[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
May 7th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 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 501)
---------------------------------------
Vector Time (GMT): 2014/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3114030
31 A = 6790090
86 meter
Y = 2983197
80 meter E =
0003959
Z = 5243969
03 I = 51
31824
XDOT = -4452
815475 Wp = 23
34942
YDOT = 6175
691307 meter/sec RA = 300
57218 deg
ZDOT = -865
225025 TA = 74
98931
MA = 74
94549
Ha = 227
300 n
mi
Hp = 221
874
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10216634
87 X = 3054966
34
Y = 9787394
37 feet Y = 3017690
69 meter
Z = 17204622
80 Z = 5258953
19
XDOT = -14608
974654 XDOT = -4517
339488
YDOT = 20261
454420 feet/sec YDOT = 6125
536284 meter/sec
ZDOT = -2838
664781 ZDOT = -887
013134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14071223
63 X = 4288908
96
Y = -85729
83 feet Y = -26130
45 meter
Z = 17267457
20 Z = 5263120
96
XDOT = 3757
161654 XDOT = 1145
182872
YDOT = 23656
852788 feet/sec YDOT = 7210
608730 meter/sec
ZDOT = -2931
852388 ZDOT = -893
628608
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
54684806
00016717 00000-0 10270-3 0 9003
2 25544 51
6441 301
0235 0002327 324
7865 35
3131 15
49852518 5027
Satellite: ISS
Catalog Number: 25544
Epoch time: 14127
54684806 = yrday
fracday
Element set: 900
Inclination: 51
6441 deg
RA of node: 301
0235 deg
Eccentricity:
0002327
Arg of perigee: 324
7865 deg
Mean anomaly: 35
3131 deg
Mean motion: 15
49852518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 502
Checksum: 284
Coasting Arc #2 (Orbit 516)
---------------------------------------
Vector Time (GMT): 2014/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3160566
09 A = 6790125
20 meter
Y = -3037525
27 meter E =
0012668
Z = -5196638
82 I = 51
30444
XDOT = 4110
369345 Wp = 91
33871
YDOT = -6340
449755 meter/sec RA = 295
59411 deg
ZDOT = 1208
474691 TA = 190
32225
MA = 190
34829
Ha = 227
326 n
mi
Hp = 221
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10369311
31 X = -3101121
04
Y = -9965634
10 feet Y = -3072536
46 meter
Z = -17049339
96 Z = -5211848
12
XDOT = 13485
463730 XDOT = 4175
093757
YDOT = -20802
000508 feet/sec YDOT = -6294
123050 meter/sec
ZDOT = 3964
811978 ZDOT = 1228
599802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14302454
04 X = -4359387
99
Y = 312073
97 feet Y = 95120
15 meter
Z = -17113120
44 Z = -5216079
11
XDOT = -5343
206106 XDOT = -1628
609221
YDOT = -23145
819513 feet/sec YDOT = -7054
845788 meter/sec
ZDOT = 4050
986818 ZDOT = 1234
740782
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
51400611
00016717 00000-0 10270-3 0 9012
2 25544 51
6445 296
2326 0002301 328
6872 31
4142 15
49925237 5174
Satellite: ISS
Catalog Number: 25544
Epoch time: 14128
51400611 = yrday
fracday
Element set: 901
Inclination: 51
6445 deg
RA of node: 296
2326 deg
Eccentricity:
0002301
Arg of perigee: 328
6872 deg
Mean anomaly: 31
4142 deg
Mean motion: 15
49925237 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 517
Checksum: 280
Coasting Arc #3 (Orbit 532)
---------------------------------------
Vector Time (GMT): 2014/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3204389
13 A = 6790482
61 meter
Y = 3115073
77 meter E =
0005747
Z = 5111193
08 I = 51
29235
XDOT = -3781
489681 Wp = 31
18330
YDOT = 6476
924821 meter/sec RA = 290
61432 deg
ZDOT = -1571
058608 TA = 74
08075
MA = 74
01742
Ha = 227
333 n
mi
Hp = 221
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10513087
69 X = 3144488
67
Y = 10220058
31 feet Y = 3150572
50 meter
Z = 16769006
18 Z = 5126614
18
XDOT = -12406
462207 XDOT = -3846
003279
YDOT = 21249
753349 feet/sec YDOT = 6434
