[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 21st 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 101 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 975 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
113/17:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 213
8
Coasting Arc #1 (Orbit 3597)
---------------------------------------
Vector Time (GMT): 2016/111/08:19:37
794
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6364821
64 A = 6788678
49 meter
Y = -2216556
24 meter E =
0012302
Z = -766046
90 I = 51
57610
XDOT = 2209
068745 Wp = 40
16346
YDOT = 4309
926080 meter/sec RA = 345
97231 deg
ZDOT = 5946
094670 TA = 311
54833
MA = 311
65377
Ha = 221
309 n
mi
Hp = 213
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20881960
76 X = 6392855
85
Y = -7272166
13 feet Y = -2145223
89 meter
Z = -2513277
23 Z = -735059
48
XDOT = 7247
600869 XDOT = 2131
825937
YDOT = 14140
177427 feet/sec YDOT = 4334
198019 meter/sec
ZDOT = 19508
184612 ZDOT = 5956
637899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21916936
24 X = 6680282
16
Y = 3041236
98 feet Y = 926969
03 meter
Z = -2378241
28 Z = -724887
94
XDOT = 122
889589 XDOT = 37
456747
YDOT = 14235
525678 feet/sec YDOT = 4338
988227 meter/sec
ZDOT = 19553
124969 ZDOT = 5959
792491
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 16111
34836702
00016717 00000-0 10270-3 0 9000
2 25544 51
6420 346
5375 0001826 43
8494 316
2804 15
54274926 35986
Satellite: ISS
Catalog Number: 25544
Epoch time: 16111
34836702 = yrday
fracday
Element set: 900
Inclination: 51
6420 deg
RA of node: 346
5375 deg
Eccentricity:
0001826
Arg of perigee: 43
8494 deg
Mean anomaly: 316
2804 deg
Mean motion: 15
54274926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3598
Checksum: 310
Coasting Arc #2 (Orbit 3613)
---------------------------------------
Vector Time (GMT): 2016/112/08:19:37
794
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6559869
35 A = 6788383
86 meter
Y = 1400500
79 meter E =
0009576
Z = -1022347
96 I = 51
54560
XDOT = -134
960676 Wp = 130
71268
YDOT = -4902
600447 meter/sec RA = 340
99656 deg
ZDOT = -5892
370270 TA = 60
38056
MA = 60
28521
Ha = 221
227 n
mi
Hp = 213
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21521881
05 X = -6570076
34
Y = 4594818
88 feet Y = 1327086
82 meter
Z = -3354159
97 Z = -1054239
59
XDOT = -442
784371 XDOT = -51
505475
YDOT = -16084
647135 feet/sec YDOT = -4903
643523 meter/sec
ZDOT = -19331
923457 ZDOT = -5892
822779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21328557
02 X = -6500944
18
Y = -5333485
04 feet Y = -1625646
24 meter
Z = -3492951
00 Z = -1064651
46
XDOT = 6402
741841 XDOT = 1951
555713
YDOT = -13030
540178 feet/sec YDOT = -3971
708646 meter/sec
ZDOT = -19332
916322 ZDOT = -5892
672895
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 16112
37709375
00016717 00000-0 10270-3 0 9010
2 25544 51
6431 341
4084 0001745 46
8429 313
2869 15
54287116 36142
Satellite: ISS
Catalog Number: 25544
Epoch time: 16112
37709375 = yrday
fracday
Element set: 901
Inclination: 51
6431 deg
RA of node: 341
4084 deg
Eccentricity:
0001745
Arg of perigee: 46
8429 deg
Mean anomaly: 313
2869 deg
Mean motion: 15
54287116 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3614
Checksum: 306
Coasting Arc #3 (Orbit 3629)
---------------------------------------
Vector Time (GMT): 2016/113/08:19:37
794
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6218187
