[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 21st 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 35876 11 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 453 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
There are no maneuvers
Coasting Arc #1 (Orbit 1906)
---------------------------------------
Vector Time (GMT): 2015/110/13:15:22
513
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5253619
79 A = 6780657
18 meter
Y = -3278534
65 meter E =
0005247
Z = -2753474
54 I = 51
73333
XDOT = 4695
776964 Wp = 195
22282
YDOT = -3198
213221 meter/sec RA = 11
43431 deg
ZDOT = -5154
164499 TA = 15
93971
MA = 15
92321
Ha = 216
805 n
mi
Hp = 213
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17236285
41 X = -5203192
38
Y = -10756347
28 feet Y = -3337002
24 meter
Z = -9033709
14 Z = -2778873
43
XDOT = 15406
092401 XDOT = 4756
228607
YDOT = -10492
825529 feet/sec YDOT = -3145
364226 meter/sec
ZDOT = -16909
988515 ZDOT = -5131
205913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19644011
97 X = -5987494
85
Y = 4993380
06 feet Y = 1521982
24 meter
Z = -9141957
74 Z = -2786468
72
XDOT = 3489
391570 XDOT = 1063
566550
YDOT = -17034
266590 feet/sec YDOT = -5192
044457 meter/sec
ZDOT = -16810
929215 ZDOT = -5123
971225
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 15110
57883211
00016717 00000-0 10270-3 0 9000
2 25544 51
6480 11
8347 0006110 244
3462 115
7061 15
55977680 19074
Satellite: ISS
Catalog Number: 25544
Epoch time: 15110
57883211 = yrday
fracday
Element set: 900
Inclination: 51
6480 deg
RA of node: 11
8347 deg
Eccentricity:
0006110
Arg of perigee: 244
3462 deg
Mean anomaly: 115
7061 deg
Mean motion: 15
55977680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1907
Checksum: 288
Coasting Arc #2 (Orbit 1922)
---------------------------------------
Vector Time (GMT): 2015/111/13:15:22
513
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3318889
38 A = 6775264
95 meter
Y = 3901527
23 meter E =
0006225
Z = 4435234
93 I = 51
68463
XDOT = -6654
881561 Wp = 150
62644
YDOT = 1884
703850 meter/sec RA = 6
43973 deg
ZDOT = 3314
666449 TA = 265
91561
MA = 265
98676
Ha = 216
483 n
mi
Hp = 213
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10888744
69 X = 3253469
85
Y = 12800286
19 feet Y = 3938275
57 meter
Z = 14551295
69 Z = 4451198
69
XDOT = -21833
600923 XDOT = -6691
563830
YDOT = 6183
411580 feet/sec YDOT = 1810
079612 meter/sec
ZDOT = 10874
889923 ZDOT = 3282
248646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16729638
88 X = 5099193
93
Y = 746570
56 feet Y = 227554
71 meter
Z = 14618964
02 Z = 4455860
23
XDOT = -10252
904336 XDOT = -3125
085242
YDOT = 19070
714117 feet/sec YDOT = 5812
753663 meter/sec
ZDOT = 10735
536645 ZDOT = 3272
191569
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 15111
60639719
00016717 00000-0 10270-3 0 9018
2 25544 51
6478 6
6972 0005940 248
8100 111
2419 15
56065944 19233
Satellite: ISS
Catalog Number: 25544
Epoch time: 15111
60639719 = yrday
fracday
Element set: 901
Inclination: 51
6478 deg
RA of node: 6
6972 deg
Eccentricity:
0005940
Arg of perigee: 248
8100 deg
Mean anomaly: 111
2419 deg
Mean motion: 15
56065944 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1923
Checksum: 305
Coasting Arc #3 (Orbit 1937)
---------------------------------------
Vector Time (GMT): 2015/112/13:15:22
513
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -796090
85 A = 6771564
90 meter
Y = -4189777
34 meter E =
0008642
Z = -5267290
88 I = 51
64086
XDOT = 7611
078649 Wp = 91
61201
YDOT = -443
323611 meter/sec RA = 1
42456 deg
ZDOT = -799
063678 TA = 170
75678
MA = 170
74086
Ha = 216
132 n
mi
Hp = 213
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2611846
63 X = -723593
74
Y = -13745988
65 feet Y = -4198274
49 meter
