[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 24th 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
218/16:26:51
506 -2
2 2
3 2
3
N/A 0
2 0
0 219
3
000/00:06:23
013 -0
8 -0
0 213
9
Coasting Arc #1 (Orbit 3384)
---------------------------------------
Vector Time (GMT): 2015/205/12:46:54
460
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1944730
79 A = 6786253
22 meter
Y = -6476530
29 meter E =
0011206
Z = -493337
50 I = 51
30611
XDOT = 4481
527424 Wp = 31
65681
YDOT = -1794
368590 meter/sec RA = 256
63638 deg
ZDOT = 5961
367816 TA = 322
99403
MA = 323
07127
Ha = 218
915 n
mi
Hp = 213
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6380350
35 X = -1869767
70
Y = -21248458
94 feet Y = -6497858
38 meter
Z = -1618561
35 Z = -502602
75
XDOT = 14703
173963 XDOT = 4472
301497
YDOT = -5887
036057 feet/sec YDOT = -1744
305037 meter/sec
ZDOT = 19558
293360 ZDOT = 5983
115592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11258238
37 X = -3431511
06
Y = 19113642
20 feet Y = 5825838
14 meter
Z = -1657217
39 Z = -505119
86
XDOT = -12831
007518 XDOT = -3910
891091
YDOT = -5873
497162 feet/sec YDOT = -1790
241935 meter/sec
ZDOT = 19652
142905 ZDOT = 5989
973157
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 15205
53355073
00016717 00000-0 10270-3 0 9001
2 25544 51
6431 257
5393 0001931 311
8060 48
2928 15
55149577 33850
Satellite: ISS
Catalog Number: 25544
Epoch time: 15205
53355073 = yrday
fracday
Element set: 900
Inclination: 51
6431 deg
RA of node: 257
5393 deg
Eccentricity:
0001931
Arg of perigee: 311
8060 deg
Mean anomaly: 48
2928 deg
Mean motion: 15
55149577 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3385
Checksum: 305
Coasting Arc #2 (Orbit 3400)
---------------------------------------
Vector Time (GMT): 2015/206/12:46:54
460
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 848901
46 A = 6785178
52 meter
Y = 6543977
64 meter E =
0006287
Z = -1568198
80 I = 51
31188
XDOT = -5059
641287 Wp = 144
56282
YDOT = -709
759963 meter/sec RA = 251
63775 deg
ZDOT = -5717
245755 TA = 52
66727
MA = 52
61000
Ha = 218
918 n
mi
Hp = 213
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2785109
77 X = 783279
71
Y = 21469742
93 feet Y = 6553103
79 meter
Z = -5145009
19 Z = -1564234
06
XDOT = -16599
872988 XDOT = -5023
556458
YDOT = -2328
608802 feet/sec YDOT = -766
138123 meter/sec
ZDOT = -18757
367963 ZDOT = -5741
736764
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13545553
77 X = 4128684
79
Y = -16893419
50 feet Y = -5149114
26 meter
Z = -5129148
87 Z = -1563364
57
XDOT = 8492
473404 XDOT = 2588
505894
YDOT = 12519
929203 feet/sec YDOT = 3816
074421 meter/sec
ZDOT = -18862
562427 ZDOT = -5749
309028
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 15206
56168364
00016717 00000-0 10270-3 0 9011
2 25544 51
6438 252
4053 0001827 315
1532 44
9474 15
55198911 34013
Satellite: ISS
Catalog Number: 25544
Epoch time: 15206
56168364 = yrday
fracday
Element set: 901
Inclination: 51
6438 deg
RA of node: 252
4053 deg
Eccentricity:
0001827
Arg of perigee: 315
1532 deg
Mean anomaly: 44
9474 deg
Mean motion: 15
55198911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3401
Checksum: 298
Coasting Arc #3 (Orbit 3416)
---------------------------------------
Vector Time (GMT): 2015/207/12:46:54
460
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 405286
10 A = 6781414
32 meter
Y = -5864687
70 meter E =
0011570
Z = 3369027
27 I = 51