53 A = 6785749
67 meter
Y = -451110
06 meter E =
0015166
Z = 2660320
80 I = 51
50669
XDOT = -1842
975406 Wp = 74
55669
YDOT = 5339
525410 meter/sec RA = 336
01414 deg
ZDOT = 5192
416486 TA = 315
53888
MA = 315
66051
Ha = 221
214 n
mi
Hp = 213
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20400877
73 X = 6209846
87
Y = -1480019
87 feet Y = -381620
60 meter
Z = 8728086
61 Z = 2690507
53
XDOT = -6046
507238 XDOT = -1927
769332
YDOT = 17518
127984 feet/sec YDOT = 5318
442270 meter/sec
ZDOT = 17035
487160 ZDOT = 5183
257291
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19048534
13 X = 5805993
20
Y = 7296050
15 feet Y = 2223836
08 meter
Z = 8859275
74 Z = 2700307
24
XDOT = -12478
303018 XDOT = -3803
386760
YDOT = 11861
084174 feet/sec YDOT = 3615
258456 meter/sec
ZDOT = 16994
650075 ZDOT = 5179
969343
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 16113
40581336
00016717 00000-0 10270-3 0 9021
2 25544 51
6429 336
2791 0001852 49
5765 310
5549 15
54296827 36300
Satellite: ISS
Catalog Number: 25544
Epoch time: 16113
40581336 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 336
2791 deg
Eccentricity:
0001852
Arg of perigee: 49
5765 deg
Mean anomaly: 310
5549 deg
Mean motion: 15
54296827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3630
Checksum: 315
Coasting Arc #4 (Orbit 3634)
---------------------------------------
Vector Time (GMT): 2016/113/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -238525
45 A = 6777622
73 meter
Y = -4430373
60 meter E =
0014963
Z = -5136890
32 I = 51
46752
XDOT = 7193
032982 Wp = 97
78038
YDOT = -2143
892476 meter/sec RA = 334
14192 deg
ZDOT = 1516
841893 TA = 186
87778
MA = 186
89834
Ha = 221
260 n
mi
Hp = 213
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -782563
80 X = -164012
89
Y = -14535346
47 feet Y = -4432624
64 meter
Z = -16853314
68 Z = -5137867
78
XDOT = 23599
189572 XDOT = 7209
103611
YDOT = -7033
767966 feet/sec YDOT = -2063
365247 meter/sec
ZDOT = 4976
515397 ZDOT = 1551
823682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13675514
99 X = -4168296
97
Y = 4975491
13 feet Y = 1516529
69 meter
Z = -16856681
07 Z = -5137916
39
XDOT = -13373
802826 XDOT = -4076
335101
YDOT = -19402
798983 feet/sec YDOT = -5913
973130 meter/sec
ZDOT = 5128
861588 ZDOT = 1563
277012
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 16113
72728648
00016717 00000-0 10270-3 0 9036
2 25544 51
6417 334
6724 0001629 66
3066 293
8257 15
54314939 36357
Satellite: ISS
Catalog Number: 25544
Epoch time: 16113
72728648 = yrday
fracday
Element set: 903
Inclination: 51
6417 deg
RA of node: 334
6724 deg
Eccentricity:
0001629
Arg of perigee: 66
3066 deg
Mean anomaly: 293
8257 deg
Mean motion: 15
54314939 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3635
Checksum: 327
Coasting Arc #5 (Orbit 3650)
---------------------------------------
Vector Time (GMT): 2016/114/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1458536
97 A = 6780720
20 meter
Y = 4949607
46 meter E =
0011072
Z = 4392223
43 I = 51
44838
XDOT = -6832
185261 Wp = 70
50932
YDOT = 971
134855 meter/sec RA = 329
13222 deg
ZDOT = -3352
626156 TA = 53
51259
MA = 53
41063
Ha = 221
350 n
mi
Hp = 213
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4785226
29 X = -1535112
27
Y = 16238869
63 feet Y = 4932869
17 meter
Z = 14410181
86 Z = 4384951
87
XDOT = -22415
305973 XDOT = -6826
251009
YDOT = 3186
137977 feet/sec YDOT = 894
765847 meter/sec
