[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 30th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 107 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 3 032 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 2325)
---------------------------------------
Vector Time (GMT): 2016/029/12:23:33
678
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1965126
28 A = 6776852
16 meter
Y = 3711110
42 meter E =
0008425
Z = 5312074
09 I = 51
82883
XDOT = -6526
671002 Wp = 68
13986
YDOT = -4019
669508 meter/sec RA = 33
95768 deg
ZDOT = 396
324483 TA = 18
10924
MA = 18
07925
Ha = 223
020 n
mi
Hp = 212
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6447264
69 X = -2032282
18
Y = 12175559
11 feet Y = 3688759
83 meter
Z = 17428064
61 Z = 5302364
85
XDOT = -21412
962604 XDOT = -6483
162138
YDOT = -13187
892086 feet/sec YDOT = -4092
411776 meter/sec
ZDOT = 1300
277176 ZDOT = 364
725870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13364114
42 X = -4073382
07
Y = 3564283
52 feet Y = 1086393
62 meter
Z = 17385201
37 Z = 5299009
38
XDOT = -4808
141733 XDOT = -1465
521600
YDOT = -23664
589079 feet/sec YDOT = -7212
966751 meter/sec
ZDOT = 1164
044116 ZDOT = 354
800647
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 16029
56522138
00016717 00000-0 10270-3 0 9007
2 25544 51
6395 34
3188 0006563 54
8698 305
3069 15
54310511 23263
Satellite: ISS
Catalog Number: 25544
Epoch time: 16029
56522138 = yrday
fracday
Element set: 900
Inclination: 51
6395 deg
RA of node: 34
3188 deg
Eccentricity:
0006563
Arg of perigee: 54
8698 deg
Mean anomaly: 305
3069 deg
Mean motion: 15
54310511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2326
Checksum: 304
Coasting Arc #2 (Orbit 2340)
---------------------------------------
Vector Time (GMT): 2016/030/12:23:33
678
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3537433
77 A = 6777734
00 meter
Y = -2668396
36 meter E =
0018755
Z = -5144723
32 I = 51
80467
XDOT = 5846
172556 Wp = 87
70399
YDOT = 4675
628268 meter/sec RA = 28
96836 deg
ZDOT = 1600
415334 TA = 197
69073
MA = 197
75612
Ha = 222
989 n
mi
Hp = 212
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11605753
84 X = 3592000
08
Y = -8754581
22 feet Y = -2628533
56 meter
Z = -16879013
52 Z = -5127406
91
XDOT = 19180
356154 XDOT = 5785
679992
YDOT = 15339
987756 feet/sec YDOT = 4740
665880 meter/sec
ZDOT = 5250
706476 ZDOT = 1628
667105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14444942
36 X = 4402818
43
Y = 2286417
17 feet Y = 696899
95 meter
Z = -16803370
17 Z = -5121667
23
XDOT = 2528
727080 XDOT = 770
756014
YDOT = 23366
543043 feet/sec YDOT = 7122
122319 meter/sec
ZDOT = 5372
279687 ZDOT = 1637
470849
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 16030
52963178
00016717 00000-0 10270-3 0 9019
2 25544 51
6396 29
5098 0006583 57
8809 302
2982 15
54303723 23413
Satellite: ISS
Catalog Number: 25544
Epoch time: 16030
52963178 = yrday
fracday
Element set: 901
Inclination: 51
6396 deg
RA of node: 29
5098 deg
Eccentricity:
0006583
Arg of perigee: 57
8809 deg
Mean anomaly: 302
2982 deg
Mean motion: 15
54303723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2341
Checksum: 316
Coasting Arc #3 (Orbit 2356)
---------------------------------------
Vector Time (GMT): 2016/031/12:23:33
678
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4940098
39 A = 6780704
70 meter
Y = 1563449
33 meter E =
0016155
Z = 4364667
33 I = 51
78618
XDOT = -4652
101032 Wp = 66
84324
YDOT = -5037
662657 meter/sec RA = 23
98166 deg
ZDOT = -3444
588879 TA = 58
07699
MA = 57
91997
Ha = 223
038 n
mi
Hp = 212
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16207671
88 X = -4978415
56
Y = 5129426
93 feet Y = 1507991
79 meter
Z = 14319774
72 Z = 4340576
69
XDOT = -15262
