[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 4th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 5994 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 89 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 084 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
311/14:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
3
000/00:00:00
000 0
0 0
0 215
3
314/21:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 215
7
322/07:16:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
8
000/00:00:00
000 0
0 0
0 216
7
322/20:20:13
000 0
0 0
0 0
0
N/A 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 217
0
Coasting Arc #1 (Orbit 2680)
---------------------------------------
Vector Time (GMT): 2016/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4324630
33 A = 6781039
44 meter
Y = -1767269
68 meter E =
0007830
Z = 4907684
63 I = 51
99115
XDOT = 278
493946 Wp = 120
08394
YDOT = -7288
989514 meter/sec RA = 77
41209 deg
ZDOT = -2380
371959 TA = 353
09793
MA = 353
10870
Ha = 223
811 n
mi
Hp = 214
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14188419
73 X = -4328386
78
Y = -5798128
88 feet Y = -1815651
60 meter
Z = 16101327
51 Z = 4886667
08
XDOT = 913
694050 XDOT = 371
543661
YDOT = -23914
007593 feet/sec YDOT = -7285
354937 meter/sec
ZDOT = -7809
619289 ZDOT = -2378
793063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14376460
94 X = 4381945
29
Y = -5585032
68 feet Y = -1702317
96 meter
Z = 16009593
42 Z = 4879724
07
XDOT = 15294
228233 XDOT = 4661
680765
YDOT = 17015
605145 feet/sec YDOT = 5186
356448 meter/sec
ZDOT = -7801
371040 ZDOT = -2377
857893
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 16309
54410407
00016717 00000-0 10270-3 0 9001
2 25544 51
6414 78
0075 0007508 173
2436 186
8819 15
53500653 26817
Satellite: ISS
Catalog Number: 25544
Epoch time: 16309
54410407 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 78
0075 deg
Eccentricity:
0007508
Arg of perigee: 173
2436 deg
Mean anomaly: 186
8819 deg
Mean motion: 15
53500653 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2681
Checksum: 302
Coasting Arc #2 (Orbit 2695)
---------------------------------------
Vector Time (GMT): 2016/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4377620
13 A = 6783985
44 meter
Y = 3157909
93 meter E =
0012164
Z = -4122532
67 I = 51
99314
XDOT = -1086
400181 Wp = 143
44595
YDOT = 6530
744895 meter/sec RA = 72
45052 deg
ZDOT = 3845
335210 TA = 166
17080
MA = 166
13745
Ha = 223
456 n
mi
Hp = 215
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14362270
76 X = 4362008
07
Y = 10360596
87 feet Y = 3206776
13 meter
Z = -13525369
66 Z = -4101304
81
XDOT = -3564
305055 XDOT = -1178
027221
YDOT = 21426
328397 feet/sec YDOT = 6518
083718 meter/sec
ZDOT = 12615
929168 ZDOT = 3839
835105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17576981
49 X = -5357463
96
Y = 2675332
11 feet Y = 815441
23 meter
Z = -13432971
86 Z = -4094369
82
XDOT = -12158
393857 XDOT = -3705
878448
YDOT = -16601
805728 feet/sec YDOT = -5060
230386 meter/sec
ZDOT = 12590
630761 ZDOT = 3837
624256
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 16310
50900158
00016717 00000-0 10270-3 0 9017
2 25544 51
6413 73
2028 0007427 178
0373 182
0809 15
53529892 26963
Satellite: ISS
Catalog Number: 25544
Epoch time: 16310
50900158 = yrday
fracday
Element set: 901
Inclination: 51
6413 deg
RA of node: 73
2028 deg
Eccentricity:
