[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 2nd 2014
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) : 127 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 378 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 393)
---------------------------------------
Vector Time (GMT): 2014/120/13:41:36
513
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 485048
89 A = 6791592
22 meter
Y = -4601295
64 meter E =
0010316
Z = -4981235
96 I = 51
48175
XDOT = 7201
619430 Wp = 102
08716
YDOT = -1513
913826 meter/sec RA = 334
99147 deg
ZDOT = 2101
284911 TA = 188
44786
MA = 188
46524
Ha = 227
221 n
mi
Hp = 222
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1591367
74 X = 560663
31
Y = -15096114
31 feet Y = -4595448
75 meter
Z = -16342637
67 Z = -4978695
93
XDOT = 23627
360335 XDOT = 7207
805536
YDOT = -4966
908879 feet/sec YDOT = -1433
346097 meter/sec
ZDOT = 6893
979367 ZDOT = 2136
285114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12683151
77 X = -3865824
66
Y = -8363047
73 feet Y = -2549056
95 meter
Z = -16331075
24 Z = -4977711
73
XDOT = 5671
640366 XDOT = 1728
715983
YDOT = -22343
116763 feet/sec YDOT = -6810
181989 meter/sec
ZDOT = 7042
233180 ZDOT = 2146
472673
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 14120
58294017
00016717 00000-0 10270-3 0 9001
2 25544 51
6447 335
5117 0002229 301
0320 59
0611 15
49772228 3943
Satellite: ISS
Catalog Number: 25544
Epoch time: 14120
58294017 = yrday
fracday
Element set: 900
Inclination: 51
6447 deg
RA of node: 335
5117 deg
Eccentricity:
0002229
Arg of perigee: 301
0320 deg
Mean anomaly: 59
0611 deg
Mean motion: 15
49772228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 394
Checksum: 278
Coasting Arc #2 (Orbit 409)
---------------------------------------
Vector Time (GMT): 2014/121/13:41:36
513
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -411535
96 A = 6792008
92 meter
Y = 4715577
91 meter E =
0006324
Z = 4869164
96 I = 51
45555
XDOT = -7037
907296 Wp = 40
01908
YDOT = 1860
654455 meter/sec RA = 330
02612 deg
ZDOT = -2390
320618 TA = 73
52325
MA = 73
45377
Ha = 227
232 n
mi
Hp = 222
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1350183
61 X = -487889
31
Y = 15471056
12 feet Y = 4710548
87 meter
Z = 15974950
66 Z = 4866980
34
XDOT = -23090
247033 XDOT = -7046
578856
YDOT = 6104
509366 feet/sec YDOT = 1781
903602 meter/sec
ZDOT = -7842
259246 ZDOT = -2424
531448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13268848
06 X = 4044344
89
Y = 8089265
18 feet Y = 2465608
03 meter
Z = 15964870
25 Z = 4866092
45
XDOT = -4029
987800 XDOT = -1228
340281
YDOT = 22415
886245 feet/sec YDOT = 6832
362127 meter/sec
ZDOT = -7987
235392 ZDOT = -2434
509348
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 14121
61466126
00016717 00000-0 10270-3 0 9019
2 25544 51
6447 330
4021 0002322 303
8065 56
2864 15
49778839 4103
Satellite: ISS
Catalog Number: 25544
Epoch time: 14121
61466126 = yrday
fracday
Element set: 901
Inclination: 51
6447 deg
RA of node: 330
4021 deg
Eccentricity:
0002322
Arg of perigee: 303
8065 deg
Mean anomaly: 56
2864 deg
Mean motion: 15
49778839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 410
Checksum: 286
Coasting Arc #3 (Orbit 424)
---------------------------------------
Vector Time (GMT): 2014/122/13:41:36
513
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 310524
43 A = 6792349
38 meter
Y = -4845651
43 meter E =
0008999
Z = -4758183
51 I = 51
43050
XDOT = 6834
493148 Wp = 103
86694
YDOT = -2179
850882 meter/sec RA = 325
05759 deg
ZDOT = 2668
097540 TA = 192
60023
MA = 192
62274
Ha = 227
230 n
mi
Hp = 222
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1018780
94 X = 387800
61
Y = -15897806
54 feet Y = -4841746
76 meter
Z = -15610838
27 Z = -4756487
41