798662 XDOT = -4578
690734
YDOT = -16527
764624 feet/sec YDOT = -5089
275201 meter/sec
ZDOT = -11301
144616 ZDOT = -3467
008898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15182535
24 X = -4627636
74
Y = -7840951
56 feet Y = -2389922
04 meter
Z = 14214981
48 Z = 4332726
36
XDOT = 291
587113 XDOT = 88
875752
YDOT = -21324
793315 feet/sec YDOT = -6499
797002 meter/sec
ZDOT = -11397
342531 ZDOT = -3473
910004
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 16031
55832576
00016717 00000-0 10270-3 0 9021
2 25544 51
6392 24
3791 0006567 60
7941 299
3868 15
54352216 23571
Satellite: ISS
Catalog Number: 25544
Epoch time: 16031
55832576 = yrday
fracday
Element set: 902
Inclination: 51
6392 deg
RA of node: 24
3791 deg
Eccentricity:
0006567
Arg of perigee: 60
7941 deg
Mean anomaly: 299
3868 deg
Mean motion: 15
54352216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2357
Checksum: 326
Coasting Arc #4 (Orbit 2371)
---------------------------------------
Vector Time (GMT): 2016/032/12:23:33
678
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5995459
79 A = 6784641
47 meter
Y = -545179
30 meter E =
0011183
Z = -3132638
61 I = 51
76966
XDOT = 3000
681148 Wp = 68
02323
YDOT = 5094
704536 meter/sec RA = 19
00441 deg
ZDOT = 4874
286020 TA = 255
98777
MA = 256
11213
Ha = 223
070 n
mi
Hp = 212
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19670143
65 X = 6016327
38
Y = -1788645
99 feet Y = -478017
51 meter
Z = -10277685
72 Z = -3103463
75
XDOT = 9844
754423 XDOT = 2919
810932
YDOT = 16714
909895 feet/sec YDOT = 5127
808106 meter/sec
ZDOT = 15991
752033 ZDOT = 4888
665873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15482784
33 X = 4719152
66
Y = 12368671
81 feet Y = 3769971
17 meter
Z = -10151057
90 Z = -3094042
45
XDOT = -3637
351468 XDOT = -1108
664728
YDOT = 17678
889298 feet/sec YDOT = 5388
525458 meter/sec
ZDOT = 16053
063378 ZDOT = 4892
973718
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 16032
52271758
00016717 00000-0 10270-3 0 9039
2 25544 51
6392 19
5700 0006705 64
6189 295
5658 15
54343396 23729
Satellite: ISS
Catalog Number: 25544
Epoch time: 16032
52271758 = yrday
fracday
Element set: 903
Inclination: 51
6392 deg
RA of node: 19
5700 deg
Eccentricity:
0006705
Arg of perigee: 64
6189 deg
Mean anomaly: 295
5658 deg
Mean motion: 15
54343396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2372
Checksum: 322
Coasting Arc #5 (Orbit 2387)
---------------------------------------
Vector Time (GMT): 2016/033/12:23:33
678
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6601462
73 A = 6787689
97 meter
Y = -440110
95 meter E =
0018714
Z = 1489113
23 I = 51
74992
XDOT = -987
250144 Wp = 102
17777
YDOT = -4943
869815 meter/sec RA = 14
03454 deg
ZDOT = -5780
357955 TA = 61
58543
MA = 61
39694
Ha = 222
964 n
mi
Hp = 212
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21658342
28 X = -6603284
06
Y = -1443933
56 feet Y = -513943
04 meter
Z = 4885542
09 Z = 1457040
88
XDOT = -3239
009660 XDOT = -903
814992
YDOT = -16220
045325 feet/sec YDOT = -4954
443483 meter/sec
ZDOT = -18964
428986 ZDOT = -5784
950987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14928919
32 X = -4550334
61
Y = -15799835
81 feet Y = -4815789
96 meter
Z = 4746557
92 Z = 1446750
86
XDOT = 7586
298845 XDOT = 2312
303888
YDOT = -12929
339143 feet/sec YDOT = -3940
862571 meter/sec
ZDOT = -18983
326836 ZDOT = -5786
118020
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 16033
55139111
00016717 00000-0 10270-3 0 9040
2 25544 51
6394 14
4388 0006647 67
1013 293
0841 15
54388390 23883
Satellite: ISS
Catalog Number: 25544
Epoch time: 16033
55139111 = yrday
fracday
Element set: 904
Inclination: 51
6394 deg
RA of node: 14
4388 deg
Eccentricity:
0006647
Arg of perigee: 67
1013 deg
