 6113
151509 meter/sec
ZDOT = -1994
223670 ZDOT = -585
430375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6430692
19 X = -1960074
98
Y = -12346376
48 feet Y = -3763175
55 meter
Z = -17368641
96 Z = -5293962
07
XDOT = 22322
975617 XDOT = 6804
042968
YDOT = -8957
019965 feet/sec YDOT = -2730
099685 meter/sec
ZDOT = -1896
383972 ZDOT = -578
017835
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 17164
49899828
00016717 00000-0 10270-3 0 9047
2 25544 51
6429 56
7197 0004774 273
7597 86
3010 15
54038084 21173
Satellite: ISS
Catalog Number: 25544
Epoch time: 17164
49899828 = yrday
fracday
Element set: 904
Inclination: 51
6429 deg
RA of node: 56
7197 deg
Eccentricity:
0004774
Arg of perigee: 273
7597 deg
Mean anomaly: 86
3010 deg
Mean motion: 15
54038084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2117
Checksum: 344
Coasting Arc #6 (Orbit 2130)
---------------------------------------
Vector Time (GMT): 2017/165/09:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5025435
58 A = 6781131
09 meter
Y = 648935
49 meter E =
0004969
Z = -4511465
93 I = 51
92883
XDOT = 2041
108385 Wp = 122
14269
YDOT = 6642
939919 meter/sec RA = 51
57571 deg
ZDOT = 3229
193720 TA = 180
22017
MA = 180
22039
Ha = 219
539 n
mi
Hp = 216
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16487649
54 X = 5039719
94
Y = 2129053
43 feet Y = 705213
72 meter
Z = -14801397
42 Z = -4487019
22
XDOT = 6696
549818 XDOT = 1950
987792
YDOT = 21794
422307 feet/sec YDOT = 6665
260694 meter/sec
ZDOT = 10594
467585 ZDOT = 3238
890674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13738508
68 X = 4187497
44
Y = -9529429
39 feet Y = -2904570
08 meter
Z = -14693542
00 Z = -4478591
60
XDOT = 18825
794509 XDOT = 5738
102166
YDOT = 10741
278248 feet/sec YDOT = 3273
941610 meter/sec
ZDOT = 10636
043891 ZDOT = 3241
866178
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 17165
39929034
00016717 00000-0 10270-3 0 9051
2 25544 51
6411 52
2314 0004699 277
8756 82
1863 15
54025563 21318
Satellite: ISS
Catalog Number: 25544
Epoch time: 17165
39929034 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 52
2314 deg
Eccentricity:
0004699
Arg of perigee: 277
8756 deg
Mean anomaly: 82
1863 deg
Mean motion: 15
54025563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2131
Checksum: 313
Coasting Arc #7 (Orbit 2146)
---------------------------------------
Vector Time (GMT): 2017/166/09:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5529419
18 A = 6784871
28 meter
Y = -1984671
04 meter E =
0007934
Z = 3388287
19 I = 51
92026
XDOT = -691
720527 Wp = 84
32956
YDOT = -6048
902472 meter/sec RA = 46
61016 deg
ZDOT = -4661
822057 TA = 56
27244
MA = 56
19685
Ha = 219
633 n
mi
Hp = 216
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18141139
04 X = -5523273
70
Y = -6511387
93 feet Y = -2046470
75 meter
Z = 11116427
78 Z = 3361441
76
XDOT = -2269
424300 XDOT = -601
383917
YDOT = -19845
480550 feet/sec YDOT = -6056
132164 meter/sec
ZDOT = -15294
691788 ZDOT = -4664
963439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17754754
17 X = -5411649
07
Y = 7673436
34 feet Y = 2338863
40 meter
Z = 10998233
68 Z = 3352261
63
XDOT = -14572
378764 XDOT = -4441
661047
YDOT = -11729
451855 feet/sec YDOT = -3575
136925 meter/sec
ZDOT = -15307
419157 ZDOT = -4665
701359
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 17166
42819322
00016717 00000-0 10270-3 0 9065
2 25544 51
6410 47
1040 0004735 281
8957 78
1665 15
54023235 21471
Satellite: ISS
Catalog Number: 25544
Epoch time: 17166
42819322 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 47
1040 deg
Eccentricity:
0004735
Arg of perigee: 281
8957 deg
Mean anomaly: 78
1665 deg
Mean motion: 15
54023235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2147
