[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 6th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8880 23 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 819 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
250/04:29:38
826 0
3 1
8 1
8
N/A 1
3 -0
0 219
4
000/00:09:17
652 1
2 -0
1 213
6
254/21:27:00
000 0
0 0
0 0
0
N/A 0
0 0
0 219
2
000/00:00:00
000 0
0 0
0 213
4
257/01:13:16
660 7
4 7
5 7
5
N/A -0
9 0
0 219
4
000/00:02:33
320 -1
1 0
0 217
5
Coasting Arc #1 (Orbit 37)
---------------------------------------
Vector Time (GMT): 2015/247/10:57:53
829
Vector Time (MET): N/A
Weight (LBS) : 942160
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5480626
05 A = 6783356
18 meter
Y = -3132866
27 meter E =
0013957
Z = 2463521
25 I = 51
92577
XDOT = 699
635572 Wp = 108
77960
YDOT = -5450
960383 meter/sec RA = 47
55386 deg
ZDOT = -5355
173951 TA = 43
71676
MA = 43
60632
Ha = 219
189 n
mi
Hp = 212
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17981056
60 X = -5457153
10
Y = -10278432
65 feet Y = -3194022
82 meter
Z = 8082418
80 Z = 2436954
69
XDOT = 2295
392298 XDOT = 786
550934
YDOT = -17883
728290 feet/sec YDOT = -5442
650994 meter/sec
ZDOT = -17569
468343 ZDOT = -5351
563777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9487506
23 X = 2891791
90
Y = 18460269
10 feet Y = 5626690
02 meter
Z = 7968422
55 Z = 2428775
19
XDOT = -10442
126576 XDOT = -3182
760180
YDOT = 12972
595762 feet/sec YDOT = 3954
047188 meter/sec
ZDOT = -17552
853181 ZDOT = -5350
109650
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 15247
49388983
00016717 00000-0 10270-3 0 9008
2 25544 51
6412 48
0394 0000851 184
4595 175
6551 15
55323053 382
Satellite: ISS
Catalog Number: 25544
Epoch time: 15247
49388983 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 48
0394 deg
Eccentricity:
0000851
Arg of perigee: 184
4595 deg
Mean anomaly: 175
6551 deg
Mean motion: 15
55323053 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 38
Checksum: 314
Coasting Arc #2 (Orbit 52)
---------------------------------------
Vector Time (GMT): 2015/248/10:57:53
829
Vector Time (MET): N/A
Weight (LBS) : 942160
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5216051
92 A = 6785806
21 meter
Y = 4309311
92 meter E =
0010545
Z = -456518
48 I = 51
91163
XDOT = -2712
102375 Wp = 45
91545
YDOT = 3910
073468 meter/sec RA = 42
59371 deg
ZDOT = 6014
529764 TA = 309
17782
MA = 309
27144
Ha = 219
230 n
mi
Hp = 212
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17113031
22 X = 5169694
07
Y = 14138162
48 feet Y = 4367382
02 meter
Z = -1497764
06 Z = -431292
86
XDOT = -8897
973672 XDOT = -2784
840439
YDOT = 12828
325026 feet/sec YDOT = 3879
338618 meter/sec
ZDOT = 19732
709199 ZDOT = 6001
178027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6979794
79 X = -2127441
45
Y = -21079320
09 feet Y = -6424976
76 meter
Z = -1389785
02 Z = -423606
47
XDOT = 12928
394421 XDOT = 3940
574620
YDOT = -5556
316537 feet/sec YDOT = -1693
565280 meter/sec
ZDOT = 19674
363164 ZDOT = 5996
745892
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 15248
45769174
00016717 00000-0 10270-3 0 9011
2 25544 51
6410 43
2255 0001042 174
5217 185
5948 15
55313978 539
Satellite: ISS
Catalog Number: 25544
Epoch time: 15248
45769174 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 43
