[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 24th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18298 65 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 2917)
---------------------------------------
Vector Time (GMT): 2015/175/11:19:27
751
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 733418
85 A = 6778952
95 meter
Y = 5404943
56 meter E =
0013815
Z = 4014874
24 I = 51
91200
XDOT = -6219
606088 Wp = 97
68049
YDOT = -2114
285456 meter/sec RA = 47
03947 deg
ZDOT = 3969
034761 TA = 311
18552
MA = 311
30457
Ha = 220
240 n
mi
Hp = 211
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2406229
82 X = 653422
24
Y = 17732754
45 feet Y = 5412697
53 meter
Z = 13172159
59 Z = 4018243
15
XDOT = -20405
531786 XDOT = -6214
781445
YDOT = -6936
632074 feet/sec YDOT = -2183
810492 meter/sec
ZDOT = 13021
767589 ZDOT = 3938
832714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17881383
04 X = 5450245
55
Y = 379319
88 feet Y = 115616
70 meter
Z = 13185543
88 Z = 4018953
78
XDOT = -9918
928574 XDOT = -3023
289429
YDOT = 17903
444747 feet/sec YDOT = 5456
969959 meter/sec
ZDOT = 12892
288602 ZDOT = 3929
569566
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 15175
52733347
00016717 00000-0 10270-3 0 9000
2 25544 51
6447 47
3829 0003102 85
5264 274
6243 15
55336222 29180
Satellite: ISS
Catalog Number: 25544
Epoch time: 15175
52733347 = yrday
fracday
Element set: 900
Inclination: 51
6447 deg
RA of node: 47
3829 deg
Eccentricity:
0003102
Arg of perigee: 85
5264 deg
Mean anomaly: 274
6243 deg
Mean motion: 15
55336222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2918
Checksum: 304
Coasting Arc #2 (Orbit 2932)
---------------------------------------
Vector Time (GMT): 2015/176/11:19:27
751
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1111966
38 A = 6774754
06 meter
Y = -4362612
30 meter E =
0015998
Z = -5076868
26 I = 51
87609
XDOT = 6386
952300 Wp = 78
01752
YDOT = 3793
143747 meter/sec RA = 42
05220 deg
ZDOT = -1862
302193 TA = 173
98611
MA = 173
96688
Ha = 220
054 n
mi
Hp = 211
648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3648183
68 X = 1185329
07
Y = -14313032
48 feet Y = -4349766
96 meter
Z = -16656391
92 Z = -5071288
69
XDOT = 20954
567912 XDOT = 6353
108141
YDOT = 12444
697332 feet/sec YDOT = 3864
377744 meter/sec
ZDOT = -6109
915331 ZDOT = -1831
357479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13683472
60 X = -4170722
45
Y = -5635915
33 feet Y = -1717826
99 meter
Z = -16631493
34 Z = -5069279
17
XDOT = 14730
497991 XDOT = 4489
855788
YDOT = -18141
139049 feet/sec YDOT = -5529
419182 meter/sec
ZDOT = -5977
595621 ZDOT = -1821
971145
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 15176
49109451
00016717 00000-0 10270-3 0 9011
2 25544 51
6446 42
5692 0002881 87
6586 272
4898 15
55400640 29332
Satellite: ISS
Catalog Number: 25544
Epoch time: 15176
49109451 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 42
5692 deg
Eccentricity:
0002881
Arg of perigee: 87
6586 deg
Mean anomaly: 272
4898 deg
Mean motion: 15
55400640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2933
Checksum: 327
Coasting Arc #3 (Orbit 2948)
---------------------------------------
Vector Time (GMT): 2015/177/11:19:27
751
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2991666
26 A = 6773650
12 meter
Y = 2960644
71 meter E =
0005522
Z = 5302663
28 I = 51
84877
XDOT = -5846
716828 Wp = 78
75629
YDOT = -4943
234415 meter/sec RA = 37
05445 deg
ZDOT = -537
123897 TA = 16
35826
MA = 16
34044
Ha = 220
085 n
mi
Hp = 211
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9815178
01 X = -3050308
98
Y = 9713401
27 feet Y = 2926861
58 meter
Z = 17397189
26 Z = 5287988
12
XDOT = -19182
141825 XDOT = -5788
396700
YDOT = -16217
960678 feet/sec YDOT = -5008