Checksum: 300
Coasting Arc #8 (Orbit 2161)
---------------------------------------
Vector Time (GMT): 2017/167/09:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 907581
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5733085
48 A = 6788081
25 meter
Y = 3063639
32 meter E =
0006724
Z = -1940456
72 I = 51
90847
XDOT = -847
925153 Wp = 357
84566
YDOT = 5144
237118 meter/sec RA = 41
65155 deg
ZDOT = 5622
558037 TA = 340
84217
MA = 340
86745
Ha = 219
693 n
mi
Hp = 216
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18809335
55 X = 5707826
74
Y = 10051310
10 feet Y = 3127609
52 meter
Z = -6366327
83 Z = -1912668
26
XDOT = -2781
906670 XDOT = -932
697944
YDOT = 16877
418365 feet/sec YDOT = 5134
280523 meter/sec
ZDOT = 18446
712721 ZDOT = 5618
233666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20538842
69 X = 6260239
25
Y = -5875051
15 feet Y = -1790715
59 meter
Z = -6244179
99 Z = -1903226
06
XDOT = 9216
046569 XDOT = 2809
050994
YDOT = 12655
411120 feet/sec YDOT = 3857
369309 meter/sec
ZDOT = 18426
633121 ZDOT = 5616
437775
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 17167
39278726
00016717 00000-0 10270-3 0 9070
2 25544 51
6415 42
2960 0004832 285
2268 74
8350 15
54028641 21621
Satellite: ISS
Catalog Number: 25544
Epoch time: 17167
39278726 = yrday
fracday
Element set: 907
Inclination: 51
6415 deg
RA of node: 42
2960 deg
Eccentricity:
0004832
Arg of perigee: 285
2268 deg
Mean anomaly: 74
8350 deg
Mean motion: 15
54028641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2162
Checksum: 315
Coasting Arc #9 (Orbit 2163)
---------------------------------------
Vector Time (GMT): 2017/167/11:41:08
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5605550
96 A = 6789088
02 meter
Y = -3615700
68 meter E =
0009273
Z = 1235848
86 I = 51
91058
XDOT = 1690
119475 Wp = 130
32833
YDOT = -4634
689524 meter/sec RA = 41
17266 deg
ZDOT = -5870
517047 TA = 36
28859
MA = 36
22574
Ha = 219
659 n
mi
Hp = 216
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18390915
22 X = -5570705
77
Y = -11862535
05 feet Y = -3678191
04 meter
Z = 4054622
25 Z = 1208703
15
XDOT = 5545
011401 XDOT = 1770
336245
YDOT = -15205
674292 feet/sec YDOT = -4615
340398 meter/sec
ZDOT = -19260
226532 ZDOT = -5862
112572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15060294
05 X = -4590377
63
Y = 15908660
55 feet Y = 4848959
74 meter
Z = 3935419
22 Z = 1199515
78
XDOT = -12737
977811 XDOT = -3882
535637
YDOT = -7284
278714 feet/sec YDOT = -2220
248152 meter/sec
ZDOT = -19222
223422 ZDOT = -5858
933699
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 17167
52139968
00016717 00000-0 10270-3 0 9080
2 25544 51
6428 41
6563 0004768 284
6201 75
4422 15
54001844 21640
Satellite: ISS
Catalog Number: 25544
Epoch time: 17167
52139968 = yrday
fracday
Element set: 908
Inclination: 51
6428 deg
RA of node: 41
6563 deg
Eccentricity:
0004768
Arg of perigee: 284
6201 deg
Mean anomaly: 75
4422 deg
Mean motion: 15
54001844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2164
Checksum: 314
Coasting Arc #10 (Orbit 2166)
---------------------------------------
Vector Time (GMT): 2017/167/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3171033
41 A = 6786551
49 meter
Y = -5388062
25 meter E =
0001805
Z = -2637146
00 I = 51
89446
XDOT = 5546
342344 Wp = 194
84111
YDOT = -697
706245 meter/sec RA = 40
20402 deg
ZDOT = -5244
587412 TA = 14
75732
MA = 14
75206
Ha = 219
588 n
mi
Hp = 216
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10403652
91 X = -3097737
05
Y = -17677369
60 feet Y = -5423112
83 meter
Z = -8652053
81 Z = -2652372
36
XDOT = 18196
661235 XDOT = 5579
207688
YDOT = -2289
062484 feet/sec YDOT = -635
499047 meter/sec
ZDOT = -17206
651613 ZDOT = -5217