Z = -17281138
05 Z = -5270982
02
XDOT = 24970
730477 XDOT = 7619
351928
YDOT = -1454
473790 feet/sec YDOT = -358
165312 meter/sec
ZDOT = -2621
599995 ZDOT = -762
069948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11927393
22 X = -3635469
45
Y = -7279616
54 feet Y = -2218827
12 meter
Z = -17296131
16 Z = -5271860
78
XDOT = 15009
163975 XDOT = 4574
793179
YDOT = -18750
843083 feet/sec YDOT = -5715
256972 meter/sec
ZDOT = -2462
917640 ZDOT = -750
697297
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 15112
56968910
00016717 00000-0 10270-3 0 9023
2 25544 51
6470 1
8803 0006164 253
1876 106
8602 15
56181508 19388
Satellite: ISS
Catalog Number: 25544
Epoch time: 15112
56968910 = yrday
fracday
Element set: 902
Inclination: 51
6470 deg
RA of node: 1
8803 deg
Eccentricity:
0006164
Arg of perigee: 253
1876 deg
Mean anomaly: 106
8602 deg
Mean motion: 15
56181508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1938
Checksum: 305
Coasting Arc #4 (Orbit 1953)
---------------------------------------
Vector Time (GMT): 2015/113/13:15:22
513
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1881865
97 A = 6772379
47 meter
Y = 4117749
05 meter E =
0002271
Z = 5038382
57 I = 51
61278
XDOT = -7358
998955 Wp = 321
46531
YDOT = -1042
078500 meter/sec RA = 356
40223 deg
ZDOT = -1895
686157 TA = 146
92089
MA = 146
90668
Ha = 215
820 n
mi
Hp = 213
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6174100
96 X = -1952246
57
Y = 13509675
35 feet Y = 4096311
35 meter
Z = 16530126
54 Z = 5029069
73
XDOT = -24143
697360 XDOT = -7337
590622
YDOT = -3418
892716 feet/sec YDOT = -1124
251961 meter/sec
ZDOT = -6219
442773 ZDOT = -1931
383085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6142559
82 X = 1872252
23
Y = 13573690
71 feet Y = 4137260
93 meter
Z = 16489384
88 Z = 5025964
51
XDOT = -17327
998657 XDOT = -5281
573991
YDOT = 15587
680035 feet/sec YDOT = 4751
124875 meter/sec
ZDOT = -6372
266877 ZDOT = -1942
266944
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 15113
59715004
00016717 00000-0 10270-3 0 9032
2 25544 51
6472 356
7426 0006339 257
0347 103
0099 15
56266037 19541
Satellite: ISS
Catalog Number: 25544
Epoch time: 15113
59715004 = yrday
fracday
Element set: 903
Inclination: 51
6472 deg
RA of node: 356
7426 deg
Eccentricity:
0006339
Arg of perigee: 257
0347 deg
Mean anomaly: 103
0099 deg
Mean motion: 15
56266037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1954
Checksum: 307
Coasting Arc #5 (Orbit 1968)
---------------------------------------
Vector Time (GMT): 2015/114/13:15:22
513
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4266466
17 A = 6776992
72 meter
Y = -3672530
89 meter E =
0002385
Z = -3774710
83 I = 51
59600
XDOT = 5891
063062 Wp = 194
47860
YDOT = 2496
531094 meter/sec RA = 351
38770 deg
ZDOT = 4226
739998 TA = 120
23137
MA = 120
20775
Ha = 215
492 n
mi
Hp = 213
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13997592
41 X = 4325552
45
Y = -12048985
86 feet Y = -3624490
18 meter
Z = -12384221
89 Z = -3753841
43
XDOT = 19327
634717 XDOT = 5842
176352
YDOT = 8190
718813 feet/sec YDOT = 2562
135557 meter/sec
ZDOT = 13867
257210 ZDOT = 4255
239050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -266902
56 X = -81351
90
Y = -18527417
97 feet Y = -5647157
00 meter
Z = -12294029
11 Z = -3747220
07
XDOT = 17248
062523 XDOT = 5257
209457
YDOT = -9537
173482 feet/sec YDOT = -2906
930477 meter/sec
ZDOT = 13988
932203 ZDOT = 4263
826536
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 15114
56034793
00016717 00000-0 10270-3 0 9040
2 25544 51
6462 351
9245 0006445 260
6637 99
3789 15
56321721 19697
Satellite: ISS
Catalog Number: 25544
Epoch time: 15114
56034793 = yrday
fracday
Element set: 904
Inclination: 51
6462 deg
RA of node: 351
9245 deg
Eccentricity:
0006445