2255 deg
Eccentricity:
0001042
Arg of perigee: 174
5217 deg
Mean anomaly: 185
5948 deg
Mean motion: 15
55313978 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 53
Checksum: 304
Coasting Arc #3 (Orbit 68)
---------------------------------------
Vector Time (GMT): 2015/249/10:57:53
829
Vector Time (MET): N/A
Weight (LBS) : 942160
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4308016
70 A = 6784541
67 meter
Y = -4966727
64 meter E =
0008415
Z = -1660326
11 I = 51
88403
XDOT = 4633
591444 Wp = 144
46922
YDOT = -2108
948786 meter/sec RA = 37
63523 deg
ZDOT = -5735
166462 TA = 53
66261
MA = 53
58497
Ha = 219
101 n
mi
Hp = 212
683
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14133913
06 X = -4244092
17
Y = -16295038
20 feet Y = -5014545
40 meter
Z = -5447264
14 Z = -1681097
94
XDOT = 15202
071667 XDOT = 4684
688972
YDOT = -6919
123314 feet/sec YDOT = -2056
847556 meter/sec
ZDOT = -18816
162934 ZDOT = -5712
533271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3637877
86 X = 1108825
17
Y = 21238835
47 feet Y = 6473597
05 meter
Z = -5535898
07 Z = -1687341
73
XDOT = -15144
043446 XDOT = -4615
904442
YDOT = -2267
084680 feet/sec YDOT = -691
007410 meter/sec
ZDOT = -18718
127865 ZDOT = -5705
285373
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 15249
48573434
00016717 00000-0 10270-3 0 9028
2 25544 51
6412 38
0910 0000807 173
1777 186
9387 15
55359276 695
Satellite: ISS
Catalog Number: 25544
Epoch time: 15249
48573434 = yrday
fracday
Element set: 902
Inclination: 51
6412 deg
RA of node: 38
0910 deg
Eccentricity:
0000807
Arg of perigee: 173
1777 deg
Mean anomaly: 186
9387 deg
Mean motion: 15
55359276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 69
Checksum: 327
Coasting Arc #4 (Orbit 79)
---------------------------------------
Vector Time (GMT): 2015/250/04:34:17
652
Vector Time (MET): N/A
Weight (LBS) : 941980
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5982439
68 A = 6786336
70 meter
Y = 3004509
53 meter E =
0009732
Z = -1082956
88 I = 51
87139
XDOT = -1303
398780 Wp = 31
91175
YDOT = 4713
189428 meter/sec RA = 33
96146 deg
ZDOT = 5908
098265 TA = 316
37534
MA = 316
45224
Ha = 219
404 n
mi
Hp = 213
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19627426
77 X = 5953658
46
Y = 9857314
75 feet Y = 3071248
12 meter
Z = -3553008
14 Z = -1053965
68
XDOT = -4276
242715 XDOT = -1384
705036
YDOT = 15463
219908 feet/sec YDOT = 4698
159725 meter/sec
ZDOT = 19383
524493 ZDOT = 5901
568879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19581184
57 X = 5968345
06
Y = -9992432
18 feet Y = -3045693
33 meter
Z = -3428543
76 Z = -1045020
14
XDOT = 9124
790918 XDOT = 2781
236272
YDOT = 11277
764054 feet/sec YDOT = 3437
462484 meter/sec
ZDOT = 19354
443937 ZDOT = 5899
234512
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 15250
19250837
00016717 00000-0 10270-3 0 9038
2 25544 51
6450 34
5655 0001044 311
3326 48
7737 15
54997889 808
Satellite: ISS
Catalog Number: 25544
Epoch time: 15250
19250837 = yrday
fracday
Element set: 903
Inclination: 51
6450 deg
RA of node: 34
5655 deg
Eccentricity:
0001044
Arg of perigee: 311
3326 deg
Mean anomaly: 48
7737 deg
Mean motion: 15
54997889 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 80
Checksum: 310
Coasting Arc #5 (Orbit 95)
---------------------------------------