0007427
Arg of perigee: 178
0373 deg
Mean anomaly: 182
0809 deg
Mean motion: 15
53529892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2696
Checksum: 304
Coasting Arc #3 (Orbit 2711)
---------------------------------------
Vector Time (GMT): 2016/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4303904
22 A = 6787364
27 meter
Y = -4304443
22 meter E =
0015886
Z = 2979853
84 I = 51
99432
XDOT = 1980
963652 Wp = 125
50595
YDOT = -5460
169450 meter/sec RA = 67
49535 deg
ZDOT = -5016
391725 TA = 20
57577
MA = 20
51186
Ha = 223
484 n
mi
Hp = 215
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14120420
67 X = -4269926
03
Y = -14122189
05 feet Y = -4352382
37 meter
Z = 9776423
37 Z = 2959028
77
XDOT = 6499
224580 XDOT = 2066
241287
YDOT = -17913
941765 feet/sec YDOT = -5437
540187 meter/sec
ZDOT = -16457
978100 ZDOT = -5006
561396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20014053
35 X = 6100283
46
Y = -141037
61 feet Y = -42988
26 meter
Z = 9686007
15 Z = 2952294
98
XDOT = 8070
898968 XDOT = 2460
010005
YDOT = 15840
628220 feet/sec YDOT = 4828
223481 meter/sec
ZDOT = -16413
900017 ZDOT = -5002
956725
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 16311
53822078
00016717 00000-0 10270-3 0 9026
2 25544 51
6418 68
0767 0007507 181
5222 178
5909 15
53532977 27129
Satellite: ISS
Catalog Number: 25544
Epoch time: 16311
53822078 = yrday
fracday
Element set: 902
Inclination: 51
6418 deg
RA of node: 68
0767 deg
Eccentricity:
0007507
Arg of perigee: 181
5222 deg
Mean anomaly: 178
5909 deg
Mean motion: 15
53532977 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2712
Checksum: 319
Coasting Arc #4 (Orbit 2712)
---------------------------------------
Vector Time (GMT): 2016/311/14:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3939554
07 A = 6779067
19 meter
Y = -1417298
17 meter E =
0016383
Z = -5344375
41 I = 51
96650
XDOT = 2836
276076 Wp = 117
90584
YDOT = 7109
292618 meter/sec RA = 67
08852 deg
ZDOT = 198
398264 TA = 154
02056
MA = 153
93823
Ha = 223
278 n
mi
Hp = 215
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12925046
16 X = 3981070
94
Y = -4649928
38 feet Y = -1373011
32 meter
Z = -17534040
05 Z = -5325136
90
XDOT = 9305
367705 XDOT = 2755
603601
YDOT = 23324
450847 feet/sec YDOT = 7140
558695 meter/sec
ZDOT = 650
912940 ZDOT = 211
980421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1506497
41 X = 459180
41
Y = 13761047
54 feet Y = 4194367
29 meter
Z = -17449505
69 Z = -5318609
33
XDOT = -23840
672850 XDOT = -7266
637085
YDOT = 3538
330968 feet/sec YDOT = 1078
483279 meter/sec
ZDOT = 709
079175 ZDOT = 216
127332
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 16311
60254524
00016717 00000-0 10270-3 0 9030
2 25544 51
6425 67
7581 0007283 183
1004 177
0104 15
53546897 27132
Satellite: ISS
Catalog Number: 25544
Epoch time: 16311
60254524 = yrday
fracday
Element set: 903
Inclination: 51
6425 deg
RA of node: 67
7581 deg
Eccentricity:
0007283
Arg of perigee: 183
1004 deg
Mean anomaly: 177
0104 deg
Mean motion: 15
53546897 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2713
Checksum: 296
Coasting Arc #5 (Orbit 2728)
---------------------------------------
Vector Time (GMT): 2016/312/14:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4499236
32 A = 6780086
05 meter
Y = -24836
19 meter E =
0005474
Z = 5067638
39 I = 51
95775
XDOT = -2094
217509 Wp = 135
21609
YDOT = -7131
876227 meter/sec RA = 62
