[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 29th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 453 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
126/05:21:57
957 -0
4 4
8 4
8
N/A -4
1 -0
0 216
7
000/00:13:55
914 -2
5 0
2 215
5
Coasting Arc #1 (Orbit 2045)
---------------------------------------
Vector Time (GMT): 2015/119/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3693259
88 A = 6780188
14 meter
Y = -5003601
23 meter E =
0004296
Z = -2693614
19 I = 51
45854
XDOT = 5519
489939 Wp = 336
46267
YDOT = 1292
734945 meter/sec RA = 326
61575 deg
ZDOT = 5167
519023 TA = 352
99721
MA = 353
00321
Ha = 215
845 n
mi
Hp = 213
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12116994
37 X = 3762021
56
Y = -16416014
54 feet Y = -4961916
49 meter
Z = -8837316
91 Z = -2675505
53
XDOT = 18108
562792 XDOT = 5479
521906
YDOT = 4241
256380 feet/sec YDOT = 1354
234343 meter/sec
ZDOT = 16953
802569 ZDOT = 5194
234756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 94379
42 X = 28766
85
Y = -20437244
93 feet Y = -6229272
26 meter
Z = -8758730
96 Z = -2669661
20
XDOT = 15529
666267 XDOT = 4733
442278
YDOT = -7241
654521 feet/sec YDOT = -2207
256298 meter/sec
ZDOT = 17068
048780 ZDOT = 5202
341268
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15119
50538221
00016717 00000-0 10270-3 0 9000
2 25544 51
6451 327
2049 0005839 281
0028 79
0469 15
56232355 20461
Satellite: ISS
Catalog Number: 25544
Epoch time: 15119
50538221 = yrday
fracday
Element set: 900
Inclination: 51
6451 deg
RA of node: 327
2049 deg
Eccentricity:
0005839
Arg of perigee: 281
0028 deg
Mean anomaly: 79
0469 deg
Mean motion: 15
56232355 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2046
Checksum: 295
Coasting Arc #2 (Orbit 2061)
---------------------------------------
Vector Time (GMT): 2015/120/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5105446
84 A = 6783035
65 meter
Y = 4441400
94 meter E =
0007894
Z = 391156
85 I = 51
44248
XDOT = -3406
428753 Wp = 149
17235
YDOT = -3384
739618 meter/sec RA = 321
61968 deg
ZDOT = -5982
236571 TA = 26
59557
MA = 26
55510
Ha = 215
944 n
mi
Hp = 213
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16750153
66 X = -5156632
31
Y = 14571525
41 feet Y = 4384022
33 meter
Z = 1283323
00 Z = 366230
64
XDOT = -11175
947352 XDOT = -3339
266747
YDOT = -11104
788773 feet/sec YDOT = -3422
457377 meter/sec
ZDOT = -19626
760403 ZDOT = -5998
621226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4508815
11 X = -1374286
85
Y = 21744709
26 feet Y = 6627787
38 meter
Z = 1175637
66 Z = 358334
36
XDOT = -13934
825154 XDOT = -4247
334707
YDOT = -1815
437647 feet/sec YDOT = -553
345395 meter/sec
ZDOT = -19696
320162 ZDOT = -6003
438385
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15120
53281171
00016717 00000-0 10270-3 0 9015
2 25544 51
6450 322
0673 0005833 285
7935 74
2576 15
56277073 20628
Satellite: ISS
Catalog Number: 25544
Epoch time: 15120
53281171 = yrday
fracday
Element set: 901
Inclination: 51
6450 deg
RA of node: 322
0673 deg
Eccentricity:
0005833
Arg of perigee: 285
7935 deg
Mean anomaly: 74
2576 deg
Mean motion: 15
56277073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2062
Checksum: 297
Coasting Arc #3 (Orbit 2077)
---------------------------------------
Vector Time (GMT): 2015/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5653938
32 A = 6781242
16 meter
Y = -3158624
83 meter E =
0010098
Z = 1989206
28 I = 51
41132
XDOT = 948
723565 Wp = 46
72866
YDOT = 5205