Arg of perigee: 260
6637 deg
Mean anomaly: 99
3789 deg
Mean motion: 15
56321721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1969
Checksum: 331
Coasting Arc #6 (Orbit 1984)
---------------------------------------
Vector Time (GMT): 2015/115/13:15:22
513
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5922655
31 A = 6781537
90 meter
Y = 2819673
78 meter E =
0009061
Z = 1698459
85 I = 51
58110
XDOT = -3451
202251 Wp = 137
29223
YDOT = -3811
908933 meter/sec RA = 346
39240 deg
ZDOT = -5695
018639 TA = 24
04913
MA = 24
00684
Ha = 215
192 n
mi
Hp = 213
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19431283
83 X = -5961995
92
Y = 9250898
24 feet Y = 2753222
87 meter
Z = 5572374
84 Z = 1669592
94
XDOT = -11322
842031 XDOT = -3380
655656
YDOT = -12506
262902 feet/sec YDOT = -3850
108263 meter/sec
ZDOT = -18684
444355 ZDOT = -5711
612529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4971269
36 X = -1515242
90
Y = 20971653
57 feet Y = 6392160
01 meter
Z = 5448072
90 Z = 1660572
62
XDOT = -15238
409117 XDOT = -4644
667099
YDOT = 1269
802815 feet/sec YDOT = 387
035898 meter/sec
ZDOT = -18754
821868 ZDOT = -5716
469705
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 15115
58770766
00016717 00000-0 10270-3 0 9051
2 25544 51
6464 346
7865 0006452 265
2104 94
8313 15
56408589 19856
Satellite: ISS
Catalog Number: 25544
Epoch time: 15115
58770766 = yrday
fracday
Element set: 905
Inclination: 51
6464 deg
RA of node: 346
7865 deg
Eccentricity:
0006452
Arg of perigee: 265
2104 deg
Mean anomaly: 94
8313 deg
Mean motion: 15
56408589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1985
Checksum: 341
Coasting Arc #7 (Orbit 2000)
---------------------------------------
Vector Time (GMT): 2015/116/13:15:22
513
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6548668
52 A = 6782235
46 meter
Y = -1571201
93 meter E =
0008738
Z = 754489
66 I = 51
55242
XDOT = 469
869911 Wp = 27
73193
YDOT = 4824
137581 meter/sec RA = 341
40514 deg
ZDOT = 5947
694639 TA = 340
44094
MA = 340
47445
Ha = 214
910 n
mi
Hp = 213
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21485132
96 X = 6562086
32
Y = -5154861
99 feet Y = -1497895
39 meter
Z = 2475359
78 Z = 786334
64
XDOT = 1541
567951 XDOT = 386
998513
YDOT = 15827
223035 feet/sec YDOT = 4828
928873 meter/sec
ZDOT = 19513
433856 ZDOT = 5949
775689
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9074843
37 X = 2766012
26
Y = -20127958
50 feet Y = -6135001
75 meter
Z = 2612173
56 Z = 796190
50
XDOT = 11913
044219 XDOT = 3631
095878
YDOT = 7912
669745 feet/sec YDOT = 2411
781738 meter/sec
ZDOT = 19521
401662 ZDOT = 5950
123227
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 15116
61501469
00016717 00000-0 10270-3 0 9069
2 25544 51
6452 341
6463 0006620 268
1820 91
8575 15
56479707 20012
Satellite: ISS
Catalog Number: 25544
Epoch time: 15116
61501469 = yrday
fracday
Element set: 906
Inclination: 51
6452 deg
RA of node: 341
6463 deg
Eccentricity:
0006620
Arg of perigee: 268
1820 deg
Mean anomaly: 91
8575 deg
Mean motion: 15
56479707 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2001
Checksum: 305
Coasting Arc #8 (Orbit 2015)
---------------------------------------
Vector Time (GMT): 2015/117/13:15:22
513
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6041210
22 A = 6778200
88 meter
Y = -26232
95 meter E =
0002483
Z = -3070502
93 I = 51
50906
XDOT = 2512
218189 Wp = 248
47688
YDOT = -5344
165050 meter/sec RA = 336
41074 deg
ZDOT = -4894
832641 TA = 326
89473
MA = 326
91026
Ha = 214
779 n
mi
Hp = 213
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19820243
51 X = -6025552
44
Y = -86066
13 feet Y = -93702
33 meter
Z = -10073828
50 Z = -3099812
10
XDOT = 8242
185658 XDOT = 2595
568609
YDOT = -17533
349901 feet/sec YDOT = -5315