XDOT = 22422
877783 XDOT = 6845
399816
YDOT = -7151
741738 feet/sec YDOT = -2103
362271 meter/sec
ZDOT = 8753
600854 ZDOT = 2701
325501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13933848
13 X = -4247036
91
Y = -7738016
94 feet Y = -2358547
56 meter
Z = -15602801
32 Z = -4755733
84
XDOT = 2419
114877 XDOT = 737
346215
YDOT = -22276
546920 feet/sec YDOT = -6789
891501 meter/sec
ZDOT = 8894
477046 ZDOT = 2711
036604
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 14122
58188310
00016717 00000-0 10270-3 0 9023
2 25544 51
6445 325
6105 0002187 308
2088 51
8865 15
49823354 4254
Satellite: ISS
Catalog Number: 25544
Epoch time: 14122
58188310 = yrday
fracday
Element set: 902
Inclination: 51
6445 deg
RA of node: 325
6105 deg
Eccentricity:
0002187
Arg of perigee: 308
2088 deg
Mean anomaly: 51
8865 deg
Mean motion: 15
49823354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 425
Checksum: 301
Coasting Arc #4 (Orbit 440)
---------------------------------------
Vector Time (GMT): 2014/123/13:41:36
513
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -219362
40 A = 6792894
13 meter
Y = 4980985
74 meter E =
0007780
Z = 4610866
50 I = 51
40729
XDOT = -6624
749298 Wp = 50
01637
YDOT = 2458
606242 meter/sec RA = 320
08837 deg
ZDOT = -2962
902876 TA = 69
67779
MA = 69
59420
Ha = 227
254 n
mi
Hp = 222
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -719692
90 X = -297442
99
Y = 16341816
75 feet Y = 4978096
00 meter
Z = 15127514
75 Z = 4609611
32
XDOT = -21734
741792 XDOT = -6637
356612
YDOT = 8066
293444 feet/sec YDOT = 2384
453625 meter/sec
ZDOT = -9720
809959 ZDOT = -2995
115938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14593425
76 X = 4448076
17
Y = 7402176
45 feet Y = 2256183
38 meter
Z = 15121320
82 Z = 4608978
59
XDOT = -924
546358 XDOT = -281
801730
YDOT = 22014
929602 feet/sec YDOT = 6710
150543 meter/sec
ZDOT = -9857
443278 ZDOT = -3004
548711
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 14123
61356846
00016717 00000-0 10270-3 0 9030
2 25544 51
6443 320
5005 0002267 311
3132 48
7823 15
49828018 4418
Satellite: ISS
Catalog Number: 25544
Epoch time: 14123
61356846 = yrday
fracday
Element set: 903
Inclination: 51
6443 deg
RA of node: 320
5005 deg
Eccentricity:
0002267
Arg of perigee: 311
3132 deg
Mean anomaly: 48
7823 deg
Mean motion: 15
49828018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 441
Checksum: 282
Coasting Arc #5 (Orbit 455)
---------------------------------------
Vector Time (GMT): 2014/124/13:41:36
513
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 92727
16 A = 6793325
11 meter
Y = -5125265
96 meter E =
0007400
Z = -4465035
33 I = 51
38679
XDOT = 6385
017406 Wp = 102
86863
YDOT = -2705
569140 meter/sec RA = 315
11711 deg
ZDOT = 3241
174876 TA = 199
92974
MA = 199
95866
Ha = 227
249 n
mi
Hp = 221
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 304222
97 X = 171722
08
Y = -16815177
03 feet Y = -5123787
25 meter
Z = -14649066
03 Z = -4464393
09
XDOT = 20948
219836 XDOT = 6399
052398
YDOT = -8876
539172 feet/sec YDOT = -2634
089367 meter/sec
ZDOT = 10633
775840 ZDOT = 3272
226740
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15317989
05 X = -4668923
06
Y = -6950401
94 feet Y = -2118482
51 meter
Z = -14645442
64 Z = -4463930
92
XDOT = -495
438517 XDOT = -151
009660
YDOT = -21572
222151 feet/sec YDOT = -6575
213312 meter/sec
ZDOT = 10765
541042 ZDOT = 3281
336910
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 14124
58075659
00016717 00000-0 10270-3 0 9048
2 25544 51
6451 315
7095 0002167 316
2573 43
8405 15
49875968 4568
Satellite: ISS
Catalog Number: 25544
Epoch time: 14124
58075659 = yrday
fracday
Element set: 904
Inclination: 51
6451 deg
RA of node: 315
7095 deg
Eccentricity:
0002167
Arg of perigee: 316
2573 deg