412269 meter/sec RA = 316
62240 deg
ZDOT = 5558
011444 TA = 335
33461
MA = 335
38287
Ha = 215
886 n
mi
Hp = 213
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18549666
40 X = 5679175
62
Y = -10362942
37 feet Y = -3095257
58 meter
Z = 6526267
31 Z = 2016733
95
XDOT = 3112
610122 XDOT = 863
445695
YDOT = 17078
124241 feet/sec YDOT = 5215
545005 meter/sec
ZDOT = 18234
945681 ZDOT = 5562
412816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8114784
25 X = 2473386
24
Y = -19597683
32 feet Y = -5973373
88 meter
Z = 6644843
73 Z = 2025348
37
XDOT = 11500
958642 XDOT = 3505
492194
YDOT = 10963
051171 feet/sec YDOT = 3341
537997 meter/sec
ZDOT = 18252
799319 ZDOT = 5563
453232
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15121
56021877
00016717 00000-0 10270-3 0 9025
2 25544 51
6437 316
9274 0005884 288
0334 72
0179 15
56313893 20780
Satellite: ISS
Catalog Number: 25544
Epoch time: 15121
56021877 = yrday
fracday
Element set: 902
Inclination: 51
6437 deg
RA of node: 316
9274 deg
Eccentricity:
0005884
Arg of perigee: 288
0334 deg
Mean anomaly: 72
0179 deg
Mean motion: 15
56313893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2078
Checksum: 319
Coasting Arc #4 (Orbit 2092)
---------------------------------------
Vector Time (GMT): 2015/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5350842
71 A = 6776096
98 meter
Y = 1246476
52 meter E =
0004590
Z = -3970618
63 I = 51
37118
XDOT = 1451
089458 Wp = 16
06049
YDOT = -6401
355486 meter/sec RA = 311
61031 deg
ZDOT = -3961
817207 TA = 212
51245
MA = 212
54072
Ha = 216
187 n
mi
Hp = 213
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17555258
23 X = -5345095
26
Y = 4089489
90 feet Y = 1186671
87 meter
Z = -13026964
01 Z = -3996598
59
XDOT = 4760
792186 XDOT = 1541
808496
YDOT = -21001
822459 feet/sec YDOT = -6384
621382 meter/sec
ZDOT = -12998
087948 ZDOT = -3954
547334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10943964
24 X = -3335720
30
Y = 14220458
13 feet Y = 4334395
64 meter
Z = -13138532
19 Z = -4004624
61
XDOT = -8500
748399 XDOT = -2591
028112
YDOT = -18531
063264 feet/sec YDOT = -5648
268083 meter/sec
ZDOT = -12965
700214 ZDOT = -3951
945425
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15122
52339441
00016717 00000-0 10270-3 0 9032
2 25544 51
6429 312
1100 0005812 293
2014 66
8528 15
56339457 20931
Satellite: ISS
Catalog Number: 25544
Epoch time: 15122
52339441 = yrday
fracday
Element set: 903
Inclination: 51
6429 deg
RA of node: 312
1100 deg
Eccentricity:
0005812
Arg of perigee: 293
2014 deg
Mean anomaly: 66
8528 deg
Mean motion: 15
56339457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2093
Checksum: 287
Coasting Arc #5 (Orbit 2108)
---------------------------------------
Vector Time (GMT): 2015/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4316294
06 A = 6771728
65 meter
Y = 1047996
15 meter E =
0001325
Z = 5112682
37 I = 51
33578
XDOT = -3435
882990 Wp = 266
94798
YDOT = 6685
762906 meter/sec RA = 306
57507 deg
ZDOT = 1530
513657 TA = 168
24923
MA = 168
24614
Ha = 216
277 n
mi
Hp = 213
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14161069
74 X = 4279418
28
Y = 3438307
57 feet Y = 1096057
71 meter
Z = 16773892
30 Z = 5133560
95
XDOT = -11272
581987 XDOT = -3517
824241
YDOT = 21934
917670 feet/sec YDOT = 6646
882494 meter/sec
ZDOT = 5021
370266 ZDOT = 1513
623247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12951008
74 X = 3947467
46
Y = -6451874
30 feet Y = -1966531
29 meter
Z = 16863155
36 Z = 5139889
75
XDOT = 5068
