[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 10th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22604 21 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 104 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 055 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
048/10:49:56
644 1
5 2
9 2
9
N/A -2
3 -0
4 222
1
000/00:09:53
288 0
8 0
2 213
2
Coasting Arc #1 (Orbit 2513)
---------------------------------------
Vector Time (GMT): 2016/041/14:38:11
336
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2027945
68 A = 6780106
38 meter
Y = 4823852
93 meter E =
0016014
Z = 4299108
40 I = 51
47912
XDOT = -6824
073699 Wp = 81
44731
YDOT = 266
986515 meter/sec RA = 333
64541 deg
ZDOT = -3505
064923 TA = 44
32215
MA = 44
19404
Ha = 222
643 n
mi
Hp = 211
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6653365
09 X = -2102619
25
Y = 15826289
13 feet Y = 4800757
95 meter
Z = 14104686
36 Z = 4289075
57
XDOT = -22388
693239 XDOT = -6809
526299
YDOT = 875
940009 feet/sec YDOT = 190
756226 meter/sec
ZDOT = -11499
556833 ZDOT = -3538
178544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7068822
29 X = -2154577
03
Y = 15685106
87 feet Y = 4780820
57 meter
Z = 14060229
22 Z = 4285557
87
XDOT = -21183
915022 XDOT = -6456
857299
YDOT = 929
896344 feet/sec YDOT = 283
432405 meter/sec
ZDOT = -11643
157754 ZDOT = -3548
834483
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 16041
65165517
00016717 00000-0 10270-3 0 9005
2 25544 51
6446 334
0449 0006483 95
9362 264
2530 15
54614707 25144
Satellite: ISS
Catalog Number: 25544
Epoch time: 16041
65165517 = yrday
fracday
Element set: 900
Inclination: 51
6446 deg
RA of node: 334
0449 deg
Eccentricity:
0006483
Arg of perigee: 95
9362 deg
Mean anomaly: 264
2530 deg
Mean motion: 15
54614707 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2514
Checksum: 303
Coasting Arc #2 (Orbit 2528)
---------------------------------------
Vector Time (GMT): 2016/042/14:38:11
336
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3563215
47 A = 6784163
57 meter
Y = -4949791
75 meter E =
0010526
Z = -2979338
17 I = 51
46478
XDOT = 5723
053989 Wp = 85
96356
YDOT = 1141
905555 meter/sec RA = 328
64522 deg
ZDOT = 4963
404421 TA = 239
90252
MA = 240
00691
Ha = 222
554 n
mi
Hp = 211
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11690339
45 X = 3632772
53
Y = -16239474
26 feet Y = -4909556
88 meter
Z = -9774731
53 Z = -2961859
85
XDOT = 18776
423848 XDOT = 5685
749907
YDOT = 3746
409300 feet/sec YDOT = 1205
696439 meter/sec
ZDOT = 16284
135240 ZDOT = 4991
114384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11808424
87 X = 3599207
90
Y = -16200004
03 feet Y = -4937761
23 meter
Z = -9697984
78 Z = -2955945
76
XDOT = 17477
204091 XDOT = 5327
051807
YDOT = 2950
757650 feet/sec YDOT = 899
390932 meter/sec
ZDOT = 16404
022926 ZDOT = 4999
946188
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 16042
61588738
00016717 00000-0 10270-3 0 9017
2 25544 51
6448 329
2344 0006399 99
8869 260
3007 15
54629789 25295
Satellite: ISS
Catalog Number: 25544
Epoch time: 16042
61588738 = yrday
fracday
Element set: 901
Inclination: 51
6448 deg
RA of node: 329
2344 deg
Eccentricity:
0006399
Arg of perigee: 99
8869 deg
Mean anomaly: 260
3007 deg
Mean motion: 15
54629789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2529
Checksum: 356
Coasting Arc #3 (Orbit 2544)
---------------------------------------
Vector Time (GMT): 2016/043/14:38:11
336
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4731371