11738 deg
ZDOT = -1896
818636 TA = 333
06803
MA = 333
09643
Ha = 223
148 n
mi
Hp = 215
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14761274
00 X = -4523240
95
Y = -81483
57 feet Y = -75283
82 meter
Z = 16626110
21 Z = 5045723
62
XDOT = -6870
792354 XDOT = -2005
097341
YDOT = -23398
544051 feet/sec YDOT = -7154
796900 meter/sec
ZDOT = -6223
158254 ZDOT = -1906
775394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3271182
84 X = 997056
53
Y = -14504614
10 feet Y = -4421006
38 meter
Z = 16530121
69 Z = 5038381
09
XDOT = 23262
307898 XDOT = 7090
351447
YDOT = -1884
530210 feet/sec YDOT = -574
404808 meter/sec
ZDOT = -6265
429707 ZDOT = -1909
702975
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 16312
63175443
00016717 00000-0 10270-3 0 9047
2 25544 51
6433 62
6318 0007138 187
0035 173
1018 15
53600047 27295
Satellite: ISS
Catalog Number: 25544
Epoch time: 16312
63175443 = yrday
fracday
Element set: 904
Inclination: 51
6433 deg
RA of node: 62
6318 deg
Eccentricity:
0007138
Arg of perigee: 187
0035 deg
Mean anomaly: 173
1018 deg
Mean motion: 15
53600047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2729
Checksum: 286
Coasting Arc #6 (Orbit 2743)
---------------------------------------
Vector Time (GMT): 2016/313/14:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4990881
20 A = 6782848
04 meter
Y = 1399445
04 meter E =
0012314
Z = -4387059
46 I = 51
94972
XDOT = 1142
747556 Wp = 144
75056
YDOT = 6741
783739 meter/sec RA = 57
15089 deg
ZDOT = 3445
651823 TA = 160
12475
MA = 160
07674
Ha = 222
941 n
mi
Hp = 215
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16374282
17 X = 4996172
06
Y = 4591355
13 feet Y = 1455285
89 meter
Z = -14393239
71 Z = -4362801
86
XDOT = 3749
171772 XDOT = 1050
536548
YDOT = 22118
713055 feet/sec YDOT = 6754
047223 meter/sec
ZDOT = 11304
631966 ZDOT = 3450
978923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7758434
52 X = -2364770
84
Y = 15232996
28 feet Y = 4643017
26 meter
Z = -14287250
47 Z = -4354753
94
XDOT = -21298
884467 XDOT = -6491
899986
YDOT = -209
031946 feet/sec YDOT = -63
712937 meter/sec
ZDOT = 11326
688264 ZDOT = 3452
374583
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 16313
59663339
00016717 00000-0 10270-3 0 9050
2 25544 51
6420 57
8269 0007123 188
9530 171
1496 15
53600964 27449
Satellite: ISS
Catalog Number: 25544
Epoch time: 16313
59663339 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 57
8269 deg
Eccentricity:
0007123
Arg of perigee: 188
9530 deg
Mean anomaly: 171
1496 deg
Mean motion: 15
53600964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2744
Checksum: 323
Coasting Arc #7 (Orbit 2759)
---------------------------------------
Vector Time (GMT): 2016/314/14:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5306624
40 A = 6786236
59 meter
Y = -2589961
66 meter E =
0013158
Z = 3327132
63 I = 51
94318
XDOT = -13
194860 Wp = 123
17257
YDOT = -6048
115843 meter/sec RA = 52
19036 deg
ZDOT = -4722
683013 TA = 18
26026
MA = 18
21306
Ha = 222
867 n
mi
Hp = 215
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17410185
04 X = -5293430
41
Y = -8497249
54 feet Y = -2649229
99 meter
Z = 10915789
47 Z = 3301386
13
XDOT = -43
290224 XDOT = 77
378814
YDOT = -19842
899748 feet/sec YDOT = -6047
757161 meter/sec
ZDOT = -15494
366841 ZDOT = -4722
526871
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11520375
15 X = 3511410
35
Y = -15653669