Mean anomaly: 43
8405 deg
Mean motion: 15
49875968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 456
Checksum: 330
Coasting Arc #6 (Orbit 471)
---------------------------------------
Vector Time (GMT): 2014/125/13:41:36
513
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 25256
34 A = 6793981
49 meter
Y = 5274099
46 meter E =
0009229
Z = 4278651
56 I = 51
36713
XDOT = -6146
294955 Wp = 60
13526
YDOT = 2905
428563 meter/sec RA = 310
14468 deg
ZDOT = -3534
850308 TA = 66
10946
MA = 66
01279
Ha = 227
281 n
mi
Hp = 221
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 82862
00 X = -54506
21
Y = 17303475
93 feet Y = 5273935
87 meter
Z = 14037570
74 Z = 4278580
57
XDOT = -20165
009695 XDOT = -6161
155994
YDOT = 9532
245941 feet/sec YDOT = 2836
613693 meter/sec
ZDOT = -11597
277912 ZDOT = -3564
744462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16034631
54 X = 4887355
69
Y = 6507089
99 feet Y = 1983361
03 meter
Z = 14036342
43 Z = 4278277
17
XDOT = 1757
539271 XDOT = 535
697970
YDOT = 21031
763394 feet/sec YDOT = 6410
481483 meter/sec
ZDOT = -11724
180020 ZDOT = -3573
530070
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 14125
61240616
00016717 00000-0 10270-3 0 9051
2 25544 51
6446 310
5992 0002231 319
5724 40
5260 15
49880746 4728
Satellite: ISS
Catalog Number: 25544
Epoch time: 14125
61240616 = yrday
fracday
Element set: 905
Inclination: 51
6446 deg
RA of node: 310
5992 deg
Eccentricity:
0002231
Arg of perigee: 319
5724 deg
Mean anomaly: 40
5260 deg
Mean motion: 15
49880746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 472
Checksum: 293
Coasting Arc #7 (Orbit 486)
---------------------------------------
Vector Time (GMT): 2014/126/13:41:36
513
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -184491
00 A = 6794496
77 meter
Y = -5422863
94 meter E =
0005686
Z = -4094762
41 I = 51
35132
XDOT = 5889
003883 Wp = 95
25986
YDOT = -3071
903796 meter/sec RA = 305
17133 deg
ZDOT = 3806
989382 TA = 214
26960
MA = 214
30630
Ha = 227
270 n
mi
Hp = 221
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -605285
44 X = -103946
40
Y = -17791548
35 feet Y = -5424476
68 meter
Z = -13434259
89 Z = -4095463
02
XDOT = 19320
878880 XDOT = 5904
423641
YDOT = -10078
424527 feet/sec YDOT = -3005
962960 meter/sec
ZDOT = 12490
122644 ZDOT = 3835
635014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16788838
03 X = -5117237
83
Y = -5914924
53 feet Y = -1802869
00 meter
Z = -13436275
05 Z = -4095376
64
XDOT = -2911
287817 XDOT = -887
360527
YDOT = -20355
061725 feet/sec YDOT = -6204
222814 meter/sec
ZDOT = 12611
770445 ZDOT = 3844
067632
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 14126
57956021
00016717 00000-0 10270-3 0 9062
2 25544 51
6458 305
8086 0002218 324
5239 35
5764 15
49928521 4877
Satellite: ISS
Catalog Number: 25544
Epoch time: 14126
57956021 = yrday
fracday
Element set: 906
Inclination: 51
6458 deg
RA of node: 305
8086 deg
Eccentricity:
0002218
Arg of perigee: 324
5239 deg
Mean anomaly: 35
5764 deg
Mean motion: 15
49928521 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 487
Checksum: 323
Coasting Arc #8 (Orbit 502)
---------------------------------------
Vector Time (GMT): 2014/127/13:41:36
513
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 335420
40 A = 6795229
28 meter
Y = 5574083
13 meter E =
0010561
Z = 3866259
19 I = 51
33597
XDOT = -5641
462153 Wp = 70
14415
YDOT = 3186
012941 meter/sec RA = 300
19635 deg
ZDOT = -4091
259204 TA = 63
05109
MA = 62
94326
Ha = 227
302 n
mi
Hp = 221
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1100460
64 X = 254283
61
Y = 18287674
32 feet Y = 5577380
39 meter
Z = 12684577
39 Z = 3867691
50
XDOT = -18508
734099 XDOT = -5656
795391
YDOT = 10452
798364 feet/sec YDOT = 3122
840721 meter/sec