94 A = 6787284
99 meter
Y = 4696345
73 meter E =
0020026
Z = 1228058
35 I = 51
44793
XDOT = -4197
039265 Wp = 116
12992
YDOT = -2685
352767 meter/sec RA = 323
65466 deg
ZDOT = -5835
362806 TA = 50
47536
MA = 50
29852
Ha = 222
560 n
mi
Hp = 211
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15522873
83 X = -4789501
30
Y = 15407958
43 feet Y = 4643111
49 meter
Z = 4029062
84 Z = 1204933
22
XDOT = -13769
813863 XDOT = -4138
353757
YDOT = -8810
212489 feet/sec YDOT = -2731
959264 meter/sec
ZDOT = -19144
891097 ZDOT = -5855
607904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15334680
61 X = -4674010
65
Y = 15621053
36 feet Y = 4761297
07 meter
Z = 3927900
80 Z = 1197224
16
XDOT = -12627
593267 XDOT = -3848
890428
YDOT = -7504
907253 feet/sec YDOT = -2287
495731 meter/sec
ZDOT = -19232
111650 ZDOT = -5861
947631
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 16043
64438105
00016717 00000-0 10270-3 0 9024
2 25544 51
6444 324
1032 0006492 105
2555 254
9316 15
54624581 25452
Satellite: ISS
Catalog Number: 25544
Epoch time: 16043
64438105 = yrday
fracday
Element set: 902
Inclination: 51
6444 deg
RA of node: 324
1032 deg
Eccentricity:
0006492
Arg of perigee: 105
2555 deg
Mean anomaly: 254
9316 deg
Mean motion: 15
54624581 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2545
Checksum: 290
Coasting Arc #4 (Orbit 2560)
---------------------------------------
Vector Time (GMT): 2016/044/14:38:11
336
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5388695
18 A = 6787457
73 meter
Y = -4069115
06 meter E =
0017499
Z = 631219
22 I = 51
42383
XDOT = 2440
951260 Wp = 69
02812
YDOT = 4175
626072 meter/sec RA = 318
66683 deg
ZDOT = 5952
160090 TA = 297
80940
MA = 297
98666
Ha = 222
333 n
mi
Hp = 211
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17679446
13 X = 5430730
37
Y = -13350115
02 feet Y = -4008620
01 meter
Z = 2070929
20 Z = 657498
31
XDOT = 8008
370275 XDOT = 2365
164240
YDOT = 13699
560605 feet/sec YDOT = 4202
499157 meter/sec
ZDOT = 19528
084284 ZDOT = 5963
833066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17243808
23 X = 5255912
75
Y = -13890689
01 feet Y = -4233882
01 meter
Z = 2185628
19 Z = 666179
47
XDOT = 7290
487021 XDOT = 2222
140444
YDOT = 12193
171577 feet/sec YDOT = 3716
478697 meter/sec
ZDOT = 19577
856669 ZDOT = 5967
330713
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 16044
67284911
00016717 00000-0 10270-3 0 9033
2 25544 51
6441 318
9713 0006270 108
1838 251
9998 15
54708667 25615
Satellite: ISS
Catalog Number: 25544
Epoch time: 16044
67284911 = yrday
fracday
Element set: 903
Inclination: 51
6441 deg
RA of node: 318
9713 deg
Eccentricity:
0006270
Arg of perigee: 108
1838 deg
Mean anomaly: 251
9998 deg
Mean motion: 15
54708667 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2561
Checksum: 332
Coasting Arc #5 (Orbit 2575)
---------------------------------------
Vector Time (GMT): 2016/045/14:38:11
336
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5572957
52 A = 6784987
69 meter
Y = 2973194
15 meter E =
0011327
Z = -2476544
66 I = 51
39164
XDOT = -593
304048 Wp = 120
55595
YDOT = -5506
347419 meter/sec RA = 313
67466 deg
ZDOT = -5299
245706 TA = 87
29174
MA = 87
16209
Ha = 222
233 n
mi
Hp = 211
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18283981
36 X = -5593760
45
Y = 9754574
00 feet Y = 2910757
16 meter
Z = -8125146
53 Z = -2503667
16
XDOT = -1946
535591 XDOT = -505
945413
YDOT = -18065
444287 feet/sec YDOT = -5512
494050 meter/sec
ZDOT = -17385
976725 ZDOT = -5301
