[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 22nd 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7534 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 2 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
202/21:41:30
000 0
0 0
0 0
0
N/A 0
0 0
0 225
3
000/00:00:00
000 0
0 0
0 223
0
205/03:28:03
000 0
0 0
0 0
0
N/A 0
0 0
0 225
8
000/00:00:00
000 0
0 0
0 223
0
Coasting Arc #1 (Orbit 1664)
---------------------------------------
Vector Time (GMT): 2014/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1681923
61 A = 6793910
53 meter
Y = -5177928
15 meter E =
0001977
Z = -4066343
41 I = 51
30480
XDOT = 4797
957237 Wp = 143
61989
YDOT = -4572
214500 meter/sec RA = 288
75185 deg
ZDOT = 3836
952574 TA = 166
31976
MA = 166
31440
Ha = 225
228 n
mi
Hp = 222
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5518122
08 X = -1604144
99
Y = -16987953
24 feet Y = -5196301
27 meter
Z = -13341021
68 Z = -4074325
42
XDOT = 15741
329518 XDOT = 4830
089650
YDOT = -15000
703741 feet/sec YDOT = -4518
381316 meter/sec
ZDOT = 12588
427081 ZDOT = 3860
337861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12371247
61 X = -3770756
27
Y = 12849625
49 feet Y = 3916565
85 meter
Z = -13373946
44 Z = -4076378
87
XDOT = -19700
629022 XDOT = -6004
751726
YDOT = -5758
955158 feet/sec YDOT = -1755
329532 meter/sec
ZDOT = 12688
457106 ZDOT = 3867
441726
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 14202
50894293
00016717 00000-0 10270-3 0 9006
2 25544 51
6479 289
4639 0005751 277
0816 82
9675 15
50150073 16656
Satellite: ISS
Catalog Number: 25544
Epoch time: 14202
50894293 = yrday
fracday
Element set: 900
Inclination: 51
6479 deg
RA of node: 289
4639 deg
Eccentricity:
0005751
Arg of perigee: 277
0816 deg
Mean anomaly: 82
9675 deg
Mean motion: 15
50150073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1665
Checksum: 326
Coasting Arc #2 (Orbit 1671)
---------------------------------------
Vector Time (GMT): 2014/202/21:41:30
000
Vector Time (MET): N/A
Weight (LBS) : 884340
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4260627
69 A = 6794926
62 meter
Y = -3736357
74 meter E =
0005865
Z = 3744254
83 I = 51
30280
XDOT = 1680
798166 Wp = 89
99840
YDOT = 6162
796451 meter/sec RA = 286
79335 deg
ZDOT = 4231
431596 TA = 314
93894
MA = 314
98650
Ha = 225
347 n
mi
Hp = 223
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13978437
31 X = 4283903
61
Y = -12258391
54 feet Y = -3688582
85 meter
Z = 12284300
61 Z = 3765008
39
XDOT = 5514
429677 XDOT = 1591
204685
YDOT = 20219
148460 feet/sec YDOT = 6181
090898 meter/sec
ZDOT = 13882
649593 ZDOT = 4239
379539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10769310
88 X = 3282485
96
Y = 15083081
99 feet Y = 4597323
39 meter
Z = 12373014
79 Z = 3771294
91
XDOT = -19569
961151 XDOT = -5964
924159
YDOT = 2542
507413 feet/sec YDOT = 774
956259 meter/sec
ZDOT = 13915
255324 ZDOT = 4241
369823
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 14202
96021934
00016717 00000-0 10270-3 0 9011
2 25544 51
6465 287
2289 0005755 283
1809 76
8699 15
50146672 16728
Satellite: ISS
Catalog Number: 25544
Epoch time: 14202
96021934 = yrday
fracday
Element set: 901
Inclination: 51
6465 deg
RA of node: 287
2289 deg
Eccentricity:
0005755
Arg of perigee: 283
1809 deg
Mean anomaly: 76
8699 deg
Mean motion: 15
50146672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1672
Checksum: 333
Coasting Arc #3 (Orbit 1686)
---------------------------------------
Vector Time (GMT): 2014/203/21:41:30
000
Vector Time (MET): N/A
Weight (LBS) : 884340
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4058075
96 A = 6794022
45 meter
Y = 3689289
19 meter E =
0004203
Z = -4014086
