[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 4th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1877 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 94 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 554 ET - UTC (sec) : 68 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
217/02:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 212
7
220/05:58:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 212
7
223/08:44:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 212
8
Coasting Arc #1 (Orbit 1233)
---------------------------------------
Vector Time (GMT): 2016/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3291007
18 A = 6777785
57 meter
Y = 3657052
29 meter E =
0012568
Z = -4674066
12 I = 51
61675
XDOT = -6696
909687 Wp = 107
16983
YDOT = -2364
819754 meter/sec RA = 180
79556 deg
ZDOT = 2867
776684 TA = 191
34793
MA = 191
37629
Ha = 220
493 n
mi
Hp = 212
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10797267
64 X = -3308952
61
Y = 11998203
06 feet Y = 3620149
81 meter
Z = -15334862
61 Z = -4690096
15
XDOT = -21971
488474 XDOT = -6683
898043
YDOT = -7758
594994 feet/sec YDOT = -2439
636377 meter/sec
ZDOT = 9408
716154 ZDOT = 2835
277100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16073847
13 X = 4899308
61
Y = 22361
25 feet Y = 6815
71 meter
Z = -15405415
11 Z = -4695570
53
XDOT = 8844
806451 XDOT = 2695
897006
YDOT = 20446
904900 feet/sec YDOT = 6232
216613 meter/sec
ZDOT = 9267
248584 ZDOT = 2824
657368
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 16216
51107684
00016717 00000-0 10270-3 0 9005
2 25544 51
6392 181
9078 0001906 91
5358 268
6014 15
54888267 12340
Satellite: ISS
Catalog Number: 25544
Epoch time: 16216
51107684 = yrday
fracday
Element set: 900
Inclination: 51
6392 deg
RA of node: 181
9078 deg
Eccentricity:
0001906
Arg of perigee: 91
5358 deg
Mean anomaly: 268
6014 deg
Mean motion: 15
54888267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1234
Checksum: 319
Coasting Arc #2 (Orbit 1243)
---------------------------------------
Vector Time (GMT): 2016/217/02:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3191517
41 A = 6777490
30 meter
Y = -3634940
47 meter E =
0009665
Z = 4741529
78 I = 51
63908
XDOT = 6767
221421 Wp = 116
04010
YDOT = -2399
663145 meter/sec RA = 177
83661 deg
ZDOT = 2706
947439 TA = 307
17890
MA = 307
26710
Ha = 220
468 n
mi
Hp = 212
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10470857
65 X = -3173665
17
Y = -11925657
73 feet Y = -3670530
37 meter
Z = 15556200
08 Z = 4726069
88
XDOT = 22202
170018 XDOT = 6780
403231
YDOT = -7872
910580 feet/sec YDOT = -2323
913870 meter/sec
ZDOT = 8881
061151 ZDOT = 2739
852143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7978462
84 X = -2431835
47
Y = -13794245
56 feet Y = -4204486
05 meter
Z = 15489301
25 Z = 4721139
02
XDOT = 22264
068726 XDOT = 6786
088148
YDOT = -2712
031633 feet/sec YDOT = -826
627242 meter/sec
ZDOT = 9025
071671 ZDOT = 2750
841845
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 16217
15377282
00016717 00000-0 10270-3 0 9010
2 25544 51
6429 178
6971 0001879 108
7092 251
4266 15
54941575 12443
Satellite: ISS
Catalog Number: 25544
Epoch time: 16217
15377282 = yrday
fracday
Element set: 901
Inclination: 51
6429 deg
RA of node: 178
6971 deg
Eccentricity:
0001879
Arg of perigee: 108
7092 deg
Mean anomaly: 251
4266 deg
Mean motion: 15