30885
XDOT = 5332
671848 Wp = 82
11942
YDOT = 3025
810559 meter/sec RA = 246
63134 deg
ZDOT = 4613
656985 TA = 317
45206
MA = 317
54165
Ha = 219
008 n
mi
Hp = 213
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1329678
81 X = 454470
97
Y = -19241101
36 feet Y = -5859880
74 meter
Z = 11053239
08 Z = 3371115
13
XDOT = 17495
642546 XDOT = 5276
028905
YDOT = 9927
199997 feet/sec YDOT = 3085
126970 meter/sec
ZDOT = 15136
669897 ZDOT = 4639
424524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14542832
94 X = -4432655
48
Y = 12659859
04 feet Y = 3858725
03 meter
Z = 11063277
13 Z = 3372086
87
XDOT = -4286
439862 XDOT = -1306
506870
YDOT = -18282
637079 feet/sec YDOT = -5572
547782 meter/sec
ZDOT = 15246
945589 ZDOT = 4647
269016
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
58980783
00016717 00000-0 10270-3 0 9022
2 25544 51
6425 247
2716 0001816 325
0902 35
0131 15
55190439 34171
Satellite: ISS
Catalog Number: 25544
Epoch time: 15207
58980783 = yrday
fracday
Element set: 902
Inclination: 51
6425 deg
RA of node: 247
2716 deg
Eccentricity:
0001816
Arg of perigee: 325
0902 deg
Mean anomaly: 35
0131 deg
Mean motion: 15
55190439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3417
Checksum: 297
Coasting Arc #4 (Orbit 3431)
---------------------------------------
Vector Time (GMT): 2015/208/12:46:54
460
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1794530
29 A = 6776811
81 meter
Y = 4568313
94 meter E =
0010390
Z = -4683033
95 I = 51
30811
XDOT = -5187
812191 Wp = 60
95843
YDOT = -4898
618216 meter/sec RA = 241
61134 deg
ZDOT = -2790
410055 TA = 181
22406
MA = 181
22661
Ha = 218
983 n
mi
Hp = 213
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5887566
56 X = -1822732
68
Y = 14987906
63 feet Y = 4548089
01 meter
Z = -15364284
61 Z = -4691819
49
XDOT = -17020
381204 XDOT = -5119
094453
YDOT = -16071
582075 feet/sec YDOT = -4956
247289 meter/sec
ZDOT = -9154
888632 ZDOT = -2815
444696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14602077
94 X = 4450713
36
Y = -6700170
34 feet Y = -2042211
92 meter
Z = -15402891
42 Z = -4694801
31
XDOT = 454
221650 XDOT = 138
446759
YDOT = 22283
289590 feet/sec YDOT = 6791
946667 meter/sec
ZDOT = -9261
691347 ZDOT = -2822
963523
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
55366385
00016717 00000-0 10270-3 0 9037
2 25544 51
6434 242
4591 0001857 324
6885 35
4145 15
55222165 34327
Satellite: ISS
Catalog Number: 25544
Epoch time: 15208
55366385 = yrday
fracday
Element set: 903
Inclination: 51
6434 deg
RA of node: 242
4591 deg
Eccentricity:
0001857
Arg of perigee: 324
6885 deg
Mean anomaly: 35
4145 deg
Mean motion: 15
55222165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3432
Checksum: 308
Coasting Arc #5 (Orbit 3447)
---------------------------------------
Vector Time (GMT): 2015/209/12:46:54
460
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3177576
51 A = 6774224
44 meter
Y = -2838874
50 meter E =
0001794
Z = 5264766
21 I = 51
31397
XDOT = 4574
093827 Wp = 73
52579
YDOT = 6135
070401 meter/sec RA = 236
57906 deg
ZDOT = 547
788253 TA = 11
22804
MA = 11
22403
Ha = 218
913 n
mi
Hp = 213
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10425119
78 X = 3183511
39
Y = -9313892
70 feet Y = -2803308
01 meter
Z = 17272855
02 Z = 5280216
24
XDOT = 15006
869511 XDOT = 4502
489122
YDOT = 20128
183729 feet/sec YDOT = 6185
820506 meter/sec
ZDOT = 1797
205553 ZDOT = 569