277023 meter/sec
ZDOT = -5154
391759 ZDOT = -1589
585625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14579558
10 X = 4443849
31
Y = -487994
04 feet Y = -148740
58 meter
Z = 16833672
22 Z = 5130903
29
XDOT = 6819
069773 XDOT = 2078
452467
YDOT = 22551
686199 feet/sec YDOT = 6873
753954 meter/sec
ZDOT = -5233
823527 ZDOT = -1595
269411
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
54562177
00016717 00000-0 10270-3 0 9023
2 25544 51
6439 291
1216 0002331 333
5332 26
5699 15
49917039 5339
Satellite: ISS
Catalog Number: 25544
Epoch time: 14129
54562177 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 291
1216 deg
Eccentricity:
0002331
Arg of perigee: 333
5332 deg
Mean anomaly: 26
5699 deg
Mean motion: 15
49917039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 533
Checksum: 306
Coasting Arc #4 (Orbit 547)
---------------------------------------
Vector Time (GMT): 2014/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3285923
05 A = 6790689
80 meter
Y = -3194357
64 meter E =
0011575
Z = -5021553
38 I = 51
28468
XDOT = 3438
739829 Wp = 95
03888
YDOT = -6559
968712 meter/sec RA = 285
63458 deg
ZDOT = 1925
657226 TA = 193
75881
MA = 193
79038
Ha = 227
341 n
mi
Hp = 221
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10780587
45 X = -3225565
34
Y = -10480175
99 feet Y = -3230765
58 meter
Z = -16474912
65 Z = -5037369
49
XDOT = 11281
954821 XDOT = 3502
484941
YDOT = -21522
207061 feet/sec YDOT = -6521
158051 meter/sec
ZDOT = 6317
773050 ZDOT = 1942
517383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14942773
82 X = -4554557
46
Y = 760818
23 feet Y = 231897
40 meter
Z = -16541238
39 Z = -5041769
46
XDOT = -8171
086505 XDOT = -2490
547167
YDOT = -21755
302274 feet/sec YDOT = -6631
016133 meter/sec
ZDOT = 6390
162966 ZDOT = 1947
721672
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
51273936
00016717 00000-0 10270-3 0 9035
2 25544 51
6449 286
3308 0002370 336
7224 23
3819 15
49988456 5482
Satellite: ISS
Catalog Number: 25544
Epoch time: 14130
51273936 = yrday
fracday
Element set: 903
Inclination: 51
6449 deg
RA of node: 286
3308 deg
Eccentricity:
0002370
Arg of perigee: 336
7224 deg
Mean anomaly: 23
3819 deg
Mean motion: 15
49988456 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 548
Checksum: 321
Coasting Arc #5 (Orbit 563)
---------------------------------------
Vector Time (GMT): 2014/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3368156
23 A = 6791225
93 meter
Y = 3295323
76 meter E =
0007602
Z = 4888284
25 I = 51
27846
XDOT = -3119
448850 Wp = 40
72768
YDOT = 6610
807896 meter/sec RA = 280
65284 deg
ZDOT = -2299
450676 TA = 71
93340
MA = 71
85060
Ha = 227
359 n
mi
Hp = 221
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11050381
34 X = 3307310
69
Y = 10811429
66 feet Y = 3332648
52 meter
Z = 16037678
00 Z = 4904498
74
XDOT = -10234
412238 XDOT = -3181
970355
YDOT = 21689
002284 feet/sec YDOT = 6575
574601 meter/sec
ZDOT = -7544
129513 ZDOT = -2314
756770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15356089
87 X = 4680536
19
Y = -1001412
18 feet Y = -305230
43 meter
Z = 16105673
91 Z = 4909009
41
XDOT = 9370
864258 XDOT = 2856
239426
YDOT = 20902
285294 feet/sec YDOT = 6371
016558 meter/sec
ZDOT = -7609
950787 ZDOT = -2319
513000
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
54431196
00016717 00000-0 10270-3 0 9044
2 25544 51
6444 281
2192 0002393 341
7696 18
3368 15
49984840 5640
Satellite: ISS
Catalog Number: 25544
Epoch time: 14131
54431196 = yrday
fracday
Element set: 904
Inclination: 51
6444 deg
RA of node: 281
2192 deg
Eccentricity:
0002393
Arg of perigee: 341
7696 deg
Mean anomaly: 18
3368 deg
Mean motion: 15
49984840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 564