ZDOT = -10999
429647 ZDOT = -3385
801490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16950249
31 X = 5166435
99
Y = -474999
30 feet Y = -144779
79 meter
Z = 14377622
98 Z = 4382299
49
XDOT = 10013
431350 XDOT = 3052
093875
YDOT = 18973
850544 feet/sec YDOT = 5783
229646 meter/sec
ZDOT = -11143
690676 ZDOT = -3396
596918
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 16114
75599991
00016717 00000-0 10270-3 0 9048
2 25544 51
6410 329
5423 0001613 72
4687 287
6642 15
54284437 36515
Satellite: ISS
Catalog Number: 25544
Epoch time: 16114
75599991 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 329
5423 deg
Eccentricity:
0001613
Arg of perigee: 72
4687 deg
Mean anomaly: 287
6642 deg
Mean motion: 15
54284437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3651
Checksum: 327
Coasting Arc #6 (Orbit 3665)
---------------------------------------
Vector Time (GMT): 2016/115/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2912644
68 A = 6784551
29 meter
Y = -5237785
10 meter E =
0006051
Z = -3183266
84 I = 51
43556
XDOT = 5963
101272 Wp = 75
25059
YDOT = 406
853567 meter/sec RA = 324
13172 deg
ZDOT = 4795
871913 TA = 247
88480
MA = 247
94905
Ha = 221
254 n
mi
Hp = 213
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9555920
87 X = 2986461
66
Y = -17184334
32 feet Y = -5204801
32 meter
Z = -10443788
86 Z = -3168938
23
XDOT = 19563
980552 XDOT = 5934
811810
YDOT = 1334
821414 feet/sec YDOT = 473
378890 meter/sec
ZDOT = 15734
487904 ZDOT = 4824
771002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19400513
39 X = -5913276
48
Y = -3399171
75 feet Y = -1036067
55 meter
Z = -10380530
19 Z = -3163985
60
XDOT = -5422
156505 XDOT = -1652
673303
YDOT = -17394
744796 feet/sec YDOT = -5301
918214 meter/sec
ZDOT = 15859
901062 ZDOT = 4834
097844
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 16115
72041226
00016717 00000-0 10270-3 0 9050
2 25544 51
6421 324
7337 0001524 69
1227 291
0089 15
54311281 36660
Satellite: ISS
Catalog Number: 25544
Epoch time: 16115
72041226 = yrday
fracday
Element set: 905
Inclination: 51
6421 deg
RA of node: 324
7337 deg
Eccentricity:
0001524
Arg of perigee: 69
1227 deg
Mean anomaly: 291
0089 deg
Mean motion: 15
54311281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3666
Checksum: 284
Coasting Arc #7 (Orbit 3681)
---------------------------------------
Vector Time (GMT): 2016/116/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4070572
94 A = 6787735
63 meter
Y = 5188038
93 meter E =
0015078
Z = 1580454
55 I = 51
42126
XDOT = -4721
898364 Wp = 113
09881
YDOT = -1950
290002 meter/sec RA = 319
13960 deg
ZDOT = -5721
786641 TA = 49
55554
MA = 49
42415
Ha = 221
248 n
mi
Hp = 213
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13354898
11 X = -4135961
66
Y = 17021125
08 feet Y = 5142153
48 meter
Z = 5185218
34 Z = 1560521
48
XDOT = -15491
792532 XDOT = -4671
944325
YDOT = -6398
589244 feet/sec YDOT = -2002
814182 meter/sec
ZDOT = -18772
265883 ZDOT = -5744
603485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20608473
48 X = 6281462
72
Y = 6653075
39 feet Y = 2027857
38 meter
Z = 5097636
74 Z = 1553759
68
XDOT = -186
630175 XDOT = -56
884877
YDOT = 15133
646036 feet/sec YDOT = 4612
735312 meter/sec
ZDOT = -18870
960064 ZDOT = -5751
868628
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 16116
74911434
00016717 00000-0 10270-3 0 9061
2 25544 51
6424 319
6038 0001558 74
3310 285
8015 15