55 feet Y = -4771238
48 meter
Z = 10803510
47 Z = 3292909
99
XDOT = 18364
606511 XDOT = 5597
532064
YDOT = 2808
475315 feet/sec YDOT = 856
023276 meter/sec
ZDOT = -15492
528773 ZDOT = -4722
122770
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 16314
62582924
00016717 00000-0 10270-3 0 9066
2 25544 51
6424 52
7008 0007008 193
8421 166
2540 15
53609727 27603
Satellite: ISS
Catalog Number: 25544
Epoch time: 16314
62582924 = yrday
fracday
Element set: 906
Inclination: 51
6424 deg
RA of node: 52
7008 deg
Eccentricity:
0007008
Arg of perigee: 193
8421 deg
Mean anomaly: 166
2540 deg
Mean motion: 15
53609727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2760
Checksum: 303
Coasting Arc #8 (Orbit 2764)
---------------------------------------
Vector Time (GMT): 2016/314/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5354536
73 A = 6787724
43 meter
Y = -3094679
63 meter E =
0014687
Z = 2774664
59 I = 51
94009
XDOT = 586
508643 Wp = 127
73047
YDOT = -5649
707295 meter/sec RA = 50
59148 deg
ZDOT = -5159
643386 TA = 20
94513
MA = 20
88503
Ha = 222
776 n
mi
Hp = 215
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17567377
73 X = -5333011
61
Y = -10153148
39 feet Y = -3154437
18 meter
Z = 9103230
30 Z = 2748705
59
XDOT = 1924
240954 XDOT = 674
705258
YDOT = -18535
785089 feet/sec YDOT = -5642
655651 meter/sec
ZDOT = -16927
963865 ZDOT = -5156
579758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19753356
68 X = -6020823
12
Y = -4852899
65 feet Y = -1479163
81 meter
Z = 8990119
51 Z = 2740188
43
XDOT = -3552
801604 XDOT = -1082
893929
YDOT = -16931
704716 feet/sec YDOT = -5160
783597 meter/sec
ZDOT = -16913
464369 ZDOT = -5155
223940
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 16314
94745319
00016717 00000-0 10270-3 0 9071
2 25544 51
6409 51
0997 0006683 194
4433 165
6529 15
53585690 27650
Satellite: ISS
Catalog Number: 25544
Epoch time: 16314
94745319 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 51
0997 deg
Eccentricity:
0006683
Arg of perigee: 194
4433 deg
Mean anomaly: 165
6529 deg
Mean motion: 15
53585690 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2765
Checksum: 345
Coasting Arc #9 (Orbit 2779)
---------------------------------------
Vector Time (GMT): 2016/315/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5354308
03 A = 6790117
33 meter
Y = 3946838
20 meter E =
0003392
Z = -1364182
61 I = 51
92736
XDOT = -1901
045520 Wp = 77
88578
YDOT = 4590
376791 meter/sec RA = 45
63975 deg
ZDOT = 5832
296351 TA = 267
32856
MA = 267
36738
Ha = 222
503 n
mi
Hp = 215
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17566627
39 X = 5316402
27
Y = 12948944
21 feet Y = 4006501
65 meter
Z = -4475664
73 Z = -1338264
48
XDOT = -6237
025984 XDOT = -1980
566337
YDOT = 15060
291310 feet/sec YDOT = 4568
673684 meter/sec
ZDOT = 19134
830549 ZDOT = 5822
867991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20627865
29 X = 6287373
34
Y = 7193701
90 feet Y = 2192640
34 meter
Z = -4362906
78 Z = -1329813
99
XDOT = -1119
408885 XDOT = -341
195828
YDOT = 14763
017369 feet/sec YDOT = 4499
767694 meter/sec
ZDOT = 19092
650942 ZDOT = 5819
440007
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 16315
91231333
00016717 00000-0 10270-3 0 9086
2 25544 51
6412 46
2938 0006597 198
2010 161
8908 15
53597528 27801
Satellite: ISS
Catalog Number: 25544
Epoch time: 16315
91231333 = yrday
fracday
Element set: 908
Inclination: 51
