[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 16th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7584 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 96 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 743 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
170/05:52:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 214
0
171/22:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 214
0
Coasting Arc #1 (Orbit 471)
---------------------------------------
Vector Time (GMT): 2016/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906675
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3099108
36 A = 6788052
22 meter
Y = -6015870
17 meter E =
0012446
Z = 448739
30 I = 52
00260
XDOT = 4020
676907 Wp = 130
16810
YDOT = -2528
093028 meter/sec RA = 65
71391 deg
ZDOT = -6022
236523 TA = 45
01554
MA = 44
91473
Ha = 220
242 n
mi
Hp = 214
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10167678
33 X = -3033786
85
Y = -19737106
87 feet Y = -6050161
27 meter
Z = 1472241
80 Z = 433842
61
XDOT = 13191
197200 XDOT = 4077
901484
YDOT = -8294
268466 feet/sec YDOT = -2482
810628 meter/sec
ZDOT = -19757
993842 ZDOT = -6002
566182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20782750
41 X = -6334582
33
Y = 7822783
15 feet Y = 2384384
30 meter
Z = 1408515
23 Z = 429315
44
XDOT = -6127
486161 XDOT = -1867
657782
YDOT = -12673
952105 feet/sec YDOT = -3863
020602 meter/sec
ZDOT = -19671
755978 ZDOT = -5995
951222
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 16167
53300640
00016717 00000-0 10270-3 0 9009
2 25544 51
6439 66
2889 0000407 309
6139 50
4978 15
54541352 4722
Satellite: ISS
Catalog Number: 25544
Epoch time: 16167
53300640 = yrday
fracday
Element set: 900
Inclination: 51
6439 deg
RA of node: 66
2889 deg
Eccentricity:
0000407
Arg of perigee: 309
6139 deg
Mean anomaly: 50
4978 deg
Mean motion: 15
54541352 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 472
Checksum: 305
Coasting Arc #2 (Orbit 487)
---------------------------------------
Vector Time (GMT): 2016/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906675
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2245121
81 A = 6787205
34 meter
Y = 6243886
53 meter E =
0013845
Z = 1394848
66 I = 51
98698
XDOT = -4960
146649 Wp = 57
77820
YDOT = 472
706356 meter/sec RA = 60
76532 deg
ZDOT = 5832
802230 TA = 317
35776
MA = 317
46515
Ha = 220
200 n
mi
Hp = 214
085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7365885
22 X = 2168358
62
Y = 20485192
01 feet Y = 6268563
62 meter
Z = 4576275
13 Z = 1405569
20
XDOT = -16273
447011 XDOT = -4993
397381
YDOT = 1550
873870 feet/sec YDOT = 417
052163 meter/sec
ZDOT = 19136
490255 ZDOT = 5808
626173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21109715
12 X = 6434241
17
Y = -5278360
63 feet Y = -1608844
32 meter
Z = 4621740
76 Z = 1408706
58
XDOT = -458
240342 XDOT = -139
671656
YDOT = 14930
333509 feet/sec YDOT = 4550
765653 meter/sec
ZDOT = 19031
023805 ZDOT = 5800
656056
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 16168
56154377
00016717 00000-0 10270-3 0 9018
2 25544 51
6448 61
1581 0000646 329
2521 30
8594 15
54571040 4883
Satellite: ISS
Catalog Number: 25544
Epoch time: 16168
56154377 = yrday
fracday
Element set: 901
Inclination: 51
6448 deg
RA of node: 61
1581 deg
Eccentricity:
0000646
Arg of perigee: 329
2521 deg
Mean anomaly: 30
8594 deg
Mean motion: 15
54571040 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 488