290096 meter/sec
ZDOT = -1762
217511 ZDOT = -565
384989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8489737
64 X = 2587672
03
Y = 10992077
45 feet Y = 3350385
21 meter
Z = 17333455
10 Z = 5283237
11
XDOT = -17543
874988 XDOT = -5347
373096
YDOT = 16526
842080 feet/sec YDOT = 5037
381466 meter/sec
ZDOT = -1882
745651 ZDOT = -573
860875
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 15177
51908547
00016717 00000-0 10270-3 0 9029
2 25544 51
6449 37
4348 0002809 92
1754 267
9721 15
55434617 29496
Satellite: ISS
Catalog Number: 25544
Epoch time: 15177
51908547 = yrday
fracday
Element set: 902
Inclination: 51
6449 deg
RA of node: 37
4348 deg
Eccentricity:
0002809
Arg of perigee: 92
1754 deg
Mean anomaly: 267
9721 deg
Mean motion: 15
55434617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2949
Checksum: 339
Coasting Arc #4 (Orbit 2963)
---------------------------------------
Vector Time (GMT): 2015/178/11:19:27
751
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4685918
27 A = 6776234
75 meter
Y = -1421372
35 meter E =
0013190
Z = -4696562
80 I = 51
83088
XDOT = 4523
023192 Wp = 106
13466
YDOT = 5482
066836 meter/sec RA = 32
05666 deg
ZDOT = 2856
754461 TA = 192
16867
MA = 192
20056
Ha = 219
900 n
mi
Hp = 211
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15373747
62 X = 4724278
37
Y = -4663295
12 feet Y = -1368756
38 meter
Z = -15408670
59 Z = -4673706
39
XDOT = 14839
314934 XDOT = 4447
508144
YDOT = 17985
783582 feet/sec YDOT = 5532
223721 meter/sec
ZDOT = 9372
554007 ZDOT = 2878
543668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3099756
23 X = -944805
70
Y = -15859346
76 feet Y = -4833928
89 meter
Z = -15310068
53 Z = -4666508
89
XDOT = 18213
446616 XDOT = 5551
458529
YDOT = -12687
357044 feet/sec YDOT = -3867
106427 meter/sec
ZDOT = 9465
122993 ZDOT = 2884
969488
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 15178
48280693
00016717 00000-0 10270-3 0 9032
2 25544 51
6441 32
6204 0002695 94
4063 265
7398 15
55460147 29647
Satellite: ISS
Catalog Number: 25544
Epoch time: 15178
48280693 = yrday
fracday
Element set: 903
Inclination: 51
6441 deg
RA of node: 32
6204 deg
Eccentricity:
0002695
Arg of perigee: 94
4063 deg
Mean anomaly: 265
7398 deg
Mean motion: 15
55460147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2964
Checksum: 323
Coasting Arc #5 (Orbit 2979)
---------------------------------------
Vector Time (GMT): 2015/179/11:19:27
751
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5920137
68 A = 6780787
95 meter
Y = -120199
15 meter E =
0015341
Z = 3290049
58 I = 51
81946
XDOT = -2532
686678 Wp = 92
59719
YDOT = -5479
731671 meter/sec RA = 27
07115 deg
ZDOT = -4739
186865 TA = 49
24190
MA = 49
10884
Ha = 219
856 n
mi
Hp = 211
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19423023
89 X = -5934335
48
Y = -394354
17 feet Y = -186481
78 meter
Z = 10794125
93 Z = 3261256
08
XDOT = -8309
339496 XDOT = -2448
201487
YDOT = -17978
122279 feet/sec YDOT = -5507
580880 meter/sec
ZDOT = -15548
513337 ZDOT = -4751
285665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2000453
40 X = -609738
20
Y = 19392398
29 feet Y = 5910803
00 meter
Z = 10670314
04 Z = 3252311
72
XDOT = -17181
667005 XDOT = -5236
972103
YDOT = 6844
381029 feet/sec YDOT = 2086
167338 meter/sec
ZDOT = -15599
395705 ZDOT = -4754
695811
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 15179
51075375
00016717 00000-0 10270-3 0 9047
2 25544 51
6443 27
4858 0002609 94
7317 265
4134 15
55521774 29803
Satellite: ISS
Catalog Number: 25544
Epoch time: 15179
51075375 = yrday
fracday
Element set: 904
Inclination: 51
6443 deg
RA of node: 27
4858 deg
Eccentricity:
0002609
Arg of perigee: 94
7317 deg
Mean anomaly: 265
4134 deg
Mean motion: 15