606008 meter/sec
ZDOT = -16059
162209 ZDOT = -4882
425960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11899474
50 X = -3626959
83
Y = 15770389
69 feet Y = 4806814
78 meter
Z = -10199450
80 Z = -3108792
60
XDOT = -7897
241017 XDOT = -2407
079062
YDOT = -16314
777213 feet/sec YDOT = -4972
744095 meter/sec
ZDOT = -16004
932622 ZDOT = -4878
303463
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 15117
57806846
00016717 00000-0 10270-3 0 9073
2 25544 51
6444 336
8286 0006689 272
3485 87
6903 15
56545811 20165
Satellite: ISS
Catalog Number: 25544
Epoch time: 15117
57806846 = yrday
fracday
Element set: 907
Inclination: 51
6444 deg
RA of node: 336
8286 deg
Eccentricity:
0006689
Arg of perigee: 272
3485 deg
Mean anomaly: 87
6903 deg
Mean motion: 15
56545811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2016
Checksum: 342
Coasting Arc #9 (Orbit 2031)
---------------------------------------
Vector Time (GMT): 2015/118/13:15:22
513
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4515198
19 A = 6772622
43 meter
Y = 1812829
44 meter E =
0002824
Z = 4712292
40 I = 51
46184
XDOT = -4945
059576 Wp = 177
08645
YDOT = 5183
995657 meter/sec RA = 331
39201 deg
ZDOT = 2741
096199 TA = 245
71501
MA = 245
74451
Ha = 214
755 n
mi
Hp = 213
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14813642
36 X = 4471700
38
Y = 5947603
13 feet Y = 1863078
41 meter
Z = 15460276
90 Z = 4734120
77
XDOT = -16223
948739 XDOT = -5015
976047
YDOT = 17007
859767 feet/sec YDOT = 5128
300417 meter/sec
ZDOT = 8993
097766 ZDOT = 2716
901303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13432537
26 X = 4094237
36
Y = -8455434
30 feet Y = -2577216
37 meter
Z = 15553479
31 Z = 4740700
49
XDOT = 3655
673672 XDOT = 1114
249335
YDOT = 22174
406314 feet/sec YDOT = 6758
759045 meter/sec
ZDOT = 8888
382309 ZDOT = 2709
178928
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 15118
60527622
00016717 00000-0 10270-3 0 9081
2 25544 51
6441 331
6879 0006734 276
7171 83
3216 15
56590166 20325
Satellite: ISS
Catalog Number: 25544
Epoch time: 15118
60527622 = yrday
fracday
Element set: 908
Inclination: 51
6441 deg
RA of node: 331
6879 deg
Eccentricity:
0006734
Arg of perigee: 276
7171 deg
Mean anomaly: 83
3216 deg
Mean motion: 15
56590166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2032
Checksum: 310
Coasting Arc #10 (Orbit 2046)
---------------------------------------
Vector Time (GMT): 2015/119/13:15:22
513
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2288672
42 A = 6769867
51 meter
Y = -3551451
94 meter E =
0008306
Z = -5296779
63 I = 51
42513
XDOT = 6406
898078 Wp = 83
53610
YDOT = -4210
721421 meter/sec RA = 326
35316 deg
ZDOT = 55
909640 TA = 186
99254
MA = 187
00414
Ha = 214
822 n
mi
Hp = 213
085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7508767
79 X = -2223059
09
Y = -11651745
22 feet Y = -3576678
84 meter
Z = -17377885
94 Z = -5307738
08
XDOT = 21020
006818 XDOT = 6453
235599
YDOT = -13814
702824 feet/sec YDOT = -4138
816205 meter/sec
ZDOT = 183
430579 ZDOT = 87
146259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13791283
47 X = -4203583
20
Y = -578668
83 feet Y = -176378
26 meter
Z = -17424159
16 Z = -5310883
71
XDOT = 614
970758 XDOT = 187
443087
YDOT = -24137
658317 feet/sec YDOT = -7357
158255 meter/sec
ZDOT = 318
125116 ZDOT = 96
964535
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 15119
56823384
00016717 00000-0 10270-3 0 9092
2 25544 51
6431 326
8685 0006725 279
2436 80
7958 15
56703193 20473
Satellite: ISS
Catalog Number: 25544
Epoch time: 15119
56823384 = yrday
fracday
Element set: 909
Inclination: 51
6431 deg
RA of node: 326
8685 deg
Eccentricity:
0006725
Arg of perigee: 279
2436 deg
Mean anomaly: 80
7958 deg
Mean motion: 15
56703193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2047