31 I = 51
29210
XDOT = -1875
670823 Wp = 17
40952
YDOT = -6314
069646 meter/sec RA = 281
81386 deg
ZDOT = -3904
074518 TA = 211
77908
MA = 211
80445
Ha = 225
707 n
mi
Hp = 222
910
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13313897
50 X = -4079529
91
Y = 12103967
16 feet Y = 3643789
59 meter
Z = -13169574
51 Z = -4033851
42
XDOT = -6153
775666 XDOT = -1785
961524
YDOT = -20715
451593 feet/sec YDOT = -6334
542646 meter/sec
ZDOT = -12808
643432 ZDOT = -3912
968856
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10930373
00 X = -3331577
69
Y = -14214772
19 feet Y = -4332662
56 meter
Z = -13254085
33 Z = -4039845
21
XDOT = 20122
477611 XDOT = 6133
331176
YDOT = -3487
228502 feet/sec YDOT = -1062
907247 meter/sec
ZDOT = -12845
247315 ZDOT = -3915
231382
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 14203
92723531
00016717 00000-0 10270-3 0 9021
2 25544 51
6468 282
4372 0005756 288
5205 71
5320 15
50155850 16878
Satellite: ISS
Catalog Number: 25544
Epoch time: 14203
92723531 = yrday
fracday
Element set: 902
Inclination: 51
6468 deg
RA of node: 282
4372 deg
Eccentricity:
0005756
Arg of perigee: 288
5205 deg
Mean anomaly: 71
5320 deg
Mean motion: 15
50155850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1687
Checksum: 303
Coasting Arc #4 (Orbit 1702)
---------------------------------------
Vector Time (GMT): 2014/204/21:41:30
000
Vector Time (MET): N/A
Weight (LBS) : 884340
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3869070
18 A = 6793150
98 meter
Y = -3610299
58 meter E =
0004157
Z = 4256376
67 I = 51
28369
XDOT = 2100
554052 Wp = 100
39718
YDOT = 6451
965211 meter/sec RA = 276
83385 deg
ZDOT = 3559
490810 TA = 313
04551
MA = 313
08031
Ha = 225
692 n
mi
Hp = 222
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12693799
81 X = 3888478
01
Y = -11844814
90 feet Y = -3566925
02 meter
Z = 13964490
40 Z = 4275218
61
XDOT = 6891
581534 XDOT = 2010
959970
YDOT = 21167
864866 feet/sec YDOT = 6474
953680 meter/sec
ZDOT = 11678
119457 ZDOT = 3569
477843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10957236
10 X = 3339765
56
Y = 13383355
53 feet Y = 4079246
77 meter
Z = 14045068
79 Z = 4280936
97
XDOT = -20608
291092 XDOT = -6281
407125
YDOT = 4560
946874 feet/sec YDOT = 1390
176607 meter/sec
ZDOT = 11719
347360 ZDOT = 3572
057075
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 14204
95871226
00016717 00000-0 10270-3 0 9031
2 25544 51
6467 277
3265 0005780 291
6654 68
3881 15
50160953 17036
Satellite: ISS
Catalog Number: 25544
Epoch time: 14204
95871226 = yrday
fracday
Element set: 903
Inclination: 51
6467 deg
RA of node: 277
3265 deg
Eccentricity:
0005780
Arg of perigee: 291
6654 deg
Mean anomaly: 68
3881 deg
Mean motion: 15
50160953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1703
Checksum: 321
Coasting Arc #5 (Orbit 1705)
---------------------------------------
Vector Time (GMT): 2014/205/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2379361
03 A = 6795400
38 meter
Y = -5253522
44 meter E =
0001495
Z = -3592387
78 I = 51
28863
XDOT = 4011
598683 Wp = 351
98440
YDOT = -4822
137309 meter/sec RA = 275
58345 deg
ZDOT = 4396
125317 TA = 325
36127
MA = 325
37101
Ha = 225
760 n
mi
Hp = 222
978
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7806302
59 X = -2302987
70
Y = -17235966
02 feet Y = -5279702
63 meter
Z = -11786049
16 Z = -3603761
19
XDOT = 13161
413001 XDOT = 4043
868136
YDOT = -15820
660461 feet/sec YDOT = -4777
097002 meter/sec
ZDOT = 14422
983322 ZDOT = 4415
690744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5563716
18 X = -1695820
69
Y = -18053923
54 feet Y = -5502835
90 meter
Z = -11833374
25 Z = -3606812
47
XDOT = 13592