Vector Time (GMT): 2015/251/04:34:17
652
Vector Time (MET): N/A
Weight (LBS) : 941980
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5481322
97 A = 6786463
26 meter
Y = -3882547
71 meter E =
0008803
Z = -939482
55 I = 51
84498
XDOT = 3438
375734 Wp = 142
24051
YDOT = -3426
534320 meter/sec RA = 29
00213 deg
ZDOT = -5936
371606 TA = 47
90526
MA = 47
83044
Ha = 219
371 n
mi
Hp = 213
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17983343
07 X = -5432936
39
Y = -12738017
41 feet Y = -3943572
99 meter
Z = -3082291
83 Z = -965991
67
XDOT = 11280
760282 XDOT = 3505
272895
YDOT = -11241
910499 feet/sec YDOT = -3387
710522 meter/sec
ZDOT = -19476
284795 ZDOT = -5919
506088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20781379
19 X = -6334164
38
Y = 7285527
12 feet Y = 2220628
67 meter
Z = -3195874
27 Z = -974102
48
XDOT = -2044
015560 XDOT = -623
015943
YDOT = -14291
503562 feet/sec YDOT = -4356
050286 meter/sec
ZDOT = -19402
871343 ZDOT = -5913
995185
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 15251
22076588
00016717 00000-0 10270-3 0 9043
2 25544 51
6452 29
4326 0001041 309
5959 50
5102 15
54975395 968
Satellite: ISS
Catalog Number: 25544
Epoch time: 15251
22076588 = yrday
fracday
Element set: 904
Inclination: 51
6452 deg
RA of node: 29
4326 deg
Eccentricity:
0001041
Arg of perigee: 309
5959 deg
Mean anomaly: 50
5102 deg
Mean motion: 15
54975395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 96
Checksum: 305
Coasting Arc #6 (Orbit 111)
---------------------------------------
Vector Time (GMT): 2015/252/04:34:17
652
Vector Time (MET): N/A
Weight (LBS) : 941980
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4366440
63 A = 6783378
05 meter
Y = 4360492
14 meter E =
0012921
Z = 2801416
37 I = 51
80674
XDOT = -5333
546918 Wp = 75
01964
YDOT = 2037
052891 meter/sec RA = 24
03532 deg
ZDOT = 5125
992851 TA = 316
71360
MA = 316
81505
Ha = 219
366 n
mi
Hp = 213
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14325592
63 X = 4303747
96
Y = 14306076
59 feet Y = 4408970
26 meter
Z = 9190998
58 Z = 2822474
79
XDOT = -17498
513512 XDOT = -5380
829199
YDOT = 6683
244394 feet/sec YDOT = 1977
145725 meter/sec
ZDOT = 16817
561848 ZDOT = 5099
968808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19861979
74 X = 6053931
43
Y = -3704886
30 feet Y = -1129249
34 meter
Z = 9280973
26 Z = 2828840
65
XDOT = -4686
070234 XDOT = -1428
314207
YDOT = 16858
458049 feet/sec YDOT = 5138
458013 meter/sec
ZDOT = 16704
920376 ZDOT = 5091
659731
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 15252
24901199
00016717 00000-0 10270-3 0 9052
2 25544 51
6452 24
2993 0001222 326
1620 33
9455 15
55008091 1128
Satellite: ISS
Catalog Number: 25544
Epoch time: 15252
24901199 = yrday
fracday
Element set: 905
Inclination: 51
6452 deg
RA of node: 24
2993 deg
Eccentricity:
0001222
Arg of perigee: 326
1620 deg
Mean anomaly: 33
9455 deg
Mean motion: 15
55008091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 112
Checksum: 274
Coasting Arc #7 (Orbit 126)
---------------------------------------
Vector Time (GMT): 2015/253/04:34:17
652
Vector Time (MET): N/A
Weight (LBS) : 941980
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2695787
07 A = 6778812
66 meter
Y = -4509480
59 meter E =
0008194
Z = -4292376
39 I = 51
76247
XDOT = 6750
741943 Wp = 59