Checksum: 339
Coasting Arc #11 (Orbit 2062)
---------------------------------------
Vector Time (GMT): 2015/120/13:15:22
513
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -211033
85 A = 6772495
26 meter
Y = 4922025
80 meter E =
0005112
Z = 4648961
92 I = 51
40852
XDOT = -6688
441924 Wp = 7
27116
YDOT = 2425
521119 meter/sec RA = 321
31299 deg
ZDOT = -2866
278009 TA = 111
31706
MA = 111
26248
Ha = 215
038 n
mi
Hp = 213
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -692368
26 X = -288640
66
Y = 16148378
60 feet Y = 4919232
24 meter
Z = 15252499
73 Z = 4647747
94
XDOT = -21943
707101 XDOT = -6701
144076
YDOT = 7957
746452 feet/sec YDOT = 2350
655389 meter/sec
ZDOT = -9403
799243 ZDOT = -2898
800616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12976607
72 X = 3955270
03
Y = 9645982
65 feet Y = 2940095
51 meter
Z = 15246341
33 Z = 4647084
84
XDOT = -4868
978801 XDOT = -1484
064739
YDOT = 21662
377094 feet/sec YDOT = 6602
692538 meter/sec
ZDOT = -9543
647163 ZDOT = -2908
903655
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 15120
59533901
00016717 00000-0 10270-3 0 9102
2 25544 51
6431 321
7281 0006906 282
9408 77
0975 15
56763258 20634
Satellite: ISS
Catalog Number: 25544
Epoch time: 15120
59533901 = yrday
fracday
Element set: 910
Inclination: 51
6431 deg
RA of node: 321
7281 deg
Eccentricity:
0006906
Arg of perigee: 282
9408 deg
Mean anomaly: 77
0975 deg
Mean motion: 15
56763258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2063
Checksum: 310
Coasting Arc #12 (Orbit 2077)
---------------------------------------
Vector Time (GMT): 2015/121/13:15:22
513
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2500236
15 A = 6777886
67 meter
Y = -5590114
18 meter E =
0004651
Z = -2897668
36 I = 51
40283
XDOT = 5803
155285 Wp = 328
35225
YDOT = -5
820518 meter/sec RA = 316
28832 deg
ZDOT = 5018
670255 TA = 358
46807
MA = 358
46949
Ha = 215
118 n
mi
Hp = 213
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8202874
52 X = 2576636
35
Y = -18340269
61 feet Y = -5561727
88 meter
Z = -9506785
96 Z = -2885336
62
XDOT = 19039
223377 XDOT = 5778
409825
YDOT = -19
096187 feet/sec YDOT = 58
936072 meter/sec
ZDOT = 16465
453592 ZDOT = 5046
801235
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10928535
67 X = -3331017
67
Y = -16889114
48 feet Y = -5147802
09 meter
Z = -9452858
79 Z = -2881231
36
XDOT = 9022
027747 XDOT = 2749
914057
YDOT = -15120
731089 feet/sec YDOT = -4608
798836 meter/sec
ZDOT = 16586
004655 ZDOT = 5055
414219
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 15121
55820271
00016717 00000-0 10270-3 0 9119
2 25544 51
6427 316
9075 0006841 286
4940 73
5463 15
56852901 20787
Satellite: ISS
Catalog Number: 25544
Epoch time: 15121
55820271 = yrday
fracday
Element set: 911
Inclination: 51
6427 deg
RA of node: 316
9075 deg
Eccentricity:
0006841
Arg of perigee: 286
4940 deg
Mean anomaly: 73
5463 deg
Mean motion: 15
56852901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2078
Checksum: 310
Coasting Arc #13 (Orbit 2093)
---------------------------------------
Vector Time (GMT): 2015/122/13:15:22
513
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4205011
79 A = 6780987
97 meter
Y = 5298006
51 meter E =
0006473
Z = 420442
50 I = 51
39206
XDOT = -3988
889876 Wp = 150
64536
YDOT = -2689
084922 meter/sec RA = 311
28398 deg
ZDOT = -5975
683991 TA = 24
80102
MA = 24
76992
Ha = 215
295 n
mi
Hp = 212
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13795970
44 X = -4265985
23
Y = 17381911
14 feet Y = 5250642
42 meter
Z = 1379404
53 Z = 399866
64
XDOT = -13086
909043 XDOT = -3929
495209
YDOT = -8822
457093 feet/sec YDOT = -2733
359449 meter/sec
ZDOT = -19605
262438 ZDOT = -5994
917251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7478144