54941575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1244
Checksum: 327
Coasting Arc #3 (Orbit 1258)
---------------------------------------
Vector Time (GMT): 2016/218/02:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1143431
19 A = 6775192
59 meter
Y = 4080714
03 meter E =
0016398
Z = -5300370
79 I = 51
66337
XDOT = -7510
777570 Wp = 88
36990
YDOT = 1386
097233 meter/sec RA = 172
83310 deg
ZDOT = -554
156660 TA = 176
34253
MA = 176
33052
Ha = 220
410 n
mi
Hp = 212
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3751414
65 X = 1123461
00
Y = 13388169
40 feet Y = 4093388
93 meter
Z = -17389667
96 Z = -5294864
96
XDOT = -24641
658694 XDOT = -7523
027249
YDOT = 4547
563100 feet/sec YDOT = 1302
038200 meter/sec
ZDOT = -1818
099278 ZDOT = -590
671130
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1352833
09 X = 412343
52
Y = 13867183
48 feet Y = 4226717
53 meter
Z = -17366283
66 Z = -5293243
26
XDOT = -24034
445914 XDOT = -7325
699115
YDOT = -127
816265 feet/sec YDOT = -38
958397 meter/sec
ZDOT = -1977
720414 ZDOT = -602
809182
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 16218
11781671
00016717 00000-0 10270-3 0 9029
2 25544 51
6429 173
8870 0001839 108
9723 251
1629 15
54913739 12594
Satellite: ISS
Catalog Number: 25544
Epoch time: 16218
11781671 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 173
8870 deg
Eccentricity:
0001839
Arg of perigee: 108
9723 deg
Mean anomaly: 251
1629 deg
Mean motion: 15
54913739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1259
Checksum: 327
Coasting Arc #4 (Orbit 1274)
---------------------------------------
Vector Time (GMT): 2016/219/02:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 990610
81 A = 6775820
94 meter
Y = -4338472
65 meter E =
0006174
Z = 5105140
30 I = 51
69809
XDOT = 7484
620599 Wp = 69
75164
YDOT = -263
231561 meter/sec RA = 167
82801 deg
ZDOT = -1672
302933 TA = 36
39234
MA = 36
35038
Ha = 220
315 n
mi
Hp = 212
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3250035
48 X = 1014252
97
Y = -14233834
15 feet Y = -4327262
66 meter
Z = 16749147
96 Z = 5110009
88
XDOT = 24555
841859 XDOT = 7495
131029
YDOT = -863
620606 feet/sec YDOT = -179
474803 meter/sec
ZDOT = -5486
558180 ZDOT = -1635
919655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5457545
67 X = 1663459
92
Y = -13514591
50 feet Y = -4119247
49 meter
Z = 16771098
18 Z = 5111830
73
XDOT = 23408
302580 XDOT = 7134
850626
YDOT = 2826
289024 feet/sec YDOT = 861
452895 meter/sec
ZDOT = -5327
672804 ZDOT = -1623
874671
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 16219
14612557
00016717 00000-0 10270-3 0 9030
2 25544 51
6431 168
7549 0001826 112
2404 247
8943 15
54952049 12759
Satellite: ISS
Catalog Number: 25544
Epoch time: 16219
14612557 = yrday
fracday
Element set: 903
Inclination: 51
6431 deg
RA of node: 168
7549 deg
Eccentricity:
0001826
Arg of perigee: 112
2404 deg
Mean anomaly: 247
8943 deg
Mean motion: 15
54952049 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1275
Checksum: 313
Coasting Arc #5 (Orbit 1289)
---------------------------------------
Vector Time (GMT): 2016/220/02:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2963247
47 A = 6779295
99 meter
Y = 4404295
64 meter E =
0010015
Z = -4227146
54 I = 51
74109
XDOT = -6657
995367 Wp = 111
60480
YDOT = -966
813135 meter/sec RA = 162
83338 deg
ZDOT = 3663
329600 TA = 195
89756
MA = 195
92902
Ha = 220
329 n
mi