55521774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2980
Checksum: 324
Coasting Arc #6 (Orbit 2994)
---------------------------------------
Vector Time (GMT): 2015/180/11:19:27
751
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6477831
48 A = 6784574
80 meter
Y = 1467001
27 meter E =
0010236
Z = -1369563
96 I = 51
80198
XDOT = 95
083971 Wp = 49
79839
YDOT = 4985
819034 meter/sec RA = 22
09795 deg
ZDOT = 5825
386084 TA = 295
31082
MA = 295
41682
Ha = 219
784 n
mi
Hp = 211
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21252727
95 X = 6467598
51
Y = 4812996
29 feet Y = 1539383
59 meter
Z = -4493320
07 Z = -1338120
49
XDOT = 311
955284 XDOT = 11
026682
YDOT = 16357
673995 feet/sec YDOT = 4986
411542 meter/sec
ZDOT = 19112
159069 ZDOT = 5825
644495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6193343
92 X = 1887731
23
Y = -20920806
85 feet Y = -6376661
93 meter
Z = -4358398
33 Z = -1328439
81
XDOT = 14811
357852 XDOT = 4514
501873
YDOT = 427
847194 feet/sec YDOT = 130
407825 meter/sec
ZDOT = 19112
215377 ZDOT = 5825
403247
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 15180
47443474
00016717 00000-0 10270-3 0 9054
2 25544 51
6430 22
6710 0002519 99
6768 260
4670 15
55505504 29956
Satellite: ISS
Catalog Number: 25544
Epoch time: 15180
47443474 = yrday
fracday
Element set: 905
Inclination: 51
6430 deg
RA of node: 22
6710 deg
Eccentricity:
0002519
Arg of perigee: 99
6768 deg
Mean anomaly: 260
4670 deg
Mean motion: 15
55505504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2995
Checksum: 314
Coasting Arc #7 (Orbit 3010)
---------------------------------------
Vector Time (GMT): 2015/181/11:19:27
751
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6207524
15 A = 6784933
75 meter
Y = -2597807
40 meter E =
0012240
Z = -830293
78 I = 51
77330
XDOT = 2516
458196 Wp = 133
51443
YDOT = -4130
766188 meter/sec RA = 17
13166 deg
ZDOT = -5952
633462 TA = 55
45369
MA = 55
33822
Ha = 219
665 n
mi
Hp = 211
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20365892
87 X = -6173980
23
Y = -8522990
15 feet Y = -2667036
32 meter
Z = -2724060
95 Z = -860367
60
XDOT = 8256
096443 XDOT = 2591
378009
YDOT = -13552
382506 feet/sec YDOT = -4102
205734 meter/sec
ZDOT = -19529
637344 ZDOT = -5940
227640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9493972
81 X = -2893762
91
Y = 19913743
78 feet Y = 6069709
11 meter
Z = -2852849
51 Z = -869548
53
XDOT = -11682
477514 XDOT = -3560
819146
YDOT = -8331
409491 feet/sec YDOT = -2539
413613 meter/sec
ZDOT = -19475
404975 ZDOT = -5936
103436
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 15181
50233906
00016717 00000-0 10270-3 0 9067
2 25544 51
6425 17
5359 0002510 105
5361 254
6069 15
55530427 30118
Satellite: ISS
Catalog Number: 25544
Epoch time: 15181
50233906 = yrday
fracday
Element set: 906
Inclination: 51
6425 deg
RA of node: 17
5359 deg
Eccentricity:
0002510
Arg of perigee: 105
5361 deg
Mean anomaly: 254
6069 deg
Mean motion: 15
55530427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3011
Checksum: 279
Coasting Arc #8 (Orbit 3026)
---------------------------------------
Vector Time (GMT): 2015/182/11:19:27
751
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5113578
94 A = 6781512
42 meter
Y = 3405832
41 meter E =
0015429
Z = 2855543
14 I = 51
73109
XDOT = -4878
684029 Wp = 85
01265
YDOT = 3047
781513 meter/sec RA = 12
15622 deg
ZDOT = 5079
133342 TA = 307
45560
MA = 307
59585
Ha = 219
467 n
mi
Hp = 211
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16776833
79 X = 5061242
97
Y = 11173990
85 feet Y = 3462722
75 meter
Z = 9368579
84 Z = 2880257
17
XDOT = -16006
181198 XDOT = -4937
074849
YDOT = 9999
283180 feet/sec YDOT = 2992
897641 meter/sec
ZDOT = 16663
823300 ZDOT = 5055