Checksum: 318
Coasting Arc #6 (Orbit 578)
---------------------------------------
Vector Time (GMT): 2014/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3491420
61 A = 6791621
32 meter
Y = -3384778
51 meter E =
0009916
Z = -4750315
32 I = 51
27685
XDOT = 2797
688304 Wp = 96
63611
YDOT = -6610
017941 meter/sec RA = 275
67232 deg
ZDOT = 2657
298751 TA = 199
76864
MA = 199
80710
Ha = 227
355 n
mi
Hp = 221
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11454792
04 X = -3430235
76
Y = -11104916
38 feet Y = -3423479
72 meter
Z = -15585024
00 Z = -4767127
89
XDOT = 9178
767403 XDOT = 2858
486509
YDOT = -21686
410567 feet/sec YDOT = -6578
392451 meter/sec
ZDOT = 8718
171754 ZDOT = 2671
037498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15824510
68 X = -4823310
85
Y = 1383270
03 feet Y = 421620
71 meter
Z = -15655536
63 Z = -4771807
57
XDOT = -10410
761925 XDOT = -3173
200235
YDOT = -19894
103895 feet/sec YDOT = -6063
722867 meter/sec
ZDOT = 8777
361687 ZDOT = 2675
339842
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
51138901
00016717 00000-0 10270-3 0 9051
2 25544 51
6456 276
4285 0002514 343
8671 16
2399 15
50049930 5794
Satellite: ISS
Catalog Number: 25544
Epoch time: 14132
51138901 = yrday
fracday
Element set: 905
Inclination: 51
6456 deg
RA of node: 276
4285 deg
Eccentricity:
0002514
Arg of perigee: 343
8671 deg
Mean anomaly: 16
2399 deg
Mean motion: 15
50049930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 579
Checksum: 309
Coasting Arc #7 (Orbit 594)
---------------------------------------
Vector Time (GMT): 2014/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3616972
63 A = 6792320
70 meter
Y = 3492831
39 meter E =
0009438
Z = 4563163
14 I = 51
27708
XDOT = -2510
685356 Wp = 51
19209
YDOT = 6574
564239 meter/sec RA = 270
69014 deg
ZDOT = -3032
288764 TA = 69
33533
MA = 69
23416
Ha = 227
381 n
mi
Hp = 221
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11866708
12 X = 3555479
28
Y = 11459420
58 feet Y = 3532934
78 meter
Z = 14971007
69 Z = 4580585
00
XDOT = -8237
156680 XDOT = -2569
286795
YDOT = 21570
092649 feet/sec YDOT = 6546
160550 meter/sec
ZDOT = -9948
453950 ZDOT = -3044
627804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16336593
95 X = 4979393
83
Y = -1749126
90 feet Y = -533133
88 meter
Z = 15044082
10 Z = 4585436
22
XDOT = 11260
798893 XDOT = 3432
291502
YDOT = 18867
694254 feet/sec YDOT = 5750
873209 meter/sec
ZDOT = -10001
717453 ZDOT = -3048
523480
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
54291858
00016717 00000-0 10270-3 0 9067
2 25544 51
6456 271
3168 0002515 349
1633 10
9463 15
50054614 5952
Satellite: ISS
Catalog Number: 25544
Epoch time: 14133
54291858 = yrday
fracday
Element set: 906
Inclination: 51
6456 deg
RA of node: 271
3168 deg
Eccentricity:
0002515
Arg of perigee: 349
1633 deg
Mean anomaly: 10
9463 deg
Mean motion: 15
50054614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 595
Checksum: 303
Coasting Arc #8 (Orbit 609)
---------------------------------------
Vector Time (GMT): 2014/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3782988
93 A = 6792896
68 meter
Y = -3575052
19 meter E =
0007900
Z = -4371937
55 I = 51
28114
XDOT = 2232
680379 Wp = 93
31790
YDOT = -6493
801270 meter/sec RA = 265
70980 deg
ZDOT = 3383
113127 TA = 211
16055
MA = 211
20742
Ha = 227
377 n
mi
Hp = 221
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12411381
01 X = -3721492
77
Y = -11729173
86 feet Y = -3617011
96 meter
Z = -14343627
15 Z = -4390166
00
XDOT = 7325
066859 XDOT = 2288
695140
YDOT = -21305
122278 feet/sec YDOT = -6468
520960 meter/sec
ZDOT = 11099
452515 ZDOT = 3394
095193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16857450