Hp = 212
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9721940
50 X = -2991743
83
Y = 14449788
85 feet Y = 4370999
17 meter
Z = -13868591
01 Z = -4241610
38
XDOT = -21843
816820 XDOT = -6664
483990
YDOT = -3171
959104 feet/sec YDOT = -1041
303461 meter/sec
ZDOT = 12018
797900 ZDOT = 3630
971488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11674584
60 X = -3558413
39
Y = 12854625
43 feet Y = 3918089
83 meter
Z = -13932444
90 Z = -4246609
21
XDOT = -20267
909090 XDOT = -6177
658690
YDOT = -5545
716579 feet/sec YDOT = -1690
334413 meter/sec
ZDOT = 11877
667954 ZDOT = 3620
313192
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 16220
11016195
00016717 00000-0 10270-3 0 9046
2 25544 51
6431 163
9448 0001866 115
7683 244
3663 15
54951851 12903
Satellite: ISS
Catalog Number: 25544
Epoch time: 16220
11016195 = yrday
fracday
Element set: 904
Inclination: 51
6431 deg
RA of node: 163
9448 deg
Eccentricity:
0001866
Arg of perigee: 115
7683 deg
Mean anomaly: 244
3663 deg
Mean motion: 15
54951851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1290
Checksum: 303
Coasting Arc #6 (Orbit 1292)
---------------------------------------
Vector Time (GMT): 2016/220/05:58:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4670113
83 A = 6778825
04 meter
Y = -2149954
72 meter E =
0011514
Z = 4410959
02 I = 51
74241
XDOT = 5247
372798 Wp = 109
08578
YDOT = -4476
338986 meter/sec RA = 162
14554 deg
ZDOT = 3363
009469 TA = 306
93491
MA = 307
04032
Ha = 220
576 n
mi
Hp = 212
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15321895
78 X = -4667151
63
Y = -7053657
21 feet Y = -2202162
36 meter
Z = 14471650
32 Z = 4388280
37
XDOT = 17215
790019 XDOT = 5280
702547
YDOT = -14686
151529 feet/sec YDOT = -4417
472897 meter/sec
ZDOT = 11033
495634 ZDOT = 3388
580602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15903394
51 X = -4847354
65
Y = 5868815
48 feet Y = 1788814
96 meter
Z = 14372970
51 Z = 4380881
41
XDOT = 2229
790161 XDOT = 679
640041
YDOT = -21342
033123 feet/sec YDOT = -6505
051696 meter/sec
ZDOT = 11145
859912 ZDOT = 3397
258101
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 16220
30296886
00016717 00000-0 10270-3 0 9055
2 25544 51
6419 162
9834 0002054 105
6299 254
5080 15
54936239 12930
Satellite: ISS
Catalog Number: 25544
Epoch time: 16220
30296886 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 162
9834 deg
Eccentricity:
0002054
Arg of perigee: 105
6299 deg
Mean anomaly: 254
5080 deg
Mean motion: 15
54936239 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1293
Checksum: 319
Coasting Arc #7 (Orbit 1307)
---------------------------------------
Vector Time (GMT): 2016/221/05:58:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2935841
10 A = 6775620
47 meter
Y = 3214298
73 meter E =
0015674
Z = -5205894
98 I = 51
76304
XDOT = -6496
675345 Wp = 83
77390
YDOT = 3842
868443 meter/sec RA = 157
15096 deg
ZDOT = -1292
737310 TA = 173
82515
MA = 173
80580
Ha = 220
425 n
mi
Hp = 212
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9632024
62 X = 2924967
50
Y = 10545599
49 feet Y = 3247068
32 meter
Z = -17079707
95 Z = -5191660
07
XDOT = -21314
551657 XDOT = -6532
884940
YDOT = 12607
836099 feet/sec YDOT = 3770
015780 meter/sec
ZDOT = -4241
264142 ZDOT = -1324
384213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14351226
67 X = 4374253
89
Y = 360379
94 feet Y = 109843
80 meter
Z = -17018061
29 Z = -5187105