Checksum: 305
Coasting Arc #3 (Orbit 502)
---------------------------------------
Vector Time (GMT): 2016/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906675
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1096818
08 A = 6783935
80 meter
Y = -5933956
68 meter E =
0004013
Z = -3102108
70 I = 51
95952
XDOT = 5680
448027 Wp = 99
54691
YDOT = 1516
855090 meter/sec RA = 55
81096 deg
ZDOT = -4916
055336 TA = 115
93925
MA = 115
89789
Ha = 220
154 n
mi
Hp = 214
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3598484
50 X = -1015312
75
Y = -19468361
81 feet Y = -5945765
93 meter
Z = -10177522
00 Z = -3107239
56
XDOT = 18636
640510 XDOT = 5686
944247
YDOT = 4976
558694 feet/sec YDOT = 1580
414557 meter/sec
ZDOT = -16128
790474 ZDOT = -4888
444966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19692621
32 X = -6002310
98
Y = 1932834
56 feet Y = 589127
97 meter
Z = -10198675
04 Z = -3108556
15
XDOT = 6628
118175 XDOT = 2020
250420
YDOT = -16835
952376 feet/sec YDOT = -5131
598284 meter/sec
ZDOT = -16008
760333 ZDOT = -4879
470149
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 16169
52578985
00016717 00000-0 10270-3 0 9021
2 25544 51
6447 56
3493 0000635 319
9558 40
1548 15
54573728 5030
Satellite: ISS
Catalog Number: 25544
Epoch time: 16169
52578985 = yrday
fracday
Element set: 902
Inclination: 51
6447 deg
RA of node: 56
3493 deg
Eccentricity:
0000635
Arg of perigee: 319
9558 deg
Mean anomaly: 40
1548 deg
Mean motion: 15
54573728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 503
Checksum: 335
Coasting Arc #4 (Orbit 514)
---------------------------------------
Vector Time (GMT): 2016/170/05:52:30
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1354115
18 A = 6777816
58 meter
Y = 4493456
09 meter E =
0006330
Z = 4886519
88 I = 51
92159
XDOT = -5812
513016 Wp = 118
23132
YDOT = -4385
285050 meter/sec RA = 52
10476 deg
ZDOT = 2416
527418 TA = 308
15216
MA = 308
20919
Ha = 220
191 n
mi
Hp = 214
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4442635
10 X = -1427998
25
Y = 14742310
01 feet Y = 4477899
73 meter
Z = 16031889
36 Z = 4879763
02
XDOT = -19069
924593 XDOT = -5774
782184
YDOT = -14387
418143 feet/sec YDOT = -4450
073793 meter/sec
ZDOT = 7928
239562 ZDOT = 2388
382562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6017544
29 X = -1834147
50
Y = 14206857
63 feet Y = 4330250
21 meter
Z = 16001516
95 Z = 4877262
37
XDOT = -16527
266696 XDOT = -5037
510889
YDOT = -15812
598857 feet/sec YDOT = -4819
680132 meter/sec
ZDOT = 7806
471032 ZDOT = 2379
412371
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 16170
29718212
00016717 00000-0 10270-3 0 9037
2 25544 51
6407 52
5004 0000593 327
5830 32
5287 15
54611970 5153
Satellite: ISS
Catalog Number: 25544
Epoch time: 16170
29718212 = yrday
fracday
Element set: 903
Inclination: 51
6407 deg
RA of node: 52
5004 deg
Eccentricity:
0000593
Arg of perigee: 327
5830 deg
Mean anomaly: 32
5287 deg
Mean motion: 15
54611970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 515
Checksum: 284
Coasting Arc #5 (Orbit 529)
---------------------------------------
Vector Time (GMT): 2016/171/05:52:30
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2796651
93 A = 6776010
98 meter
Y = -3132070
04 meter E =
0014660
Z = -5330841
40 I = 51
89545
XDOT = 5402
647656 Wp = 85
12889
YDOT = 5416
957687 meter/sec RA = 47
11979 deg
ZDOT = -347
954501 TA = 181
55881
MA = 181
56338
Ha = 220
188 n
mi
Hp = 214
