[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 26th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 124 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 730 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 3410)
---------------------------------------
Vector Time (GMT): 2015/207/04:36:20
318
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4578897
23 A = 6776637
97 meter
Y = -785809
92 meter E =
0012291
Z = -4944795
93 I = 51
28454
XDOT = -1055
087847 Wp = 103
41808
YDOT = -7280
274372 meter/sec RA = 248
29686 deg
ZDOT = 2135
661026 TA = 187
50851
MA = 187
52693
Ha = 219
765 n
mi
Hp = 213
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15022628
69 X = -4545749
98
Y = -2578116
54 feet Y = -836828
51 meter
Z = -16223083
74 Z = -4966958
72
XDOT = -3461
574300 XDOT = -983
973827
YDOT = -23885
414606 feet/sec YDOT = -7291
675569 meter/sec
ZDOT = 7006
761897 ZDOT = 2130
707915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15131116
67 X = -4611964
36
Y = 527530
15 feet Y = 160791
19 meter
Z = -16318257
39 Z = -4973804
85
XDOT = -8280
612797 XDOT = -2523
930781
YDOT = -21558
661947 feet/sec YDOT = -6571
080161 meter/sec
ZDOT = 6986
777351 ZDOT = 2129
569737
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 15207
20427758
00016717 00000-0 10270-3 0 9007
2 25544 51
6410 249
1955 0000572 350
2801 9
8341 15
54890627 34118
Satellite: ISS
Catalog Number: 25544
Epoch time: 15207
20427758 = yrday
fracday
Element set: 900
Inclination: 51
6410 deg
RA of node: 249
1955 deg
Eccentricity:
0000572
Arg of perigee: 350
2801 deg
Mean anomaly: 9
8341 deg
Mean motion: 15
54890627 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3411
Checksum: 289
Coasting Arc #2 (Orbit 3426)
---------------------------------------
Vector Time (GMT): 2015/208/04:36:20
318
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4848573
85 A = 6780556
33 meter
Y = 2678120
09 meter E =
0011129
Z = 3903361
37 I = 51
30953
XDOT = -339
092573 Wp = 77
41422
YDOT = 6515
340438 meter/sec RA = 243
27330 deg
ZDOT = -4036
872202 TA = 55
02408
MA = 54
91964
Ha = 219
696 n
mi
Hp = 213
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15907394
53 X = 4799305
20
Y = 8786483
23 feet Y = 2732064
25 meter
Z = 12806303
71 Z = 3926795
15
XDOT = -1112
508443 XDOT = -392
314024
YDOT = 21375
788837 feet/sec YDOT = 6511
251211 meter/sec
ZDOT = -13244
331373 ZDOT = -4038
648207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17378400
97 X = 5296936
61
Y = 5065511
42 feet Y = 1543967
88 meter
Z = 12906613
70 Z = 3933935
86
XDOT = 4099
556120 XDOT = 1249
544706
YDOT = 19804
396766 feet/sec YDOT = 6036
380134 meter/sec
ZDOT = -13253
140030 ZDOT = -4039
557081
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 15208
23259990
00016717 00000-0 10270-3 0 9013
2 25544 51
6403 244
0623 0000574 353
5339 6
5807 15
54885574 34273
Satellite: ISS
Catalog Number: 25544
Epoch time: 15208
23259990 = yrday
fracday
Element set: 901
Inclination: 51
6403 deg
RA of node: 244
0623 deg
Eccentricity:
0000574
Arg of perigee: 353
5339 deg
Mean anomaly: 6
5807 deg
Mean motion: 15
54885574 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3427
Checksum: 310
Coasting Arc #3 (Orbit 3441)
---------------------------------------
Vector Time (GMT): 2015/209/04:36:20
318
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4794803
37 A = 6784629
38 meter
Y = -4185632
76 meter E =
0006084
Z = -2345409
70 I = 51
33978
XDOT = 1869
615185 Wp = 42
17990
YDOT = -5143
287408 meter/sec RA = 238
26528 deg
ZDOT = 5369
167511 TA = 291
53701
MA = 291
60184
Ha = 219
727 n
mi
Hp = 213
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15730982
18 X = -4736249
27
Y = -13732390
93 feet Y = -4238923
80 meter
Z = -7694913
70 Z = -2368559
79
XDOT = 6133