269919 XDOT = 4142
923871
YDOT = -13694
577716 feet/sec YDOT = -4174
107288 meter/sec
ZDOT = 14506
844793 ZDOT = 4421
686293
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 14205
15211193
00016717 00000-0 10270-3 0 9046
2 25544 51
6451 276
3662 0005939 291
6709 68
3809 15
50159815 17064
Satellite: ISS
Catalog Number: 25544
Epoch time: 14205
15211193 = yrday
fracday
Element set: 904
Inclination: 51
6451 deg
RA of node: 276
3662 deg
Eccentricity:
0005939
Arg of perigee: 291
6709 deg
Mean anomaly: 68
3809 deg
Mean motion: 15
50159815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1706
Checksum: 314
Coasting Arc #6 (Orbit 1721)
---------------------------------------
Vector Time (GMT): 2014/206/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2574721
60 A = 6796196
47 meter
Y = 5362514
88 meter E =
0007446
Z = 3282994
30 I = 51
28969
XDOT = -3809
517559 Wp = 72
54893
YDOT = 4707
761820 meter/sec RA = 270
60439 deg
ZDOT = -4691
076214 TA = 69
19159
MA = 69
11184
Ha = 225
993 n
mi
Hp = 222
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8447249
35 X = 2498617
93
Y = 17593552
76 feet Y = 5390881
28 meter
Z = 10770978
68 Z = 3295317
32
XDOT = -12498
417189 XDOT = -3839
090365
YDOT = 15445
412796 feet/sec YDOT = 4664
996381 meter/sec
ZDOT = -15390
669992 ZDOT = -4709
653423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6479500
28 X = 1974951
69
Y = 18379238
70 feet Y = 5601991
96 meter
Z = 10822327
06 Z = 3298645
29
XDOT = -12618
913239 XDOT = -3846
244755
YDOT = 13579
393154 feet/sec YDOT = 4138
999033 meter/sec
ZDOT = -15470
313866 ZDOT = -4715
351666
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 14206
18358074
00016717 00000-0 10270-3 0 9051
2 25544 51
6453 271
2553 0006133 296
0944 63
9576 15
50195759 17223
Satellite: ISS
Catalog Number: 25544
Epoch time: 14206
18358074 = yrday
fracday
Element set: 905
Inclination: 51
6453 deg
RA of node: 271
2553 deg
Eccentricity:
0006133
Arg of perigee: 296
0944 deg
Mean anomaly: 63
9576 deg
Mean motion: 15
50195759 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1722
Checksum: 318
Coasting Arc #7 (Orbit 1736)
---------------------------------------
Vector Time (GMT): 2014/207/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2800159
44 A = 6797092
50 meter
Y = -5433174
98 meter E =
0004598
Z = -2966644
45 I = 51
29154
XDOT = 3632
593689 Wp = 348
63624
YDOT = -4576
202642 meter/sec RA = 265
62412 deg
ZDOT = 4955
324563 TA = 337
33863
MA = 337
35893
Ha = 226
064 n
mi
Hp = 222
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9186874
82 X = -2724785
61
Y = -17825377
21 feet Y = -5464066
51 meter
Z = -9733085
45 Z = -2980064
27
XDOT = 11917
958297 XDOT = 3659
424957
YDOT = -15013
788194 feet/sec YDOT = -4535
430968 meter/sec
ZDOT = 16257
626520 ZDOT = 4973
035690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7517472
88 X = -2291325
73
Y = -18561708
07 feet Y = -5657608
62 meter
Z = -9789090
31 Z = -2983714
73
XDOT = 11740
130656 XDOT = 3578
391824
YDOT = -13363
406881 feet/sec YDOT = -4073
166417 meter/sec
ZDOT = 16333
567228 ZDOT = 4978
471291
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 14207
15058006
00016717 00000-0 10270-3 0 9062
2 25544 51
6438 266
4624 0005867 299
0333 61
0229 15
50173107 17372
Satellite: ISS
Catalog Number: 25544
Epoch time: 14207
15058006 = yrday
fracday
Element set: 906
Inclination: 51
6438 deg
RA of node: 266
4624 deg
Eccentricity:
0005867
Arg of perigee: 299
0333 deg
Mean anomaly: 61
0229 deg
Mean motion: 15
50173107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1737
Checksum: 298
Coasting Arc #8 (Orbit 1752)
---------------------------------------