834630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13893653
85 X = -4234785
69
Y = -283277
17 feet Y = -86342
88 meter
Z = 17339820
55 Z = 5285177
30
XDOT = 2846
331513 XDOT = 867
561845
YDOT = -23922
466487 feet/sec YDOT = -7291
567785 meter/sec
ZDOT = 1890
953581 ZDOT = 576
362652
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
58176830
00016717 00000-0 10270-3 0 9046
2 25544 51
6417 237
3248 0001890 331
6802 28
4249 15
55238645 34488
Satellite: ISS
Catalog Number: 25544
Epoch time: 15209
58176830 = yrday
fracday
Element set: 904
Inclination: 51
6417 deg
RA of node: 237
3248 deg
Eccentricity:
0001890
Arg of perigee: 331
6802 deg
Mean anomaly: 28
4249 deg
Mean motion: 15
55238645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3448
Checksum: 318
Coasting Arc #6 (Orbit 3462)
---------------------------------------
Vector Time (GMT): 2015/210/12:46:54
460
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4424821
38 A = 6775174
92 meter
Y = 933052
05 meter E =
0012058
Z = -5055890
60 I = 51
33572
XDOT = -3430
034628 Wp = 96
18369
YDOT = -6614
140134 meter/sec RA = 231
54587 deg
ZDOT = 1783
678996 TA = 191
15093
MA = 191
17768
Ha = 219
039 n
mi
Hp = 213
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14517130
51 X = -4410366
92
Y = 3061194
40 feet Y = 883652
02 meter
Z = -16587567
58 Z = -5077349
98
XDOT = -11253
394448 XDOT = -3364
483092
YDOT = -21699
934824 feet/sec YDOT = -6652
130651 meter/sec
ZDOT = 5851
965209 ZDOT = 1767
175528
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12723475
13 X = 3878115
22
Y = 7426597
21 feet Y = 2263626
83 meter
Z = -16680054
61 Z = -5084080
65
XDOT = -5694
444141 XDOT = -1735
666574
YDOT = 22724
903457 feet/sec YDOT = 6926
550574 meter/sec
ZDOT = 5782
126015 ZDOT = 1762
392009
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
54560730
00016717 00000-0 10270-3 0 9051
2 25544 51
6420 232
5122 0002024 332
7720 27
3326 15
55230408 34631
Satellite: ISS
Catalog Number: 25544
Epoch time: 15210
54560730 = yrday
fracday
Element set: 905
Inclination: 51
6420 deg
RA of node: 232
5122 deg
Eccentricity:
0002024
Arg of perigee: 332
7720 deg
Mean anomaly: 27
3326 deg
Mean motion: 15
55230408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3463
Checksum: 256
Coasting Arc #7 (Orbit 3478)
---------------------------------------
Vector Time (GMT): 2015/211/12:46:54
460
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5352147
40 A = 6778894
44 meter
Y = 944171
31 meter E =
0010492
Z = 4046496
05 I = 51
36778
XDOT = 1800
932421 Wp = 66
13512
YDOT = 6381
247477 meter/sec RA = 226
52120 deg
ZDOT = -3858
857080 TA = 64
00272
MA = 63
89470
Ha = 218
946 n
mi
Hp = 213
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17559538
71 X = 5321535
71
Y = 3097674
91 feet Y = 1003851
12 meter
Z = 13275905
67 Z = 4072420
92
XDOT = 5908
570935 XDOT = 1748
186421
YDOT = 20935
851301 feet/sec YDOT = 6401
092010 meter/sec
ZDOT = -12660
292256 ZDOT = -3850
236386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11089301
76 X = -3380019
18
Y = -13856064
40 feet Y = -4223328
43 meter
Z = 13387289
75 Z = 4080445
92
XDOT = 8297
725320 XDOT = 2529
146677
YDOT = -18876
113878 feet/sec YDOT = -5753
439510 meter/sec
ZDOT = -12624
308362 ZDOT = -3847
889189
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
57369222
00016717 00000-0 10270-3 0 9069
2 25544 51
6405 227
3774 0002091 338
4322 21
6743 15
55285458 34796
Satellite: ISS
Catalog Number: 25544