6412 deg
RA of node: 46
2938 deg
Eccentricity:
0006597
Arg of perigee: 198
2010 deg
Mean anomaly: 161
8908 deg
Mean motion: 15
53597528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2780
Checksum: 321
Coasting Arc #10 (Orbit 2795)
---------------------------------------
Vector Time (GMT): 2016/316/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5042727
30 A = 6790838
70 meter
Y = -4529875
81 meter E =
0015552
Z = -187465
19 I = 51
90716
XDOT = 3284
954830 Wp = 158
50724
YDOT = -3414
238380 meter/sec RA = 40
69109 deg
ZDOT = -6034
614289 TA = 23
50578
MA = 23
43478
Ha = 222
360 n
mi
Hp = 216
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16544380
90 X = -4990787
63
Y = -14861797
29 feet Y = -4585976
57 meter
Z = -615043
28 Z = -211835
71
XDOT = 10777
410858 XDOT = 3352
203821
YDOT = -11201
569488 feet/sec YDOT = -3377
128066 meter/sec
ZDOT = -19798
603311 ZDOT = -6018
492929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20340346
53 X = -6199737
62
Y = -8984344
52 feet Y = -2738428
21 meter
Z = -720897
41 Z = -219729
53
XDOT = 6227
661156 XDOT = 1898
191120
YDOT = -12554
979857 feet/sec YDOT = -3826
757861 meter/sec
ZDOT = -19727
333984 ZDOT = -6012
891398
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 16316
94148967
00016717 00000-0 10270-3 0 9091
2 25544 51
6417 41
1677 0006546 202
0491 158
0381 15
53603854 27961
Satellite: ISS
Catalog Number: 25544
Epoch time: 16316
94148967 = yrday
fracday
Element set: 909
Inclination: 51
6417 deg
RA of node: 41
1677 deg
Eccentricity:
0006546
Arg of perigee: 202
0491 deg
Mean anomaly: 158
0381 deg
Mean motion: 15
53603854 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2796
Checksum: 326
Coasting Arc #11 (Orbit 2811)
---------------------------------------
Vector Time (GMT): 2016/317/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4442717
42 A = 6789516
65 meter
Y = 4841298
57 meter E =
0009696
Z = 1700600
72 I = 51
87805
XDOT = -4605
844265 Wp = 89
29573
YDOT = 2209
670905 meter/sec RA = 35
74040 deg
ZDOT = 5713
973905 TA = 289
27584
MA = 289
38070
Ha = 222
177 n
mi
Hp = 216
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14575844
54 X = 4379989
57
Y = 15883525
50 feet Y = 4890629
34 meter
Z = 5579398
70 Z = 1722030
42
XDOT = -15111
037616 XDOT = -4657
967832
YDOT = 7249
576461 feet/sec YDOT = 2157
873983 meter/sec
ZDOT = 18746
633547 ZDOT = 5691
472590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18935698
15 X = 5771600
80
Y = 10253569
17 feet Y = 3125287
88 meter
Z = 5672298
56 Z = 1728916
60
XDOT = -11274
152843 XDOT = -3436
361787
YDOT = 10454
556171 feet/sec YDOT = 3186
548721 meter/sec
ZDOT = 18647
657470 ZDOT = 5683
805997
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 16317
97065708
00016717 00000-0 10270-3 0 9108
2 25544 51
6418 36
0421 0006580 206
4533 153
6284 15
53628851 28121
Satellite: ISS
Catalog Number: 25544
Epoch time: 16317
97065708 = yrday
fracday
Element set: 910
Inclination: 51
6418 deg
RA of node: 36
0421 deg
Eccentricity:
0006580
Arg of perigee: 206
4533 deg
Mean anomaly: 153
6284 deg
Mean motion: 15
53628851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2812
Checksum: 303
Coasting Arc #12 (Orbit 2826)
---------------------------------------
Vector Time (GMT): 2016/318/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3497381
22 A = 6786581
87 meter
Y = -4917336
92 meter E =
0006765
Z = -3098746
67 I = 51
84309