154301 XDOT = 1544
773431
YDOT = 23102
834622 feet/sec YDOT = 7041
743993 meter/sec
ZDOT = 4947
708209 ZDOT = 1508
061462
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15123
55076114
00016717 00000-0 10270-3 0 9042
2 25544 51
6427 306
9701 0005822 297
3315 62
7245 15
56319203 21093
Satellite: ISS
Catalog Number: 25544
Epoch time: 15123
55076114 = yrday
fracday
Element set: 904
Inclination: 51
6427 deg
RA of node: 306
9701 deg
Eccentricity:
0005822
Arg of perigee: 297
3315 deg
Mean anomaly: 62
7245 deg
Mean motion: 15
56319203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2109
Checksum: 289
Coasting Arc #6 (Orbit 2123)
---------------------------------------
Vector Time (GMT): 2015/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2804426
69 A = 6771282
49 meter
Y = -3355746
22 meter E =
0008903
Z = -5177178
16 I = 51
31666
XDOT = 4763
661359 Wp = 86
48826
YDOT = -5878
323426 meter/sec RA = 301
52839 deg
ZDOT = 1232
157985 TA = 195
38077
MA = 195
40785
Ha = 216
327 n
mi
Hp = 212
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9200874
98 X = -2741544
16
Y = -11009666
07 feet Y = -3386755
58 meter
Z = -16985492
64 Z = -5190649
06
XDOT = 15628
810234 XDOT = 4823
054628
YDOT = -19285
838012 feet/sec YDOT = -5824
720957 meter/sec
ZDOT = 4042
513073 ZDOT = 1255
443734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14095358
09 X = -4296265
15
Y = -2290736
18 feet Y = -698216
39 meter
Z = -17042570
69 Z = -5194575
55
XDOT = -1139
004868 XDOT = -347
168684
YDOT = -23759
900008 feet/sec YDOT = -7242
017523 meter/sec
ZDOT = 4143
419089 ZDOT = 1262
914138
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15124
51389481
00016717 00000-0 10270-3 0 9054
2 25544 51
6426 302
1516 0005749 299
9465 60
1118 15
56396456 21249
Satellite: ISS
Catalog Number: 25544
Epoch time: 15124
51389481 = yrday
fracday
Element set: 905
Inclination: 51
6426 deg
RA of node: 302
1516 deg
Eccentricity:
0005749
Arg of perigee: 299
9465 deg
Mean anomaly: 60
1118 deg
Mean motion: 15
56396456 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2124
Checksum: 317
Coasting Arc #7 (Orbit 2139)
---------------------------------------
Vector Time (GMT): 2015/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911686
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1058856
79 A = 6775461
44 meter
Y = 5272730
53 meter E =
0007765
Z = 4120632
98 I = 51
31493
XDOT = -5354
494838 Wp = 42
30831
YDOT = 4013
200530 meter/sec RA = 296
48919 deg
ZDOT = -3749
570269 TA = 86
50888
MA = 86
42006
Ha = 216
520 n
mi
Hp = 212
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3473939
59 X = 979800
25
Y = 17298984
67 feet Y = 5284129
27 meter
Z = 13519137
07 Z = 4125584
85
XDOT = -17567
240282 XDOT = -5380
759046
YDOT = 13166
668406 feet/sec YDOT = 3953
176266 meter/sec
ZDOT = -12301
739729 ZDOT = -3775
645662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14131801
53 X = 4307373
11
Y = 10538902
16 feet Y = 3212257
38 meter
Z = 13539347
14 Z = 4126793
01
XDOT = -3341
604361 XDOT = -1018
521009
YDOT = 20470
551491 feet/sec YDOT = 6239
424095 meter/sec
ZDOT = -12414
239041 ZDOT = -3783
860060
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 15125
54121713
00016717 00000-0 10270-3 0 9061
2 25544 51
6426 297
0123 0005872 303
5041 56
5552 15
56411290 21407
Satellite: ISS
Catalog Number: 25544
Epoch time: 15125
54121713 = yrday
fracday
Element set: 906
Inclination: 51
6426 deg
RA of node: 297
0123 deg
Eccentricity:
0005872
Arg of perigee: 303
5041 deg