Epoch time: 15211
57369222 = yrday
fracday
Element set: 906
Inclination: 51
6405 deg
RA of node: 227
3774 deg
Eccentricity:
0002091
Arg of perigee: 338
4322 deg
Mean anomaly: 21
6743 deg
Mean motion: 15
55285458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3479
Checksum: 309
Coasting Arc #8 (Orbit 3493)
---------------------------------------
Vector Time (GMT): 2015/212/12:46:54
460
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5798047
41 A = 6783369
84 meter
Y = -2540975
67 meter E =
0006566
Z = -2431033
74 I = 51
40530
XDOT = 187
299143 Wp = 32
66071
YDOT = -5512
404241 meter/sec RA = 221
51404 deg
ZDOT = 5327
142057 TA = 300
03690
MA = 300
10202
Ha = 219
066 n
mi
Hp = 212
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19022465
26 X = -5757393
91
Y = -8336534
35 feet Y = -2605585
83 meter
Z = -7975832
47 Z = -2459100
24
XDOT = 614
498501 XDOT = 223
049592
YDOT = -18085
315750 feet/sec YDOT = -5510
110071 meter/sec
ZDOT = 17477
500186 ZDOT = 5328
138498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9080466
71 X = 2767726
25
Y = 18626942
63 feet Y = 5677492
11 meter
Z = -8096173
51 Z = -2467713
69
XDOT = -10718
701855 XDOT = -3267
060325
YDOT = 12807
041707 feet/sec YDOT = 3903
586312 meter/sec
ZDOT = 17482
734220 ZDOT = 5328
737390
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
53751387
00016717 00000-0 10270-3 0 9074
2 25544 51
6405 222
5645 0002038 344
9284 15
1809 15
55288420 34940
Satellite: ISS
Catalog Number: 25544
Epoch time: 15212
53751387 = yrday
fracday
Element set: 907
Inclination: 51
6405 deg
RA of node: 222
5645 deg
Eccentricity:
0002038
Arg of perigee: 344
9284 deg
Mean anomaly: 15
1809 deg
Mean motion: 15
55288420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3494
Checksum: 308
Coasting Arc #9 (Orbit 3509)
---------------------------------------
Vector Time (GMT): 2015/213/12:46:54
460
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5624625
74 A = 6785843
07 meter
Y = 3766432
92 meter E =
0011219
Z = 401756
08 I = 51
43740
XDOT = -2364
319262 Wp = 123
77073
YDOT = 4180
754752 meter/sec RA = 216
51954 deg
ZDOT = -5979
366224 TA = 51
88385
MA = 51
78275
Ha = 219
163 n
mi
Hp = 212
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18453496
51 X = 5580139
01
Y = 12357063
38 feet Y = 3829082
43 meter
Z = 1318097
37 Z = 428970
80
XDOT = -7756
952958 XDOT = -2381
848905
YDOT = 13716
386981 feet/sec YDOT = 4154
217481 meter/sec
ZDOT = -19617
343255 ZDOT = -5990
893858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6445884
57 X = -1964705
62
Y = -21245198
83 feet Y = -6475536
60 meter
Z = 1434583
00 Z = 437260
90
XDOT = 13043
213996 XDOT = 3975
571626
YDOT = -5308
669455 feet/sec YDOT = -1618
082450 meter/sec
ZDOT = -19667
663610 ZDOT = -5994
703868
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
56558029
00016717 00000-0 10270-3 0 9087
2 25544 51
6399 217
4291 0002191 348
0934 12
0167 15
55300494 35107
Satellite: ISS
Catalog Number: 25544
Epoch time: 15213
56558029 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 217
4291 deg
Eccentricity:
0002191
Arg of perigee: 348
0934 deg
Mean anomaly: 12
0167 deg
Mean motion: 15
55300494 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3510
Checksum: 298
Coasting Arc #10 (Orbit 3525)
---------------------------------------
Vector Time (GMT): 2015/214/12:46:54
460
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4791059
34 A = 6784646
28 meter