Mean anomaly: 293
0841 deg
Mean motion: 15
54388390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2388
Checksum: 307
Coasting Arc #6 (Orbit 2403)
---------------------------------------
Vector Time (GMT): 2016/034/12:23:33
678
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6653791
44 A = 6788452
33 meter
Y = 1277890
92 meter E =
0018923
Z = 269994
43 I = 51
72136
XDOT = -1143
819537 Wp = 56
26458
YDOT = 4623
344017 meter/sec RA = 9
06947 deg
ZDOT = 6013
889673 TA = 306
64287
MA = 306
81671
Ha = 222
940 n
mi
Hp = 211
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21830024
42 X = 6637695
73
Y = 4192555
50 feet Y = 1352208
03 meter
Z = 885808
51 Z = 302277
40
XDOT = -3752
688769 XDOT = -1224
646438
YDOT = 15168
451499 feet/sec YDOT = 4610
101173 meter/sec
ZDOT = 19730
609162 ZDOT = 6008
137008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13465325
27 X = 4104231
14
Y = 17678955
07 feet Y = 5388545
50 meter
Z = 1025527
98 Z = 312580
93
XDOT = -11718
806997 XDOT = -3571
892373
YDOT = 7734
656540 feet/sec YDOT = 2357
523313 meter/sec
ZDOT = 19704
709896 ZDOT = 6005
995576
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 16034
58005338
00016717 00000-0 10270-3 0 9058
2 25544 51
6392 9
3088 0006632 72
8054 287
3824 15
54417444 24042
Satellite: ISS
Catalog Number: 25544
Epoch time: 16034
58005338 = yrday
fracday
Element set: 905
Inclination: 51
6392 deg
RA of node: 9
3088 deg
Eccentricity:
0006632
Arg of perigee: 72
8054 deg
Mean anomaly: 287
3824 deg
Mean motion: 15
54417444 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2404
Checksum: 304
Coasting Arc #7 (Orbit 2418)
---------------------------------------
Vector Time (GMT): 2016/035/12:23:33
678
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6125998
96 A = 6786625
09 meter
Y = -2072201
39 meter E =
0011046
Z = -2061403
15 I = 51
68447
XDOT = 3264
054132 Wp = 105
37874
YDOT = -4159
754033 meter/sec RA = 4
09999 deg
ZDOT = -5546
089252 TA = 97
39387
MA = 97
26833
Ha = 222
915 n
mi
Hp = 211
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20098421
79 X = -6092358
54
Y = -6798560
99 feet Y = -2140518
27 meter
Z = -6763133
69 Z = -2091079
57
XDOT = 10708
839016 XDOT = 3337
267052
YDOT = -13647
486985 feet/sec YDOT = -4122
843854 meter/sec
ZDOT = -18195
830879 ZDOT = -5530
055711
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10724278
90 X = -3268760
21
Y = -18259398
94 feet Y = -5565464
80 meter
Z = -6891383
00 Z = -2100493
54
XDOT = 15784
472615 XDOT = 4811
107253
YDOT = -2463
444671 feet/sec YDOT = -750
857936 meter/sec
ZDOT = -18125
449385 ZDOT = -5524
636973
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 16035
54441582
00016717 00000-0 10270-3 0 9061
2 25544 51
6400 4
4983 0006636 74
1503 286
0381 15
54413077 24198
Satellite: ISS
Catalog Number: 25544
Epoch time: 16035
54441582 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 4
4983 deg
Eccentricity:
0006636
Arg of perigee: 74
1503 deg
Mean anomaly: 286
0381 deg
Mean motion: 15
54413077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2419
Checksum: 293
Coasting Arc #8 (Orbit 2434)
---------------------------------------
Vector Time (GMT): 2016/036/12:23:33
678
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5067572
33 A = 6782897
71 meter
Y = 2742000
52 meter E =
0018372
Z = 3562398
85 I = 51
64077
XDOT = -5100
449808 Wp = 87
81416
YDOT = 3607
882067 meter/sec RA = 359
12124 deg
ZDOT = 4459
299735 TA = 314
30295
MA = 314
45347
Ha = 222
769 n
mi
Hp = 211
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16625893
48 X = 5019229
69
Y = 8996064
69 feet Y = 2798399
17 meter
Z = 11687660
27 Z = 3586897
98
XDOT = -16733
759213 XDOT = -5162
075922
YDOT = 11836
883421 feet/sec YDOT = 3550
500888 meter/sec
ZDOT = 14630