99 X = -5138151
06
Y = 2289651
08 feet Y = 697885
65 meter
Z = -14420103
39 Z = -4395247
51
XDOT = -11932
221217 XDOT = -3636
941027
YDOT = -17747
499942 feet/sec YDOT = -5409
437982 meter/sec
ZDOT = 11146
963957 ZDOT = 3397
594614
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
50995543
00016717 00000-0 10270-3 0 9077
2 25544 51
6467 266
5260 0002707 350
3543 9
7555 15
50109394 6102
Satellite: ISS
Catalog Number: 25544
Epoch time: 14134
50995543 = yrday
fracday
Element set: 907
Inclination: 51
6467 deg
RA of node: 266
5260 deg
Eccentricity:
0002707
Arg of perigee: 350
3543 deg
Mean anomaly: 9
7555 deg
Mean motion: 15
50109394 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 610
Checksum: 303
Coasting Arc #9 (Orbit 625)
---------------------------------------
Vector Time (GMT): 2014/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3950346
66 A = 6793722
45 meter
Y = 3671912
85 meter E =
0011159
Z = 4126181
09 I = 51
28756
XDOT = -2001
591792 Wp = 62
32725
YDOT = 6378
091490 meter/sec RA = 260
72875 deg
ZDOT = -3746
702628 TA = 66
53020
MA = 66
41295
Ha = 227
414 n
mi
Hp = 220
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12960454
93 X = 3888948
82
Y = 12046958
17 feet Y = 3715744
60 meter
Z = 13537339
54 Z = 4145222
83
XDOT = -6566
902205 XDOT = -2054
563632
YDOT = 20925
497013 feet/sec YDOT = 6355
412468 meter/sec
ZDOT = -12292
331457 ZDOT = -3756
554535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17405755
64 X = 5305274
32
Y = -2823550
37 feet Y = -860618
15 meter
Z = 13617246
00 Z = 4150536
58
XDOT = 12385
481682 XDOT = 3775
094817
YDOT = 16658
549730 feet/sec YDOT = 5077
525958 meter/sec
ZDOT = -12335
044165 ZDOT = -3759
721462
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 14135
54144221
00016717 00000-0 10270-3 0 9082
2 25544 51
6470 261
4147 0002678 356
2175 3
8955 15
50124512 6262
Satellite: ISS
Catalog Number: 25544
Epoch time: 14135
54144221 = yrday
fracday
Element set: 908
Inclination: 51
6470 deg
RA of node: 261
4147 deg
Eccentricity:
0002678
Arg of perigee: 356
2175 deg
Mean anomaly: 3
8955 deg
Mean motion: 15
50124512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 626
Checksum: 288
Coasting Arc #10 (Orbit 640)
---------------------------------------
Vector Time (GMT): 2014/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4153339
68 A = 6794440
13 meter
Y = -3728970
92 meter E =
0006163
Z = -3878477
21 I = 51
29682
XDOT = 1789
593397 Wp = 79
25562
YDOT = -6228
041554 meter/sec RA = 255
74941 deg
ZDOT = 4078
217320 TA = 233
75752
MA = 233
81449
Ha = 227
415 n
mi
Hp = 220
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13626442
52 X = -4092492
07
Y = -12234156
56 feet Y = -3775075
70 meter
Z = -12724662
76 Z = -3898506
40
XDOT = 5871
369414 XDOT = 1839
292751
YDOT = -20433
207197 feet/sec YDOT = -6207
751613 meter/sec
ZDOT = 13379
978084 ZDOT = 4087
031284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17905700
88 X = -5457657
63
Y = 3548729
72 feet Y = 1081652
82 meter
Z = -12808745
38 Z = -3904105
59
XDOT = -12664
090552 XDOT = -3860
014800
YDOT = -15545
471244 feet/sec YDOT = -4738
259635 meter/sec
ZDOT = 13418
275336 ZDOT = 4089
890323
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 14136
50843933
00016717 00000-0 10270-3 0 9096
2 25544 51
6475 256
6238 0002917 356
7728 3
3403 15
50167431 6416
Satellite: ISS
Catalog Number: 25544
Epoch time: 14136
50843933 = yrday
fracday
Element set: 909
Inclination: 51
6475 deg
RA of node: 256
6238 deg
Eccentricity:
0002917
Arg of perigee: 356
7728 deg
Mean anomaly: 3
3403 deg
Mean motion: 15
50167431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 641
Checksum: 306
Coasting Arc #11 (Orbit 656)
---------------------------------------