96361
YDOT = -641
733356 meter/sec RA = 19
05436 deg
ZDOT = -3566
639519 TA = 173
69597
MA = 173
68566
Ha = 219
301 n
mi
Hp = 213
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8844445
78 X = -2624310
10
Y = -14794883
81 feet Y = -4539227
43 meter
Z = -14082599
69 Z = -4305297
78
XDOT = 22148
103487 XDOT = 6774
741427
YDOT = -2105
424396 feet/sec YDOT = -566
108285 meter/sec
ZDOT = -11701
573224 ZDOT = -3533
787761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17172115
93 X = -5234060
94
Y = -826712
55 feet Y = -251981
98 meter
Z = -14137446
84 Z = -4309093
80
XDOT = 10402
961762 XDOT = 3170
822745
YDOT = -18465
559807 feet/sec YDOT = -5628
302629 meter/sec
ZDOT = -11559
763062 ZDOT = -3523
415781
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 15253
21298153
00016717 00000-0 10270-3 0 9060
2 25544 51
6453 19
4872 0001373 322
3447 37
7610 15
55039418 1271
Satellite: ISS
Catalog Number: 25544
Epoch time: 15253
21298153 = yrday
fracday
Element set: 906
Inclination: 51
6453 deg
RA of node: 19
4872 deg
Eccentricity:
0001373
Arg of perigee: 322
3447 deg
Mean anomaly: 37
7610 deg
Mean motion: 15
55039418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 127
Checksum: 295
Coasting Arc #8 (Orbit 142)
---------------------------------------
Vector Time (GMT): 2015/254/04:34:17
652
Vector Time (MET): N/A
Weight (LBS) : 941980
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 659872
74 A = 6775366
84 meter
Y = 4352916
25 meter E =
0003476
Z = 5147586
08 I = 51
72090
XDOT = -7494
410780 Wp = 114
93685
YDOT = -649
810646 meter/sec RA = 14
05772 deg
ZDOT = 1507
979685 TA = 320
55030
MA = 320
57561
Ha = 219
367 n
mi
Hp = 213
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2164936
82 X = 586143
55
Y = 14281221
30 feet Y = 4359883
74 meter
Z = 16888405
78 Z = 5150612
00
XDOT = -24587
961876 XDOT = -7493
912563
YDOT = -2131
924691 feet/sec YDOT = -733
615122 meter/sec
ZDOT = 4947
439910 ZDOT = 1471
574970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13163410
84 X = 4012207
62
Y = 5912074
99 feet Y = 1802000
46 meter
Z = 16900605
54 Z = 5151304
57
XDOT = -14553
926347 XDOT = -4436
036750
YDOT = 18689
259368 feet/sec YDOT = 5696
486255 meter/sec
ZDOT = 4790
568544 ZDOT = 1460
165292
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 15254
24120690
00016717 00000-0 10270-3 0 9075
2 25544 51
6456 14
3542 0001321 331
7590 28
3492 15
55050645 1435
Satellite: ISS
Catalog Number: 25544
Epoch time: 15254
24120690 = yrday
fracday
Element set: 907
Inclination: 51
6456 deg
RA of node: 14
3542 deg
Eccentricity:
0001321
Arg of perigee: 331
7590 deg
Mean anomaly: 28
3492 deg
Mean motion: 15
55050645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 143
Checksum: 274
Coasting Arc #9 (Orbit 153)
---------------------------------------
Vector Time (GMT): 2015/254/21:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 927453
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3178978
48 A = 6778382
05 meter
Y = 4095308
90 meter E =
0008553
Z = 4360813
36 I = 51
70593
XDOT = -6687
337346 Wp = 103
40068
YDOT = 1517
736405 meter/sec RA = 10
56182 deg
ZDOT = 3442
047455 TA = 311
70181
MA = 311
77495
Ha = 219
241 n
mi
Hp = 213
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10429719
43 X = 3111764
47
Y = 13436052
83 feet Y = 4130483
06 meter