908088 XDOT = 1900
908604
YDOT = -16874
302521 feet/sec YDOT = -5122
205623 meter/sec
ZDOT = 17615
378972 ZDOT = 5378
325213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18501073
92 X = -5639127
33
Y = -9603217
71 feet Y = -2927060
76 meter
Z = -7793749
50 Z = -2375534
85
XDOT = 1129
563409 XDOT = 344
290927
YDOT = -16472
128602 feet/sec YDOT = -5020
704798 meter/sec
ZDOT = 17655
687013 ZDOT = 5381
453402
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 15209
19664260
00016717 00000-0 10270-3 0 9020
2 25544 51
6415 239
2510 0000616 359
8768
2385 15
54920313 34429
Satellite: ISS
Catalog Number: 25544
Epoch time: 15209
19664260 = yrday
fracday
Element set: 902
Inclination: 51
6415 deg
RA of node: 239
2510 deg
Eccentricity:
0000616
Arg of perigee: 359
8768 deg
Mean anomaly:
2385 deg
Mean motion: 15
54920313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3442
Checksum: 293
Coasting Arc #4 (Orbit 3457)
---------------------------------------
Vector Time (GMT): 2015/210/04:36:20
318
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4314935
02 A = 6786878
91 meter
Y = 5213872
87 meter E =
0012448
Z = 425323
84 I = 51
36399
XDOT = -3452
923803 Wp = 128
01045
YDOT = 3353
857015 meter/sec RA = 233
26865 deg
ZDOT = -5971
533477 TA = 47
38397
MA = 47
27906
Ha = 219
727 n
mi
Hp = 213
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14156610
95 X = 4254245
51
Y = 17105882
13 feet Y = 5261785
94 meter
Z = 1395419
43 Z = 446137
66
XDOT = -11328
490167 XDOT = -3461
163788
YDOT = 11003
467897 feet/sec YDOT = 3315
198571 meter/sec
ZDOT = -19591
645267 ZDOT = -5988
326594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18039510
37 X = 5498442
76
Y = 12936062
69 feet Y = 3942911
91 meter
Z = 1484041
78 Z = 452335
93
XDOT = -7086
623969 XDOT = -2160
002986
YDOT = 12177
938288 feet/sec YDOT = 3711
835590 meter/sec
ZDOT = -19664
481448 ZDOT = -5993
733945
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 15210
22494562
00016717 00000-0 10270-3 0 9033
2 25544 51
6405 234
1180 0000686 358
6523 1
4628 15
54942221 34580
Satellite: ISS
Catalog Number: 25544
Epoch time: 15210
22494562 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 234
1180 deg
Eccentricity:
0000686
Arg of perigee: 358
6523 deg
Mean anomaly: 1
4628 deg
Mean motion: 15
54942221 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3458
Checksum: 287
Coasting Arc #5 (Orbit 3473)
---------------------------------------
Vector Time (GMT): 2015/211/04:36:20
318
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3411234
13 A = 6785937
96 meter
Y = -5656028
43 meter E =
0014281
Z = 1525194
38 I = 51
38183
XDOT = 4896
618451 Wp = 60
16225
YDOT = -1396
694441 meter/sec RA = 228
27587 deg
ZDOT = 5738
786289 TA = 316
57377
MA = 316
68618
Ha = 219
730 n
mi
Hp = 213
322
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11191713
01 X = -3355142
20
Y = -18556523
73 feet Y = -5693861
57 meter
Z = 5003918
57 Z = 1508759
43
XDOT = 16065
021164 XDOT = 4883
996369
YDOT = -4582
330843 feet/sec YDOT = -1342
008215 meter/sec
ZDOT = 18828
039006 ZDOT = 5762
541896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15838668
70 X = -4827626
22
Y = -14813120
15 feet Y = -4515039
02 meter
Z = 4934192
87 Z = 1503941
99
XDOT = 13022
607699 XDOT = 3969
290827
YDOT = -7581
459166 feet/sec YDOT = -2310
828754 meter/sec
ZDOT = 18930
492686 ZDOT = 5770
014171
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 15211
25323882
00016717 00000-0 10270-3 0 9044
2 25544 51
6416 228
9855 0000625 9
3272 350
7892 15
54966763 34744
Satellite: ISS
Catalog Number: 25544
Epoch time: 15211
25323882 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 228
9855 deg
Eccentricity:
0000625
Arg of perigee: 9
3272 deg
Mean anomaly: 350
7892 deg