085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9175367
23 X = 2857362
71
Y = -10275820
34 feet Y = -3100455
80 meter
Z = -17489637
15 Z = -5317108
90
XDOT = 17725
221969 XDOT = 5343
362559
YDOT = 17772
170888 feet/sec YDOT = 5477
042257 meter/sec
ZDOT = -1141
583007 ZDOT = -321
852896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10121046
63 X = 3084895
01
Y = -9458166
88 feet Y = -2882849
27 meter
Z = -17429135
08 Z = -5312400
37
XDOT = 15481
695253 XDOT = 4718
820713
YDOT = 18465
190673 feet/sec YDOT = 5628
190117 meter/sec
ZDOT = -1028
941113 ZDOT = -313
621251
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 16171
26141712
00016717 00000-0 10270-3 0 9041
2 25544 51
6413 47
6902 0000570 339
2026 20
9104 15
54602132 5300
Satellite: ISS
Catalog Number: 25544
Epoch time: 16171
26141712 = yrday
fracday
Element set: 904
Inclination: 51
6413 deg
RA of node: 47
6902 deg
Eccentricity:
0000570
Arg of perigee: 339
2026 deg
Mean anomaly: 20
9104 deg
Mean motion: 15
54602132 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 530
Checksum: 255
Coasting Arc #6 (Orbit 540)
---------------------------------------
Vector Time (GMT): 2016/171/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5685330
18 A = 6784427
90 meter
Y = -2303937
77 meter E =
0012981
Z = 2884372
47 I = 51
91143
XDOT = -255
795244 Wp = 97
82590
YDOT = -5746
131499 meter/sec RA = 43
68477 deg
ZDOT = -5076
238135 TA = 49
44771
MA = 49
33476
Ha = 220
165 n
mi
Hp = 214
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18652658
07 X = -5673155
49
Y = -7558850
94 feet Y = -2367447
27 meter
Z = 9463164
27 Z = 2856783
72
XDOT = -839
223241 XDOT = -166
863322
YDOT = -18852
137465 feet/sec YDOT = -5748
493972 meter/sec
ZDOT = -16654
324591 ZDOT = -5077
265574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15295175
89 X = 4661969
61
Y = -13166923
40 feet Y = -4013278
25 meter
Z = 9343397
74 Z = 2847867
63
XDOT = 16131
543536 XDOT = 4916
894470
YDOT = 6876
665304 feet/sec YDOT = 2096
007585 meter/sec
ZDOT = -16657
606050 ZDOT = -5077
238324
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 16171
96851632
00016717 00000-0 10270-3 0 9058
2 25544 51
6442 44
1620 0000458 314
6802 45
4314 15
54631366 5413
Satellite: ISS
Catalog Number: 25544
Epoch time: 16171
96851632 = yrday
fracday
Element set: 905
Inclination: 51
6442 deg
RA of node: 44
1620 deg
Eccentricity:
0000458
Arg of perigee: 314
6802 deg
Mean anomaly: 45
4314 deg
Mean motion: 15
54631366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 541
Checksum: 285
Coasting Arc #7 (Orbit 555)
---------------------------------------
Vector Time (GMT): 2016/172/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5734637
98 A = 6787451
38 meter
Y = 3431356
72 meter E =
0009610
Z = -1161207
58 I = 51
89650
XDOT = -1592
443314 Wp = 34
07868
YDOT = 4644
217446 meter/sec RA = 38
72607 deg
ZDOT = 5890
592255 TA = 313
35577
MA = 313
43580
Ha = 220
187 n
mi
Hp = 214
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18814429
06 X = 5701482
11
Y = 11257732
03 feet Y = 3495300
05 meter
Z = -3809736
16 Z = -1133430
19
XDOT = -5224
551554 XDOT = -1672
871682
YDOT = 15236
933879 feet/sec YDOT = 4625
959101 meter/sec
ZDOT = 19326
090074 ZDOT = 5882
661918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18438481
07 X = -5620049
03
Y = 11901437
22 feet Y = 3627558
06 meter
Z = -3689385
92 Z = -1124524
83
XDOT = -10423
892500 XDOT = -3177
202434
YDOT = -10202
246227 feet/sec YDOT = -3109
644650 meter/sec