XDOT = 5798
189234 Wp = 169
88633
YDOT = -1035
513262 meter/sec RA = 30
78220 deg
ZDOT = -4908
968429 TA = 45
63120
MA = 45
57580
Ha = 221
929 n
mi
Hp = 216
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11474347
82 X = -3427081
55
Y = -16132995
15 feet Y = -4956053
93 meter
Z = -10166491
70 Z = -3115565
79
XDOT = 19022
930558 XDOT = 5833
184014
YDOT = -3397
353223 feet/sec YDOT = -970
478365 meter/sec
ZDOT = -16105
539466 ZDOT = -4880
716459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16254259
76 X = -4954298
38
Y = -11236108
72 feet Y = -3424765
94 meter
Z = -10239172
06 Z = -3120899
64
XDOT = 15977
812750 XDOT = 4870
037326
YDOT = -8574
110017 feet/sec YDOT = -2613
388733 meter/sec
ZDOT = -15981
612587 ZDOT = -4871
195516
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 16318
93549267
00016717 00000-0 10270-3 0 9113
2 25544 51
6431 31
2362 0006426 210
3776 149
7004 15
53652460 28274
Satellite: ISS
Catalog Number: 25544
Epoch time: 16318
93549267 = yrday
fracday
Element set: 911
Inclination: 51
6431 deg
RA of node: 31
2362 deg
Eccentricity:
0006426
Arg of perigee: 210
3776 deg
Mean anomaly: 149
7004 deg
Mean motion: 15
53652460 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2827
Checksum: 301
Coasting Arc #13 (Orbit 2842)
---------------------------------------
Vector Time (GMT): 2016/319/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2301665
49 A = 6783139
05 meter
Y = 4793951
44 meter E =
0010187
Z = 4210847
12 I = 51
80289
XDOT = -6719
443699 Wp = 142
16992
YDOT = -25
605293 meter/sec RA = 25
81463 deg
ZDOT = 3689
445246 TA = 270
00734
MA = 270
12408
Ha = 221
811 n
mi
Hp = 216
414
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7551395
95 X = 2227432
18
Y = 15728187
14 feet Y = 4819275
04 meter
Z = 13815115
22 Z = 4221848
15
XDOT = -22045
418959 XDOT = -6736
580198
YDOT = -84
006866 feet/sec YDOT = -100
842529 meter/sec
ZDOT = 12104
479154 ZDOT = 3656
761339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12616995
83 X = 3845660
33
Y = 11996001
97 feet Y = 3656381
40 meter
Z = 13862330
72 Z = 4225238
40
XDOT = -19799
781263 XDOT = -6034
973329
YDOT = 6954
922435 feet/sec YDOT = 2119
860358 meter/sec
ZDOT = 11961
358349 ZDOT = 3645
822025
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 16319
96464192
00016717 00000-0 10270-3 0 9121
2 25544 51
6425 26
1104 0006407 213
6692 146
4054 15
53656832 28430
Satellite: ISS
Catalog Number: 25544
Epoch time: 16319
96464192 = yrday
fracday
Element set: 912
Inclination: 51
6425 deg
RA of node: 26
1104 deg
Eccentricity:
0006407
Arg of perigee: 213
6692 deg
Mean anomaly: 146
4054 deg
Mean motion: 15
53656832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2843
Checksum: 305
Coasting Arc #14 (Orbit 2857)
---------------------------------------
Vector Time (GMT): 2016/320/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -854122
08 A = 6780086
69 meter
Y = -4525658
39 meter E =
0008457
Z = -4982427
71 I = 51
76383
XDOT = 7292
904971 Wp = 100
97070
YDOT = 972
731208 meter/sec RA = 20
83613 deg
ZDOT = -2138
402897 TA = 148
24161
MA = 148
19057
Ha = 221
632 n
mi
Hp = 216
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2802237
80 X = -779248
47
Y = -14847960
60 feet Y = -4534790
88 meter
Z = -16346547
61 Z = -4986395
27
XDOT = 23926
853578 XDOT = 7291
873300
YDOT = 3191
375354 feet/sec YDOT = 1054
279696 meter/sec
ZDOT = -7015
757536 ZDOT = -2102