Mean anomaly: 56
5552 deg
Mean motion: 15
56411290 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2140
Checksum: 272
Coasting Arc #8 (Orbit 2150)
---------------------------------------
Vector Time (GMT): 2015/126/05:28:55
914
Vector Time (MET): N/A
Weight (LBS) : 911172
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4506198
70 A = 6774386
69 meter
Y = 256058
11 meter E =
0006794
Z = -5057596
56 I = 51
29675
XDOT = 1554
999794 Wp = 52
28779
YDOT = -7298
986060 meter/sec RA = 292
87221 deg
ZDOT = -1752
539206 TA = 200
66374
MA = 200
69122
Ha = 216
743 n
mi
Hp = 215
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14784116
48 X = -4484158
70
Y = 840085
65 feet Y = 205790
20 meter
Z = -16593164
57 Z = -5079433
69
XDOT = 5101
705361 XDOT = 1645
016569
YDOT = -23946
804658 feet/sec YDOT = -7281
093680 meter/sec
ZDOT = -5749
800543 ZDOT = -1744
766699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9137615
80 X = -2785145
30
Y = -11517990
90 feet Y = -3510683
63 meter
Z = -16686785
71 Z = -5086132
28
XDOT = 21697
594199 XDOT = 6613
426712
YDOT = -8921
988936 feet/sec YDOT = -2719
422228 meter/sec
ZDOT = -5715
103394 ZDOT = -1741
963514
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 15126
24749791
00016717 00000-0 10270-3 0 9072
2 25544 51
6468 293
4835 0007662 278
4828 81
5457 15
55492657 21514
Satellite: ISS
Catalog Number: 25544
Epoch time: 15126
24749791 = yrday
fracday
Element set: 907
Inclination: 51
6468 deg
RA of node: 293
4835 deg
Eccentricity:
0007662
Arg of perigee: 278
4828 deg
Mean anomaly: 81
5457 deg
Mean motion: 15
55492657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2151
Checksum: 350
Coasting Arc #9 (Orbit 2166)
---------------------------------------
Vector Time (GMT): 2015/127/05:28:55
914
Vector Time (MET): N/A
Weight (LBS) : 911172
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3774309
26 A = 6773408
11 meter
Y = 2020187
24 meter E =
0005824
Z = 5253668
19 I = 51
28235
XDOT = -2848
772139 Wp = 301
25459
YDOT = 7086
143542 meter/sec RA = 287
83329 deg
ZDOT = -675
815641 TA = 155
24598
MA = 155
21802
Ha = 217
122 n
mi
Hp = 215
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12382904
40 X = 3725917
75
Y = 6627910
88 feet Y = 2062123
27 meter
Z = 17236444
19 Z = 5271885
89
XDOT = -9346
365287 XDOT = -2924
516441
YDOT = 23248
502434 feet/sec YDOT = 7053
863223 meter/sec
ZDOT = -2217
242918 ZDOT = -689
838386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1884913
98 X = 574521
78
Y = 13821311
65 feet Y = 4212735
79 meter
Z = 17314126
49 Z = 5277345
75
XDOT = -23270
427375 XDOT = -7092
826264
YDOT = 6037
959343 feet/sec YDOT = 1840
370008 meter/sec
ZDOT = -2278
676514 ZDOT = -694
540601
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 15127
27543018
00016717 00000-0 10270-3 0 9081
2 25544 51
6467 288
3487 0007869 282
3760 77
6513 15
55538160 21673
Satellite: ISS
Catalog Number: 25544
Epoch time: 15127
27543018 = yrday
fracday
Element set: 908
Inclination: 51
6467 deg
RA of node: 288
3487 deg
Eccentricity:
0007869
Arg of perigee: 282
3760 deg
Mean anomaly: 77
6513 deg
Mean motion: 15
55538160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2167
Checksum: 338
Coasting Arc #10 (Orbit 2181)
---------------------------------------
Vector Time (GMT): 2015/128/05:28:55
914
Vector Time (MET): N/A
Weight (LBS) : 911172
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2824490
75 A = 6776270
20 meter
Y = -4125789
29 meter E =
0002337
Z = -4575960
24 I = 51
28359
XDOT = 3814