Z = 14307130
43 Z = 4376092
30
XDOT = -21940
083157 XDOT = -6720
532053
YDOT = 4979
450149 feet/sec YDOT = 1442
769024 meter/sec
ZDOT = 11292
806611 ZDOT = 3409
481153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3217280
97 X = -980627
24
Y = 16645988
86 feet Y = 5073697
41 meter
Z = 14372219
80 Z = 4380652
60
XDOT = -17098
853035 XDOT = -5211
730405
YDOT = -12955
010282 feet/sec YDOT = -3948
687134 meter/sec
ZDOT = 11152
072921 ZDOT = 3399
151826
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 15254
94810448
00016717 00000-0 10270-3 0 9080
2 25544 51
6420 10
8243 0001253 330
0670 30
0411 15
55088947 1549
Satellite: ISS
Catalog Number: 25544
Epoch time: 15254
94810448 = yrday
fracday
Element set: 908
Inclination: 51
6420 deg
RA of node: 10
8243 deg
Eccentricity:
0001253
Arg of perigee: 330
0670 deg
Mean anomaly: 30
0411 deg
Mean motion: 15
55088947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 154
Checksum: 273
Coasting Arc #10 (Orbit 168)
---------------------------------------
Vector Time (GMT): 2015/255/21:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 927453
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1105939
08 A = 6775166
60 meter
Y = -4229720
63 meter E =
0013893
Z = -5188133
33 I = 51
66375
XDOT = 7534
789630 Wp = 74
32330
YDOT = -329
013789 meter/sec RA = 5
55980 deg
ZDOT = -1337
250598 TA = 182
81243
MA = 182
82025
Ha = 219
425 n
mi
Hp = 213
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3628409
05 X = -1033357
27
Y = -13877036
17 feet Y = -4241682
84 meter
Z = -17021434
82 Z = -5193328
87
XDOT = 24720
438418 XDOT = 7544
404563
YDOT = -1079
441565 feet/sec YDOT = -244
701230 meter/sec
ZDOT = -4387
305112 ZDOT = -1300
624886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7860075
98 X = 2395751
16
Y = -11967523
48 feet Y = -3647701
16 meter
Z = -17043013
70 Z = -5194710
57
XDOT = 16634
726089 XDOT = 5070
264512
YDOT = 16951
593407 feet/sec YDOT = 5166
845670 meter/sec
ZDOT = -4229
310474 ZDOT = -1289
093833
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 15255
91204939
00016717 00000-0 10270-3 0 9091
2 25544 51
6423 6
0114 0001309 341
9709 18
1398 15
55070210 1693
Satellite: ISS
Catalog Number: 25544
Epoch time: 15255
91204939 = yrday
fracday
Element set: 909
Inclination: 51
6423 deg
RA of node: 6
0114 deg
Eccentricity:
0001309
Arg of perigee: 341
9709 deg
Mean anomaly: 18
1398 deg
Mean motion: 15
55070210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 169
Checksum: 288
Coasting Arc #11 (Orbit 184)
---------------------------------------
Vector Time (GMT): 2015/256/21:27:00
000
Vector Time (MET): N/A
Weight (LBS) : 927453
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1124041
25 A = 6774886
17 meter
Y = 4139593
07 meter E =
0004271
Z = 5242155
90 I = 51
63141
XDOT = -7565
880262 Wp = 38
48543
YDOT = -833
262315 meter/sec RA =
55068 deg
ZDOT = -960
604156 TA = 60
72531
MA = 60
68262
Ha = 219
463 n
mi
Hp = 213
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3687799
37 X = -1195712
01
Y = 13581342
08 feet Y = 4126623
30 meter
Z = 17198674
21 Z = 5236520
87
XDOT = -24822
441803 XDOT = -7551
333964
YDOT = -2733
800246 feet/sec YDOT = -917
787775 meter/sec
ZDOT = -3151
588437 ZDOT = -997
322181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12471437
61 X = -3801294
18