Vector Time (GMT): 2014/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4353744
09 A = 6795330
48 meter
Y = 3796641
12 meter E =
0012641
Z = 3571449
68 I = 51
30853
XDOT = -1636
474482 Wp = 73
86937
YDOT = 6045
651070 meter/sec RA = 250
77046 deg
ZDOT = -4415
404328 TA = 63
77439
MA = 63
64451
Ha = 227
466 n
mi
Hp = 220
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14283937
29 X = 4293616
43
Y = 12456171
65 feet Y = 3844990
98 meter
Z = 11717354
60 Z = 3592454
11
XDOT = -5369
010767 XDOT = -1682
507809
YDOT = 19834
813221 feet/sec YDOT = 6027
093956 meter/sec
ZDOT = -14486
234671 ZDOT = -4423
465483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18409693
69 X = 5611274
64
Y = -4265599
04 feet Y = -1300154
59 meter
Z = 11805563
04 Z = 3598335
61
XDOT = 12711
139307 XDOT = 3874
355261
YDOT = 14521
056008 feet/sec YDOT = 4426
017871 meter/sec
ZDOT = -14521
315203 ZDOT = -4426
096874
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 14137
53988375
00016717 00000-0 10270-3 0 9102
2 25544 51
6475 251
5127 0002864 3
4823 356
6348 15
50193046 6570
Satellite: ISS
Catalog Number: 25544
Epoch time: 14137
53988375 = yrday
fracday
Element set: 910
Inclination: 51
6475 deg
RA of node: 251
5127 deg
Eccentricity:
0002864
Arg of perigee: 3
4823 deg
Mean anomaly: 356
6348 deg
Mean motion: 15
50193046 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 657
Checksum: 316
Coasting Arc #12 (Orbit 671)
---------------------------------------
Vector Time (GMT): 2014/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4580823
04 A = 6796120
09 meter
Y = -3812565
88 meter E =
0006012
Z = -3266362
38 I = 51
32274
XDOT = 1509
700205 Wp = 53
55632
YDOT = -5844
000487 meter/sec RA = 245
79273 deg
ZDOT = 4713
576024 TA = 268
44551
MA = 268
51438
Ha = 227
470 n
mi
Hp = 220
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15028946
99 X = -4521982
54
Y = -12508418
24 feet Y = -3863462
31 meter
Z = -10716412
02 Z = -3288472
96
XDOT = 4953
084663 XDOT = 1552
039714
YDOT = -19173
229944 feet/sec YDOT = -5826
881708 meter/sec
ZDOT = 15464
488269 ZDOT = 4721
012352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18804465
57 X = -5731601
11
Y = 5169345
53 feet Y = 1575616
52 meter
Z = -10809310
90 Z = -3294677
96
XDOT = -12612
843415 XDOT = -3844
394673
YDOT = -13542
099323 feet/sec YDOT = -4127
631874 meter/sec
ZDOT = 15496
888421 ZDOT = 4723
451591
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 14138
50684163
00016717 00000-0 10270-3 0 9119
2 25544 51
6476 246
7213 0003123 3
4958 356
6214 15
50224264 6727
Satellite: ISS
Catalog Number: 25544
Epoch time: 14138
50684163 = yrday
fracday
Element set: 911
Inclination: 51
6476 deg
RA of node: 246
7213 deg
Eccentricity:
0003123
Arg of perigee: 3
4958 deg
Mean anomaly: 356
6214 deg
Mean motion: 15
50224264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 672
Checksum: 290
Coasting Arc #13 (Orbit 687)
---------------------------------------
Vector Time (GMT): 2014/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4798302
08 A = 6796982
69 meter
Y = 3835903
22 meter E =
0013705
Z = 2898350
21 I = 51
33899
XDOT = -1451
926748 Wp = 85
45194
YDOT = 5615
991735 meter/sec RA = 240
81630 deg
ZDOT = -5007
336031 TA = 61
42435
MA = 61
28650
Ha = 227
535 n
mi
Hp = 220
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15742460
89 X = 4740972
19
Y = 12584984
32 feet Y = 3889240
16 meter
Z = 9509023
00 Z = 2921520
83
XDOT = -4763
539198 XDOT = -1490
293977
YDOT = 18425
169734 feet/sec YDOT = 5599
541188 meter/sec
ZDOT = -16428
267818 ZDOT = -5014
482118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19176885
53 X = 5845114
71
Y = -6049150
82 feet Y = -1843781
17 meter
Z = 9606417