54325655 36820
Satellite: ISS
Catalog Number: 25544
Epoch time: 16116
74911434 = yrday
fracday
Element set: 906
Inclination: 51
6424 deg
RA of node: 319
6038 deg
Eccentricity:
0001558
Arg of perigee: 74
3310 deg
Mean anomaly: 285
8015 deg
Mean motion: 15
54325655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3682
Checksum: 305
Coasting Arc #8 (Orbit 3697)
---------------------------------------
Vector Time (GMT): 2016/117/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4815428
88 A = 6788723
61 meter
Y = -4773507
53 meter E =
0013978
Z = 162739
06 I = 51
40141
XDOT = 3261
709906 Wp = 50
18580
YDOT = 3505
989316 meter/sec RA = 314
15270 deg
ZDOT = 5991
122213 TA = 311
57354
MA = 311
69328
Ha = 221
275 n
mi
Hp = 213
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15798651
17 X = 4867659
01
Y = -15661113
94 feet Y = -4719366
16 meter
Z = 533920
79 Z = 186258
45
XDOT = 10701
147984 XDOT = 3193
159908
YDOT = 11502
589620 feet/sec YDOT = 3542
080671 meter/sec
ZDOT = 19655
912771 ZDOT = 6006
800502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20325622
66 X = -6195249
79
Y = -9034171
17 feet Y = -2753615
37 meter
Z = 636988
87 Z = 194154
21
XDOT = 6223
481081 XDOT = 1896
917034
YDOT = -12546
545697 feet/sec YDOT = -3824
187128 meter/sec
ZDOT = 19723
303299 ZDOT = 6011
662845
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 16117
77781183
00016717 00000-0 10270-3 0 9072
2 25544 51
6428 314
4748 0001674 74
9451 285
1887 15
54332167 36989
Satellite: ISS
Catalog Number: 25544
Epoch time: 16117
77781183 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 314
4748 deg
Eccentricity:
0001674
Arg of perigee: 74
9451 deg
Mean anomaly: 285
1887 deg
Mean motion: 15
54332167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3698
Checksum: 345
Coasting Arc #9 (Orbit 3712)
---------------------------------------
Vector Time (GMT): 2016/118/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5186595
80 A = 6787045
62 meter
Y = 3926554
72 meter E =
0007762
Z = -1929438
61 I = 51
37451
XDOT = -1697
852733 Wp = 129
76786
YDOT = -4974
557231 meter/sec RA = 309
16347 deg
ZDOT = -5579
389337 TA = 71
57662
MA = 71
49225
Ha = 221
187 n
mi
Hp = 213
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17016390
41 X = -5220745
54
Y = 12882397
39 feet Y = 3868363
81 meter
Z = -6330179
17 Z = -1954717
06
XDOT = -5570
382981 XDOT = -1614
997204
YDOT = -16320
725823 feet/sec YDOT = -4993
080487 meter/sec
ZDOT = -18305
083126 ZDOT = -5587
435923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18353255
87 X = 5594072
39
Y = 10828668
89 feet Y = 3300578
28 meter
Z = -6440714
47 Z = -1963129
77
XDOT = -12249
778521 XDOT = -3733
732493
YDOT = 9892
159697 feet/sec YDOT = 3015
130276 meter/sec
ZDOT = -18339
050711 ZDOT = -5589
742657
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 16118
74221101
00016717 00000-0 10270-3 0 9080
2 25544 51
6429 309
6662 0001582 80
0771 280
0560 15
54350430 37135
Satellite: ISS
Catalog Number: 25544
Epoch time: 16118
74221101 = yrday
fracday
Element set: 908
Inclination: 51
6429 deg
RA of node: 309
6662 deg
Eccentricity:
0001582
Arg of perigee: 80
0771 deg
Mean anomaly: 280
0560 deg
Mean motion: 15
54350430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3713
Checksum: 279
Coasting Arc #10 (Orbit 3728)
---------------------------------------
Vector Time (GMT): 2016/119/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5169144