Y = 6586257
25 feet Y = 2007491
21 meter
Z = 17173571
87 Z = 5234504
71
XDOT = -14594
650374 XDOT = -4448
449434
YDOT = -18974
027735 feet/sec YDOT = -5783
283654 meter/sec
ZDOT = -3309
741152 ZDOT = -1008
809103
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 15256
94024542
00016717 00000-0 10270-3 0 9107
2 25544 51
6426
8788 0001434 344
7855 15
3255 15
55089623 1854
Satellite: ISS
Catalog Number: 25544
Epoch time: 15256
94024542 = yrday
fracday
Element set: 910
Inclination: 51
6426 deg
RA of node:
8788 deg
Eccentricity:
0001434
Arg of perigee: 344
7855 deg
Mean anomaly: 15
3255 deg
Mean motion: 15
55089623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 185
Checksum: 305
Coasting Arc #12 (Orbit 186)
---------------------------------------
Vector Time (GMT): 2015/257/01:14:33
320
Vector Time (MET): N/A
Weight (LBS) : 926688
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -674690
38 A = 6778606
21 meter
Y = -4188992
02 meter E =
0008626
Z = -5293929
44 I = 51
62870
XDOT = 7623
741533 Wp = 79
77142
YDOT = -490
991269 meter/sec RA = 359
77569 deg
ZDOT = -582
414272 TA = 184
66048
MA = 184
66851
Ha = 219
389 n
mi
Hp = 217
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2213551
11 X = -602082
03
Y = -13743412
14 feet Y = -4196131
63 meter
Z = -17368534
89 Z = -5297029
99
XDOT = 25012
275371 XDOT = 7631
494448
YDOT = -1610
863745 feet/sec YDOT = -405
694303 meter/sec
ZDOT = -1910
807979 ZDOT = -545
360797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4573029
63 X = -1393859
43
Y = -13131351
28 feet Y = -4002435
87 meter
Z = -17381087
53 Z = -5297755
48
XDOT = 23353
427847 XDOT = 7118
124808
YDOT = -5812
288039 feet/sec YDOT = -1771
585394 meter/sec
ZDOT = -1750
953211 ZDOT = -533
690539
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 15257
06877282
00016717 00000-0 10270-3 0 9119
2 25544 51
6456
2383 0006203 273
7542 86
2902 15
53729964 1870
Satellite: ISS
Catalog Number: 25544
Epoch time: 15257
06877282 = yrday
fracday
Element set: 911
Inclination: 51
6456 deg
RA of node:
2383 deg
Eccentricity:
0006203
Arg of perigee: 273
7542 deg
Mean anomaly: 86
2902 deg
Mean motion: 15
53729964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 187
Checksum: 313
Coasting Arc #13 (Orbit 202)
---------------------------------------
Vector Time (GMT): 2015/258/01:14:33
320
Vector Time (MET): N/A
Weight (LBS) : 926688
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -977978
88 A = 6778925
75 meter
Y = 4233469
34 meter E =
0004336
Z = 5206475
30 I = 51
59801
XDOT = -7565
843893 Wp = 317
53001
YDOT = -265
734150 meter/sec RA = 354
77833 deg
ZDOT = -1202
543762 TA = 144
03234
MA = 144
00315
Ha = 219
491 n
mi
Hp = 217
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3208592
13 X = -1050537
03
Y = 13889335
10 feet Y = 4222127
98 meter
Z = 17081611
89 Z = 5201547
63
XDOT = -24822
322484 XDOT = -7556
468561
YDOT = -871
831201 feet/sec YDOT = -350
288151 meter/sec
ZDOT = -3945
353551 ZDOT = -1239
274405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -484306
36 X = -147616
58
Y = 14273316
83 feet Y = 4350506
97 meter
Z = 17059543
71 Z = 5199748
92
XDOT = -23432
672877 XDOT = -7142
278693
YDOT = 4119
606656 feet/sec YDOT = 1255
656109 meter/sec
ZDOT = -4103
655396 ZDOT = -1250
794165
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 15258