ZDOT = -13422
766416 ZDOT = -4118
702138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17525729
30 X = 5341842
29
Y = 5326320
71 feet Y = 1623462
55 meter
Z = 12689667
83 Z = 3867810
75
XDOT = 3871
795798 XDOT = 1180
123359
YDOT = 19615
950908 feet/sec YDOT = 5978
941837 meter/sec
ZDOT = -13539
343453 ZDOT = -4126
791884
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 14127
61117364
00016717 00000-0 10270-3 0 9078
2 25544 51
6451 300
6980 0002260 327
7949 32
3063 15
49937076 5037
Satellite: ISS
Catalog Number: 25544
Epoch time: 14127
61117364 = yrday
fracday
Element set: 907
Inclination: 51
6451 deg
RA of node: 300
6980 deg
Eccentricity:
0002260
Arg of perigee: 327
7949 deg
Mean anomaly: 32
3063 deg
Mean motion: 15
49937076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 503
Checksum: 299
Coasting Arc #9 (Orbit 517)
---------------------------------------
Vector Time (GMT): 2014/128/13:41:36
513
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -530588
48 A = 6795814
44 meter
Y = -5714651
03 meter E =
0004489
Z = -3641868
75 I = 51
32476
XDOT = 5387
868517 Wp = 73
76054
YDOT = -3268
464919 meter/sec RA = 295
22124 deg
ZDOT = 4349
470071 TA = 242
90208
MA = 242
94788
Ha = 227
293 n
mi
Hp = 221
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1740775
87 X = -448955
32
Y = -18748855
10 feet Y = -5720128
04 meter
Z = -11948388
30 Z = -3644247
92
XDOT = 17676
733979 XDOT = 5402
888250
YDOT = -10723
310102 feet/sec YDOT = -3208
130259 meter/sec
ZDOT = 14269
914931 ZDOT = 4375
680379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18261631
70 X = -5566145
34
Y = -4565705
85 feet Y = -1391627
14 meter
Z = -11957465
81 Z = -3644635
58
XDOT = -4704
925382 XDOT = -1434
061256
YDOT = -18796
704500 feet/sec YDOT = -5729
235532 meter/sec
ZDOT = 14381
288663 ZDOT = 4383
416784
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 14128
57829330
00016717 00000-0 10270-3 0 9088
2 25544 51
6463 295
9075 0002354 332
2990 27
8035 15
49979549 5187
Satellite: ISS
Catalog Number: 25544
Epoch time: 14128
57829330 = yrday
fracday
Element set: 908
Inclination: 51
6463 deg
RA of node: 295
9075 deg
Eccentricity:
0002354
Arg of perigee: 332
2990 deg
Mean anomaly: 27
8035 deg
Mean motion: 15
49979549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 518
Checksum: 339
Coasting Arc #10 (Orbit 533)
---------------------------------------
Vector Time (GMT): 2014/129/13:41:36
513
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 716320
72 A = 6796570
85 meter
Y = 5854499
38 meter E =
0011666
Z = 3369263
90 I = 51
31454
XDOT = -5153
734671 Wp = 80
05002
YDOT = 3295
317575 meter/sec RA = 290
24452 deg
ZDOT = -4614
625100 TA = 60
49755
MA = 60
38125
Ha = 227
322 n
mi
Hp = 221
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2350133
61 X = 634434
14
Y = 19207675
13 feet Y = 5862051
96 meter
Z = 11054015
42 Z = 3372544
70
XDOT = -16908
578316 XDOT = -5167
783972
YDOT = 10811
409367 feet/sec YDOT = 3237
606545 meter/sec
ZDOT = -15139
846130 ZDOT = -4639
695731
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18964781
80 X = 5780465
49
Y = 3809224
85 feet Y = 1161051
74 meter
Z = 11066888
72 Z = 3373187
68
XDOT = 5319
711705 XDOT = 1621
448128
YDOT = 17959
446473 feet/sec YDOT = 5474
039285 meter/sec
ZDOT = -15246
400131 ZDOT = -4647
102760
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 14129
60987019
00016717 00000-0 10270-3 0 9093
2 25544 51
6458 290
7966 0002361 335
5720 24
5319 15
49995613 5345
Satellite: ISS
Catalog Number: 25544
Epoch time: 14129
60987019 = yrday
fracday
Element set: 909
Inclination: 51
6458 deg
RA of node: 290
7966 deg
Eccentricity:
0002361
Arg of perigee: 335
5720 deg
Mean anomaly: 24
5319 deg
Mean motion: 15
49995613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 534