23 A = 6783467
44 meter
Y = -2715579
61 meter E =
0013865
Z = 3440611
66 I = 51
34441
XDOT = 205
997304 Wp = 89
89221
YDOT = 6175
313064 meter/sec RA = 304
16488 deg
ZDOT = 4548
633003 TA = 310
65615
MA = 310
77660
Ha = 221
085 n
mi
Hp = 213
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16959134
63 X = 5182413
17
Y = -8909381
91 feet Y = -2657700
59 meter
Z = 11288095
99 Z = 3465754
54
XDOT = 675
844174 XDOT = 114
832594
YDOT = 20260
213463 feet/sec YDOT = 6177
106949 meter/sec
ZDOT = 14923
336624 ZDOT = 4549
412240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14850855
00 X = -4526540
60
Y = -11998027
18 feet Y = -3656998
68 meter
Z = 11397802
15 Z = 3474050
10
XDOT = 17512
200833 XDOT = 5337
718814
YDOT = -7448
293668 feet/sec YDOT = -2270
239910 meter/sec
ZDOT = 14925
520932 ZDOT = 4549
298780
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 16119
77089710
00016717 00000-0 10270-3 0 9093
2 25544 51
6439 304
5369 0001599 82
6945 277
4389 15
54383310 37292
Satellite: ISS
Catalog Number: 25544
Epoch time: 16119
77089710 = yrday
fracday
Element set: 909
Inclination: 51
6439 deg
RA of node: 304
5369 deg
Eccentricity:
0001599
Arg of perigee: 82
6945 deg
Mean anomaly: 277
4389 deg
Mean motion: 15
54383310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3729
Checksum: 349
Coasting Arc #11 (Orbit 3743)
---------------------------------------
Vector Time (GMT): 2016/120/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4859820
26 A = 6779645
87 meter
Y = 1160566
30 meter E =
0011819
Z = -4594062
76 I = 51
31367
XDOT = 1151
439120 Wp = 71
45990
YDOT = -6961
047414 meter/sec RA = 299
15448 deg
ZDOT = -2979
200694 TA = 168
66361
MA = 168
63696
Ha = 221
207 n
mi
Hp = 213
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15944292
18 X = -4850120
66
Y = 3807632
21 feet Y = 1106274
74 meter
Z = -15072384
39 Z = -4617647
19
XDOT = 3777
687401 XDOT = 1243
665496
YDOT = -22838
082068 feet/sec YDOT = -6947
655622 meter/sec
ZDOT = -9774
280491 ZDOT = -2973
383161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9976069
56 X = 3040706
00
Y = 12887672
59 feet Y = 3928162
61 meter
Z = -15175019
57 Z = -4625345
96
XDOT = -21462
647932 XDOT = -6541
815090
YDOT = 5146
142378 feet/sec YDOT = 1568
544197 meter/sec
ZDOT = -9747
678681 ZDOT = -2971
092462
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 16120
73528780
00016717 00000-0 10270-3 0 9108
2 25544 51
6435 299
7289 0001546 82
4619 277
6709 15
54345182 37442
Satellite: ISS
Catalog Number: 25544
Epoch time: 16120
73528780 = yrday
fracday
Element set: 910
Inclination: 51
6435 deg
RA of node: 299
7289 deg
Eccentricity:
0001546
Arg of perigee: 82
4619 deg
Mean anomaly: 277
6709 deg
Mean motion: 15
54345182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3744
Checksum: 334
Coasting Arc #12 (Orbit 3759)
---------------------------------------
Vector Time (GMT): 2016/121/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4305718
70 A = 6776945
71 meter
Y = 577475
83 meter E =
0005074
Z = 5197590
21 I = 51
29024
XDOT = -2288
512723 Wp = 111
88919
YDOT = 7241
925174 meter/sec RA = 294
13254 deg
ZDOT = 1088
492700 TA = 327
62018
MA = 327
65130
Ha = 220
997 n
mi
Hp = 213
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14126373
70 X = 4273693
38
Y = 1894605
74 feet Y = 625446
29 meter
Z = 17052461
33 Z = 5218428
67
XDOT = -7508
243842 XDOT = -2374
611118
YDOT = 23759
597027 feet/sec YDOT = 7215