Mean motion: 15
54966763 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3474
Checksum: 322
Coasting Arc #6 (Orbit 3488)
---------------------------------------
Vector Time (GMT): 2015/212/04:36:20
318
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2059830
09 A = 6782336
09 meter
Y = 5558587
43 meter E =
0004725
Z = -3299622
88 I = 51
39124
XDOT = -6037
867421 Wp = 87
98999
YDOT = -542
474744 meter/sec RA = 223
27669 deg
ZDOT = -4688
735693 TA = 130
50108
MA = 130
45990
Ha = 219
750 n
mi
Hp = 213
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6757972
72 X = 2013547
50
Y = 18236835
40 feet Y = 5581363
18 meter
Z = -10825534
38 Z = -3289728
98
XDOT = -19809
276315 XDOT = -6008
576984
YDOT = -1779
772782 feet/sec YDOT = -609
830132 meter/sec
ZDOT = -15382
991120 ZDOT = -4717
994710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11788592
30 X = 3593162
93
Y = 15497766
04 feet Y = 4723719
09 meter
Z = -10783918
33 Z = -3286938
31
XDOT = -18258
776389 XDOT = -5565
275043
YDOT = 3110
174025 feet/sec YDOT = 947
981043 meter/sec
ZDOT = -15508
801456 ZDOT = -4727
082684
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 15212
21725591
00016717 00000-0 10270-3 0 9055
2 25544 51
6412 224
1735 0000678 7
6336 352
4827 15
54957543 34894
Satellite: ISS
Catalog Number: 25544
Epoch time: 15212
21725591 = yrday
fracday
Element set: 905
Inclination: 51
6412 deg
RA of node: 224
1735 deg
Eccentricity:
0000678
Arg of perigee: 7
6336 deg
Mean anomaly: 352
4827 deg
Mean motion: 15
54957543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3489
Checksum: 313
Coasting Arc #7 (Orbit 3504)
---------------------------------------
Vector Time (GMT): 2015/213/04:36:20
318
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -390950
20 A = 6777839
57 meter
Y = -4970647
12 meter E =
0008376
Z = 4585751
09 I = 51
40130
XDOT = 6699
926224 Wp = 109
69458
YDOT = 2241
344792 meter/sec RA = 218
26543 deg
ZDOT = 2993
424062 TA = 310
32278
MA = 310
39593
Ha = 219
664 n
mi
Hp = 213
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1282645
00 X = -357613
50
Y = -16307897
36 feet Y = -4974832
70 meter
Z = 15045115
14 Z = 4583932
82
XDOT = 21981
385249 XDOT = 6659
824426
YDOT = 7353
493413 feet/sec YDOT = 2316
043462 meter/sec
ZDOT = 9820
945085 ZDOT = 3025
872898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6276390
15 X = -1913043
72
Y = -15113224
84 feet Y = -4606510
93 meter
Z = 15038136
38 Z = 4583623
97
XDOT = 22014
775635 XDOT = 6710
103614
YDOT = 791
805735 feet/sec YDOT = 241
342388 meter/sec
ZDOT = 9960
208854 ZDOT = 3035
871659
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 15213
24552919
00016717 00000-0 10270-3 0 9062
2 25544 51
6420 219
0405 0000706 8
8716 351
2450 15
55009137 35053
Satellite: ISS
Catalog Number: 25544
Epoch time: 15213
24552919 = yrday
fracday
Element set: 906
Inclination: 51
6420 deg
RA of node: 219
0405 deg
Eccentricity:
0000706
Arg of perigee: 8
8716 deg
Mean anomaly: 351
2450 deg
Mean motion: 15
55009137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3505
Checksum: 279
Coasting Arc #8 (Orbit 3519)
---------------------------------------
Vector Time (GMT): 2015/214/04:36:20
318
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1483124
06 A = 6775108
29 meter
Y = 4035136
67 meter E =
0014749
Z = -5249340
12 I = 51
41787
XDOT = -6714
421401 Wp = 80
39369
YDOT = -3583
515894 meter/sec RA = 213
24427 deg
ZDOT = -857
215889 TA = 181
37259
MA = 181
37665
Ha = 219
723 n
mi
Hp = 213
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4865892
59 X = -1502636
94
Y = 13238637
38 feet Y = 4018442
33 meter
Z = -17222244
50 Z = -5256592
07
XDOT = -22028
941605 XDOT = -6669
686694
YDOT = -11756
941910 feet/sec YDOT = -3658
350831 meter/sec
ZDOT = -2812
388088 ZDOT = -889