09787485
00016717 00000-0 10270-3 0 9129
2 25544 51
6454 355
1115 0006381 278
1421 81
9008 15
53765261 2033
Satellite: ISS
Catalog Number: 25544
Epoch time: 15258
09787485 = yrday
fracday
Element set: 912
Inclination: 51
6454 deg
RA of node: 355
1115 deg
Eccentricity:
0006381
Arg of perigee: 278
1421 deg
Mean anomaly: 81
9008 deg
Mean motion: 15
53765261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 203
Checksum: 306
Coasting Arc #14 (Orbit 217)
---------------------------------------
Vector Time (GMT): 2015/259/01:14:33
320
Vector Time (MET): N/A
Weight (LBS) : 926688
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2549347
07 A = 6781291
08 meter
Y = -4217750
93 meter E =
0004233
Z = -4662213
66 I = 51
57451
XDOT = 7021
589317 Wp = 120
52379
YDOT = 1057
791350 meter/sec RA = 349
78173 deg
ZDOT = 2882
378423 TA = 178
16872
MA = 178
16717
Ha = 219
731 n
mi
Hp = 217
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8363999
56 X = 2618968
91
Y = -13837765
51 feet Y = -4188853
81 meter
Z = -15295976
59 Z = -4649659
69
XDOT = 23036
710359 XDOT = 6995
237393
YDOT = 3470
444062 feet/sec YDOT = 1136
164443 meter/sec
ZDOT = 9456
622124 ZDOT = 2916
423947
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5272353
31 X = 1607013
29
Y = -15340150
19 feet Y = -4675677
78 meter
Z = -15241037
55 Z = -4645468
25
XDOT = 22064
655401 XDOT = 6725
306966
YDOT = -1958
088173 feet/sec YDOT = -596
825275 meter/sec
ZDOT = 9603
181646 ZDOT = 2927
049766
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 15259
06265036
00016717 00000-0 10270-3 0 9131
2 25544 51
6458 350
3048 0006341 282
2899 77
7543 15
53748928 2184
Satellite: ISS
Catalog Number: 25544
Epoch time: 15259
06265036 = yrday
fracday
Element set: 913
Inclination: 51
6458 deg
RA of node: 350
3048 deg
Eccentricity:
0006341
Arg of perigee: 282
2899 deg
Mean anomaly: 77
7543 deg
Mean motion: 15
53748928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 218
Checksum: 329
Coasting Arc #15 (Orbit 233)
---------------------------------------
Vector Time (GMT): 2015/260/01:14:33
320
Vector Time (MET): N/A
Weight (LBS) : 926688
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3938317
79 A = 6784682
69 meter
Y = 4107874
08 meter E =
0006398
Z = 3691726
17 I = 51
55455
XDOT = -6042
631992 Wp = 63
84517
YDOT = -1907
385765 meter/sec RA = 344
79079 deg
ZDOT = -4315
282732 TA = 72
13684
MA = 72
06707
Ha = 219
947 n
mi
Hp = 217
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12920990
11 X = -4001893
48
Y = 13477277
17 feet Y = 4063478
22 meter
Z = 12111962
51 Z = 3672439
50
XDOT = -19824
908111 XDOT = -5999
891857
YDOT = -6257
827313 feet/sec YDOT = -1974
720040 meter/sec
ZDOT = -14157
751746 ZDOT = -4344
532815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9503639
57 X = -2896709
34
Y = 16133691
74 feet Y = 4917549
24 meter
Z = 12028027
56 Z = 3666142
80
XDOT = -19472
508108 XDOT = -5935
220471
YDOT = -800
621947 feet/sec YDOT = -244
029570 meter/sec
ZDOT = -14283
464174 ZDOT = -4353
599880
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 15260
09173331
00016717 00000-0 10270-3 0 9143
2 25544 51
6454 345
1779 0006299 286
9849 73
0613 15
53767869 2341
Satellite: ISS
Catalog Number: 25544
Epoch time: 15260
09173331 = yrday
fracday
Element set: 914
Inclination: 51
6454 deg