Vector Time (GMT): 2014/208/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3028562
66 A = 6797818
44 meter
Y = 5492054
76 meter E =
0008142
Z = 2615545
30 I = 51
29751
XDOT = -3494
723565 Wp = 87
61484
YDOT = 4409
647826 meter/sec RA = 260
64587 deg
ZDOT = -5198
282615 TA = 62
83312
MA = 62
75013
Ha = 226
291 n
mi
Hp = 222
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9936229
20 X = 2954218
94
Y = 18018552
36 feet Y = 5525506
27 meter
Z = 8581185
36 Z = 2630077
06
XDOT = -11465
628493 XDOT = -3518
522463
YDOT = 14467
348511 feet/sec YDOT = 4370
434798 meter/sec
ZDOT = -17054
732989 ZDOT = -5215
316697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8576593
94 X = 2614145
83
Y = 18676000
00 feet Y = 5692444
80 meter
Z = 8641914
27 Z = 2634055
47
XDOT = -10995
543239 XDOT = -3351
441579
YDOT = 12996
719636 feet/sec YDOT = 3961
400145 meter/sec
ZDOT = -17127
766230 ZDOT = -5220
543147
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 14208
18203730
00016717 00000-0 10270-3 0 9073
2 25544 51
6437 261
3512 0006084 303
3231 56
7336 15
50209850 17532
Satellite: ISS
Catalog Number: 25544
Epoch time: 14208
18203730 = yrday
fracday
Element set: 907
Inclination: 51
6437 deg
RA of node: 261
3512 deg
Eccentricity:
0006084
Arg of perigee: 303
3231 deg
Mean anomaly: 56
7336 deg
Mean motion: 15
50209850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1753
Checksum: 279
Coasting Arc #9 (Orbit 1767)
---------------------------------------
Vector Time (GMT): 2014/209/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3277631
30 A = 6798605
99 meter
Y = -5503468
37 meter E =
0007674
Z = -2263638
46 I = 51
30513
XDOT = 3388
318488 Wp = 356
31331
YDOT = -4239
979775 meter/sec RA = 255
66697 deg
ZDOT = 5408
824150 TA = 338
41535
MA = 338
44768
Ha = 226
350 n
mi
Hp = 222
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10753383
53 X = -3204850
86
Y = -18055998
60 feet Y = -5539713
93 meter
Z = -7426635
36 Z = -2279383
84
XDOT = 11116
530472 XDOT = 3409
205303
YDOT = -13910
694799 feet/sec YDOT = -4201
972842 meter/sec
ZDOT = 17745
486057 ZDOT = 5425
334348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9717762
83 X = -2961974
11
Y = -18607427
46 feet Y = -5671543
89 meter
Z = -7492528
57 Z = -2283722
71
XDOT = 10381
467637 XDOT = 3164
271336
YDOT = -12587
199605 feet/sec YDOT = -3836
578440 meter/sec
ZDOT = 17816
261370 ZDOT = 5430
396466
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 14209
14902607
00016717 00000-0 10270-3 0 9080
2 25544 51
6429 256
5582 0005758 306
6325 53
4296 15
50187551 17681
Satellite: ISS
Catalog Number: 25544
Epoch time: 14209
14902607 = yrday
fracday
Element set: 908
Inclination: 51
6429 deg
RA of node: 256
5582 deg
Eccentricity:
0005758
Arg of perigee: 306
6325 deg
Mean anomaly: 53
4296 deg
Mean motion: 15
50187551 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1768
Checksum: 325
Coasting Arc #10 (Orbit 1783)
---------------------------------------
Vector Time (GMT): 2014/210/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3520579
62 A = 6799180
40 meter
Y = 5501731
51 meter E =
0008423
Z = 1877376
44 I = 51
31564
XDOT = -3326
803590 Wp = 100
82188
YDOT = 4043
463261 meter/sec RA = 250
69005 deg
ZDOT = -5591
005340 TA = 58
45324
MA = 58
37101
Ha = 226
567 n
mi
Hp = 222
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11550458
07 X = 3449676
83
Y = 18050300
23 feet Y = 5540704
42 meter
Z = 6159371
53 Z = 1894306
50
XDOT = -10914
709940 XDOT = -3344
612492
YDOT = 13265
955582 feet/sec YDOT = 4006
161355 meter/sec
ZDOT = -18343
193372 ZDOT = -5607
209329
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10841095
09 X = 3304365
78
Y = 18461261
93 feet Y = 5626992
64 meter
Z = 6230308