52 X = 2279338
45
Y = 20899165
03 feet Y = 6370065
50 meter
Z = 1290212
25 Z = 393256
69
XDOT = -12812
355403 XDOT = -3905
205927
YDOT = 5807
175464 feet/sec YDOT = 1770
027081 meter/sec
ZDOT = -19687
160422 ZDOT = -6000
646497
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 15122
58520460
00016717 00000-0 10270-3 0 9121
2 25544 51
6426 311
7664 0007104 292
4828 67
5573 15
56979224 20949
Satellite: ISS
Catalog Number: 25544
Epoch time: 15122
58520460 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 311
7664 deg
Eccentricity:
0007104
Arg of perigee: 292
4828 deg
Mean anomaly: 67
5573 deg
Mean motion: 15
56979224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2094
Checksum: 314
Coasting Arc #14 (Orbit 2109)
---------------------------------------
Vector Time (GMT): 2015/123/13:15:22
513
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5054036
71 A = 6778885
28 meter
Y = -3949594
72 meter E =
0010027
Z = 2173308
07 I = 51
36507
XDOT = 1654
434689 Wp = 42
61207
YDOT = 5128
681758 meter/sec RA = 306
28032 deg
ZDOT = 5465
512495 TA = 341
64406
MA = 341
68022
Ha = 215
199 n
mi
Hp = 212
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16581485
28 X = 5087269
05
Y = -12957987
93 feet Y = -3892891
31 meter
Z = 7130275
83 Z = 2197940
95
XDOT = 5427
935331 XDOT = 1570
411598
YDOT = 16826
383722 feet/sec YDOT = 5146
713058 meter/sec
ZDOT = 17931
471440 ZDOT = 5473
345381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2637192
07 X = -803816
14
Y = -20841616
03 feet Y = -6352524
57 meter
Z = 7236587
47 Z = 2205711
86
XDOT = 15650
792606 XDOT = 4770
361586
YDOT = 4265
541198 feet/sec YDOT = 1300
136957 meter/sec
ZDOT = 17964
048447 ZDOT = 5475
441967
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 15123
61215655
00016717 00000-0 10270-3 0 9134
2 25544 51
6424 306
6239 0006946 294
5083 65
5346 15
57014168 21100
Satellite: ISS
Catalog Number: 25544
Epoch time: 15123
61215655 = yrday
fracday
Element set: 913
Inclination: 51
6424 deg
RA of node: 306
6239 deg
Eccentricity:
0006946
Arg of perigee: 294
5083 deg
Mean anomaly: 65
5346 deg
Mean motion: 15
57014168 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2110
Checksum: 298
Coasting Arc #15 (Orbit 2124)
---------------------------------------
Vector Time (GMT): 2015/124/13:15:22
513
Vector Time (MET): N/A
Weight (LBS) : 923717
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5002412
28 A = 6772909
53 meter
Y = 1690433
91 meter E =
0006583
Z = -4247141
63 I = 51
32878
XDOT = 754
003791 Wp = 15
42192
YDOT = -6744
923774 meter/sec RA = 301
25806 deg
ZDOT = -3567
724363 TA = 217
97285
MA = 218
01928
Ha = 215
410 n
mi
Hp = 212
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16412113
79 X = -5000311
85
Y = 5546043
02 feet Y = 1634505
39 meter
Z = -13934191
71 Z = -4271437
82
XDOT = 2473
765718 XDOT = 846
702146
YDOT = -22129
015008 feet/sec YDOT = -6735
973720 meter/sec
ZDOT = -11705
132426 ZDOT = -3563
836289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3325697
67 X = -1013672
65
Y = 16915512
17 feet Y = 5155848
11 meter
Z = -14038623
65 Z = -4278972
49
XDOT = -16684
373405 XDOT = -5085
397014
YDOT = -12993
145556 feet/sec YDOT = -3960
310765 meter/sec
ZDOT = -11687
178148 ZDOT = -3562
251900
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 15124
57487426
00016717 00000-0 10270-3 0 9148
2 25544 51
6433 301
8040 0006974 299
5780 60
4678 15
57104019 21250
Satellite: ISS
Catalog Number: 25544
Epoch time: 15124
57487426 = yrday
fracday
Element set: 914
Inclination: 51
6433 deg
RA of node: 301
8040 deg
Eccentricity:
0006974
Arg of perigee: 299
5780 deg
Mean anomaly: 60
4678 deg
Mean motion: 15
57104019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2125
Checksum: 312
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