565243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 753735
14 X = 229738
47
Y = 20469660
59 feet Y = 6239152
55 meter
Z = -8718274
13 Z = -2657329
95
XDOT = -15721
647276 XDOT = -4791
958090
YDOT = -6697
471384 feet/sec YDOT = -2041
389278 meter/sec
ZDOT = -17087
172706 ZDOT = -5208
170241
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 17167
71431690
00016717 00000-0 10270-3 0 9099
2 25544 51
6394 40
6892 0004655 284
3892 75
6743 15
54053825 21671
Satellite: ISS
Catalog Number: 25544
Epoch time: 17167
71431690 = yrday
fracday
Element set: 909
Inclination: 51
6394 deg
RA of node: 40
6892 deg
Eccentricity:
0004655
Arg of perigee: 284
3892 deg
Mean anomaly: 75
6743 deg
Mean motion: 15
54053825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2167
Checksum: 334
Coasting Arc #11 (Orbit 2182)
---------------------------------------
Vector Time (GMT): 2017/168/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1935107
99 A = 6782897
13 meter
Y = 5161989
18 meter E =
0006383
Z = 3946873
80 I = 51
85654
XDOT = -6475
108255 Wp = 96
02172
YDOT = -676
721099 meter/sec RA = 35
23838 deg
ZDOT = 4053
461090 TA = 311
72575
MA = 311
78032
Ha = 219
613 n
mi
Hp = 216
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6348779
50 X = 1858069
43
Y = 16935660
04 feet Y = 5183197
78 meter
Z = 12949061
04 Z = 3956087
31
XDOT = -21243
793486 XDOT = -6486
749515
YDOT = -2220
213578 feet/sec YDOT = -749
195587 meter/sec
ZDOT = 13298
756857 ZDOT = 4021
978601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2184764
03 X = 665916
08
Y = -17925419
07 feet Y = -5463667
73 meter
Z = 12988761
34 Z = 3958974
46
XDOT = 16640
645587 XDOT = 5072
068775
YDOT = 11578
671775 feet/sec YDOT = 3529
179157 meter/sec
ZDOT = 13159
848481 ZDOT = 4011
121817
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 17168
74321286
00016717 00000-0 10270-3 0 9104
2 25544 51
6392 35
5601 0004658 285
8445 74
2194 15
54054133 21839
Satellite: ISS
Catalog Number: 25544
Epoch time: 17168
74321286 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 35
5601 deg
Eccentricity:
0004658
Arg of perigee: 285
8445 deg
Mean anomaly: 74
2194 deg
Mean motion: 15
54054133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2183
Checksum: 307
Coasting Arc #12 (Orbit 2197)
---------------------------------------
Vector Time (GMT): 2017/169/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -453388
82 A = 6779499
31 meter
Y = -4700635
61 meter E =
0008753
Z = -4872241
34 I = 51
81851
XDOT = 7015
870051 Wp = 53
73695
YDOT = 1863
863970 meter/sec RA = 30
26333 deg
ZDOT = -2449
097610 TA = 192
25590
MA = 192
27721
Ha = 219
790 n
mi
Hp = 216
363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1487496
13 X = -377124
28
Y = -15422032
84 feet Y = -4705278
86 meter
Z = -15985043
78 Z = -4874258
96
XDOT = 23017
946363 XDOT = 7006
402984
YDOT = 6115
039272 feet/sec YDOT = 1942
267467 meter/sec
ZDOT = -8035
097147 ZDOT = -2415
039314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5583792
52 X = -1701939
96
Y = 14443582
11 feet Y = 4402403
83 meter
Z = -15993047
34 Z = -4874680
83
XDOT = -16930
507990 XDOT = -5160
418835
YDOT = -15283
362789 feet/sec YDOT = -4658
368978 meter/sec
ZDOT = -7885
051292 ZDOT = -2403
363634
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 17169
70780256
00016717 00000-0 10270-3 0 9118
2 25544 51
6397 30
7539 0004529 290
7125 69
3542 15
54049399 21984
Satellite: ISS
Catalog Number: 25544
Epoch time: 17169
70780256 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 30
7539 deg
Eccentricity:
0004529
Arg of perigee: 290
7125 deg
Mean anomaly: 69
3542 deg
Mean motion: 15
54049399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2198
Checksum: 336
Coasting Arc #13 (Orbit 2213)