39 Z = 1898998
00
XDOT = -9932
573354 XDOT = -3027
448358
YDOT = 12068
426249 feet/sec YDOT = 3678
456321 meter/sec
ZDOT = -18412
630678 ZDOT = -5612
169831
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 14210
18047195
00016717 00000-0 10270-3 0 9099
2 25544 51
6426 251
4465 0005974 310
8571 49
2061 15
50224472 17847
Satellite: ISS
Catalog Number: 25544
Epoch time: 14210
18047195 = yrday
fracday
Element set: 909
Inclination: 51
6426 deg
RA of node: 251
4465 deg
Eccentricity:
0005974
Arg of perigee: 310
8571 deg
Mean anomaly: 49
2061 deg
Mean motion: 15
50224472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1784
Checksum: 300
Coasting Arc #11 (Orbit 1798)
---------------------------------------
Vector Time (GMT): 2014/211/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3772527
46 A = 6799783
28 meter
Y = -5447367
66 meter E =
0010503
Z = -1497082
17 I = 51
32901
XDOT = 3299
329228 Wp = 5
61118
YDOT = -3858
899924 meter/sec RA = 245
71337 deg
ZDOT = 5740
838089 TA = 337
99314
MA = 338
03820
Ha = 226
622 n
mi
Hp = 222
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12377058
60 X = -3704061
15
Y = -17871941
15 feet Y = -5489171
66 meter
Z = -4911686
91 Z = -1515242
01
XDOT = 10824
570959 XDOT = 3314
348457
YDOT = -12660
432823 feet/sec YDOT = -3821
920776 meter/sec
ZDOT = 18834
770634 ZDOT = 5756
901930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11994803
03 X = -3656015
96
Y = -18109898
16 feet Y = -5519896
96 meter
Z = -4987866
97 Z = -1520301
85
XDOT = 9630
304234 XDOT = 2935
316730
YDOT = -11572
776241 feet/sec YDOT = -3527
382198 meter/sec
ZDOT = 18903
577864 ZDOT = 5761
810533
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 14211
14745002
00016717 00000-0 10270-3 0 9100
2 25544 51
6430 246
6536 0005652 314
5089 45
5599 15
50204464 17995
Satellite: ISS
Catalog Number: 25544
Epoch time: 14211
14745002 = yrday
fracday
Element set: 910
Inclination: 51
6430 deg
RA of node: 246
6536 deg
Eccentricity:
0005652
Arg of perigee: 314
5089 deg
Mean anomaly: 45
5599 deg
Mean motion: 15
50204464 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1799
Checksum: 299
Coasting Arc #12 (Orbit 1814)
---------------------------------------
Vector Time (GMT): 2014/212/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4008696
12 A = 6800140
24 meter
Y = 5381065
86 meter E =
0008132
Z = 1083790
71 I = 51
34364
XDOT = -3318
573334 Wp = 111
94645
YDOT = 3657
918137 meter/sec RA = 240
73844 deg
ZDOT = -5854
592062 TA = 56
27173
MA = 56
19426
Ha = 226
827 n
mi
Hp = 222
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13151890
14 X = 3942961
24
Y = 17654415
56 feet Y = 5425526
14 meter
Z = 3555743
79 Z = 1103104
44
XDOT = -10887
707790 XDOT = -3330
791058
YDOT = 12001
043756 feet/sec YDOT = 3620
739396 meter/sec
ZDOT = -19207
979206 ZDOT = -5870
742665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13088387
32 X = 3989340
46
Y = 17685061
08 feet Y = 5390406
62 meter
Z = 3636845
99 Z = 1108510
66
XDOT = -9504
811485 XDOT = -2897
066541
YDOT = 11020
000875 feet/sec YDOT = 3358
896267 meter/sec
ZDOT = -19277
118352 ZDOT = -5875
665674
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 14212
17888484
00016717 00000-0 10270-3 0 9117
2 25544 51
6424 241
5416 0005849 318
6880 41
3827 15
50238648 18159
Satellite: ISS
Catalog Number: 25544
Epoch time: 14212
17888484 = yrday
fracday
Element set: 911
Inclination: 51
6424 deg
RA of node: 241
5416 deg
Eccentricity:
0005849
Arg of perigee: 318
6880 deg
Mean anomaly: 41
3827 deg
Mean motion: 15
50238648 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1815
Checksum: 320
Coasting Arc #13 (Orbit 1829)
---------------------------------------