ZDOT = 19290
552201 ZDOT = 5879
760311
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 16172
93273834
00016717 00000-0 10270-3 0 9069
2 25544 51
6434 39
3524 0000653 325
2664 34
8446 15
54588906 5569
Satellite: ISS
Catalog Number: 25544
Epoch time: 16172
93273834 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 39
3524 deg
Eccentricity:
0000653
Arg of perigee: 325
2664 deg
Mean anomaly: 34
8446 deg
Mean motion: 15
54588906 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 556
Checksum: 322
Coasting Arc #8 (Orbit 571)
---------------------------------------
Vector Time (GMT): 2016/173/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5260380
62 A = 6787580
88 meter
Y = -4217761
59 meter E =
0009890
Z = -741423
48 I = 51
87107
XDOT = 3487
675321 Wp = 139
49841
YDOT = -3308
778254 meter/sec RA = 33
77111 deg
ZDOT = -5974
127686 TA = 48
48888
MA = 48
40406
Ha = 220
089 n
mi
Hp = 213
957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17258466
59 X = -5209224
09
Y = -13837800
49 feet Y = -4276300
53 meter
Z = -2432491
74 Z = -766853
34
XDOT = 11442
504333 XDOT = 3553
435295
YDOT = -10855
571699 feet/sec YDOT = -3269
408194 meter/sec
ZDOT = -19600
156451 ZDOT = -5957
026268
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19881474
71 X = 6059873
49
Y = -9670540
88 feet Y = -2947580
86 meter
Z = -2542441
67 Z = -774936
22
XDOT = 4163
634352 XDOT = 1269
075751
YDOT = 13650
300923 feet/sec YDOT = 4160
611721 meter/sec
ZDOT = -19524
922775 ZDOT = -5951
196462
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 16173
96123690
00016717 00000-0 10270-3 0 9078
2 25544 51
6426 34
2220 0000465 327
8844 32
2281 15
54641721 5728
Satellite: ISS
Catalog Number: 25544
Epoch time: 16173
96123690 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 34
2220 deg
Eccentricity:
0000465
Arg of perigee: 327
8844 deg
Mean anomaly: 32
2281 deg
Mean motion: 15
54641721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 572
Checksum: 290
Coasting Arc #9 (Orbit 587)
---------------------------------------
Vector Time (GMT): 2016/174/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4278905
77 A = 6785081
14 meter
Y = 4613853
30 meter E =
0013618
Z = 2520351
08 I = 51
83592
XDOT = -5196
610365 Wp = 73
36782
YDOT = 1906
650228 meter/sec RA = 28
80968 deg
ZDOT = 5312
214491 TA = 314
85467
MA = 314
96521
Ha = 220
098 n
mi
Hp = 213
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14038404
76 X = 4214751
80
Y = 15137313
97 feet Y = 4661343
83 meter
Z = 8268868
36 Z = 2540981
58
XDOT = -17049
246603 XDOT = -5243
349032
YDOT = 6255
414134 feet/sec YDOT = 1848
276223 meter/sec
ZDOT = 17428
525234 ZDOT = 5286
857583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19554876
42 X = -5960326
33
Y = 6507152
05 feet Y = 1983379
94 meter
Z = 8357813
53 Z = 2547461
56
XDOT = 1842
389819 XDOT = 561
560417
YDOT = -16789
139026 feet/sec YDOT = -5117
329575 meter/sec
ZDOT = 17317
604557 ZDOT = 5278
405869
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 16174
98972764
00016717 00000-0 10270-3 0 9086
2 25544 51
6430 29
0907 0000551 339
9704 20
1427 15
54643730 5889
Satellite: ISS
Catalog Number: 25544
Epoch time: 16174
98972764 = yrday
fracday
Element set: 908
Inclination: 51
6430 deg
RA of node: 29
0907 deg
Eccentricity:
0000551
Arg of perigee: 339
9704 deg
Mean anomaly: 20
1427 deg
Mean motion: 15
54643730 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 588
Checksum: 319
Coasting Arc #10 (Orbit 602)