977404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8074242
91 X = -2461029
24
Y = -12750789
40 feet Y = -3886440
61 meter
Z = -16363008
90 Z = -4987445
11
XDOT = 22486
256432 XDOT = 6853
810960
YDOT = -5454
174409 feet/sec YDOT = -1662
432360 meter/sec
ZDOT = -6860
824536 ZDOT = -2091
179319
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 16320
92946213
00016717 00000-0 10270-3 0 9139
2 25544 51
6429 21
3046 0006338 217
6506 142
4204 15
53684975 28585
Satellite: ISS
Catalog Number: 25544
Epoch time: 16320
92946213 = yrday
fracday
Element set: 913
Inclination: 51
6429 deg
RA of node: 21
3046 deg
Eccentricity:
0006338
Arg of perigee: 217
6506 deg
Mean anomaly: 142
4204 deg
Mean motion: 15
53684975 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2858
Checksum: 308
Coasting Arc #15 (Orbit 2873)
---------------------------------------
Vector Time (GMT): 2016/321/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -690761
34 A = 6778597
14 meter
Y = 4158821
83 meter E =
0005845
Z = 5310084
57 I = 51
72852
XDOT = -7446
993524 Wp = 198
55671
YDOT = -1773
808660 meter/sec RA = 15
85017 deg
ZDOT = 415
208281 TA = 247
45673
MA = 247
51860
Ha = 221
419 n
mi
Hp = 216
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2266277
35 X = -763009
59
Y = 13644428
56 feet Y = 4150693
01 meter
Z = 17421537
32 Z = 5306553
71
XDOT = -24432
393453 XDOT = -7428
621802
YDOT = -5819
582217 feet/sec YDOT = -1856
983241 meter/sec
ZDOT = 1362
231894 ZDOT = 379
076500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3150823
88 X = 960371
12
Y = 13488758
62 feet Y = 4111373
63 meter
Z = 17405232
15 Z = 5305114
76
XDOT = -23785
247406 XDOT = -7249
743409
YDOT = 3979
510010 feet/sec YDOT = 1212
954651 meter/sec
ZDOT = 1204
370918 ZDOT = 367
092256
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 16321
95859380
00016717 00000-0 10270-3 0 9142
2 25544 51
6428 16
1785 0006502 222
7791 137
2856 15
53715306 28748
Satellite: ISS
Catalog Number: 25544
Epoch time: 16321
95859380 = yrday
fracday
Element set: 914
Inclination: 51
6428 deg
RA of node: 16
1785 deg
Eccentricity:
0006502
Arg of perigee: 222
7791 deg
Mean anomaly: 137
2856 deg
Mean motion: 15
53715306 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2874
Checksum: 324
Coasting Arc #16 (Orbit 2879)
---------------------------------------
Vector Time (GMT): 2016/322/07:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4681313
42 A = 6782926
72 meter
Y = 2344252
96 meter E =
0005643
Z = 4306637
36 I = 51
72965
XDOT = -5357
453441 Wp = 113
86538
YDOT = -4196
738288 meter/sec RA = 13
86220 deg
ZDOT = -3537
689449 TA = 12
12011
MA = 12
10654
Ha = 221
784 n
mi
Hp = 216
721
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15358639
82 X = -4728099
66
Y = 7691118
62 feet Y = 2291641
53 meter
Z = 14129387
67 Z = 4283782
83
XDOT = -17576
946986 XDOT = -5292
941407
YDOT = -13768
826404 feet/sec YDOT = -4256
288020 meter/sec
ZDOT = -11606
592681 ZDOT = -3563
558591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16918861
87 X = 5156869
10
Y = -3409502
36 feet Y = -1039216
32 meter
Z = 14028831
94 Z = 4275987
98
XDOT = 13069
200110 XDOT = 3983
492194
YDOT = 16614
022738 feet/sec YDOT = 5063
954131 meter/sec
ZDOT = -11719
020451 ZDOT = -3571
957433
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 16322
34451780
00016717 00000-0 10270-3 0 9159
2 25544 51
6424 14
2509 0006769 219
8683 140
1973 15