915241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17740504
18 X = -5407305
67
Y = 10620572
43 feet Y = 3237150
48 meter
Z = -8243278
91 Z = -2512551
41
XDOT = -1928
410221 XDOT = -587
779435
YDOT = -16664
036238 feet/sec YDOT = -5079
198245 meter/sec
ZDOT = -17396
469517 ZDOT = -5302
443909
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 16045
63702037
00016717 00000-0 10270-3 0 9045
2 25544 51
6435 314
1602 0006169 112
9276 247
2528 15
54699111 25765
Satellite: ISS
Catalog Number: 25544
Epoch time: 16045
63702037 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 314
1602 deg
Eccentricity:
0006169
Arg of perigee: 112
9276 deg
Mean anomaly: 247
2528 deg
Mean motion: 15
54699111 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2576
Checksum: 304
Coasting Arc #6 (Orbit 2591)
---------------------------------------
Vector Time (GMT): 2016/046/14:38:11
336
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5280936
65 A = 6780816
36 meter
Y = -1538367
73 meter E =
0016986
Z = 3954714
98 I = 51
35617
XDOT = -1106
519475 Wp = 105
53687
YDOT = 6470
069062 meter/sec RA = 308
66928 deg
ZDOT = 3975
676641 TA = 302
82970
MA = 302
99315
Ha = 222
126 n
mi
Hp = 211
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17325907
64 X = 5278536
48
Y = -5047138
22 feet Y = -1479326
00 meter
Z = 12974786
68 Z = 3980362
42
XDOT = -3630
313237 XDOT = -1198
099064
YDOT = 21227
260701 feet/sec YDOT = 6457
183389 meter/sec
ZDOT = 13043
558532 ZDOT = 3970
078724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16875702
98 X = 5143714
27
Y = -6161711
19 feet Y = -1878089
57 meter
Z = 13086242
14 Z = 3988686
60
XDOT = -2768
387831 XDOT = -843
804611
YDOT = 20195
154904 feet/sec YDOT = 6155
483215 meter/sec
ZDOT = 13018
038320 ZDOT = 3967
898080
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 16046
66544835
00016717 00000-0 10270-3 0 9050
2 25544 51
6431 309
0277 0006189 114
6582 245
5216 15
54732406 25921
Satellite: ISS
Catalog Number: 25544
Epoch time: 16046
66544835 = yrday
fracday
Element set: 905
Inclination: 51
6431 deg
RA of node: 309
0277 deg
Eccentricity:
0006189
Arg of perigee: 114
6582 deg
Mean anomaly: 245
5216 deg
Mean motion: 15
54732406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2592
Checksum: 315
Coasting Arc #7 (Orbit 2606)
---------------------------------------
Vector Time (GMT): 2016/047/14:38:11
336
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4624266
09 A = 6776861
13 meter
Y = -224394
59 meter E =
0017466
Z = -4964212
24 I = 51
32318
XDOT = 2577
406119 Wp = 88
55198
YDOT = -6898
680347 meter/sec RA = 303
64922 deg
ZDOT = -2095
043938 TA = 160
96319
MA = 160
89782
Ha = 222
033 n
mi
Hp = 211
470
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15171476
68 X = -4597299
49
Y = -736202
72 feet Y = -275955
64 meter
Z = -16286785
57 Z = -4986609
95
XDOT = 8456
056822 XDOT = 2664
533995
YDOT = -22633
465705 feet/sec YDOT = -6869
371015 meter/sec
ZDOT = -6873
503734 ZDOT = -2082
311789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15076072
97 X = -4595187
04
Y = 507679
83 feet Y = 154740
81 meter
Z = -16383814
22 Z = -4993786
57
XDOT = 6640
953395 XDOT = 2024
162595
YDOT = -22158
761916 feet/sec YDOT = -6753
990632 meter/sec
ZDOT = -6816
989286 ZDOT = -2077
818335
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 16047
62957767
00016717 00000-0 10270-3 0 9060
2 25544 51
6421 304
2158 0006058 119
5797 240
5961 15
54788978 26076
Satellite: ISS
Catalog Number: 25544
Epoch time: 16047
62957767 = yrday
fracday
Element set: 906