Vector Time (GMT): 2014/213/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4241142
62 A = 6800491
56 meter
Y = -5261416
11 meter E =
0012894
Z = -683360
88 I = 51
36203
XDOT = 3370
786513 Wp = 15
38694
YDOT = -3483
403460 meter/sec RA = 235
76470 deg
ZDOT = 5937
740017 TA = 337
21280
MA = 337
26998
Ha = 226
883 n
mi
Hp = 221
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13914509
90 X = -4178673
54
Y = -17261863
89 feet Y = -5308494
02 meter
Z = -2241997
64 Z = -703811
77
XDOT = 11059
010871 XDOT = 3380
644901
YDOT = -11428
489043 feet/sec YDOT = -3445
654005 meter/sec
ZDOT = 19480
774333 ZDOT = 5954
138596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14155592
54 X = -4314624
61
Y = -17053207
71 feet Y = -5197817
71 meter
Z = -2327958
55 Z = -709561
77
XDOT = 9521
401799 XDOT = 2902
123268
YDOT = -10556
096644 feet/sec YDOT = -3217
498257 meter/sec
ZDOT = 19550
935905 ZDOT = 5959
125264
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 14213
14585196
00016717 00000-0 10270-3 0 9120
2 25544 51
6438 236
7492 0005593 322
4534 37
6225 15
50223878 18305
Satellite: ISS
Catalog Number: 25544
Epoch time: 14213
14585196 = yrday
fracday
Element set: 912
Inclination: 51
6438 deg
RA of node: 236
7492 deg
Eccentricity:
0005593
Arg of perigee: 322
4534 deg
Mean anomaly: 37
6225 deg
Mean motion: 15
50223878 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1830
Checksum: 309
Coasting Arc #14 (Orbit 1845)
---------------------------------------
Vector Time (GMT): 2014/214/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4448659
46 A = 6800584
54 meter
Y = 5133953
68 meter E =
0007157
Z = 252556
83 I = 51
38030
XDOT = -3466
638346 Wp = 120
30925
YDOT = 3304
012891 meter/sec RA = 230
79241 deg
ZDOT = -5976
990551 TA = 56
96524
MA = 56
89651
Ha = 227
072 n
mi
Hp = 221
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14595339
45 X = 4389692
95
Y = 16843680
04 feet Y = 5183371
75 meter
Z = 828598
54 Z = 274024
38
XDOT = -11373
485386 XDOT = -3474
292870
YDOT = 10839
937306 feet/sec YDOT = 3265
203894 meter/sec
ZDOT = -19609
549051 ZDOT = -5993
849450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15122764
41 X = 4609418
59
Y = 16366968
95 feet Y = 4988652
13 meter
Z = 918907
29 Z = 280082
94
XDOT = -9702
894468 XDOT = -2957
442234
YDOT = 10090
829790 feet/sec YDOT = 3075
684920 meter/sec
ZDOT = -19681
635813 ZDOT = -5998
962596
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 14214
17727582
00016717 00000-0 10270-3 0 9132
2 25544 51
6432 231
6371 0005760 326
5490 33
5296 15
50251996 18463
Satellite: ISS
Catalog Number: 25544
Epoch time: 14214
17727582 = yrday
fracday
Element set: 913
Inclination: 51
6432 deg
RA of node: 231
6371 deg
Eccentricity:
0005760
Arg of perigee: 326
5490 deg
Mean anomaly: 33
5296 deg
Mean motion: 15
50251996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1846
Checksum: 309
Coasting Arc #15 (Orbit 1861)
---------------------------------------
Vector Time (GMT): 2014/215/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4639907
53 A = 6800639
15 meter
Y = -4956854
00 meter E =
0014677
Z = 158793
90 I = 51
40239
XDOT = 3591
279531 Wp = 25
33576
YDOT = -3163
631825 meter/sec RA = 225
82189 deg
ZDOT = 5988
678244 TA = 336
37860
MA = 336
44592
Ha = 227
139 n
mi
Hp = 221
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15222793
75 X = -4584905
37
Y = -16262644
37 feet Y = -5008432
91 meter
Z = 520977
36 Z = 136387
58
XDOT = 11782
413159 XDOT = 3597
298178
YDOT = -10379
369503 feet/sec YDOT = -3123
438206 meter/sec
ZDOT = 19647
894502 ZDOT = 6006
138668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16008582
71 X = -4879416
01
Y = -15492634
49 feet Y = -4722154