248473 ZDOT = 4434
373800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6938296
14 X = 2114792
66
Y = 17513667
61 feet Y = 5338165
89 meter
Z = 11793320
56 Z = 3594604
11
XDOT = -19227
074861 XDOT = -5860
412418
YDOT = -2203
288265 feet/sec YDOT = -671
562263 meter/sec
ZDOT = 14521
426884 ZDOT = 4426
130914
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 16036
57305633
00016717 00000-0 10270-3 0 9072
2 25544 51
6404 359
3684 0006506 79
0870 281
1014 15
54453419 24350
Satellite: ISS
Catalog Number: 25544
Epoch time: 16036
57305633 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 359
3684 deg
Eccentricity:
0006506
Arg of perigee: 79
0870 deg
Mean anomaly: 281
1014 deg
Mean motion: 15
54453419 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2435
Checksum: 306
Coasting Arc #9 (Orbit 2449)
---------------------------------------
Vector Time (GMT): 2016/037/12:23:33
678
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3554046
33 A = 6778994
59 meter
Y = -3378008
97 meter E =
0017396
Z = -4697758
18 I = 51
59600
XDOT = 6492
418951 Wp = 74
25524
YDOT = -2914
917536 meter/sec RA = 354
12718 deg
ZDOT = -2819
854465 TA = 167
72758
MA = 167
68515
Ha = 222
898 n
mi
Hp = 211
676
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11660256
98 X = -3493189
27
Y = -11082706
58 feet Y = -3417412
45 meter
Z = -15412592
46 Z = -4714874
62
XDOT = 21300
587110 XDOT = 6538
229091
YDOT = -9563
377744 feet/sec YDOT = -2842
058898 meter/sec
ZDOT = -9251
491028 ZDOT = -2788
205313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2044273
05 X = -623094
43
Y = -15885127
86 feet Y = -4841786
97 meter
Z = -15486111
36 Z = -4720166
74
XDOT = 21473
303588 XDOT = 6545
062934
YDOT = 6108
273509 feet/sec YDOT = 1861
801766 meter/sec
ZDOT = -9113
666378 ZDOT = -2777
845512
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 16037
53739887
00016717 00000-0 10270-3 0 9082
2 25544 51
6407 354
5576 0006593 81
2503 278
9397 15
54443910 24504
Satellite: ISS
Catalog Number: 25544
Epoch time: 16037
53739887 = yrday
fracday
Element set: 908
Inclination: 51
6407 deg
RA of node: 354
5576 deg
Eccentricity:
0006593
Arg of perigee: 81
2503 deg
Mean anomaly: 278
9397 deg
Mean motion: 15
54443910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2450
Checksum: 340
Coasting Arc #10 (Orbit 2465)
---------------------------------------
Vector Time (GMT): 2016/038/12:23:33
678
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1752518
49 A = 6776526
45 meter
Y = 3904117
04 meter E =
0009316
Z = 5246422
53 I = 51
55699
XDOT = -7327
912322 Wp = 95
85065
YDOT = 2113
559416 meter/sec RA = 349
12302 deg
ZDOT = 872
755400 TA = 345
78971
MA = 345
81589
Ha = 222
743 n
mi
Hp = 211
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5749732
60 X = 1683247
21
Y = 12808782
95 feet Y = 3923327
70 meter
Z = 17212672
36 Z = 5254767
26
XDOT = -24041
707092 XDOT = -7355
241409
YDOT = 6934
250051 feet/sec YDOT = 2031
461063 meter/sec
ZDOT = 2863
370734 ZDOT = 837
092673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3416598
78 X = -1041379
31
Y = 13573206
37 feet Y = 4137113
30 meter
Z = 17248053
71 Z = 5257206
77
XDOT = -22257
016772 XDOT = -6783
938712
YDOT = -9053
445954 feet/sec YDOT = -2759
490327 meter/sec
ZDOT = 2708
315608 ZDOT = 825
494597
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 16038
56601793
00016717 00000-0 10270-3 0 9091
2 25544 51
6414 349
4278 0006440 84
9499 275
2389 15
54485567 24661
Satellite: ISS
Catalog Number: 25544
Epoch time: 16038
56601793 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 349
4278 deg
Eccentricity:
0006440
Arg of perigee: 84
9499 deg
Mean anomaly: 275
2389 deg
Mean motion: 15
54485567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2466
Checksum: 356