08
XDOT = -5765
139095 XDOT = -1757
214396
YDOT = 23006
151224 feet/sec YDOT = 7012
274893 meter/sec
ZDOT = -4380
071141 ZDOT = -1335
045684
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 16221
26699991
00016717 00000-0 10270-3 0 9066
2 25544 51
6429 158
1727 0001943 109
6557 250
4806 15
54927831 13082
Satellite: ISS
Catalog Number: 25544
Epoch time: 16221
26699991 = yrday
fracday
Element set: 906
Inclination: 51
6429 deg
RA of node: 158
1727 deg
Eccentricity:
0001943
Arg of perigee: 109
6557 deg
Mean anomaly: 250
4806 deg
Mean motion: 15
54927831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1308
Checksum: 332
Coasting Arc #8 (Orbit 1323)
---------------------------------------
Vector Time (GMT): 2016/222/05:58:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -988543
57 A = 6775217
72 meter
Y = -4156053
93 meter E =
0004954
Z = 5254614
76 I = 51
78956
XDOT = 7049
554063 Wp = 78
57775
YDOT = -2879
140740 meter/sec RA = 152
15237 deg
ZDOT = -949
273248 TA = 20
49023
MA = 20
47036
Ha = 220
464 n
mi
Hp = 212
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3243253
19 X = -967520
47
Y = -13635347
53 feet Y = -4166990
82 meter
Z = 17239549
73 Z = 5249863
86
XDOT = 23128
458213 XDOT = 7085
836523
YDOT = -9445
999803 feet/sec YDOT = -2800
105068 meter/sec
ZDOT = -3114
413544 ZDOT = -914
940421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12236264
04 X = -3729613
28
Y = -6885288
83 feet Y = -2098636
04 meter
Z = 17219468
88 Z = 5248494
11
XDOT = 8453
503916 XDOT = 2576
627993
YDOT = -22450
042568 feet/sec YDOT = -6842
772975 meter/sec
ZDOT = -2964
015023 ZDOT = -903
431779
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 16222
29529529
00016717 00000-0 10270-3 0 9070
2 25544 51
6411 153
0408 0002051 111
1878 248
9494 15
54951816 13241
Satellite: ISS
Catalog Number: 25544
Epoch time: 16222
29529529 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 153
0408 deg
Eccentricity:
0002051
Arg of perigee: 111
1878 deg
Mean anomaly: 248
9494 deg
Mean motion: 15
54951816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1324
Checksum: 305
Coasting Arc #9 (Orbit 1338)
---------------------------------------
Vector Time (GMT): 2016/223/05:58:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -936600
21 A = 6778014
13 meter
Y = 4904425
95 meter E =
0012007
Z = -4595615
37 I = 51
82828
XDOT = -6847
239691 Wp = 110
86534
YDOT = 1556
999709 meter/sec RA = 147
15990 deg
ZDOT = 3059
394120 TA = 189
65816
MA = 189
68126
Ha = 220
360 n
mi
Hp = 212
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3072835
34 X = -969049
80
Y = 16090636
32 feet Y = 4893770
76 meter
Z = -15077478
26 Z = -4600243
99
XDOT = -22464
697148 XDOT = -6879
002651
YDOT = 5108
266763 feet/sec YDOT = 1480
251744 meter/sec
ZDOT = 10037
382284 ZDOT = 3026
055049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9919567
47 X = 3023484
16
Y = 13012268
62 feet Y = 3966139
47 meter
Z = -15098486
39 Z = -4602018
65
XDOT = -10400
802584 XDOT = -3170
164628
YDOT = 19397
509342 feet/sec YDOT = 5912
360847 meter/sec
ZDOT = 9891
519622 ZDOT = 3014
935181
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 16223
25931708
00016717 00000-0 10270-3 0 9084
2 25544 51
6425 148
2298 0001837 112
9099 247
2248 15
54935972 13394
Satellite: ISS
Catalog Number: 25544
Epoch time: 16223
25931708 = yrday
fracday
Element set: 908
Inclination: 51
6425 deg
RA of node: 148