99 meter
Z = 426643
62 Z = 130040
98
XDOT = 10003
367920 XDOT = 3049
026542
YDOT = -9772
134974 feet/sec YDOT = -2978
546740 meter/sec
ZDOT = 19722
514466 ZDOT = 6011
422409
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 14215
20869511
00016717 00000-0 10270-3 0 9147
2 25544 51
6448 226
5256 0005600 330
5304 29
5530 15
50245101 18622
Satellite: ISS
Catalog Number: 25544
Epoch time: 14215
20869511 = yrday
fracday
Element set: 914
Inclination: 51
6448 deg
RA of node: 226
5256 deg
Eccentricity:
0005600
Arg of perigee: 330
5304 deg
Mean anomaly: 29
5530 deg
Mean motion: 15
50245101 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1862
Checksum: 273
Coasting Arc #16 (Orbit 1876)
---------------------------------------
Vector Time (GMT): 2014/216/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4798776
31 A = 6800441
87 meter
Y = 4778980
38 meter E =
0005532
Z = -596571
07 I = 51
42372
XDOT = -3751
227813 Wp = 123
39001
YDOT = 3029
475399 meter/sec RA = 220
85269 deg
ZDOT = -5949
279206 TA = 63
05449
MA = 62
99799
Ha = 227
301 n
mi
Hp = 221
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15744016
76 X = 4747877
93
Y = 15679069
50 feet Y = 4832358
82 meter
Z = -1957254
18 Z = -573382
95
XDOT = -12307
177863 XDOT = -3755
925765
YDOT = 9939
223749 feet/sec YDOT = 2987
500595 meter/sec
ZDOT = -19518
632567 ZDOT = -5967
513403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16762997
99 X = 5109361
79
Y = 14597330
56 feet Y = 4449266
35 meter
Z = -1859561
02 Z = -566794
20
XDOT = -10432
480482 XDOT = -3179
820051
YDOT = 9502
765848 feet/sec YDOT = 2896
443030 meter/sec
ZDOT = -19596
520492 ZDOT = -5973
019446
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 14216
17564436
00016717 00000-0 10270-3 0 9153
2 25544 51
6442 221
7334 0005726 334
2510 25
8355 15
50265233 18777
Satellite: ISS
Catalog Number: 25544
Epoch time: 14216
17564436 = yrday
fracday
Element set: 915
Inclination: 51
6442 deg
RA of node: 221
7334 deg
Eccentricity:
0005726
Arg of perigee: 334
2510 deg
Mean anomaly: 25
8355 deg
Mean motion: 15
50265233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1877
Checksum: 294
Coasting Arc #17 (Orbit 1892)
---------------------------------------
Vector Time (GMT): 2014/217/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4930201
26 A = 6800183
59 meter
Y = -4559136
20 meter E =
0015725
Z = 1008735
43 I = 51
44818
XDOT = 3933
444461 Wp = 35
39696
YDOT = -2943
830220 meter/sec RA = 215
88523 deg
ZDOT = 5886
098249 TA = 335
55312
MA = 335
62761
Ha = 227
396 n
mi
Hp = 221
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16175200
98 X = -4883753
61
Y = -14957795
94 feet Y = -4614009
22 meter
Z = 3309499
45 Z = 984898
01
XDOT = 12905
001511 XDOT = 3937
478097
YDOT = -9658
235629 feet/sec YDOT = -2899
821553 meter/sec
ZDOT = 19311
345960 ZDOT = 5905
215955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17389445
74 X = -5300303
06
Y = -13551201
39 feet Y = -4130406
19 meter
Z = 3209001
43 Z = 978103
64
XDOT = 10943
079752 XDOT = 3335
450708
YDOT = -9423
357189 feet/sec YDOT = -2872
239271 meter/sec
ZDOT = 19392
977931 ZDOT = 5910
979673
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 14217
20705128
00016717 00000-0 10270-3 0 9164
2 25544 51
6454 216
6220 0005660 338
3463 21
7447 15
50265589 18935
Satellite: ISS
Catalog Number: 25544
Epoch time: 14217
20705128 = yrday
fracday
Element set: 916
Inclination: 51
6454 deg
RA of node: 216
6220 deg
Eccentricity:
0005660
Arg of perigee: 338
3463 deg
Mean anomaly: 21
7447 deg
Mean motion: 15
50265589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1893
Checksum: 303
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