---------------------------------------
Vector Time (GMT): 2016/175/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2810892
13 A = 6780924
44 meter
Y = -4694818
50 meter E =
0007183
Z = -4012642
04 I = 51
79334
XDOT = 6534
526999 Wp = 66
92861
YDOT = -525
421674 meter/sec RA = 23
83660 deg
ZDOT = -3965
644069 TA = 161
88406
MA = 161
85845
Ha = 220
144 n
mi
Hp = 213
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9222087
03 X = -2738693
08
Y = -15402947
83 feet Y = -4725847
60 meter
Z = -13164836
10 Z = -4026121
73
XDOT = 21438
736872 XDOT = 6559
179943
YDOT = -1723
824389 feet/sec YDOT = -452
209922 meter/sec
ZDOT = -13010
643272 ZDOT = -3933
841453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17763656
99 X = 5414362
65
Y = -2286060
34 feet Y = -696791
19 meter
Z = -13222595
02 Z = -4030246
96
XDOT = -7109
985087 XDOT = -2167
123455
YDOT = 19149
023699 feet/sec YDOT = 5836
622424 meter/sec
ZDOT = -12871
923090 ZDOT = -3923
362158
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 16175
95393233
00016717 00000-0 10270-3 0 9093
2 25544 51
6428 24
2807 0000585 350
9581 9
1561 15
54652146 6030
Satellite: ISS
Catalog Number: 25544
Epoch time: 16175
95393233 = yrday
fracday
Element set: 909
Inclination: 51
6428 deg
RA of node: 24
2807 deg
Eccentricity:
0000585
Arg of perigee: 350
9581 deg
Mean anomaly: 9
1561 deg
Mean motion: 15
54652146 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 603
Checksum: 307
Coasting Arc #11 (Orbit 618)
---------------------------------------
Vector Time (GMT): 2016/176/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1008081
04 A = 6777201
27 meter
Y = 4487528
12 meter E =
0005708
Z = 4974117
34 I = 51
75071
XDOT = -7333
073342 Wp = 118
11529
YDOT = -724
644068 meter/sec RA = 18
84931 deg
ZDOT = 2135
423579 TA = 311
10169
MA = 311
15096
Ha = 220
097 n
mi
Hp = 213
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3307352
49 X = 933663
57
Y = 14722861
28 feet Y = 4498384
55 meter
Z = 16319282
63 Z = 4978834
02
XDOT = -24058
639575 XDOT = -7334
798049
YDOT = -2377
441167 feet/sec YDOT = -806
657243 meter/sec
ZDOT = 7005
982872 ZDOT = 2099
797420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14835638
17 X = -4521902
51
Y = -2639066
30 feet Y = -804387
41 meter
Z = 16338891
62 Z = 4980094
17
XDOT = 11173
421329 XDOT = 3405
658821
YDOT = -20305
942349 feet/sec YDOT = -6189
251228 meter/sec
ZDOT = 6850
867668 ZDOT = 2088
144465
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 16176
98241094
00016717 00000-0 10270-3 0 9106
2 25544 51
6422 19
1501 0000631 349
8427 10
2713 15
54674774 6196
Satellite: ISS
Catalog Number: 25544
Epoch time: 16176
98241094 = yrday
fracday
Element set: 910
Inclination: 51
6422 deg
RA of node: 19
1501 deg
Eccentricity:
0000631
Arg of perigee: 349
8427 deg
Mean anomaly: 10
2713 deg
Mean motion: 15
54674774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 619
Checksum: 296
Coasting Arc #12 (Orbit 633)
---------------------------------------
Vector Time (GMT): 2016/177/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 979660
33 A = 6775819
75 meter
Y = -4088543
43 meter E =
0014821
Z = -5326522
63 I = 51
71624
XDOT = 7440
308555 Wp = 86
97951
YDOT = 1815
005320 meter/sec RA = 13
85101 deg
ZDOT = -24
031026 TA = 182
78732
MA = 182
79558
Ha = 220
156 n
mi
Hp = 213
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3214108
68 X = 1051180
38
Y = -13413856
40 feet Y = -4077187
86 meter
Z = -17475467