Inclination: 51
6421 deg
RA of node: 304
2158 deg
Eccentricity:
0006058
Arg of perigee: 119
5797 deg
Mean anomaly: 240
5961 deg
Mean motion: 15
54788978 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2607
Checksum: 350
Coasting Arc #8 (Orbit 2619)
---------------------------------------
Vector Time (GMT): 2016/048/10:54:53
288
Vector Time (MET): N/A
Weight (LBS) : 922176
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1382189
49 A = 6780333
80 meter
Y = -4891509
63 meter E =
0013487
Z = -4501016
20 I = 51
31670
XDOT = 5391
818777 Wp = 116
46941
YDOT = -4426
662050 meter/sec RA = 299
37439 deg
ZDOT = 3156
431849 TA = 185
39920
MA = 185
41375
Ha = 222
068 n
mi
Hp = 213
216
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4534742
42 X = -1305525
05
Y = -16048259
94 feet Y = -4906537
72 meter
Z = -14767113
50 Z = -4507544
00
XDOT = 17689
694151 XDOT = 5425
585745
YDOT = -14523
169455 feet/sec YDOT = -4366
178221 meter/sec
ZDOT = 10355
747536 ZDOT = 3182
705722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9503162
46 X = 2896563
92
Y = -13674495
66 feet Y = -4167986
28 meter
Z = -14794466
83 Z = -4509353
49
XDOT = 21436
052937 XDOT = 6533
708935
YDOT = 3574
273535 feet/sec YDOT = 1089
438573 meter/sec
ZDOT = 10470
469424 ZDOT = 3191
399080
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 16048
46514428
00016717 00000-0 10270-3 0 9077
2 25544 51
6437 300
0457 0004077 131
6664 228
4839 15
54264459 26203
Satellite: ISS
Catalog Number: 25544
Epoch time: 16048
46514428 = yrday
fracday
Element set: 907
Inclination: 51
6437 deg
RA of node: 300
0457 deg
Eccentricity:
0004077
Arg of perigee: 131
6664 deg
Mean anomaly: 228
4839 deg
Mean motion: 15
54264459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2620
Checksum: 314
Coasting Arc #9 (Orbit 2635)
---------------------------------------
Vector Time (GMT): 2016/049/10:54:53
288
Vector Time (MET): N/A
Weight (LBS) : 922176
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 243496
28 A = 6784210
74 meter
Y = 5902869
04 meter E =
0015831
Z = 3318091
34 I = 51
31455
XDOT = -5388
754009 Wp = 101
74826
YDOT = 2851
397957 meter/sec RA = 294
36372 deg
ZDOT = -4661
445129 TA = 39
39807
MA = 39
28304
Ha = 221
990 n
mi
Hp = 213
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 798872
31 X = 161353
31
Y = 19366368
25 feet Y = 5905132
85 meter
Z = 10886126
45 Z = 3319074
37
XDOT = -17679
639138 XDOT = -5397
595708
YDOT = 9354
980174 feet/sec YDOT = 2791
087679 meter/sec
ZDOT = -15293
455147 ZDOT = -4687
643428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14201974
11 X = -4328761
71
Y = 13188251
87 feet Y = 4019779
17 meter
Z = 10889265
78 Z = 3319048
21
XDOT = -17597
288011 XDOT = -5363
653386
YDOT = -6185
630857 feet/sec YDOT = -1885
380285 meter/sec
ZDOT = -15407
543901 ZDOT = -4696
219381
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 16049
49387811
00016717 00000-0 10270-3 0 9086
2 25544 51
6434 294
9163 0004122 135
5551 224
5933 15
54280719 26360
Satellite: ISS
Catalog Number: 25544
Epoch time: 16049
49387811 = yrday
fracday
Element set: 908
Inclination: 51
6434 deg
RA of node: 294
9163 deg
Eccentricity:
0004122
Arg of perigee: 135
5551 deg
Mean anomaly: 224
5933 deg
Mean motion: 15
54280719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2636
Checksum: 320
Coasting Arc #10 (Orbit 2650)
---------------------------------------
Vector Time (GMT): 2016/050/10:58:53
288
Vector Time (MET): N/A
Weight (LBS) : 922176
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1946561