2298 deg
Eccentricity:
0001837
Arg of perigee: 112
9099 deg
Mean anomaly: 247
2248 deg
Mean motion: 15
54935972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1339
Checksum: 332
Coasting Arc #10 (Orbit 1340)
---------------------------------------
Vector Time (GMT): 2016/223/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5578860
56 A = 6780733
90 meter
Y = -40676
57 meter E =
0007771
Z = -3861281
41 I = 51
83792
XDOT = -2832
095581 Wp = 84
13999
YDOT = 5778
648576 meter/sec RA = 146
63309 deg
ZDOT = -4159
158636 TA = 142
22914
MA = 142
17457
Ha = 220
389 n
mi
Hp = 212
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18303348
28 X = 5597657
07
Y = -133453
31 feet Y = 21815
03 meter
Z = -12668246
11 Z = -3834135
27
XDOT = -9291
652168 XDOT = -2876
300167
YDOT = 18958
820789 feet/sec YDOT = 5746
730973 meter/sec
ZDOT = -13645
533584 ZDOT = -4173
023578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 54758
19 X = 16690
30
Y = -18385251
74 feet Y = -5603824
73 meter
Z = -12549675
19 Z = -3825141
00
XDOT = 17521
110304 XDOT = 5340
434421
YDOT = 9394
030631 feet/sec YDOT = 2863
300536 meter/sec
ZDOT = -13707
024729 ZDOT = -4177
901138
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 16223
38785389
00016717 00000-0 10270-3 0 9091
2 25544 51
6400 147
5876 0001871 110
9901 249
1452 15
54951359 13417
Satellite: ISS
Catalog Number: 25544
Epoch time: 16223
38785389 = yrday
fracday
Element set: 909
Inclination: 51
6400 deg
RA of node: 147
5876 deg
Eccentricity:
0001871
Arg of perigee: 110
9901 deg
Mean anomaly: 249
1452 deg
Mean motion: 15
54951359 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1341
Checksum: 322
Coasting Arc #11 (Orbit 1356)
---------------------------------------
Vector Time (GMT): 2016/224/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4412470
27 A = 6776626
43 meter
Y = -1447520
05 meter E =
0008338
Z = 4930647
67 I = 51
85072
XDOT = 4461
231449 Wp = 120
72251
YDOT = -5812
274877 meter/sec RA = 141
64998 deg
ZDOT = 2279
030455 TA = 307
04933
MA = 307
12557
Ha = 220
355 n
mi
Hp = 212
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14476608
49 X = -4419906
56
Y = -4749081
53 feet Y = -1496904
81 meter
Z = 16176665
60 Z = 4909195
11
XDOT = 14636
586120 XDOT = 4514
823748
YDOT = -19069
143298 feet/sec YDOT = -5762
086746 meter/sec
ZDOT = 7477
134040 ZDOT = 2300
832015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4646854
36 X = -1416361
21
Y = 14613284
05 feet Y = 4454128
98 meter
Z = 16083194
72 Z = 4902157
75
XDOT = -18103
081915 XDOT = -5517
819368
YDOT = -14117
124677 feet/sec YDOT = -4302
899602 meter/sec
ZDOT = 7573
312148 ZDOT = 2308
345543
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 16224
41613677
00016717 00000-0 10270-3 0 9108
2 25544 51
6397 142
4561 0001668 115
8867 244
2458 15
54983465 13578
Satellite: ISS
Catalog Number: 25544
Epoch time: 16224
41613677 = yrday
fracday
Element set: 910
Inclination: 51
6397 deg
RA of node: 142
4561 deg
Eccentricity:
0001668
Arg of perigee: 115
8867 deg
Mean anomaly: 244
2458 deg
Mean motion: 15
54983465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1357
Checksum: 330
Coasting Arc #12 (Orbit 1371)
---------------------------------------
Vector Time (GMT): 2016/225/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2926636
13 A = 6774946
14 meter
Y = 2999087
89 meter E =
0016399
Z = -5337660
92 I = 51
86952
XDOT = -5535