95 Z = -5321590
37
XDOT = 24410
461139 XDOT = 7419
576463
YDOT = 5954
741862 feet/sec YDOT = 1898
091890 meter/sec
ZDOT = -78
841949 ZDOT = 12
061646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11280931
51 X = 3438427
93
Y = 7986460
75 feet Y = 2434273
24 meter
Z = -17453109
95 Z = -5319707
91
XDOT = -13857
779559 XDOT = -4223
851210
YDOT = 19739
760278 feet/sec YDOT = 6016
678933 meter/sec
ZDOT = 78
068368 ZDOT = 23
795239
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 16177
94660474
00016717 00000-0 10270-3 0 9111
2 25544 51
6434 14
3397 0000714 353
8669 6
2475 15
54656465 6348
Satellite: ISS
Catalog Number: 25544
Epoch time: 16177
94660474 = yrday
fracday
Element set: 911
Inclination: 51
6434 deg
RA of node: 14
3397 deg
Eccentricity:
0000714
Arg of perigee: 353
8669 deg
Mean anomaly: 6
2475 deg
Mean motion: 15
54656465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 634
Checksum: 323
Coasting Arc #13 (Orbit 649)
---------------------------------------
Vector Time (GMT): 2016/178/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2938455
98 A = 6777173
31 meter
Y = 3526483
81 meter E =
0006770
Z = 4982757
64 I = 51
68944
XDOT = -6852
165978 Wp = 50
89651
YDOT = -2741
706581 meter/sec RA = 8
85148 deg
ZDOT = -2094
401789 TA = 59
49723
MA = 59
43040
Ha = 220
213 n
mi
Hp = 213
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9640603
61 X = -3001875
58
Y = 11569828
77 feet Y = 3493269
05 meter
Z = 16347630
07 Z = 4968329
67
XDOT = -22480
859509 XDOT = -6810
824610
YDOT = -8995
100330 feet/sec YDOT = -2818
100753 meter/sec
ZDOT = -6871
396947 ZDOT = -2127
587532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7452134
52 X = -2271410
60
Y = -13166010
49 feet Y = -4013000
00 meter
Z = 16284011
90 Z = 4963366
83
XDOT = 15287
113415 XDOT = 4659
512169
YDOT = -17354
328472 feet/sec YDOT = -5289
599318 meter/sec
ZDOT = -7015
434296 ZDOT = -2138
304373
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 16178
97506980
00016717 00000-0 10270-3 0 9127
2 25544 51
6431 9
2094 0000842 2
5605 357
5552 15
54708982 6500
Satellite: ISS
Catalog Number: 25544
Epoch time: 16178
97506980 = yrday
fracday
Element set: 912
Inclination: 51
6431 deg
RA of node: 9
2094 deg
Eccentricity:
0000842
Arg of perigee: 2
5605 deg
Mean anomaly: 357
5552 deg
Mean motion: 15
54708982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 650
Checksum: 311
Coasting Arc #14 (Orbit 664)
---------------------------------------
Vector Time (GMT): 2016/179/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4644168
77 A = 6780903
20 meter
Y = -2875781
57 meter E =
0006868
Z = -4024453
80 I = 51
67038
XDOT = 5569
622425 Wp = 99
63862
YDOT = 3493
812242 meter/sec RA = 3
85748 deg
ZDOT = 3935
279863 TA = 211
23724
MA = 211
27807
Ha = 220
215 n
mi
Hp = 213
787
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15236774
19 X = 4695530
35
Y = -9434978
90 feet Y = -2823559
89 meter
Z = -13203588
57 Z = -4001769
09
XDOT = 18273
039451 XDOT = 5511
023926
YDOT = 11462
638589 feet/sec YDOT = 3555
767526 meter/sec
ZDOT = 12911
023171 ZDOT = 3962
193598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3811645
71 X = 1161789
61
Y = 17585958
09 feet Y = 5360200
03 meter
Z = -13104132
96 Z = -3994139
73
XDOT = -15572
043329 XDOT = -4746
358807
YDOT = 13071
258072 feet/sec YDOT = 3984
119460 meter/sec
ZDOT = 13027
561637 ZDOT = 3970
800787
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 16179
93925259