292391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11687793
52 X = 3562439
47
Y = -16362353
09 feet Y = -4987245
22 meter
Z = 9474143
52 Z = 2887718
95
XDOT = 8303
350364 XDOT = 2530
861191
YDOT = 15561
973742 feet/sec YDOT = 4743
289597 meter/sec
ZDOT = 16560
640085 ZDOT = 5047
683098
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 15182
53021908
00016717 00000-0 10270-3 0 9079
2 25544 51
6417 12
3991 0002360 109
7381 250
4028 15
55600917 30273
Satellite: ISS
Catalog Number: 25544
Epoch time: 15182
53021908 = yrday
fracday
Element set: 907
Inclination: 51
6417 deg
RA of node: 12
3991 deg
Eccentricity:
0002360
Arg of perigee: 109
7381 deg
Mean anomaly: 250
4028 deg
Mean motion: 15
55600917 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3027
Checksum: 286
Coasting Arc #9 (Orbit 3041)
---------------------------------------
Vector Time (GMT): 2015/183/11:19:27
751
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3275441
14 A = 6776572
76 meter
Y = -3947497
95 meter E =
0011319
Z = -4439365
75 I = 51
68249
XDOT = 6665
614906 Wp = 77
21487
YDOT = -1804
776129 meter/sec RA = 7
16397 deg
ZDOT = -3317
881429 TA = 159
30579
MA = 159
25992
Ha = 219
510 n
mi
Hp = 211
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10746197
96 X = -3209491
27
Y = -12951108
77 feet Y = -3983756
70 meter
Z = -14564848
25 Z = -4455117
43
XDOT = 21868
815309 XDOT = 6701
417809
YDOT = -5921
181526 feet/sec YDOT = -1730
036204 meter/sec
ZDOT = -10885
437759 ZDOT = -3285
414769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13098331
15 X = -3992371
34
Y = 10473412
36 feet Y = 3192296
09 meter
Z = -14631751
37 Z = -4459757
82
XDOT = -4855
029207 XDOT = -1479
812902
YDOT = -21062
202959 feet/sec YDOT = -6419
759462 meter/sec
ZDOT = -10745
422680 ZDOT = -3275
204833
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 15183
49383821
00016717 00000-0 10270-3 0 9081
2 25544 51
6407 7
5838 0002463 110
6161 249
5256 15
55617076 30422
Satellite: ISS
Catalog Number: 25544
Epoch time: 15183
49383821 = yrday
fracday
Element set: 908
Inclination: 51
6407 deg
RA of node: 7
5838 deg
Eccentricity:
0002463
Arg of perigee: 110
6161 deg
Mean anomaly: 249
5256 deg
Mean motion: 15
55617076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3042
Checksum: 307
Coasting Arc #10 (Orbit 3057)
---------------------------------------
Vector Time (GMT): 2015/184/11:19:27
751
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 971281
16 A = 6773348
61 meter
Y = 4182297
07 meter E =
0005962
Z = 5234475
73 I = 51
64005
XDOT = -7592
544841 Wp = 117
70511
YDOT = 506
753503 meter/sec RA = 2
15377 deg
ZDOT = 1000
356482 TA = 322
70584
MA = 322
74721
Ha = 219
504 n
mi
Hp = 211
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3186617
99 X = 899014
75
Y = 13721447
06 feet Y = 4192753
83 meter
Z = 17173476
81 Z = 5239018
97
XDOT = -24909
924020 XDOT = -7602
506479
YDOT = 1662
577108 feet/sec YDOT = 421
792868 meter/sec
ZDOT = 3282
009457 ZDOT = 963
449727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13712536
83 X = 4179581
23
Y = -3123788
87 feet Y = -952130
85 meter
Z = 17192126
86 Z = 5240160
27
XDOT = 1519
732174 XDOT = 463
214367
YDOT = 23924
591976 feet/sec YDOT = 7292
215634 meter/sec
ZDOT = 3123
177029 ZDOT = 951
944359
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 15184
52167699
00016717 00000-0 10270-3 0 9090
2 25544 51
6409 2
4472 0002463 113
4627 246
6785 15
55605086 30580
Satellite: ISS
Catalog Number: 25544
Epoch time: 15184
52167699 = yrday
fracday
Element set: 909
Inclination: 51
6409 deg
RA of node: 2
4472 deg
Eccentricity:
0002463
Arg of perigee: 113
4627 deg
Mean anomaly: 246
6785 deg
Mean motion: 15
55605086 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3058
Checksum: 324