51 A = 6788678
09 meter
Y = -6488478
29 meter E =
0011477
Z = -392868
46 I = 51
31813
XDOT = 4694
076059 Wp = 62
20087
YDOT = 1055
290305 meter/sec RA = 289
36074 deg
ZDOT = 5968
375801 TA = 293
54570
MA = 293
66623
Ha = 221
833 n
mi
Hp = 213
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6386356
66 X = 2020880
95
Y = -21287658
44 feet Y = -6466295
03 meter
Z = -1288938
53 Z = -383231
88
XDOT = 15400
512006 XDOT = 4652
935535
YDOT = 3462
238535 feet/sec YDOT = 1107
552896 meter/sec
ZDOT = 19581
285435 ZDOT = 5991
077939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19978922
79 X = 6089575
67
Y = -9741743
18 feet Y = -2969283
32 meter
Z = -1245953
38 Z = -379766
59
XDOT = 7105
510268 XDOT = 2165
759530
YDOT = 12115
858712 feet/sec YDOT = 3692
913736 meter/sec
ZDOT = 19679
483667 ZDOT = 5998
306622
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 16050
45829562
00016717 00000-0 10270-3 0 9099
2 25544 51
6439 290
1070 0003949 140
0714 220
0729 15
54329850 26519
Satellite: ISS
Catalog Number: 25544
Epoch time: 16050
45829562 = yrday
fracday
Element set: 909
Inclination: 51
6439 deg
RA of node: 290
1070 deg
Eccentricity:
0003949
Arg of perigee: 140
0714 deg
Mean anomaly: 220
0729 deg
Mean motion: 15
54329850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2651
Checksum: 302
Coasting Arc #11 (Orbit 2666)
---------------------------------------
Vector Time (GMT): 2016/051/10:58:53
288
Vector Time (MET): N/A
Weight (LBS) : 922176
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2711441
49 A = 6787908
58 meter
Y = 6056741
35 meter E =
0012497
Z = -1403050
36 I = 51
30571
XDOT = -3977
030545 Wp = 143
47137
YDOT = -3109
309130 meter/sec RA = 284
36654 deg
ZDOT = -5773
069430 TA = 51
89768
MA = 51
78506
Ha = 221
734 n
mi
Hp = 213
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8895805
40 X = -2772152
70
Y = 19871198
65 feet Y = 6026080
65 meter
Z = -4603183
61 Z = -1416369
45
XDOT = -13048
000477 XDOT = -3913
923500
YDOT = -10201
145439 feet/sec YDOT = -3153
430500 meter/sec
ZDOT = -18940
516502 ZDOT = -5792
234869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20491453
46 X = -6245795
01
Y = 7318125
18 feet Y = 2230564
56 meter
Z = -4662034
72 Z = -1420988
18
XDOT = -1020
103928 XDOT = -310
927677
YDOT = -14899
879363 feet/sec YDOT = -4541
483230 meter/sec
ZDOT = -19023
009565 ZDOT = -5798
213315
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 16051
48698873
00016717 00000-0 10270-3 0 9104
2 25544 51
6438 284
9771 0003977 146
3115 213
8292 15
54321807 26678
Satellite: ISS
Catalog Number: 25544
Epoch time: 16051
48698873 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 284
9771 deg
Eccentricity:
0003977
Arg of perigee: 146
3115 deg
Mean anomaly: 213
8292 deg
Mean motion: 15
54321807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2667
Checksum: 336
Coasting Arc #12 (Orbit 2682)
---------------------------------------
Vector Time (GMT): 2016/052/10:58:53
288
Vector Time (MET): N/A
Weight (LBS) : 922176
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3283721
21 A = 6784747
22 meter
Y = -5114632
49 meter E =
0015186
Z = 3003987
32 I = 51
28806
XDOT = 3182
375141 Wp = 96
23335
YDOT = 4947
676597 meter/sec RA = 279
36510 deg
ZDOT = 4922
148902 TA = 298
36557
MA = 298
51861
Ha = 221
591 n
mi
Hp = 213
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10773363
57 X = 3326078
53
Y = -16780290
31 feet Y = -5077674
62 meter
Z = 9855601
45 Z = 3020041
78
XDOT = 10440
863323 XDOT = 3102
903382
YDOT = 16232