00016717 00000-0 10270-3 0 9139
2 25544 51
6436 4
3994 0000887 11
6023 348
5151 15
54700714 6650
Satellite: ISS
Catalog Number: 25544
Epoch time: 16179
93925259 = yrday
fracday
Element set: 913
Inclination: 51
6436 deg
RA of node: 4
3994 deg
Eccentricity:
0000887
Arg of perigee: 11
6023 deg
Mean anomaly: 348
5151 deg
Mean motion: 15
54700714 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 665
Checksum: 313
Coasting Arc #15 (Orbit 680)
---------------------------------------
Vector Time (GMT): 2016/180/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5927236
31 A = 6784989
91 meter
Y = 2112417
21 meter E =
0013763
Z = 2522344
10 I = 51
65118
XDOT = -3728
365137 Wp = 100
45413
YDOT = -4114
964957 meter/sec RA = 358
87388 deg
ZDOT = -5292
945348 TA = 51
22330
MA = 51
10043
Ha = 220
235 n
mi
Hp = 213
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19446313
34 X = -5962669
84
Y = 6930502
64 feet Y = 2045936
56 meter
Z = 8275407
14 Z = 2493465
14
XDOT = -12232
169086 XDOT = -3656
362578
YDOT = -13500
541199 feet/sec YDOT = -4156
254973 meter/sec
ZDOT = -17365
306259 ZDOT = -5310
882314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -417315
65 X = -127197
81
Y = -20690357
21 feet Y = -6306420
88 meter
Z = 8149128
73 Z = 2483854
44
XDOT = 15130
390273 XDOT = 4611
742955
YDOT = -7204
136059 feet/sec YDOT = -2195
820671 meter/sec
ZDOT = -17442
591404 ZDOT = -5316
501860
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 16180
96770693
00016717 00000-0 10270-3 0 9145
2 25544 51
6427 359
2686 0000946 15
6001 344
5181 15
54721686 6814
Satellite: ISS
Catalog Number: 25544
Epoch time: 16180
96770693 = yrday
fracday
Element set: 914
Inclination: 51
6427 deg
RA of node: 359
2686 deg
Eccentricity:
0000946
Arg of perigee: 15
6001 deg
Mean anomaly: 344
5181 deg
Mean motion: 15
54721686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 681
Checksum: 323
Coasting Arc #16 (Orbit 695)
---------------------------------------
Vector Time (GMT): 2016/181/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 891443
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6619205
57 A = 6787340
76 meter
Y = -1285788
43 meter E =
0011436
Z = -726126
44 I = 51
62829
XDOT = 1536
641503 Wp = 37
86582
YDOT = 4579
450480 meter/sec RA = 353
89840 deg
ZDOT = 5957
212010 TA = 314
28498
MA = 314
37874
Ha = 220
178 n
mi
Hp = 213
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21716553
70 X = 6636618
84
Y = -4218465
97 feet Y = -1211670
62 meter
Z = -2382304
58 Z = -693929
73
XDOT = 5041
474749 XDOT = 1456
381076
YDOT = 15024
443831 feet/sec YDOT = 4596
184849 meter/sec
ZDOT = 19544
658825 ZDOT = 5964
482185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2483447
74 X = -756954
87
Y = 21997421
93 feet Y = 6704814
20 meter
Z = -2241751
72 Z = -683285
92
XDOT = -14204
568979 XDOT = -4329
552625
YDOT = 370
444565 feet/sec YDOT = 112
911503 meter/sec
ZDOT = 19575
365065 ZDOT = 5966
571272
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 16181
93187655
00016717 00000-0 10270-3 0 9154
2 25544 51
6438 354
4586 0000929 15
2607 344
8573 15
54743834 6964
Satellite: ISS
Catalog Number: 25544
Epoch time: 16181
93187655 = yrday
fracday
Element set: 915
Inclination: 51
6438 deg
RA of node: 354
4586 deg
Eccentricity:
0000929
Arg of perigee: 15
2607 deg
Mean anomaly: 344
8573 deg
Mean motion: 15
54743834 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 696
Checksum: 342
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