195241 Wp = 92
43434
YDOT = 5291
485411 meter/sec RA = 136
65745 deg
ZDOT = -62
644955 TA = 176
97475
MA = 176
96482
Ha = 220
264 n
mi
Hp = 212
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9601824
57 X = 2918809
89
Y = 9839527
19 feet Y = 3031771
77 meter
Z = -17512010
91 Z = -5323463
17
XDOT = -18160
089373 XDOT = -5593
650283
YDOT = 17360
516440 feet/sec YDOT = 5229
260317 meter/sec
ZDOT = -205
528066 ZDOT = -89
675248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9600926
37 X = 2926362
36
Y = -9949111
90 feet Y = -3032489
31 meter
Z = -17450479
70 Z = -5318906
21
XDOT = 17067
611034 XDOT = 5202
207843
YDOT = 17034
558999 feet/sec YDOT = 5192
133583 meter/sec
ZDOT = -324
480916 ZDOT = -98
901783
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 16225
38014903
00016717 00000-0 10270-3 0 9113
2 25544 51
6397 137
6441 0001709 117
8422 242
2905 15
54958617 13729
Satellite: ISS
Catalog Number: 25544
Epoch time: 16225
38014903 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 137
6441 deg
Eccentricity:
0001709
Arg of perigee: 117
8422 deg
Mean anomaly: 242
2905 deg
Mean motion: 15
54958617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1372
Checksum: 306
Coasting Arc #13 (Orbit 1387)
---------------------------------------
Vector Time (GMT): 2016/226/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1297860
33 A = 6776365
27 meter
Y = -4409113
43 meter E =
0007069
Z = 4974519
35 I = 51
89863
XDOT = 6030
387027 Wp = 69
44572
YDOT = -4222
910293 meter/sec RA = 131
66711 deg
ZDOT = -2164
695288 TA = 41
58806
MA = 41
53432
Ha = 220
247 n
mi
Hp = 212
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4258071
95 X = -1272623
86
Y = -14465595
24 feet Y = -4423485
95 meter
Z = 16320601
55 Z = 4968275
96
XDOT = 19784
734341 XDOT = 6087
675532
YDOT = -13854
692561 feet/sec YDOT = -4155
154118 meter/sec
ZDOT = -7102
018663 ZDOT = -2135
262418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14271581
76 X = -4349978
12
Y = 4957057
39 feet Y = 1510911
09 meter
Z = 16294053
93 Z = 4966427
64
XDOT = -14300
934841 XDOT = -4358
924940
YDOT = -18200
447002 feet/sec YDOT = -5547
496246 meter/sec
ZDOT = -6972
725474 ZDOT = -2125
286724
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 16226
40842146
00016717 00000-0 10270-3 0 9126
2 25544 51
6409 132
5122 0001631 121
8886 238
2426 15
54979659 13885
Satellite: ISS
Catalog Number: 25544
Epoch time: 16226
40842146 = yrday
fracday
Element set: 912
Inclination: 51
6409 deg
RA of node: 132
5122 deg
Eccentricity:
0001631
Arg of perigee: 121
8886 deg
Mean anomaly: 238
2426 deg
Mean motion: 15
54979659 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1388
Checksum: 315
Coasting Arc #14 (Orbit 1402)
---------------------------------------
Vector Time (GMT): 2016/227/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -271422
72 A = 6780299
60 meter
Y = 5521734
01 meter E =
0008179
Z = -3934283
91 I = 51
93256
XDOT = -5933
621473 Wp = 109
77460
YDOT = 2613
621118 meter/sec RA = 126
68698 deg
ZDOT = 4081
740238 TA = 202
79351
MA = 202
82983
Ha = 220
179 n
mi
Hp = 212
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -890494
48 X = -314037
17
Y = 18115925
21 feet Y = 5518460
58 meter
Z = -12907755
62 Z = -3935705
80
XDOT = -19467
262052 XDOT = -5982
233713
YDOT = 8574
872435 feet/sec YDOT = 2546
995512 meter/sec
ZDOT = 13391
536215 ZDOT = 4052