RA of node: 345
1779 deg
Eccentricity:
0006299
Arg of perigee: 286
9849 deg
Mean anomaly: 73
0613 deg
Mean motion: 15
53767869 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 234
Checksum: 338
Coasting Arc #16 (Orbit 248)
---------------------------------------
Vector Time (GMT): 2015/261/01:14:33
320
Vector Time (MET): N/A
Weight (LBS) : 926688
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5025455
70 A = 6787971
20 meter
Y = -3876076
58 meter E =
0006528
Z = -2395407
37 I = 51
53542
XDOT = 4714
546443 Wp = 342
19867
YDOT = 2802
084326 meter/sec RA = 339
80555 deg
ZDOT = 5358
989525 TA = 350
99446
MA = 351
00616
Ha = 220
180 n
mi
Hp = 217
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16487715
56 X = 5080061
52
Y = -12716786
67 feet Y = -3819573
58 meter
Z = -7858948
05 Z = -2370861
38
XDOT = 15467
672056 XDOT = 4656
830266
YDOT = 9193
190046 feet/sec YDOT = 2854
483407 meter/sec
ZDOT = 17581
986629 ZDOT = 5381
751556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12842120
53 X = 3914278
34
Y = -16440949
07 feet Y = -5011201
28 meter
Z = -7752394
86 Z = -2362929
95
XDOT = 15964
527321 XDOT = 4865
987927
YDOT = 4137
029707 feet/sec YDOT = 1260
966655 meter/sec
ZDOT = 17679
552048 ZDOT = 5388
727464
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 15261
05648820
00016717 00000-0 10270-3 0 9151
2 25544 51
6456 340
3705 0006438 290
7632 69
2831 15
53780811 2494
Satellite: ISS
Catalog Number: 25544
Epoch time: 15261
05648820 = yrday
fracday
Element set: 915
Inclination: 51
6456 deg
RA of node: 340
3705 deg
Eccentricity:
0006438
Arg of perigee: 290
7632 deg
Mean anomaly: 69
2831 deg
Mean motion: 15
53780811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 249
Checksum: 309
Coasting Arc #17 (Orbit 264)
---------------------------------------
Vector Time (GMT): 2015/262/01:14:33
320
Vector Time (MET): N/A
Weight (LBS) : 926688
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5765907
60 A = 6790118
55 meter
Y = 3471653
23 meter E =
0007330
Z = 866993
56 I = 51
51263
XDOT = -3137
419481 Wp = 136
50090
YDOT = -3726
208601 meter/sec RA = 334
82639 deg
ZDOT = -5919
994590 TA = 34
10507
MA = 34
05799
Ha = 220
288 n
mi
Hp = 217
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18917019
68 X = -5808511
50
Y = 11389938
41 feet Y = 3406936
93 meter
Z = 2844467
07 Z = 838879
82
XDOT = -10293
371002 XDOT = -3066
761559
YDOT = -12225
093835 feet/sec YDOT = -3760
898833 meter/sec
ZDOT = -19422
554430 ZDOT = -5935
063690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15221410
14 X = -4639485
81
Y = 16017844
09 feet Y = 4882238
88 meter
Z = 2722621
49 Z = 829855
03
XDOT = -11887
911676 XDOT = -3623
435479
YDOT = -7970
213426 feet/sec YDOT = -2429
321052 meter/sec
ZDOT = -19486
779168 ZDOT = -5939
570291
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 15262
08555166
00016717 00000-0 10270-3 0 9166
2 25544 51
6453 335
2434 0006324 293
6201 66
4287 15
53756283 2659
Satellite: ISS
Catalog Number: 25544
Epoch time: 15262
08555166 = yrday
fracday
Element set: 916
Inclination: 51
6453 deg
RA of node: 335
2434 deg
Eccentricity:
0006324
Arg of perigee: 293
6201 deg
Mean anomaly: 66
4287 deg
Mean motion: 15
53756283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 265
Checksum: 309
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