Y = -4494676
73 meter E =
0014535
Z = 1664118
60 I = 51
45991
XDOT = 4432
184993 Wp = 56
08341
YDOT = -2604
880644 meter/sec RA = 211
53044 deg
ZDOT = 5697
012357 TA = 322
21375
MA = 322
31571
Ha = 219
061 n
mi
Hp = 212
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15718698
64 X = -4748526
20
Y = -14746314
75 feet Y = -4548015
69 meter
Z = 5459706
70 Z = 1640948
38
XDOT = 14541
289347 XDOT = 4433
310626
YDOT = -8546
196340 feet/sec YDOT = -2555
310740 meter/sec
ZDOT = 18690
985422 ZDOT = 5718
545330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3217650
48 X = 980739
87
Y = 21336563
69 feet Y = 6503384
61 meter
Z = 5360732
99 Z = 1633951
42
XDOT = -15057
082586 XDOT = -4589
398772
YDOT = -2472
097936 feet/sec YDOT = -753
495451 meter/sec
ZDOT = 18784
102610 ZDOT = 5725
394475
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
59363461
00016717 00000-0 10270-3 0 9096
2 25544 51
6399 212
2950 0002027 346
8896 13
2204 15
55351881 35261
Satellite: ISS
Catalog Number: 25544
Epoch time: 15214
59363461 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 212
2950 deg
Eccentricity:
0002027
Arg of perigee: 346
8896 deg
Mean anomaly: 13
2204 deg
Mean motion: 15
55351881 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3526
Checksum: 311
Coasting Arc #11 (Orbit 3540)
---------------------------------------
Vector Time (GMT): 2015/215/12:46:54
460
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3313138
64 A = 6780724
76 meter
Y = 4772069
44 meter E =
0005432
Z = -3503596
15 I = 51
47421
XDOT = -6126
808501 Wp = 62
79223
YDOT = 949
049383 meter/sec RA = 206
53275 deg
ZDOT = -4504
053464 TA = 158
51758
MA = 158
49477
Ha = 219
236 n
mi
Hp = 212
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10869877
42 X = 3276548
82
Y = 15656395
80 feet Y = 4808914
49 meter
Z = -11494738
01 Z = -3487590
79
XDOT = -20101
077758 XDOT = -6115
087028
YDOT = 3113
679078 feet/sec YDOT = 880
600860 meter/sec
ZDOT = -14777
078293 ZDOT = -4533
787324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 792231
40 X = 241472
13
Y = -19084295
16 feet Y = -5816893
16 meter
Z = -11426636
17 Z = -3482838
70
XDOT = 16403
872255 XDOT = 4999
900263
YDOT = 9599
561458 feet/sec YDOT = 2925
946332 meter/sec
ZDOT = -14905
225237 ZDOT = -4543
112652
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
55743019
00016717 00000-0 10270-3 0 9106
2 25544 51
6400 207
4805 0002258 354
7469 5
3660 15
55318818 35417
Satellite: ISS
Catalog Number: 25544
Epoch time: 15215
55743019 = yrday
fracday
Element set: 910
Inclination: 51
6400 deg
RA of node: 207
4805 deg
Eccentricity:
0002258
Arg of perigee: 354
7469 deg
Mean anomaly: 5
3660 deg
Mean motion: 15
55318818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3541
Checksum: 297
Coasting Arc #12 (Orbit 3556)
---------------------------------------
Vector Time (GMT): 2015/216/12:46:54
460
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1352752
08 A = 6776124
67 meter
Y = -4613749
36 meter E =
0006508
Z = 4769892
08 I = 51
48828
XDOT = 7189
694742 Wp = 101
73781
YDOT = 599
171301 meter/sec RA = 201
52313 deg
ZDOT = 2614
249441 TA = 322
42983
MA = 322
47529
Ha = 219
178 n
mi
Hp = 212
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4438163
00 X = -1324229
51
Y = -15136972
97 feet Y = -4628717
16 meter
Z = 15649252
21 Z = 4763390
12
XDOT = 23588
237344 XDOT = 7169
761443
YDOT = 1965
785108 feet/sec YDOT = 679
459783 meter/sec
ZDOT = 8576