043241 Wp = 121
38050
YDOT = -5937
497682 meter/sec RA = 282
79705 deg
ZDOT = 2999
121332 TA = 178
70506
MA = 178
70445
Ha = 217
290 n
mi
Hp = 215
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9266701
93 X = -2755916
68
Y = -13536054
11 feet Y = -4156990
99 meter
Z = -15012992
91 Z = -4589514
85
XDOT = 12513
265225 XDOT = 3865
585486
YDOT = -19479
979272 feet/sec YDOT = -5894
558487 meter/sec
ZDOT = 9839
636916 ZDOT = 3017
774415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5257628
78 X = 1602525
25
Y = -15483211
18 feet Y = -4719282
77 meter
Z = -15070301
68 Z = -4593427
95
XDOT = 21916
513504 XDOT = 6680
153316
YDOT = -2214
130677 feet/sec YDOT = -674
867030 meter/sec
ZDOT = 9920
689908 ZDOT = 3023
826284
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 15128
23909927
00016717 00000-0 10270-3 0 9094
2 25544 51
6472 283
5348 0007883 286
7143 73
3145 15
55538855 21823
Satellite: ISS
Catalog Number: 25544
Epoch time: 15128
23909927 = yrday
fracday
Element set: 909
Inclination: 51
6472 deg
RA of node: 283
5348 deg
Eccentricity:
0007883
Arg of perigee: 286
7143 deg
Mean anomaly: 73
3145 deg
Mean motion: 15
55538855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2182
Checksum: 341
Coasting Arc #11 (Orbit 2197)
---------------------------------------
Vector Time (GMT): 2015/129/05:28:55
914
Vector Time (MET): N/A
Weight (LBS) : 911172
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1734966
13 A = 6781009
14 meter
Y = 5764581
16 meter E =
0005854
Z = 3118337
68 I = 51
29330
XDOT = -4448
564564 Wp = 72
88172
YDOT = 3957
841531 meter/sec RA = 277
77490 deg
ZDOT = -4832
195491 TA = 71
00305
MA = 70
93963
Ha = 217
603 n
mi
Hp = 215
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5692146
10 X = 1655228
41
Y = 18912667
84 feet Y = 5783536
73 meter
Z = 10230766
68 Z = 3126572
43
XDOT = -14595
028098 XDOT = -4469
018245
YDOT = 12985
044393 feet/sec YDOT = 3907
980588 meter/sec
ZDOT = -15853
659746 ZDOT = -4853
855496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11407943
12 X = -3477141
06
Y = 16101153
07 feet Y = 4907631
46 meter
Z = 10264980
40 Z = 3128766
03
XDOT = -17987
257164 XDOT = -5482
515984
YDOT = -2558
199645 feet/sec YDOT = -779
739252 meter/sec
ZDOT = -15947
223562 ZDOT = -4860
713742
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 15129
26699201
00016717 00000-0 10270-3 0 9101
2 25544 51
6469 278
4002 0007829 291
1014 68
9303 15
55562024 21984
Satellite: ISS
Catalog Number: 25544
Epoch time: 15129
26699201 = yrday
fracday
Element set: 910
Inclination: 51
6469 deg
RA of node: 278
4002 deg
Eccentricity:
0007829
Arg of perigee: 291
1014 deg
Mean anomaly: 68
9303 deg
Mean motion: 15
55562024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2198
Checksum: 309
Coasting Arc #12 (Orbit 2212)
---------------------------------------
Vector Time (GMT): 2015/130/05:28:55
914
Vector Time (MET): N/A
Weight (LBS) : 911172
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -583379
43 A = 6784480
61 meter
Y = -6656996
98 meter E =
0010859
Z = -1128547
83 I = 51
30217
XDOT = 4760
586511 Wp = 352
09457
YDOT = -1408
419169 meter/sec RA = 272
76704 deg
ZDOT = 5850
842465 TA = 355
58571
MA = 355
59528
Ha = 217
711 n
mi
Hp = 215
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1913974
51 X = -503413
85
Y = -21840541
28 feet Y = -6663073
57 meter
Z = -3702584
75 Z = -1131187
74
XDOT = 15618
722150 XDOT = 4747
560571
YDOT = -4620
797800 feet/sec YDOT = -1355
256165 meter/sec
ZDOT = 19195