852121 meter/sec
ZDOT = 3571
170275 ZDOT = 1077
166315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4257436
99 X = -1297666
79
Y = -13488057
59 feet Y = -4111159
95 meter
Z = 17142839
18 Z = 5225137
38
XDOT = 23720
332742 XDOT = 7229
957420
YDOT = -3001
371912 feet/sec YDOT = -914
818159 meter/sec
ZDOT = 3520
606929 ZDOT = 1073
080992
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 16121
76396480
00016717 00000-0 10270-3 0 9113
2 25544 51
6434 294
5996 0001558 85
0199 275
1132 15
54396272 37601
Satellite: ISS
Catalog Number: 25544
Epoch time: 16121
76396480 = yrday
fracday
Element set: 911
Inclination: 51
6434 deg
RA of node: 294
5996 deg
Eccentricity:
0001558
Arg of perigee: 85
0199 deg
Mean anomaly: 275
1132 deg
Mean motion: 15
54396272 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3760
Checksum: 328
Coasting Arc #13 (Orbit 3774)
---------------------------------------
Vector Time (GMT): 2016/122/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3615053
50 A = 6776919
81 meter
Y = -2376356
70 meter E =
0015940
Z = -5230416
63 I = 51
27745
XDOT = 3184
015517 Wp = 95
78678
YDOT = -6900
548325 meter/sec RA = 289
10578 deg
ZDOT = 935
381221 TA = 183
21640
MA = 183
22666
Ha = 221
171 n
mi
Hp = 213
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11860411
74 X = -3562804
48
Y = -7796445
87 feet Y = -2416490
67 meter
Z = -17160159
56 Z = -5247850
82
XDOT = 10446
245136 XDOT = 3256
398811
YDOT = -22639
594242 feet/sec YDOT = -6864
537794 meter/sec
ZDOT = 3068
836028 ZDOT = 951
024545
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1807304
27 X = -550866
34
Y = 13985674
09 feet Y = 4262833
46 meter
Z = -17235416
51 Z = -5253354
95
XDOT = -23896
630489 XDOT = -7283
692973
YDOT = 775
599155 feet/sec YDOT = 236
402622 meter/sec
ZDOT = 3138
065888 ZDOT = 956
482483
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 16122
72834603
00016717 00000-0 10270-3 0 9125
2 25544 51
6432 289
7913 0001581 82
9436 277
1897 15
54382795 37751
Satellite: ISS
Catalog Number: 25544
Epoch time: 16122
72834603 = yrday
fracday
Element set: 912
Inclination: 51
6432 deg
RA of node: 289
7913 deg
Eccentricity:
0001581
Arg of perigee: 82
9436 deg
Mean anomaly: 277
1897 deg
Mean motion: 15
54382795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3775
Checksum: 340
Coasting Arc #14 (Orbit 3790)
---------------------------------------
Vector Time (GMT): 2016/123/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2820005
22 A = 6779293
08 meter
Y = 4051633
39 meter E =
0009705
Z = 4640599
78 I = 51
27615
XDOT = -3865
310979 Wp = 67
03792
YDOT = 5978
011888 meter/sec RA = 284
08077 deg
ZDOT = -2861
918859 TA = 51
56774
MA = 51
48066
Ha = 221
058 n
mi
Hp = 213
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9251985
64 X = 2751946
98
Y = 13292760
47 feet Y = 4082788
23 meter
Z = 15225064
89 Z = 4654133
33
XDOT = -12681
466468 XDOT = -3917
969201
YDOT = 19612
899894 feet/sec YDOT = 5934
492855 meter/sec
ZDOT = -9389
497569 ZDOT = -2880
823936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7641430
35 X = 2329107
97
Y = -14217435
36 feet Y = -4333474
30 meter
Z = 15283075
41 Z = 4658281
39
XDOT = 22175
193518 XDOT = 6758
998984
YDOT = 1705
863803 feet/sec YDOT = 519
947287 meter/sec
ZDOT = -9472
704909 ZDOT = -2887
280456
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 16123
75701272
00016717 00000-0 10270-3 0 9135
2 25544 51
6433 284
6613 0001617 82