798561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18130945
35 X = 5526312
14
Y = -253622
80 feet Y = -77304
23 meter
Z = -12914889
79 Z = -3936458
41
XDOT = 9686
317555 XDOT = 2952
389591
YDOT = 17696
334486 feet/sec YDOT = 5393
842751 meter/sec
ZDOT = 13264
638172 ZDOT = 4043
061715
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 16227
37242064
00016717 00000-0 10270-3 0 9137
2 25544 51
6410 127
7008 0001587 122
0314 238
0994 15
54975366 14032
Satellite: ISS
Catalog Number: 25544
Epoch time: 16227
37242064 = yrday
fracday
Element set: 913
Inclination: 51
6410 deg
RA of node: 127
7008 deg
Eccentricity:
0001587
Arg of perigee: 122
0314 deg
Mean anomaly: 238
0994 deg
Mean motion: 15
54975366 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1403
Checksum: 293
Coasting Arc #15 (Orbit 1418)
---------------------------------------
Vector Time (GMT): 2016/228/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1678017
94 A = 6784540
62 meter
Y = -6147368
23 meter E =
0015362
Z = 2307421
93 I = 51
96576
XDOT = 5372
419665 Wp = 109
30670
YDOT = -587
295660 meter/sec RA = 121
72237 deg
ZDOT = -5447
130993 TA = 45
08197
MA = 44
95741
Ha = 220
147 n
mi
Hp = 212
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5505308
21 X = 1735426
38
Y = -20168530
94 feet Y = -6128282
55 meter
Z = 7570281
91 Z = 2315712
54
XDOT = 17626
048771 XDOT = 5405
047037
YDOT = -1926
823031 feet/sec YDOT = -527
035175 meter/sec
ZDOT = -17871
164676 ZDOT = -5420
954322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20522771
81 X = -6255340
85
Y = -3915141
69 feet Y = -1193335
19 meter
Z = 7607544
25 Z = 2318779
49
XDOT = -3550
341907 XDOT = -1082
144213
YDOT = -16047
973421 feet/sec YDOT = -4891
422299 meter/sec
ZDOT = -17756
673610 ZDOT = -5412
234116
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 16228
40068188
00016717 00000-0 10270-3 0 9146
2 25544 51
6414 122
5688 0001599 124
9547 235
1757 15
54992086 14195
Satellite: ISS
Catalog Number: 25544
Epoch time: 16228
40068188 = yrday
fracday
Element set: 914
Inclination: 51
6414 deg
RA of node: 122
5688 deg
Eccentricity:
0001599
Arg of perigee: 124
9547 deg
Mean anomaly: 235
1757 deg
Mean motion: 15
54992086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1419
Checksum: 335
Coasting Arc #16 (Orbit 1433)
---------------------------------------
Vector Time (GMT): 2016/229/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2777451
99 A = 6786708
08 meter
Y = 6175365
86 meter E =
0011384
Z = -385935
37 I = 51
98946
XDOT = -4451
903030 Wp = 50
27663
YDOT = -1633
440760 meter/sec RA = 116
76968 deg
ZDOT = 6026
851270 TA = 305
58171
MA = 305
68775
Ha = 220
072 n
mi
Hp = 212
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9112375
29 X = -2844425
40
Y = 20260386
69 feet Y = 6143932
07 meter
Z = -1266192
17 Z = -399589
96
XDOT = -14605
981069 XDOT = -4462
581885
YDOT = -5359
057613 feet/sec YDOT = -1683
284608 meter/sec
ZDOT = 19773
134089 ZDOT = 6005
199529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21017547
36 X = 6406148
44
Y = 7184977
65 feet Y = 2189981
19 meter
Z = -1326911
40 Z = -404442
60
XDOT = -3443
251015 XDOT = -1049
502909
YDOT = 13634
378621 feet/sec YDOT = 4155
758604 meter/sec
ZDOT = 19678
782295 ZDOT = 5998
092844
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 16229
36467068
00016717 00000-0 10270-3 0 9153
2 25544 51
6416 117
7579 0001552 131
6712 228
4574 15
55005696 14342