534766 feet/sec YDOT = 4982
820130 meter/sec
ZDOT = 16148
782487 ZDOT = 4937
414223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19461151
18 X = 5931758
88
Y = -4184744
48 feet Y = -1275510
12 meter
Z = 9926121
79 Z = 3025481
92
XDOT = -4578
404396 XDOT = -1395
497660
YDOT = 17346
106942 feet/sec YDOT = 5287
093396 meter/sec
ZDOT = 16214
044481 ZDOT = 4942
040758
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 16052
51566066
00016717 00000-0 10270-3 0 9118
2 25544 51
6433 279
8467 0003772 146
9540 213
1850 15
54370259 26835
Satellite: ISS
Catalog Number: 25544
Epoch time: 16052
51566066 = yrday
fracday
Element set: 911
Inclination: 51
6433 deg
RA of node: 279
8467 deg
Eccentricity:
0003772
Arg of perigee: 146
9540 deg
Mean anomaly: 213
1850 deg
Mean motion: 15
54370259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2683
Checksum: 317
Coasting Arc #13 (Orbit 2697)
---------------------------------------
Vector Time (GMT): 2016/053/10:58:53
288
Vector Time (MET): N/A
Weight (LBS) : 922176
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3742520
48 A = 6780560
20 meter
Y = 3675038
11 meter E =
0009660
Z = -4305160
84 I = 51
26970
XDOT = -2310
673023 Wp = 91
58459
YDOT = -6422
046297 meter/sec RA = 274
35244 deg
ZDOT = -3480
447607 TA = 142
83298
MA = 142
76607
Ha = 221
380 n
mi
Hp = 213
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12278610
51 X = -3762425
39
Y = 12057211
66 feet Y = 3633074
99 meter
Z = -14124543
44 Z = -4323389
40
XDOT = -7580
948237 XDOT = -2221
782254
YDOT = -21069
705699 feet/sec YDOT = -6447
389145 meter/sec
ZDOT = -11418
791363 ZDOT = -3491
455403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17142697
70 X = -5225094
26
Y = 107389
38 feet Y = 32732
28 meter
Z = -14204215
55 Z = -4329444
90
XDOT = 9361
518567 XDOT = 2853
390859
YDOT = -19068
556874 feet/sec YDOT = -5812
096135 meter/sec
ZDOT = -11465
347507 ZDOT = -3494
637920
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 16053
48002022
00016717 00000-0 10270-3 0 9123
2 25544 51
6427 275
0369 0003648 154
1270 206
0066 15
54413454 26981
Satellite: ISS
Catalog Number: 25544
Epoch time: 16053
48002022 = yrday
fracday
Element set: 912
Inclination: 51
6427 deg
RA of node: 275
0369 deg
Eccentricity:
0003648
Arg of perigee: 154
1270 deg
Mean anomaly: 206
0066 deg
Mean motion: 15
54413454 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2698
Checksum: 288
Coasting Arc #14 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2016/054/10:58:53
288
Vector Time (MET): N/A
Weight (LBS) : 922176
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4052613
63 A = 6777358
38 meter
Y = -1919227
88 meter E =
0008448
Z = 5078509
21 I = 51
25758
XDOT = 1409
215318 Wp = 137
83860
YDOT = 7358
891436 meter/sec RA = 269
32845 deg
ZDOT = 1648
707664 TA = 296
12444
MA = 296
21133
Ha = 221
248 n
mi
Hp = 213
525
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13295976
48 X = 4049105
02
Y = -6296679
41 feet Y = -1873927
84 meter
Z = 16661775
63 Z = 5098187
10
XDOT = 4623
409835 XDOT = 1318
813090
YDOT = 24143
344605 feet/sec YDOT = 7374
144956 meter/sec
ZDOT = 5409
145878 ZDOT = 1655
332634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13912248
73 X = 4240453
41
Y = 4474319
76 feet Y = 1363772
66 meter
Z = 16747409
57 Z = 5104610
44
XDOT = -12908
564119 XDOT = -3934
530343
YDOT = 19693
444179 feet/sec YDOT = 6002
561786 meter/sec
ZDOT = 5436
554856 ZDOT = 1657
061920
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 16054
50865212
00016717 00000-0 10270-3 0 9136