61 Z = 2928036
09
XDOT = 12289
842601 XDOT = 3745
944025
YDOT = 12711
072400 feet/sec YDOT = 3874
334867 meter/sec
ZDOT = -16459
397335 ZDOT = -5016
824308
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 14139
53824443
00016717 00000-0 10270-3 0 9121
2 25544 51
6471 241
6100 0003065 10
8114 349
3102 15
50259999 6887
Satellite: ISS
Catalog Number: 25544
Epoch time: 14139
53824443 = yrday
fracday
Element set: 912
Inclination: 51
6471 deg
RA of node: 241
6100 deg
Eccentricity:
0003065
Arg of perigee: 10
8114 deg
Mean anomaly: 349
3102 deg
Mean motion: 15
50259999 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 688
Checksum: 292
Coasting Arc #14 (Orbit 702)
---------------------------------------
Vector Time (GMT): 2014/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5030117
46 A = 6797752
41 meter
Y = -3799240
68 meter E =
0007965
Z = -2537960
05 I = 51
35794
XDOT = 1423
726185 Wp = 35
80262
YDOT = -5386
754748 meter/sec RA = 235
84086 deg
ZDOT = 5256
755737 TA = 295
63134
MA = 295
71361
Ha = 227
538 n
mi
Hp = 220
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16503010
04 X = -4974931
00
Y = -12464700
38 feet Y = -3855181
98 meter
Z = -8326640
58 Z = -2562261
91
XDOT = 4671
017667 XDOT = 1458
320552
YDOT = -17673
079882 feet/sec YDOT = -5370
640578 meter/sec
ZDOT = 17246
573940 ZDOT = 5263
755768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19384290
73 X = -5908331
82
Y = 7089071
53 feet Y = 2160749
00 meter
Z = -8428841
97 Z = -2569111
03
XDOT = -11875
136160 XDOT = -3619
541501
YDOT = -11985
752891 feet/sec YDOT = -3653
257481 meter/sec
ZDOT = 17277
042463 ZDOT = 5266
042543
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 14140
50516391
00016717 00000-0 10270-3 0 9131
2 25544 51
6474 236
8179 0003316 10
3930 349
7288 15
50279189 7032
Satellite: ISS
Catalog Number: 25544
Epoch time: 14140
50516391 = yrday
fracday
Element set: 913
Inclination: 51
6474 deg
RA of node: 236
8179 deg
Eccentricity:
0003316
Arg of perigee: 10
3930 deg
Mean anomaly: 349
7288 deg
Mean motion: 15
50279189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 703
Checksum: 307
Coasting Arc #15 (Orbit 718)
---------------------------------------
Vector Time (GMT): 2014/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 918514
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5242639
55 A = 6798464
10 meter
Y = 3768716
15 meter E =
0014126
Z = 2113066
56 I = 51
37825
XDOT = -1470
805163 Wp = 96
62462
YDOT = 5140
407908 meter/sec RA = 230
86744 deg
ZDOT = -5488
824418 TA = 59
91537
MA = 59
77537
Ha = 227
603 n
mi
Hp = 220
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17200261
00 X = 5189842
62
Y = 12364554
29 feet Y = 3827047
43 meter
Z = 6932633
06 Z = 2138406
59
XDOT = -4825
476258 XDOT = -1501
513976
YDOT = 16864
855341 feet/sec YDOT = 5123
788916 meter/sec
ZDOT = -18007
954127 ZDOT = -5496
043823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19545975
88 X = 5957613
45
Y = -8074430
57 feet Y = -2461086
44 meter
Z = 7039245
75 Z = 2145562
10
XDOT = 11265
961197 XDOT = 3433
864973
YDOT = 11460
457423 feet/sec YDOT = 3493
147423 meter/sec
ZDOT = -18039
305956 ZDOT = -5498
380456
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 14141
53652626
00016717 00000-0 10270-3 0 9148
2 25544 51
6467 231
7062 0003275 17
5819 342
5445 15
50326465 7191
Satellite: ISS
Catalog Number: 25544
Epoch time: 14141
53652626 = yrday
fracday
Element set: 914
Inclination: 51
6467 deg
RA of node: 231
7062 deg
Eccentricity:
0003275
Arg of perigee: 17
5819 deg
Mean anomaly: 342
5445 deg
Mean motion: 15
50326465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 719
Checksum: 303
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