933862 ZDOT = 2649
126674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5314866
34 X = -1619971
26
Y = 14880486
78 feet Y = 4535572
37 meter
Z = 15622024
36 Z = 4761593
03
XDOT = -16704
511502 XDOT = -5091
535106
YDOT = -15143
131380 feet/sec YDOT = -4615
626445 meter/sec
ZDOT = 8726
976755 ZDOT = 2659
982515
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
58546572
00016717 00000-0 10270-3 0 9116
2 25544 51
6402 202
3465 0002324 353
1610 6
9511 15
55353913 35574
Satellite: ISS
Catalog Number: 25544
Epoch time: 15216
58546572 = yrday
fracday
Element set: 911
Inclination: 51
6402 deg
RA of node: 202
3465 deg
Eccentricity:
0002324
Arg of perigee: 353
1610 deg
Mean anomaly: 6
9511 deg
Mean motion: 15
55353913 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3557
Checksum: 284
Coasting Arc #13 (Orbit 3571)
---------------------------------------
Vector Time (GMT): 2015/217/12:46:54
460
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -875263
19 A = 6773865
59 meter
Y = 4138789
87 meter E =
0015114
Z = -5303480
93 I = 51
51092
XDOT = -7401
909629 Wp = 78
79420
YDOT = -1947
385821 meter/sec RA = 196
50212 deg
ZDOT = -295
987073 TA = 188
36335
MA = 188
38857
Ha = 219
280 n
mi
Hp = 212
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2871598
39 X = -895717
03
Y = 13578706
92 feet Y = 4128887
67 meter
Z = -17399871
82 Z = -5307782
48
XDOT = -24284
480409 XDOT = -7378
145587
YDOT = -6389
061093 feet/sec YDOT = -2030
025966 meter/sec
ZDOT = -971
086198 ZDOT = -331
885994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10108439
76 X = 3081052
44
Y = -9475138
62 feet Y = -2888022
25 meter
Z = -17419072
65 Z = -5309333
34
XDOT = 15411
203202 XDOT = 4697
334736
YDOT = 18523
041927 feet/sec YDOT = 5645
823179 meter/sec
ZDOT = -1125
320116 ZDOT = -342
997571
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
54924097
00016717 00000-0 10270-3 0 9126
2 25544 51
6405 197
5324 0002361 359
8910
2243 15
55342070 35721
Satellite: ISS
Catalog Number: 25544
Epoch time: 15217
54924097 = yrday
fracday
Element set: 912
Inclination: 51
6405 deg
RA of node: 197
5324 deg
Eccentricity:
0002361
Arg of perigee: 359
8910 deg
Mean anomaly:
2243 deg
Mean motion: 15
55342070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3572
Checksum: 291
Coasting Arc #14 (Orbit 3587)
---------------------------------------
Vector Time (GMT): 2015/218/12:46:54
460
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3087633
76 A = 6775122
10 meter
Y = -3404393
27 meter E =
0007652
Z = 4975227
43 I = 51
54640
XDOT = 6725
790167 Wp = 41
98207
YDOT = 3050
887515 meter/sec RA = 191
48235 deg
ZDOT = -2078
983666 TA = 68
30237
MA = 68
22091
Ha = 219
186 n
mi
Hp = 212
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10130032
02 X = 3101305
44
Y = -11169269
26 feet Y = -3369788
88 meter
Z = 16322924
63 Z = 4990259
63
XDOT = 22066
240707 XDOT = 6701
273372
YDOT = 10009
473474 feet/sec YDOT = 3125
962635 meter/sec
ZDOT = -6820
812552 ZDOT = -2046
370906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14580152
94 X = -4444030
62
Y = 3557208
83 feet Y = 1084237
25 meter
Z = 16388209
13 Z = 4995126
14
XDOT = -12338
202248 XDOT = -3760
684045
YDOT = -19680
429247 feet/sec YDOT = -5998
594834 meter/sec
ZDOT = -6680
892762 ZDOT = -2036
336114
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
57725668
00016717 00000-0 10270-3 0 9134
2 25544 51
6406 192
3983 0002422 1
8016 358
3146 15