Coasting Arc #11 (Orbit 2480)
---------------------------------------
Vector Time (GMT): 2016/039/12:23:33
678
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 160496
17 A = 6776883
77 meter
Y = -4351217
66 meter E =
0020498
Z = -5211019
19 I = 51
52681
XDOT = 7473
565659 Wp = 95
38436
YDOT = -1145
197952 meter/sec RA = 344
11172 deg
ZDOT = 1188
582315 TA = 186
04433
MA = 186
06910
Ha = 222
847 n
mi
Hp = 211
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 526562
24 X = 234452
87
Y = -14275648
47 feet Y = -4349009
63 meter
Z = -17096519
66 Z = -5210059
72
XDOT = 24519
572371 XDOT = 7480
042625
YDOT = -3757
211128 feet/sec YDOT = -1061
587312 meter/sec
ZDOT = 3899
548278 ZDOT = 1224
901884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9081603
34 X = 2768072
70
Y = -11034868
99 feet Y = -3363428
07 meter
Z = -17091475
62 Z = -5209481
77
XDOT = 21038
065263 XDOT = 6412
402292
YDOT = 11041
005771 feet/sec YDOT = 3365
298559 meter/sec
ZDOT = 4057
245313 ZDOT = 1236
648372
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 16039
53034008
00016717 00000-0 10270-3 0 9100
2 25544 51
6416 344
6172 0006506 88
0094 272
1804 15
54466251 24816
Satellite: ISS
Catalog Number: 25544
Epoch time: 16039
53034008 = yrday
fracday
Element set: 910
Inclination: 51
6416 deg
RA of node: 344
6172 deg
Eccentricity:
0006506
Arg of perigee: 88
0094 deg
Mean anomaly: 272
1804 deg
Mean motion: 15
54466251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2481
Checksum: 290
Coasting Arc #12 (Orbit 2496)
---------------------------------------
Vector Time (GMT): 2016/040/12:23:33
678
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2015795
14 A = 6779640
90 meter
Y = 4619800
67 meter E =
0015092
Z = 4523007
53 I = 51
50606
XDOT = -7010
221630 Wp = 77
48648
YDOT = 14
470725 meter/sec RA = 339
10412 deg
ZDOT = -3127
044132 TA = 43
93879
MA = 43
81889
Ha = 222
878 n
mi
Hp = 211
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6613501
12 X = -2089275
36
Y = 15156826
35 feet Y = 4596848
18 meter
Z = 14839263
55 Z = 4513036
75
XDOT = -22999
414795 XDOT = -6994
672974
YDOT = 47
476131 feet/sec YDOT = -63
835506 meter/sec
ZDOT = -10259
331142 ZDOT = -3161
059430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14325029
92 X = -4366269
12
Y = 8340856
87 feet Y = 2542293
18 meter
Z = 14795105
59 Z = 4509548
18
XDOT = -17991
921161 XDOT = -5483
937570
YDOT = -12370
404411 feet/sec YDOT = -3770
499264 meter/sec
ZDOT = -10406
800486 ZDOT = -3171
992788
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 16040
55893884
00016717 00000-0 10270-3 0 9110
2 25544 51
6420 339
4872 0006543 92
0076 268
1826 15
54486296 24973
Satellite: ISS
Catalog Number: 25544
Epoch time: 16040
55893884 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 339
4872 deg
Eccentricity:
0006543
Arg of perigee: 92
0076 deg
Mean anomaly: 268
1826 deg
Mean motion: 15
54486296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2497
Checksum: 337
Coasting Arc #13 (Orbit 2511)
---------------------------------------
Vector Time (GMT): 2016/041/12:23:33
678
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3596120
21 A = 6783589
18 meter
Y = -4694463
65 meter E =
0011132
Z = -3333479
13 I = 51
48985
XDOT = 5942
705179 Wp = 90
59216
YDOT = 1245
730451 meter/sec RA = 334
10416 deg
ZDOT = 4670
006295 TA = 230
53826
MA = 230
63680
Ha = 222
793 n
mi
Hp = 211
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11798294
65 X = 3664539
85
Y = -15401783
62 feet Y = -4653867
18 meter
Z = -10936611
31 Z = -3315843
87
XDOT = 19497
064237 XDOT = 5905
649054
YDOT = 4087
042161 feet/sec YDOT = 1311
978936 meter/sec
ZDOT = 15321
542962 ZDOT = 4698
783728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18549574
11 X = 5653910