Checksum: 332
Coasting Arc #11 (Orbit 548)
---------------------------------------
Vector Time (GMT): 2014/130/13:41:36
513
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -946066
02 A = 6797194
33 meter
Y = -5972348
01 meter E =
0004984
Z = -3103171
35 I = 51
30802
XDOT = 4926
190019 Wp = 43
97467
YDOT = -3296
016852 meter/sec RA = 285
26797 deg
ZDOT = 4849
872842 TA = 280
22463
MA = 280
28084
Ha = 227
330 n
mi
Hp = 221
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3103891
14 X = -864137
11
Y = -19594317
62 feet Y = -5982469
51 meter
Z = -10181008
36 Z = -3107568
14
XDOT = 16162
040746 XDOT = 4939
121206
YDOT = -10813
703583 feet/sec YDOT = -3240
856617 meter/sec
ZDOT = 15911
656306 ZDOT = 4873
835438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19620679
78 X = -5980383
20
Y = -2870906
93 feet Y = -875052
43 meter
Z = -10198586
81 Z = -3108529
26
XDOT = -5806
857034 XDOT = -1769
930024
YDOT = -17104
706643 feet/sec YDOT = -5213
514585 meter/sec
ZDOT = 16013
520762 ZDOT = 4880
921128
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 14130
57695535
00016717 00000-0 10270-3 0 9102
2 25544 51
6467 286
0058 0002553 339
6207 20
4841 15
50028760 5496
Satellite: ISS
Catalog Number: 25544
Epoch time: 14130
57695535 = yrday
fracday
Element set: 910
Inclination: 51
6467 deg
RA of node: 286
0058 deg
Eccentricity:
0002553
Arg of perigee: 339
6207 deg
Mean anomaly: 20
4841 deg
Mean motion: 15
50028760 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 549
Checksum: 302
Coasting Arc #12 (Orbit 564)
---------------------------------------
Vector Time (GMT): 2014/131/13:41:36
513
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1163253
30 A = 6797911
39 meter
Y = 6085770
01 meter E =
0012450
Z = 2785952
34 I = 51
30332
XDOT = -4728
177530 Wp = 89
86447
YDOT = 3240
564470 meter/sec RA = 280
29055 deg
ZDOT = -5084
823977 TA = 58
43731
MA = 58
31581
Ha = 227
357 n
mi
Hp = 221
295
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3816447
84 X = 1081580
87
Y = 19966437
03 feet Y = 6098321
64 meter
Z = 9140263
58 Z = 2791404
89
XDOT = -15512
393471 XDOT = -4739
361936
YDOT = 10631
773195 feet/sec YDOT = 3187
628340 meter/sec
ZDOT = -16682
493363 ZDOT = -5107
820448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20224598
03 X = 6164457
48
Y = 1945850
27 feet Y = 593095
16 meter
Z = 9162292
37 Z = 2792666
72
XDOT = 6064
722694 XDOT = 1848
527477
YDOT = 16282
380649 feet/sec YDOT = 4962
869622 meter/sec
ZDOT = -16780
260249 ZDOT = -5114
623324
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 14131
60849551
00016717 00000-0 10270-3 0 9117
2 25544 51
6467 280
8947 0002506 343
2922 16
8146 15
50053991 5657
Satellite: ISS
Catalog Number: 25544
Epoch time: 14131
60849551 = yrday
fracday
Element set: 911
Inclination: 51
6467 deg
RA of node: 280
8947 deg
Eccentricity:
0002506
Arg of perigee: 343
2922 deg
Mean anomaly: 16
8146 deg
Mean motion: 15
50053991 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 565
Checksum: 308
Coasting Arc #13 (Orbit 579)
---------------------------------------
Vector Time (GMT): 2014/132/13:41:36
513
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1420770
52 A = 6798518
34 meter
Y = -6166145
57 meter E =
0007092
Z = -2478664
27 I = 51
30178
XDOT = 4548
290478 Wp = 28
71626
YDOT = -3168
238096 meter/sec RA = 275
31327 deg
ZDOT = 5286
936924 TA = 303
42230
MA = 303
49011
Ha = 227
389 n
mi
Hp = 221
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4661320
59 X = -1339672
87
Y = -20230136
38 feet Y = -6181580
09 meter
Z = -8132100
62 Z = -2485369
35
XDOT = 14922
212854 XDOT = 4557
697593
YDOT = -10394
481942 feet/sec YDOT = -3117
323599 meter/sec
ZDOT = 17345
593583 ZDOT = 5309
055205
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20732269