---------------------------------------
Vector Time (GMT): 2017/170/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1166630
47 A = 6777750
06 meter
Y = 4063276
03 meter E =
0001807
Z = 5299126
67 I = 51
78409
XDOT = -7101
820287 Wp = 296
17436
YDOT = -2826
723710 meter/sec RA = 25
27647 deg
ZDOT = 604
915896 TA = 148
06820
MA = 148
05725
Ha = 219
989 n
mi
Hp = 216
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3827527
78 X = -1237721
16
Y = 13330958
12 feet Y = 4049831
97 meter
Z = 17385586
20 Z = 5293287
23
XDOT = -23299
935325 XDOT = -7072
621707
YDOT = -9274
027920 feet/sec YDOT = -2905
977878 meter/sec
ZDOT = 1984
632205 ZDOT = 570
487792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9256181
73 X = 2821284
19
Y = -10373564
48 feet Y = -3161862
45 meter
Z = 17359011
50 Z = 5291026
71
XDOT = 16364
793531 XDOT = 4987
989068
YDOT = 17664
489979 feet/sec YDOT = 5384
136546 meter/sec
ZDOT = 1833
150988 ZDOT = 558
744421
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 17170
73669619
00016717 00000-0 10270-3 0 9123
2 25544 51
6401 25
6245 0004642 294
5980 65
4689 15
54025970 22141
Satellite: ISS
Catalog Number: 25544
Epoch time: 17170
73669619 = yrday
fracday
Element set: 912
Inclination: 51
6401 deg
RA of node: 25
6245 deg
Eccentricity:
0004642
Arg of perigee: 294
5980 deg
Mean anomaly: 65
4689 deg
Mean motion: 15
54025970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2214
Checksum: 318
Coasting Arc #14 (Orbit 2228)
---------------------------------------
Vector Time (GMT): 2017/171/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2793617
94 A = 6778157
73 meter
Y = -3339493
71 meter E =
0009695
Z = -5203303
06 I = 51
75670
XDOT = 6662
042860 Wp = 91
35405
YDOT = 3553
463332 meter/sec RA = 20
28775 deg
ZDOT = 1298
048478 TA = 191
09347
MA = 191
11487
Ha = 220
024 n
mi
Hp = 216
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9165413
18 X = 2856028
75
Y = -10956344
18 feet Y = -3307904
01 meter
Z = -17071204
26 Z = -5189581
19
XDOT = 21857
095998 XDOT = 6615
506616
YDOT = 11658
344265 feet/sec YDOT = 3627
702458 meter/sec
ZDOT = 4258
689231 ZDOT = 1330
298335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12963012
87 X = -3951126
32
Y = 6172019
07 feet Y = 1881231
41 meter
Z = -17009960
88 Z = -5184636
08
XDOT = -14650
831352 XDOT = -4465
573396
YDOT = -18660
469179 feet/sec YDOT = -5687
711006 meter/sec
ZDOT = 4400
398952 ZDOT = 1341
241600
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 17171
70128002
00016717 00000-0 10270-3 0 9138
2 25544 51
6410 20
8179 0004579 298
3529 61
7161 15
54056388 22291
Satellite: ISS
Catalog Number: 25544
Epoch time: 17171
70128002 = yrday
fracday
Element set: 913
Inclination: 51
6410 deg
RA of node: 20
8179 deg
Eccentricity:
0004579
Arg of perigee: 298
3529 deg
Mean anomaly: 61
7161 deg
Mean motion: 15
54056388 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2229
Checksum: 303
Coasting Arc #15 (Orbit 2244)
---------------------------------------
Vector Time (GMT): 2017/172/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4301055
49 A = 6780896
79 meter
Y = 2562723
21 meter E =
0007165
Z = 4572572
35 I = 51
73392
XDOT = -5714
090487 Wp = 35
56540
YDOT = -4081
318151 meter/sec RA = 15
29968 deg
ZDOT = -3079
276304 TA = 85
23952
MA = 85
15771
Ha = 220
269 n
mi
Hp = 216
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14111074
45 X = -4351604
40
Y = 8407884
55 feet Y = 2514342
62 meter
Z = 15001877
79 Z = 4551556
53
XDOT = -18747
016032 XDOT = -5653
069676
YDOT = -13390
151415 feet/sec YDOT = -4144
875368 meter/sec
ZDOT = -10102
612546 ZDOT = -3106
886210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16376389
21 X = 4991523
43
Y = -2102246
83 feet Y = -640764