0293 278
1043 15
54409434 37917
Satellite: ISS
Catalog Number: 25544
Epoch time: 16123
75701272 = yrday
fracday
Element set: 913
Inclination: 51
6433 deg
RA of node: 284
6613 deg
Eccentricity:
0001617
Arg of perigee: 82
0293 deg
Mean anomaly: 278
1043 deg
Mean motion: 15
54409434 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3791
Checksum: 296
Coasting Arc #15 (Orbit 3805)
---------------------------------------
Vector Time (GMT): 2016/124/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2010092
68 A = 6783177
02 meter
Y = -5428140
85 meter E =
0006838
Z = -3542842
81 I = 51
28085
XDOT = 4326
101444 Wp = 94
23146
YDOT = -4498
376910 meter/sec RA = 279
06591 deg
ZDOT = 4444
613906 TA = 223
77142
MA = 223
82565
Ha = 221
149 n
mi
Hp = 213
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6594792
25 X = -1932034
60
Y = -17808861
04 feet Y = -5450182
75 meter
Z = -11623500
04 Z = -3552417
64
XDOT = 14193
246208 XDOT = 4354
491555
YDOT = -14758
454429 feet/sec YDOT = -4449
840621 meter/sec
ZDOT = 14582
066621 ZDOT = 4465
698495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12620117
44 X = -3846611
80
Y = 14157493
30 feet Y = 4315203
96 meter
Z = -11664072
55 Z = -3555209
31
XDOT = -18633
683402 XDOT = -5679
546701
YDOT = -4538
958917 feet/sec YDOT = -1383
474678 meter/sec
ZDOT = 14674
453504 ZDOT = 4472
773428
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 16124
72138485
00016717 00000-0 10270-3 0 9144
2 25544 51
6420 279
8531 0001625 89
2179 270
9160 15
54401667 38066
Satellite: ISS
Catalog Number: 25544
Epoch time: 16124
72138485 = yrday
fracday
Element set: 914
Inclination: 51
6420 deg
RA of node: 279
8531 deg
Eccentricity:
0001625
Arg of perigee: 89
2179 deg
Mean anomaly: 270
9160 deg
Mean motion: 15
54401667 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3806
Checksum: 314
Coasting Arc #16 (Orbit 3821)
---------------------------------------
Vector Time (GMT): 2016/125/17:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 945238
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1155705
41 A = 6786802
13 meter
Y = 6373744
85 meter E =
0015466
Z = 2001574
22 I = 51
28918
XDOT = -4633
926787 Wp = 109
06629
YDOT = 2589
007312 meter/sec RA = 274
06101 deg
ZDOT = -5538
562321 TA = 48
70282
MA = 48
56977
Ha = 221
137 n
mi
Hp = 213
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3791684
42 X = 1074623
74
Y = 20911236
38 feet Y = 6386215
44 meter
Z = 6566844
55 Z = 2006991
26
XDOT = -15203
171874 XDOT = -4635
628853
YDOT = 8494
118478 feet/sec YDOT = 2537
177927 meter/sec
ZDOT = -18171
136225 ZDOT = -5561
077434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16433513
72 X = 5008934
98
Y = -13464851
99 feet Y = -4104086
89 meter
Z = 6589196
67 Z = 2008387
15
XDOT = 13785
642976 XDOT = 4201
863979
YDOT = 7836
414812 feet/sec YDOT = 2388
539235 meter/sec
ZDOT = -18269
378018 ZDOT = -5568
506420
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 16125
75004202
00016717 00000-0 10270-3 0 9158
2 25544 51
6422 274
7231 0001651 87
8413 272
2928 15
54410514 38229
Satellite: ISS
Catalog Number: 25544
Epoch time: 16125
75004202 = yrday
fracday
Element set: 915
Inclination: 51
6422 deg
RA of node: 274
7231 deg
Eccentricity:
0001651
Arg of perigee: 87
8413 deg
Mean anomaly: 272
2928 deg
Mean motion: 15
54410514 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3822
Checksum: 281
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