677377 ZDOT = 5873
936958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15757579
93 X = 4802910
36
Y = -15241274
47 feet Y = -4645540
46 meter
Z = -3712667
91 Z = -1131621
18
XDOT = 12246
261120 XDOT = 3732
660390
YDOT = 7964
068959 feet/sec YDOT = 2427
448219 meter/sec
ZDOT = 19294
914783 ZDOT = 5881
090026
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 15130
23062051
00016717 00000-0 10270-3 0 9118
2 25544 51
6471 273
5856 0008023 294
9022 65
1297 15
55610650 22135
Satellite: ISS
Catalog Number: 25544
Epoch time: 15130
23062051 = yrday
fracday
Element set: 911
Inclination: 51
6471 deg
RA of node: 273
5856 deg
Eccentricity:
0008023
Arg of perigee: 294
9022 deg
Mean anomaly: 65
1297 deg
Mean motion: 15
55610650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2213
Checksum: 277
Coasting Arc #13 (Orbit 2228)
---------------------------------------
Vector Time (GMT): 2015/131/05:28:55
914
Vector Time (MET): N/A
Weight (LBS) : 911172
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -598285
04 A = 6784576
64 meter
Y = 6670105
18 meter E =
0003927
Z = -1070662
64 I = 51
30133
XDOT = -4751
897596 Wp = 198
22154
YDOT = -1367
303827 meter/sec RA = 267
76699 deg
ZDOT = -5860
615268 TA = 353
44889
MA = 353
45402
Ha = 217
942 n
mi
Hp = 214
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1962877
44 X = -667626
37
Y = 21883547
19 feet Y = 6663027
07 meter
Z = -3512672
71 Z = -1073737
36
XDOT = -15590
215210 XDOT = -4707
786051
YDOT = -4485
904944 feet/sec YDOT = -1420
195943 meter/sec
ZDOT = -19227
740379 ZDOT = -5883
592085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17992287
03 X = -5484049
09
Y = 12606299
02 feet Y = 3842399
94 meter
Z = -3527070
65 Z = -1075051
13
XDOT = -5607
202746 XDOT = -1709
075397
YDOT = -13411
987545 feet/sec YDOT = -4087
973804 meter/sec
ZDOT = -19325
967338 ZDOT = -5890
554845
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 15131
25847177
00016717 00000-0 10270-3 0 9122
2 25544 51
6467 268
4508 0008068 297
8498 62
1838 15
55594806 22294
Satellite: ISS
Catalog Number: 25544
Epoch time: 15131
25847177 = yrday
fracday
Element set: 912
Inclination: 51
6467 deg
RA of node: 268
4508 deg
Eccentricity:
0008068
Arg of perigee: 297
8498 deg
Mean anomaly: 62
1838 deg
Mean motion: 15
55594806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2229
Checksum: 350
Coasting Arc #14 (Orbit 2244)
---------------------------------------
Vector Time (GMT): 2015/132/05:28:55
914
Vector Time (MET): N/A
Weight (LBS) : 911172
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1762752
65 A = 6780837
06 meter
Y = -5766688
58 meter E =
0008380
Z = 3089036
99 I = 51
29085
XDOT = 4428
124890 Wp = 46
79591
YDOT = 3957
747802 meter/sec RA = 262
75848 deg
ZDOT = 4858
818847 TA = 348
95600
MA = 348
97438
Ha = 218
101 n
mi
Hp = 214
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5783309
23 X = 1812100
62
Y = -18919581
97 feet Y = -5746700
40 meter
Z = 10134635
78 Z = 3097720
04
XDOT = 14527
968798 XDOT = 4359
936795
YDOT = 12984
736882 feet/sec YDOT = 4006
884739 meter/sec
ZDOT = 15941
006715 ZDOT = 4880
164353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18020043
93 X = 5492509
39
Y = -8117777
06 feet Y = -2474298
45 meter
Z = 10172895
47 Z = 3100698
54
XDOT = -904
422223 XDOT = -275
667893
YDOT = 18093
826550 feet/sec YDOT = 5514
998333 meter/sec
ZDOT = 16031
779530 ZDOT = 4886
486401
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 15132
28630099
00016717 00000-0 10270-3 0 9130
2 25544 51