2 25544 51
6426 269
9063 0003675 155
8755 204
2570 15
54437776 27141
Satellite: ISS
Catalog Number: 25544
Epoch time: 16054
50865212 = yrday
fracday
Element set: 913
Inclination: 51
6426 deg
RA of node: 269
9063 deg
Eccentricity:
0003675
Arg of perigee: 155
8755 deg
Mean anomaly: 204
2570 deg
Mean motion: 15
54437776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2714
Checksum: 321
Coasting Arc #15 (Orbit 2728)
---------------------------------------
Vector Time (GMT): 2016/055/10:58:53
288
Vector Time (MET): N/A
Weight (LBS) : 922176
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4262864
83 A = 6776344
72 meter
Y = -37281
80 meter E =
0016430
Z = -5281454
72 I = 51
25500
XDOT = -436
991426 Wp = 104
70195
YDOT = -7634
068281 meter/sec RA = 264
29660 deg
ZDOT = 403
564365 TA = 169
19040
MA = 169
15505
Ha = 221
142 n
mi
Hp = 213
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13985777
01 X = -4236476
53
Y = -122315
63 feet Y = -84805
16 meter
Z = -17327607
36 Z = -5302098
19
XDOT = -1433
698903 XDOT = -353
553213
YDOT = -25046
155776 feet/sec YDOT = -7638
488423 meter/sec
ZDOT = 1324
030069 ZDOT = 401
645303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10168748
52 X = -3099434
55
Y = -9439532
45 feet Y = -2877169
49 meter
Z = -17417080
03 Z = -5308725
99
XDOT = 15121
211095 XDOT = 4608
945142
YDOT = -18737
751392 feet/sec YDOT = -5711
266624 meter/sec
ZDOT = 1317
049876 ZDOT = 401
436802
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 16055
47297366
00016717 00000-0 10270-3 0 9143
2 25544 51
6415 265
0951 0003535 161
5553 198
5728 15
54495194 27291
Satellite: ISS
Catalog Number: 25544
Epoch time: 16055
47297366 = yrday
fracday
Element set: 914
Inclination: 51
6415 deg
RA of node: 265
0951 deg
Eccentricity:
0003535
Arg of perigee: 161
5553 deg
Mean anomaly: 198
5728 deg
Mean motion: 15
54495194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2729
Checksum: 338
Coasting Arc #16 (Orbit 2744)
---------------------------------------
Vector Time (GMT): 2016/056/10:58:53
288
Vector Time (MET): N/A
Weight (LBS) : 922176
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4319203
43 A = 6778090
94 meter
Y = 1964662
32 meter E =
0006759
Z = 4834346
97 I = 51
26574
XDOT = -595
625337 Wp = 88
62263
YDOT = 7259
009703 meter/sec RA = 259
26769 deg
ZDOT = -2414
790254 TA = 25
18686
MA = 25
15392
Ha = 220
828 n
mi
Hp = 213
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14170614
93 X = 4273430
23
Y = 6445742
51 feet Y = 2012707
25 meter
Z = 15860718
42 Z = 4855216
84
XDOT = -1954
151367 XDOT = -665
023267
YDOT = 23815
648633 feet/sec YDOT = 7251
960664 meter/sec
ZDOT = -7922
540202 ZDOT = -2417
853173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6295958
10 X = 1919008
03
Y = 14136758
14 feet Y = 4308883
88 meter
Z = 15950839
90 Z = 4861816
00
XDOT = -16138
026556 XDOT = -4918
870494
YDOT = 16154
210422 feet/sec YDOT = 4923
803337 meter/sec
ZDOT = -7937
073823 ZDOT = -2419
220101
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 16056
50156298
00016717 00000-0 10270-3 0 9157
2 25544 51
6418 259
9643 0003451 167
2179 192
9062 15
54537691 27454
Satellite: ISS
Catalog Number: 25544
Epoch time: 16056
50156298 = yrday
fracday
Element set: 915
Inclination: 51
6418 deg
RA of node: 259
9643 deg
Eccentricity:
0003451
Arg of perigee: 167
2179 deg
Mean anomaly: 192
9062 deg
Mean motion: 15
54537691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2745
Checksum: 335
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