55366511 35887
Satellite: ISS
Catalog Number: 25544
Epoch time: 15218
57725668 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 192
3983 deg
Eccentricity:
0002422
Arg of perigee: 1
8016 deg
Mean anomaly: 358
3146 deg
Mean motion: 15
55366511 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3588
Checksum: 315
Coasting Arc #15 (Orbit 3589)
---------------------------------------
Vector Time (GMT): 2015/218/16:30:03
013
Vector Time (MET): N/A
Weight (LBS) : 905859
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 563785
79 A = 6775477
21 meter
Y = 4313730
96 meter E =
0012965
Z = -5205708
42 I = 51
55121
XDOT = -7551
539853 Wp = 72
36127
YDOT = -462
303732 meter/sec RA = 190
73525 deg
ZDOT = -1199
556198 TA = 186
09660
MA = 186
11240
Ha = 219
268 n
mi
Hp = 213
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1849690
91 X = 540793
88
Y = 14152660
63 feet Y = 4319907
04 meter
Z = -17079095
87 Z = -5203025
52
XDOT = -24775
393219 XDOT = -7539
982069
YDOT = -1516
744529 feet/sec YDOT = -546
685384 meter/sec
ZDOT = -3935
551832 ZDOT = -1236
211739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7022762
22 X = -2140537
93
Y = -12440667
76 feet Y = -3791915
53 meter
Z = -17068253
32 Z = -5202403
61
XDOT = 22667
792583 XDOT = 6909
143179
YDOT = -7173
874571 feet/sec YDOT = -2186
596969 meter/sec
ZDOT = -4093
307196 ZDOT = -1247
640033
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
70576011
00016717 00000-0 10270-3 0 9146
2 25544 51
6436 191
7575 0002297 317
4403 42
6572 15
54951206 35905
Satellite: ISS
Catalog Number: 25544
Epoch time: 15218
70576011 = yrday
fracday
Element set: 914
Inclination: 51
6436 deg
RA of node: 191
7575 deg
Eccentricity:
0002297
Arg of perigee: 317
4403 deg
Mean anomaly: 42
6572 deg
Mean motion: 15
54951206 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3590
Checksum: 305
Coasting Arc #16 (Orbit 3605)
---------------------------------------
Vector Time (GMT): 2015/219/16:30:03
013
Vector Time (MET): N/A
Weight (LBS) : 905859
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1585582
11 A = 6775175
99 meter
Y = -4007498
31 meter E =
0003995
Z = 5227019
54 I = 51
58171
XDOT = 7434
376524 Wp = 21
25652
YDOT = 1576
112400 meter/sec RA = 185
72135 deg
ZDOT = -1042
886276 TA = 78
75866
MA = 78
71377
Ha = 219
144 n
mi
Hp = 213
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5202041
03 X = 1604886
38
Y = -13147960
34 feet Y = -3989659
44 meter
Z = 17149014
23 Z = 5234768
75
XDOT = 24390
999095 XDOT = 7421
265426
YDOT = 5170
972442 feet/sec YDOT = 1659
175188 meter/sec
ZDOT = -3421
542901 ZDOT = -1006
803638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 338393
06 X = 103142
21
Y = 14094228
02 feet Y = 4295920
70 meter
Z = 17183044
19 Z = 5237391
87
XDOT = -23500
972919 XDOT = -7163
096546
YDOT = 4562
061304 feet/sec YDOT = 1390
516286 meter/sec
ZDOT = -3266
418678 ZDOT = -995
604413
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
73405354
00016717 00000-0 10270-3 0 9152
2 25544 51
6432 186
6250 0002443 318
2701 41
8266 15
54987338 36061
Satellite: ISS
Catalog Number: 25544
Epoch time: 15219
73405354 = yrday
fracday
Element set: 915
Inclination: 51
6432 deg
RA of node: 186
6250 deg
Eccentricity:
0002443
Arg of perigee: 318
2701 deg
Mean anomaly: 41
8266 deg
Mean motion: 15
54987338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3606
Checksum: 307
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