53662085 28804
Satellite: ISS
Catalog Number: 25544
Epoch time: 16322
34451780 = yrday
fracday
Element set: 915
Inclination: 51
6424 deg
RA of node: 14
2509 deg
Eccentricity:
0006769
Arg of perigee: 219
8683 deg
Mean anomaly: 140
1973 deg
Mean motion: 15
53662085 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2880
Checksum: 317
Coasting Arc #17 (Orbit 2887)
---------------------------------------
Vector Time (GMT): 2016/322/20:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3463775
23 A = 6780679
12 meter
Y = -3229431
34 meter E =
0010320
Z = -4861698
89 I = 51
70504
XDOT = 6485
469234 Wp = 139
90282
YDOT = 3254
619285 meter/sec RA = 11
16139 deg
ZDOT = 2453
931545 TA = 154
21382
MA = 154
16234
Ha = 221
309 n
mi
Hp = 216
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11364091
95 X = 3523246
48
Y = -10595247
18 feet Y = -3190364
29 meter
Z = -15950455
69 Z = -4844728
23
XDOT = 21277
786201 XDOT = 6436
672926
YDOT = 10677
884793 feet/sec YDOT = 3326
871186 meter/sec
ZDOT = 8050
956511 ZDOT = 2485
318422
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11182846
44 X = 3408531
59
Y = -10896412
67 feet Y = -3321226
58 meter
Z = -15875484
93 Z = -4838847
81
XDOT = 20705
694896 XDOT = 6311
095804
YDOT = 9297
817914 feet/sec YDOT = 2833
974900 meter/sec
ZDOT = 8187
736066 ZDOT = 2495
621953
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 16322
85907865
00016717 00000-0 10270-3 0 9166
2 25544 51
6421 11
6914 0006280 225
6836 134
3802 15
53696732 28885
Satellite: ISS
Catalog Number: 25544
Epoch time: 16322
85907865 = yrday
fracday
Element set: 916
Inclination: 51
6421 deg
RA of node: 11
6914 deg
Eccentricity:
0006280
Arg of perigee: 225
6836 deg
Mean anomaly: 134
3802 deg
Mean motion: 15
53696732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2888
Checksum: 325
Coasting Arc #18 (Orbit 2903)
---------------------------------------
Vector Time (GMT): 2016/323/20:20:13
000
Vector Time (MET): N/A
Weight (LBS) : 893835
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4771938
83 A = 6783877
89 meter
Y = 2669573
81 meter E =
0006327
Z = 4008641
23 I = 51
68363
XDOT = -5411
014729 Wp = 108
54674
YDOT = -3729
177648 meter/sec RA = 6
17903 deg
ZDOT = -3954
732963 TA = 22
55245
MA = 22
52466
Ha = 221
240 n
mi
Hp = 217
017
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15655967
30 X = -4820908
47
Y = 8758444
27 feet Y = 2615936
81 meter
Z = 13151710
06 Z = 3985341
28
XDOT = -17752
672997 XDOT = -5349
701371
YDOT = -12234
834803 feet/sec YDOT = -3789
344255 meter/sec
ZDOT = -12974
845678 ZDOT = -3980
869817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15343524
26 X = -4676706
20
Y = 9438398
90 feet Y = 2876823
99 meter
Z = 13049138
85 Z = 3977377
52
XDOT = -17497
205886 XDOT = -5333
148354
YDOT = -10334
266854 feet/sec YDOT = -3149
884537 meter/sec
ZDOT = -13088
536434 ZDOT = -3989
385905
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 16323
88819752
00016717 00000-0 10270-3 0 9178
2 25544 51
6418 6
5657 0006286 229
5801 130
4804 15
53695207 29043
Satellite: ISS
Catalog Number: 25544
Epoch time: 16323
88819752 = yrday
fracday
Element set: 917
Inclination: 51
6418 deg
RA of node: 6
5657 deg
Eccentricity:
0006286
Arg of perigee: 229
5801 deg
Mean anomaly: 130
4804 deg
Mean motion: 15
53695207 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2904
Checksum: 325
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