19
Y = -5832216
60 feet Y = -1777659
62 meter
Z = -10859222
44 Z = -3309891
00
XDOT = 13137
250400 XDOT = 4004
233922
YDOT = 13106
467447 feet/sec YDOT = 3994
851278 meter/sec
ZDOT = 15446
044529 ZDOT = 4707
954373
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
52323958
00016717 00000-0 10270-3 0 9129
2 25544 51
6420 334
6772 0006489 95
2884 264
9010 15
54505077 25126
Satellite: ISS
Catalog Number: 25544
Epoch time: 16041
52323958 = yrday
fracday
Element set: 912
Inclination: 51
6420 deg
RA of node: 334
6772 deg
Eccentricity:
0006489
Arg of perigee: 95
2884 deg
Mean anomaly: 264
9010 deg
Mean motion: 15
54505077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2512
Checksum: 309
Coasting Arc #14 (Orbit 2527)
---------------------------------------
Vector Time (GMT): 2016/042/12:23:33
678
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4822366
69 A = 6787042
30 meter
Y = 4453317
24 meter E =
0020270
Z = 1690912
98 I = 51
47346
XDOT = -4433
811999 Wp = 110
33791
YDOT = -2623
664724 meter/sec RA = 329
11375 deg
ZDOT = -5686
602199 TA = 51
06760
MA = 50
88709
Ha = 222
780 n
mi
Hp = 211
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15821413
03 X = -4880019
96
Y = 14610620
88 feet Y = 4399068
15 meter
Z = 5547614
76 Z = 1667347
09
XDOT = -14546
627294 XDOT = -4376
521427
YDOT = -8607
823897 feet/sec YDOT = -2672
926766 meter/sec
ZDOT = -18656
831362 ZDOT = -5708
000763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21313132
61 X = -6496242
82
Y = 3266547
79 feet Y = 995643
77 meter
Z = 5444577
67 Z = 1659507
27
XDOT = -6922
052637 XDOT = -2109
841644
YDOT = -13643
835581 feet/sec YDOT = -4158
641085 meter/sec
ZDOT = -18749
066867 ZDOT = -5714
715581
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
55181671
00016717 00000-0 10270-3 0 9138
2 25544 51
6423 329
5462 0006528 99
2165 260
9727 15
54515343 25283
Satellite: ISS
Catalog Number: 25544
Epoch time: 16042
55181671 = yrday
fracday
Element set: 913
Inclination: 51
6423 deg
RA of node: 329
5462 deg
Eccentricity:
0006528
Arg of perigee: 99
2165 deg
Mean anomaly: 260
9727 deg
Mean motion: 15
54515343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2528
Checksum: 315
Coasting Arc #15 (Orbit 2543)
---------------------------------------
Vector Time (GMT): 2016/043/12:23:33
678
Vector Time (MET): N/A
Weight (LBS) : 922504
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5543663
81 A = 6788161
04 meter
Y = -3907272
36 meter E =
0016918
Z = 103200
09 I = 51
45006
XDOT = 2669
494093 Wp = 64
72033
YDOT = 3966
025492 meter/sec RA = 324
12840 deg
ZDOT = 5996
088394 TA = 296
39438
MA = 296
56794
Ha = 222
721 n
mi
Hp = 211
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18187873
40 X = 5586442
59
Y = -12819135
04 feet Y = -3845040
24 meter
Z = 338582
96 Z = 130233
72
XDOT = 8758
182720 XDOT = 2595
820599
YDOT = 13011
894658 feet/sec YDOT = 3995
466182 meter/sec
ZDOT = 19672
206018 ZDOT = 6008
876630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22232674
19 X = 6776519
09
Y = -862193
69 feet Y = -262796
64 meter
Z = 456531
27 Z = 139150
73
XDOT = 99
483308 XDOT = 30
322512
YDOT = 13994
010286 feet/sec YDOT = 4265
374335 meter/sec
ZDOT = 19726
852246 ZDOT = 6012
744564
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
58038268
00016717 00000-0 10270-3 0 9146
2 25544 51
6419 324
4155 0006458 102
2299 257
9577 15
54527973 25445
Satellite: ISS
Catalog Number: 25544
Epoch time: 16043
58038268 = yrday
fracday
Element set: 914
Inclination: 51
6419 deg
RA of node: 324
4155 deg
Eccentricity:
0006458
Arg of perigee: 102
2299 deg
Mean anomaly: 257
9577 deg
Mean motion: 15
54527973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2544
Checksum: 335
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