Satellite: ISS
Catalog Number: 25544
Epoch time: 16229
36467068 = yrday
fracday
Element set: 915
Inclination: 51
6416 deg
RA of node: 117
7579 deg
Eccentricity:
0001552
Arg of perigee: 131
6712 deg
Mean anomaly: 228
4574 deg
Mean motion: 15
55005696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1434
Checksum: 319
Coasting Arc #17 (Orbit 1449)
---------------------------------------
Vector Time (GMT): 2016/230/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3584729
92 A = 6785655
76 meter
Y = -5520947
91 meter E =
0009406
Z = -1633065
91 I = 52
00057
XDOT = 3305
440903 Wp = 140
67022
YDOT = 3841
112072 meter/sec RA = 111
81955 deg
ZDOT = -5755
142165 TA = 57
12172
MA = 57
03124
Ha = 220
077 n
mi
Hp = 212
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11760924
93 X = 3654132
70
Y = -18113346
18 feet Y = -5480473
05 meter
Z = -5357827
80 Z = -1615483
87
XDOT = 10844
622385 XDOT = 3290
198363
YDOT = 12602
073726 feet/sec YDOT = 3877
990364 meter/sec
ZDOT = -18881
700016 ZDOT = -5739
122609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19300345
03 X = -5882745
16
Y = -9733283
39 feet Y = -2966704
78 meter
Z = -5280043
56 Z = -1609357
28
XDOT = 10609
149851 XDOT = 3233
668875
YDOT = -10877
344337 feet/sec YDOT = -3315
414554 meter/sec
ZDOT = -18812
333589 ZDOT = -5733
999278
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 16230
39291921
00016717 00000-0 10270-3 0 9162
2 25544 51
6425 112
6253 0001476 131
2323 228
8958 15
55013287 14507
Satellite: ISS
Catalog Number: 25544
Epoch time: 16230
39291921 = yrday
fracday
Element set: 916
Inclination: 51
6425 deg
RA of node: 112
6253 deg
Eccentricity:
0001476
Arg of perigee: 131
2323 deg
Mean anomaly: 228
8958 deg
Mean motion: 15
55013287 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1450
Checksum: 293
Coasting Arc #18 (Orbit 1465)
---------------------------------------
Vector Time (GMT): 2016/231/08:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 930011
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4051036
51 A = 6781960
07 meter
Y = 4249568
76 meter E =
0013606
Z = 3384149
60 I = 51
99857
XDOT = -2081
365135 Wp = 93
81722
YDOT = -5718
611934 meter/sec RA = 106
86289 deg
ZDOT = 4672
491221 TA = 305
50975
MA = 305
63659
Ha = 220
091 n
mi
Hp = 212
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13290802
21 X = -4114693
59
Y = 13942154
71 feet Y = 4203911
58 meter
Z = 11102853
03 Z = 3364316
30
XDOT = -6828
625771 XDOT = -2039
959954
YDOT = -18761
850178 feet/sec YDOT = -5741
655437 meter/sec
ZDOT = 15329
695606 ZDOT = 4662
481498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15526964
30 X = 4732618
72
Y = 11483727
53 feet Y = 3500240
15 meter
Z = 11015435
91 Z = 3357504
87
XDOT = -16891
590033 XDOT = -5148
556642
YDOT = 8121
379539 feet/sec YDOT = 2475
396483 meter/sec
ZDOT = 15286
917472 ZDOT = 4659
452446
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 16231
42116328
00016717 00000-0 10270-3 0 9175
2 25544 51
6417 107
4936 0001496 135
6974 224
4299 15
55017846 14662
Satellite: ISS
Catalog Number: 25544
Epoch time: 16231
42116328 = yrday
fracday
Element set: 917
Inclination: 51
6417 deg
RA of node: 107
4936 deg
Eccentricity:
0001496
Arg of perigee: 135
6974 deg
Mean anomaly: 224
4299 deg
Mean motion: 15
55017846 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1466
Checksum: 321
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