83 meter
Z = 14908578
64 Z = 4544134
77
XDOT = 11705
918373 XDOT = 3567
963920
YDOT = 18494
493031 feet/sec YDOT = 5637
121476 meter/sec
ZDOT = -10223
721305 ZDOT = -3116
190254
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 17172
73016925
00016717 00000-0 10270-3 0 9143
2 25544 51
6403 15
6891 0004519 302
0099 58
0614 15
54017133 22450
Satellite: ISS
Catalog Number: 25544
Epoch time: 17172
73016925 = yrday
fracday
Element set: 914
Inclination: 51
6403 deg
RA of node: 15
6891 deg
Eccentricity:
0004519
Arg of perigee: 302
0099 deg
Mean anomaly: 58
0614 deg
Mean motion: 15
54017133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2245
Checksum: 287
Coasting Arc #16 (Orbit 2259)
---------------------------------------
Vector Time (GMT): 2017/173/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5528728
62 A = 6784525
04 meter
Y = -1797893
62 meter E =
0002814
Z = -3495605
70 I = 51
71502
XDOT = 4307
714034 Wp = 23
22082
YDOT = 4426
854776 meter/sec RA = 10
31910 deg
ZDOT = 4540
085230 TA = 295
74735
MA = 295
77639
Ha = 220
360 n
mi
Hp = 216
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18138873
41 X = 5565402
27
Y = -5898601
11 feet Y = -1735862
02 meter
Z = -11468522
64 Z = -3468659
88
XDOT = 14132
920059 XDOT = 4235
837978
YDOT = 14523
801760 feet/sec YDOT = 4474
623949 meter/sec
ZDOT = 14895
292749 ZDOT = 4560
837033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19089455
09 X = -5818465
91
Y = -1458703
58 feet Y = -444612
85 meter
Z = -11349190
43 Z = -3459233
24
XDOT = -7574
488491 XDOT = -2308
704092
YDOT = -17374
851302 feet/sec YDOT = -5295
854677 meter/sec
ZDOT = 14986
045393 ZDOT = 4567
746636
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 17173
69474936
00016717 00000-0 10270-3 0 9150
2 25544 51
6408 10
8817 0004729 305
6984 54
3728 15
54035190 22600
Satellite: ISS
Catalog Number: 25544
Epoch time: 17173
69474936 = yrday
fracday
Element set: 915
Inclination: 51
6408 deg
RA of node: 10
8817 deg
Eccentricity:
0004729
Arg of perigee: 305
6984 deg
Mean anomaly: 54
3728 deg
Mean motion: 15
54035190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2260
Checksum: 324
Coasting Arc #17 (Orbit 2275)
---------------------------------------
Vector Time (GMT): 2017/174/16:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 922015
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6386009
14 A = 6787866
85 meter
Y = 1026326
79 meter E =
0009594
Z = 2046816
57 I = 51
69460
XDOT = -2532
027228 Wp = 102
75999
YDOT = -4641
940264 meter/sec RA = 5
34549 deg
ZDOT = -5552
394106 TA = 54
62856
MA = 54
53895
Ha = 220
386 n
mi
Hp = 216
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20951473
57 X = -6406953
62
Y = 3367213
86 feet Y = 954796
65 meter
Z = 6715277
46 Z = 2015744
58
XDOT = -8307
175946 XDOT = -2452
960817
YDOT = -15229
462808 feet/sec YDOT = -4669
812074 meter/sec
ZDOT = -18216
516095 ZDOT = -5564
502676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20781629
01 X = 6334240
52
Y = 4500302
67 feet Y = 1371692
25 meter
Z = 6577879
37 Z = 2004937
63
XDOT = 2414
464441 XDOT = 735
928762
YDOT = 15650
708725 feet/sec YDOT = 4770
336019 meter/sec
ZDOT = -18269
059801 ZDOT = -5568
409427
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 17174
72363343
00016717 00000-0 10270-3 0 9165
2 25544 51
6413 5
7528 0004664 309
2816 50
7922 15
54045726 22769
Satellite: ISS
Catalog Number: 25544
Epoch time: 17174
72363343 = yrday
fracday
Element set: 916
Inclination: 51
6413 deg
RA of node: 5
7528 deg
Eccentricity:
0004664
Arg of perigee: 309
2816 deg
Mean anomaly: 50
7922 deg
Mean motion: 15
54045726 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2276
Checksum: 308
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