92 X = -6319195
87
Y = -845161
39 feet Y = -257605
19 meter
Z = -8159416
30 Z = -2486990
09
XDOT = -6215
496802 XDOT = -1894
483425
YDOT = -15505
123660 feet/sec YDOT = -4725
961692 meter/sec
ZDOT = 17439
633820 ZDOT = 5315
600388
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 14132
57554625
00016717 00000-0 10270-3 0 9120
2 25544 51
6475 276
1035 0002774 346
9370 13
1708 15
50077163 5804
Satellite: ISS
Catalog Number: 25544
Epoch time: 14132
57554625 = yrday
fracday
Element set: 912
Inclination: 51
6475 deg
RA of node: 276
1035 deg
Eccentricity:
0002774
Arg of perigee: 346
9370 deg
Mean anomaly: 13
1708 deg
Mean motion: 15
50077163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 580
Checksum: 298
Coasting Arc #14 (Orbit 595)
---------------------------------------
Vector Time (GMT): 2014/133/13:41:36
513
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1660358
52 A = 6799126
13 meter
Y = 6238554
55 meter E =
0012805
Z = 2118303
87 I = 51
30231
XDOT = -4407
452030 Wp = 99
44848
YDOT = 3042
532157 meter/sec RA = 270
33625 deg
ZDOT = -5479
469705 TA = 57
00611
MA = 56
88311
Ha = 227
416 n
mi
Hp = 221
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5447370
47 X = 1580183
91
Y = 20467698
65 feet Y = 6256673
41 meter
Z = 6949815
86 Z = 2126175
25
XDOT = -14460
144457 XDOT = -4414
528617
YDOT = 9982
060883 feet/sec YDOT = 2993
205758 meter/sec
ZDOT = -17977
262812 ZDOT = -5500
898105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21168415
54 X = 6452133
06
Y = -222633
20 feet Y = -67858
60 meter
Z = 6982054
96 Z = 2128130
35
XDOT = 6143
745656 XDOT = 1872
613676
YDOT = 14812
049490 feet/sec YDOT = 4514
712685 meter/sec
ZDOT = -18068
365783 ZDOT = -5507
237891
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 14133
60704981
00016717 00000-0 10270-3 0 9138
2 25544 51
6476 270
9927 0002669 351
2778 8
8326 15
50110434 5964
Satellite: ISS
Catalog Number: 25544
Epoch time: 14133
60704981 = yrday
fracday
Element set: 913
Inclination: 51
6476 deg
RA of node: 270
9927 deg
Eccentricity:
0002669
Arg of perigee: 351
2778 deg
Mean anomaly: 8
8326 deg
Mean motion: 15
50110434 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 596
Checksum: 316
Coasting Arc #15 (Orbit 610)
---------------------------------------
Vector Time (GMT): 2014/134/13:41:36
513
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1933149
69 A = 6799641
79 meter
Y = -6268475
83 meter E =
0009767
Z = -1772365
48 I = 51
30575
XDOT = 4293
962398 Wp = 26
27227
YDOT = -2912
361081 meter/sec RA = 265
35923 deg
ZDOT = 5637
447788 TA = 314
20441
MA = 314
28459
Ha = 227
464 n
mi
Hp = 220
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6342354
63 X = -1854300
72
Y = -20565865
57 feet Y = -6289652
59 meter
Z = -5814847
38 Z = -1781565
44
XDOT = 14087
803143 XDOT = 4298
824398
YDOT = -9554
990422 feet/sec YDOT = -2864
316314 meter/sec
ZDOT = 18495
563609 ZDOT = 5658
319410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21462935
31 X = -6541902
68
Y = 1442568
90 feet Y = 439695
00 meter
Z = -5852703
81 Z = -1783904
12
XDOT = -6005
150959 XDOT = -1830
370012
YDOT = -14218
992529 feet/sec YDOT = -4333
948923 meter/sec
ZDOT = 18584
293394 ZDOT = 5664
492627
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 14134
57406637
00016717 00000-0 10270-3 0 9143
2 25544 51
6484 266
2013 0002984 354
3508 5
7608 15
50126333 6114
Satellite: ISS
Catalog Number: 25544
Epoch time: 14134
57406637 = yrday
fracday
Element set: 914
Inclination: 51
6484 deg
RA of node: 266
2013 deg
Eccentricity:
0002984
Arg of perigee: 354
3508 deg
Mean anomaly: 5
7608 deg
Mean motion: 15
50126333 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 611
Checksum: 291
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