723884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -259467
61 X = -79085
73
Y = 14063129
42 feet Y = 4286441
85 meter
Z = -17254135
84 Z = -5259060
60
XDOT = -23593
077870 XDOT = -7191
170135
YDOT = -4058
161081 feet/sec YDOT = -1236
927498 meter/sec
ZDOT = -2951
698873 ZDOT = -899
677817
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 15214
20952855
00016717 00000-0 10270-3 0 9073
2 25544 51
6423 214
2289 0000828 11
7232 348
3940 15
54993315 35201
Satellite: ISS
Catalog Number: 25544
Epoch time: 15214
20952855 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 214
2289 deg
Eccentricity:
0000828
Arg of perigee: 11
7232 deg
Mean anomaly: 348
3940 deg
Mean motion: 15
54993315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3520
Checksum: 298
Coasting Arc #9 (Orbit 3535)
---------------------------------------
Vector Time (GMT): 2015/215/04:36:20
318
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3338188
55 A = 6775348
60 meter
Y = -2866216
91 meter E =
0005144
Z = 5149656
05 I = 51
44688
XDOT = 6044
624951 Wp = 49
42012
YDOT = 4512
396697 meter/sec RA = 208
21990 deg
ZDOT = -1402
605640 TA = 54
12252
MA = 54
07477
Ha = 219
604 n
mi
Hp = 213
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10952062
17 X = 3344976
55
Y = -9403598
77 feet Y = -2828849
08 meter
Z = 16895197
01 Z = 5165888
53
XDOT = 19831
446689 XDOT = 6000
530199
YDOT = 14804
451106 feet/sec YDOT = 4579
745098 meter/sec
ZDOT = -4601
724540 ZDOT = -1373
349737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7041854
96 X = 2146357
39
Y = -12506221
21 feet Y = -3811896
23 meter
Z = 16965545
30 Z = 5171098
21
XDOT = 22775
315394 XDOT = 6941
916132
YDOT = 6732
673773 feet/sec YDOT = 2052
118966 meter/sec
ZDOT = -4476
548360 ZDOT = -1364
451940
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 15215
23778365
00016717 00000-0 10270-3 0 9080
2 25544 51
6429 209
0955 0000906 18
1953 341
9233 15
55026758 35367
Satellite: ISS
Catalog Number: 25544
Epoch time: 15215
23778365 = yrday
fracday
Element set: 908
Inclination: 51
6429 deg
RA of node: 209
0955 deg
Eccentricity:
0000906
Arg of perigee: 18
1953 deg
Mean anomaly: 341
9233 deg
Mean motion: 15
55026758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3536
Checksum: 321
Coasting Arc #10 (Orbit 3550)
---------------------------------------
Vector Time (GMT): 2015/216/04:36:20
318
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4957550
62 A = 6778598
75 meter
Y = 1628635
61 meter E =
0008895
Z = -4335503
86 I = 51
48667
XDOT = -4664
917863 Wp = 105
47613
YDOT = -4996
521735 meter/sec RA = 203
20496 deg
ZDOT = 3460
890333 TA = 199
76625
MA = 199
80074
Ha = 219
685 n
mi
Hp = 212
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16264929
85 X = -4954334
02
Y = 5343292
68 feet Y = 1573214
93 meter
Z = -14224094
05 Z = -4359578
54
XDOT = -15304
848631 XDOT = -4625
510301
YDOT = -16392
787846 feet/sec YDOT = -5048
467506 meter/sec
ZDOT = 11354
627078 ZDOT = 3438
325218
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13245778
78 X = -4037313
37
Y = 10708938
66 feet Y = 3264084
50 meter
Z = -14327998
76 Z = -4367174
02
XDOT = -19393
498345 XDOT = -5911
138295
YDOT = -8940
315941 feet/sec YDOT = -2725
008299 meter/sec
ZDOT = 11258
316951 ZDOT = 3431
535007
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 15216
20176410
00016717 00000-0 10270-3 0 9092
2 25544 51
6432 204
2842 0000850 23
0392 337
0799 15
55039205 35514
Satellite: ISS
Catalog Number: 25544
Epoch time: 15216
20176410 = yrday
fracday
Element set: 909
Inclination: 51
6432 deg
RA of node: 204
2842 deg
Eccentricity:
0000850
Arg of perigee: 23
0392 deg
Mean anomaly: 337
0799 deg
Mean motion: 15
55039205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3551