Coasting Arc #11 (Orbit 3072)
---------------------------------------
Vector Time (GMT): 2015/185/11:19:27
751
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1497906
96 A = 6773638
07 meter
Y = -4158321
99 meter E =
0016018
Z = -5147223
01 I = 51
60943
XDOT = 7463
769884 Wp = 103
86218
YDOT = 822
577019 meter/sec RA = 357
13517 deg
ZDOT = 1507
703543 TA = 180
68290
MA = 180
68509
Ha = 219
390 n
mi
Hp = 211
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4914392
91 X = 1569297
88
Y = -13642788
67 feet Y = -4141171
67 meter
Z = -16887214
59 Z = -5139773
63
XDOT = 24487
434004 XDOT = 7446
693163
YDOT = 2698
743500 feet/sec YDOT = 905
946134 meter/sec
ZDOT = 4946
533933 ZDOT = 1543
919152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13744910
58 X = -4189448
74
Y = -4739732
43 feet Y = -1444670
45 meter
Z = -16854296
98 Z = -5137189
72
XDOT = 1849
323918 XDOT = 563
673930
YDOT = -23503
551937 feet/sec YDOT = -7163
882630 meter/sec
ZDOT = 5102
108427 ZDOT = 1555
122649
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 15185
48525269
00016717 00000-0 10270-3 0 9109
2 25544 51
6405 357
6311 0002477 118
4876 241
6527 15
55682611 30734
Satellite: ISS
Catalog Number: 25544
Epoch time: 15185
48525269 = yrday
fracday
Element set: 910
Inclination: 51
6405 deg
RA of node: 357
6311 deg
Eccentricity:
0002477
Arg of perigee: 118
4876 deg
Mean anomaly: 241
6527 deg
Mean motion: 15
55682611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3073
Checksum: 317
Coasting Arc #12 (Orbit 3088)
---------------------------------------
Vector Time (GMT): 2015/186/11:19:27
751
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3761309
92 A = 6777577
63 meter
Y = 3826699
88 meter E =
0012236
Z = 4130951
54 I = 51
59130
XDOT = -6332
848335 Wp = 84
01613
YDOT = -2142
147725 meter/sec RA = 352
12376 deg
ZDOT = -3770
953893 TA = 44
86040
MA = 44
76156
Ha = 219
360 n
mi
Hp = 211
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12340255
66 X = -3823887
76
Y = 12554789
63 feet Y = 3784288
18 meter
Z = 13552990
61 Z = 4112528
45
XDOT = -20777
061467 XDOT = -6290
106055
YDOT = -7028
043716 feet/sec YDOT = -2212
726459 meter/sec
ZDOT = -12371
895973 ZDOT = -3801
613552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13016689
45 X = 3967486
94
Y = 11942924
83 feet Y = 3640203
49 meter
Z = 13472956
21 Z = 4106557
05
XDOT = -5371
104688 XDOT = -1637
112709
YDOT = 19999
521781 feet/sec YDOT = 6095
854239 meter/sec
ZDOT = -12503
294076 ZDOT = -3811
004034
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 15186
51304563
00016717 00000-0 10270-3 0 9117
2 25544 51
6408 352
4950 0002326 123
0362 237
1015 15
55704073 30890
Satellite: ISS
Catalog Number: 25544
Epoch time: 15186
51304563 = yrday
fracday
Element set: 911
Inclination: 51
6408 deg
RA of node: 352
4950 deg
Eccentricity:
0002326
Arg of perigee: 123
0362 deg
Mean anomaly: 237
1015 deg
Mean motion: 15
55704073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3089
Checksum: 281
Coasting Arc #13 (Orbit 3103)
---------------------------------------
Vector Time (GMT): 2015/187/11:19:27
751
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5469578
43 A = 6782233
46 meter
Y = -3208472
04 meter E =
0006561
Z = -2406724
18 I = 51
57626
XDOT = 4327
134691 Wp = 67
10660
YDOT = 3369
454949 meter/sec RA = 347
12615 deg
ZDOT = 5356
173309 TA = 265
96164
MA = 266
03664
Ha = 219
262 n
mi
Hp = 211
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17944811
12 X = 5516740
63
Y = -10526483
08 feet Y = -3147043
76 meter
Z = -7896076
72 Z = -2380040
06
XDOT = 14196
636125 XDOT = 4263
117098
YDOT = 11054
642221 feet/sec YDOT = 3417
485475 meter/sec
ZDOT = 17572
747077 ZDOT = 5377
038166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11500546