6461 263
3143 0008218 303
8982 56
1390 15
55645309 22459
Satellite: ISS
Catalog Number: 25544
Epoch time: 15132
28630099 = yrday
fracday
Element set: 913
Inclination: 51
6461 deg
RA of node: 263
3143 deg
Eccentricity:
0008218
Arg of perigee: 303
8982 deg
Mean anomaly: 56
1390 deg
Mean motion: 15
55645309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2245
Checksum: 303
Coasting Arc #15 (Orbit 2259)
---------------------------------------
Vector Time (GMT): 2015/133/05:28:55
914
Vector Time (MET): N/A
Weight (LBS) : 911172
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2863060
30 A = 6775835
93 meter
Y = 4102681
45 meter E =
0008937
Z = -4576518
32 I = 51
27864
XDOT = -3756
641688 Wp = 18
63520
YDOT = -5971
403809 meter/sec RA = 257
73458 deg
ZDOT = -2996
300673 TA = 221
26121
MA = 221
32879
Ha = 218
255 n
mi
Hp = 214
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9393242
44 X = -2886493
42
Y = 13460240
99 feet Y = 4070533
77 meter
Z = -15014823
87 Z = -4590483
62
XDOT = -12324
939920 XDOT = -3675
033760
YDOT = -19591
219845 feet/sec YDOT = -6012
956767 meter/sec
ZDOT = -9830
382785 ZDOT = -3014
351626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16221197
35 X = -4944220
95
Y = 2112006
73 feet Y = 643739
65 meter
Z = -15075417
44 Z = -4594987
24
XDOT = 6487
118048 XDOT = 1977
273581
YDOT = -21045
622853 feet/sec YDOT = -6414
705846 meter/sec
ZDOT = -9906
683796 ZDOT = -3019
557221
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 15133
24987062
00016717 00000-0 10270-3 0 9143
2 25544 51
6452 258
4995 0008354 306
7671 53
2715 15
55689962 22606
Satellite: ISS
Catalog Number: 25544
Epoch time: 15133
24987062 = yrday
fracday
Element set: 914
Inclination: 51
6452 deg
RA of node: 258
4995 deg
Eccentricity:
0008354
Arg of perigee: 306
7671 deg
Mean anomaly: 53
2715 deg
Mean motion: 15
55689962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2260
Checksum: 333
Coasting Arc #16 (Orbit 2275)
---------------------------------------
Vector Time (GMT): 2015/134/05:28:55
914
Vector Time (MET): N/A
Weight (LBS) : 911172
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3826455
66 A = 6772873
46 meter
Y = -1896073
61 meter E =
0005542
Z = 5259641
84 I = 51
27692
XDOT = 2726
265226 Wp = 319
67867
YDOT = 7143
349717 meter/sec RA = 252
69554 deg
ZDOT = 596
254268 TA = 124
62826
MA = 124
57600
Ha = 218
324 n
mi
Hp = 214
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12553988
38 X = 3821823
87
Y = -6220713
95 feet Y = -1853309
53 meter
Z = 17256042
78 Z = 5278219
06
XDOT = 8944
439717 XDOT = 2643
287541
YDOT = 23436
186735 feet/sec YDOT = 7173
372647 meter/sec
ZDOT = 1956
214790 ZDOT = 609
296519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13038759
69 X = 3974213
95
Y = 4850202
42 feet Y = 1478341
70 meter
Z = 17336008
79 Z = 5284015
48
XDOT = -10678
834054 XDOT = -3254
908620
YDOT = 21573
068013 feet/sec YDOT = 6575
471130 meter/sec
ZDOT = 2010
849751 ZDOT = 612
907004
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 15134
27765981
00016717 00000-0 10270-3 0 9152
2 25544 51
6456 253
3633 0008273 311
2018 48
8422 15
55708668 22766
Satellite: ISS
Catalog Number: 25544
Epoch time: 15134
27765981 = yrday
fracday
Element set: 915
Inclination: 51
6456 deg
RA of node: 253
3633 deg
Eccentricity:
0008273
Arg of perigee: 311
2018 deg
Mean anomaly: 48
8422 deg
Mean motion: 15
55708668 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2276
Checksum: 322
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