Checksum: 280
Coasting Arc #11 (Orbit 3566)
---------------------------------------
Vector Time (GMT): 2015/217/04:36:20
318
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6127052
19 A = 6783128
03 meter
Y = -386393
72 meter E =
0013678
Z = 2871086
76 I = 51
53108
XDOT = 2696
892473 Wp = 95
27335
YDOT = 5109
332803 meter/sec RA = 198
20471 deg
ZDOT = -5048
196690 TA = 51
97033
MA = 51
84694
Ha = 219
721 n
mi
Hp = 213
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20101877
27 X = 6116971
06
Y = -1267695
92 feet Y = -317933
32 meter
Z = 9419575
98 Z = 2900825
97
XDOT = 8848
072417 XDOT = 2664
080211
YDOT = 16762
902896 feet/sec YDOT = 5139
307683 meter/sec
ZDOT = -16562
325097 ZDOT = -5035
175635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18158281
92 X = 5534644
33
Y = -8575530
02 feet Y = -2613821
55 meter
Z = 9547670
75 Z = 2910130
05
XDOT = 13883
168667 XDOT = 4231
589810
YDOT = 10948
305171 feet/sec YDOT = 3337
043416 meter/sec
ZDOT = -16507
109704 ZDOT = -5031
367038
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 15217
23000039
00016717 00000-0 10270-3 0 9101
2 25544 51
6430 199
1515 0000918 32
7561 327
3648 15
55025948 35672
Satellite: ISS
Catalog Number: 25544
Epoch time: 15217
23000039 = yrday
fracday
Element set: 910
Inclination: 51
6430 deg
RA of node: 199
1515 deg
Eccentricity:
0000918
Arg of perigee: 32
7561 deg
Mean anomaly: 327
3648 deg
Mean motion: 15
55025948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3567
Checksum: 297
Coasting Arc #12 (Orbit 3581)
---------------------------------------
Vector Time (GMT): 2015/218/04:36:20
318
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6664044
02 A = 6786251
69 meter
Y = -734670
92 meter E =
0010623
Z = -1019314
13 I = 51
57230
XDOT = -356
760404 Wp = 37
34676
YDOT = -4890
043368 meter/sec RA = 193
21912 deg
ZDOT = 5897
428699 TA = 311
59135
MA = 311
68235
Ha = 219
742 n
mi
Hp = 213
085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21863661
47 X = -6650382
06
Y = -2410337
66 feet Y = -809116
25 meter
Z = -3344206
48 Z = -1051653
29
XDOT = -1170
473768 XDOT = -330
699490
YDOT = -16043
449370 feet/sec YDOT = -4893
887153 meter/sec
ZDOT = 19348
519353 ZDOT = 5895
758964
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21085835
10 X = -6426962
54
Y = 6186044
83 feet Y = 1885506
46 meter
Z = -3483323
84 Z = -1061717
11
XDOT = -6920
227009 XDOT = -2109
285192
YDOT = -12768
791798 feet/sec YDOT = -3891
927740 meter/sec
ZDOT = 19342
134541 ZDOT = 5895
482608
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 15218
19396086
00016717 00000-0 10270-3 0 9118
2 25544 51
6434 194
3394 0001078 23
5817 336
5385 15
55021971 35827
Satellite: ISS
Catalog Number: 25544
Epoch time: 15218
19396086 = yrday
fracday
Element set: 911
Inclination: 51
6434 deg
RA of node: 194
3394 deg
Eccentricity:
0001078
Arg of perigee: 23
5817 deg
Mean anomaly: 336
5385 deg
Mean motion: 15
55021971 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3582
Checksum: 319
Coasting Arc #13 (Orbit 3597)
---------------------------------------
Vector Time (GMT): 2015/219/04:36:20
318
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6471143
74 A = 6786209
31 meter
Y = 1755568
77 meter E =
0009572
Z = -1021825
06 I = 51
60245
XDOT = -2123
145266 Wp = 136
22289
YDOT = 4415
988877 meter/sec RA = 188
24158 deg
ZDOT = -5898
558096 TA = 54
86024
MA = 54
77058
Ha = 219
780 n
mi
Hp = 213
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21230786
56 X = 6455995
21
Y = 5759740
07 feet Y = 1827848
66 meter
Z = -3352444
41 Z = -990426
53
XDOT = -6965
699691 XDOT = -2143
715367
YDOT = 14488
152482 feet/sec YDOT = 4392
131513 meter/sec
ZDOT = -19352
224723 ZDOT = -5908
921761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21778155