72 X = -3505366
64
Y = -17388787
94 feet Y = -5300102
56 meter
Z = -7780655
42 Z = -2371543
77
XDOT = 8997
276614 XDOT = 2742
369912
YDOT = -13832
325955 feet/sec YDOT = -4216
092951 meter/sec
ZDOT = 17661
763037 ZDOT = 5383
305374
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 15187
47658136
00016717 00000-0 10270-3 0 9122
2 25544 51
6411 347
6793 0002450 125
4678 234
6704 15
55747404 31049
Satellite: ISS
Catalog Number: 25544
Epoch time: 15187
47658136 = yrday
fracday
Element set: 912
Inclination: 51
6411 deg
RA of node: 347
6793 deg
Eccentricity:
0002450
Arg of perigee: 125
4678 deg
Mean anomaly: 234
6704 deg
Mean motion: 15
55747404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3104
Checksum: 315
Coasting Arc #14 (Orbit 3119)
---------------------------------------
Vector Time (GMT): 2015/188/11:19:27
751
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6395891
72 A = 6784395
97 meter
Y = 2232838
37 meter E =
0014599
Z = 206297
46 I = 51
55337
XDOT = -1753
473775 Wp = 131
21867
YDOT = -4443
346743 meter/sec RA = 342
14100 deg
ZDOT = -6004
396294 TA = 46
55399
MA = 46
43263
Ha = 219
017 n
mi
Hp = 211
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20983896
73 X = -6421386
61
Y = 7325585
19 feet Y = 2161172
75 meter
Z = 676828
94 Z = 175165
98
XDOT = -5752
866717 XDOT = -1674
490066
YDOT = -14577
909262 feet/sec YDOT = -4462
513241 meter/sec
ZDOT = -19699
462908 ZDOT = -6012
722679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8820646
57 X = 2688533
07
Y = 20404609
98 feet Y = 6219325
12 meter
Z = 542497
41 Z = 165353
21
XDOT = -12647
873414 XDOT = -3855
071817
YDOT = 6021
233741 feet/sec YDOT = 1835
272044 meter/sec
ZDOT = -19734
336771 ZDOT = -6015
025848
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 15188
50432886
00016717 00000-0 10270-3 0 9130
2 25544 51
6409 342
5429 0002188 124
5769 235
5602 15
55823765 31205
Satellite: ISS
Catalog Number: 25544
Epoch time: 15188
50432886 = yrday
fracday
Element set: 913
Inclination: 51
6409 deg
RA of node: 342
5429 deg
Eccentricity:
0002188
Arg of perigee: 124
5769 deg
Mean anomaly: 235
5602 deg
Mean motion: 15
55823765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3120
Checksum: 319
Coasting Arc #15 (Orbit 3135)
---------------------------------------
Vector Time (GMT): 2015/189/11:19:27
751
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6401577
67 A = 6782634
20 meter
Y = -972421
02 meter E =
0015176
Z = 1999253
75 I = 51
51784
XDOT = -956
787512 Wp = 76
57819
YDOT = 5199
629654 meter/sec RA = 337
15445 deg
ZDOT = 5560
597149 TA = 305
56230
MA = 305
70367
Ha = 219
019 n
mi
Hp = 211
284
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21002551
41 X = 6402264
17
Y = -3190357
67 feet Y = -900830
67 meter
Z = 6559231
46 Z = 2030352
79
XDOT = -3139
066641 XDOT = -1041
871037
YDOT = 17059
152407 feet/sec YDOT = 5188
454153 meter/sec
ZDOT = 18243
428967 ZDOT = 5555
742955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5048494
34 X = -1538781
08
Y = -20591830
70 feet Y = -6276390
00 meter
Z = 6693151
60 Z = 2040072
61
XDOT = 15781
780802 XDOT = 4810
286789
YDOT = 2087
001596 feet/sec YDOT = 636
118086 meter/sec
ZDOT = 18221
473092 ZDOT = 5553
904998
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 15189
53205531
00016717 00000-0 10270-3 0 9140
2 25544 51
6411 337
4062 0002405 132
5544 227
5813 15
55826371 31364
Satellite: ISS
Catalog Number: 25544
Epoch time: 15189
53205531 = yrday
fracday
Element set: 914
Inclination: 51
6411 deg
RA of node: 337
4062 deg
Eccentricity:
0002405
Arg of perigee: 132
5544 deg
Mean anomaly: 227
5813 deg
Mean motion: 15
55826371 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3136
Checksum: 288
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