67 X = 6637981
85
Y = -3243335
87 feet Y = -988568
77 meter
Z = -3217529
40 Z = -980702
96
XDOT = -697
270121 XDOT = -212
527933
YDOT = 14426
212354 feet/sec YDOT = 4397
109525 meter/sec
ZDOT = -19397
577490 ZDOT = -5912
381619
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 15219
22217639
00016717 00000-0 10270-3 0 9120
2 25544 51
6423 189
2067 0000963 34
7616 325
3600 15
55060818 35984
Satellite: ISS
Catalog Number: 25544
Epoch time: 15219
22217639 = yrday
fracday
Element set: 912
Inclination: 51
6423 deg
RA of node: 189
2067 deg
Eccentricity:
0000963
Arg of perigee: 34
7616 deg
Mean anomaly: 325
3600 deg
Mean motion: 15
55060818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3598
Checksum: 308
Coasting Arc #14 (Orbit 3613)
---------------------------------------
Vector Time (GMT): 2015/220/04:36:20
318
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5550703
03 A = 6783073
39 meter
Y = -2604677
08 meter E =
0014070
Z = 2885212
79 I = 51
62415
XDOT = 4394
502167 Wp = 78
27709
YDOT = -3753
515436 meter/sec RA = 183
25998 deg
ZDOT = 5047
758712 TA = 314
61870
MA = 314
73338
Ha = 219
775 n
mi
Hp = 212
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18210967
95 X = -5535179
52
Y = -8545528
47 feet Y = -2666661
95 meter
Z = 9465921
23 Z = 2858286
44
XDOT = 14417
658028 XDOT = 4411
628375
YDOT = -12314
683189 feet/sec YDOT = -3704
277581 meter/sec
ZDOT = 16560
888164 ZDOT = 5069
147673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20169652
13 X = -6147709
97
Y = -156329
53 feet Y = -47649
24 meter
Z = 9350388
72 Z = 2849998
48
XDOT = 7869
736438 XDOT = 2398
695666
YDOT = -15685
194388 feet/sec YDOT = -4780
847250 meter/sec
ZDOT = 16653
619670 ZDOT = 5076
023275
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 15220
25037965
00016717 00000-0 10270-3 0 9138
2 25544 51
6426 184
0732 0000999 35
3667 324
7553 15
55095390 36143
Satellite: ISS
Catalog Number: 25544
Epoch time: 15220
25037965 = yrday
fracday
Element set: 913
Inclination: 51
6426 deg
RA of node: 184
0732 deg
Eccentricity:
0000999
Arg of perigee: 35
3667 deg
Mean anomaly: 324
7553 deg
Mean motion: 15
55095390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3614
Checksum: 315
Coasting Arc #15 (Orbit 3628)
---------------------------------------
Vector Time (GMT): 2015/221/04:36:20
318
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3985592
85 A = 6778575
35 meter
Y = 3334044
30 meter E =
0009542
Z = -4362821
56 I = 51
63981
XDOT = -6196
506689 Wp = 66
69121
YDOT = 2910
395869 meter/sec RA = 178
26780 deg
ZDOT = -3438
909320 TA = 168
39817
MA = 168
37617
Ha = 219
753 n
mi
Hp = 213
010
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13076092
03 X = 3969207
25
Y = 10938465
56 feet Y = 3378522
33 meter
Z = -14313719
03 Z = -4343500
25
XDOT = -20329
746356 XDOT = -6211
886162
YDOT = 9548
542878 feet/sec YDOT = 2841
016574 meter/sec
ZDOT = -11282
510893 ZDOT = -3469
047667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16600701
82 X = 5059893
91
Y = 4172620
01 feet Y = 1271814
58 meter
Z = -14231047
23 Z = -4337623
20
XDOT = -13837
542926 XDOT = -4217
683084
YDOT = 16153
942208 feet/sec YDOT = 4923
721585 meter/sec
ZDOT = -11412
802086 ZDOT = -3478
622076
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 15221
21431193
00016717 00000-0 10270-3 0 9147
2 25544 51
6416 179
2609 0001033 37
5002 322
6223 15
55085609 36297
Satellite: ISS
Catalog Number: 25544
Epoch time: 15221
21431193 = yrday
fracday
Element set: 914
Inclination: 51
6416 deg
RA of node: 179
2609 deg
Eccentricity:
0001033
Arg of perigee: 37
5002 deg
Mean anomaly: 322
6223 deg
Mean motion: 15
55085609 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3629
Checksum: 278
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