[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 28th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 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
There are no maneuvers
Coasting Arc #1 (Orbit 1726)
---------------------------------------
Vector Time (GMT): 2014/206/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2305163
48 A = 6796894
90 meter
Y = -5777820
54 meter E =
0005346
Z = -2729746
45 I = 51
29565
XDOT = 4026
200586 Wp = 332
83332
YDOT = -4027
721646 meter/sec RA = 268
83564 deg
ZDOT = 5125
845218 TA = 356
17489
MA = 356
17898
Ha = 225
227 n
mi
Hp = 223
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7562872
32 X = -2227123
26
Y = -18956104
14 feet Y = -5803161
80 meter
Z = -8955861
05 Z = -2740755
31
XDOT = 13209
319509 XDOT = 4046
041013
YDOT = -13214
309861 feet/sec YDOT = -3982
587549 meter/sec
ZDOT = 16817
077487 ZDOT = 5145
451443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12014868
20 X = -3662131
83
Y = 16472799
22 feet Y = 5020909
20 meter
Z = -9001566
36 Z = -2743677
43
XDOT = -16968
280991 XDOT = -5171
932046
YDOT = -3141
934338 feet/sec YDOT = -957
661586 meter/sec
ZDOT = 16900
967264 ZDOT = 5151
414822
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
50555242
00016717 00000-0 10270-3 0 9008
2 25544 51
6467 269
6596 0006864 288
5807 71
4598 15
50439307 17274
Satellite: ISS
Catalog Number: 25544
Epoch time: 14206
50555242 = yrday
fracday
Element set: 900
Inclination: 51
6467 deg
RA of node: 269
6596 deg
Eccentricity:
0006864
Arg of perigee: 288
5807 deg
Mean anomaly: 71
4598 deg
Mean motion: 15
50439307 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1727
Checksum: 336
Coasting Arc #2 (Orbit 1742)
---------------------------------------
Vector Time (GMT): 2014/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2480378
40 A = 6797719
84 meter
Y = 5896727
67 meter E =
0006988
Z = 2290541
32 I = 51
30044
XDOT = -3939
392103 Wp = 101
25017
YDOT = 3755
989370 meter/sec RA = 263
85621 deg
ZDOT = -5390
763310 TA = 53
15929
MA = 53
09523
Ha = 225
558 n
mi
Hp = 222
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8137724
43 X = 2403129
01
Y = 19346219
39 feet Y = 5924032
78 meter
Z = 7514899
33 Z = 2302403
16
XDOT = -12924
514775 XDOT = -3954
913590
YDOT = 12322
799771 feet/sec YDOT = 3711
850118 meter/sec
ZDOT = -17686
231333 ZDOT = -5409
937389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11735395
35 X = 3576948
50
Y = -17379170
27 feet Y = -5297171
10 meter
Z = 7564219
22 Z = 2305574
02
XDOT = 16063
960546 XDOT = 4896
295175
YDOT = 3095
711084 feet/sec YDOT = 943
572738 meter/sec
ZDOT = -17768
236691 ZDOT = -5415
758544
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
53683225
00016717 00000-0 10270-3 0 9016
2 25544 51
6468 264
5473 0006900 294
0081 66
0347 15
50477596 17432
Satellite: ISS
Catalog Number: 25544
Epoch time: 14207
53683225 = yrday
fracday
Element set: 901
Inclination: 51
6468 deg
RA of node: 264
5473 deg
Eccentricity:
0006900
Arg of perigee: 294
0081 deg
Mean anomaly: 66
0347 deg
Mean motion: 15
50477596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1743
Checksum: 312
Coasting Arc #3 (Orbit 1757)
---------------------------------------
Vector Time (GMT): 2014/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2675132
18 A = 6798607
48 meter
Y = -5966360
00 meter E =
0008920
Z = -1840158
93 I = 51
30641
XDOT = 3896
107574 Wp = 349
99168
YDOT = -3475
756765 meter/sec RA = 258
87729 deg
ZDOT = 5610
009782 TA = 349
69882
MA = 349
71708
Ha = 225
717 n
mi
Hp = 222
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8776680
39 X = -2599277
44
Y = -19574671
91 feet Y = -5995850
83 meter
Z = -6037266
81 Z = -1852970
13
XDOT = 12782
505164 XDOT = 3907
433663
YDOT = -11403
401459 feet/sec YDOT = -3432
124932 meter/sec
ZDOT = 18405
543904 ZDOT = 5628
963465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11258464
18 X = -3431579
88
Y = 18242747
13 feet Y = 5560389
33 meter
Z = -6090619
92 Z = -1856420
95
XDOT = -15223
997936 XDOT = -4640
274571
YDOT = -3228
324597 feet/sec YDOT = -983
993337 meter/sec
ZDOT = 18486
562471 ZDOT = 5634
704241
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
50365329
00016717 00000-0 10270-3 0 9027
2 25544 51
6459 259
7543 0006867 297
7887 62
2567 15
50443007 17580
Satellite: ISS
Catalog Number: 25544
Epoch time: 14208
50365329 = yrday
fracday
Element set: 902
Inclination: 51
6459 deg
RA of node: 259
7543 deg
Eccentricity:
0006867
Arg of perigee: 297
7887 deg
Mean anomaly: 62
2567 deg
Mean motion: 15
50443007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1758
Checksum: 341
Coasting Arc #4 (Orbit 1773)
---------------------------------------
Vector Time (GMT): 2014/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2867002
27 A = 6799126
45 meter
Y = 6009965
52 meter E =
0006959
Z = 1358592
85 I = 51
31567
XDOT = -3900
952358 Wp = 117
03382
YDOT = 3171
875923 meter/sec RA = 253
89933 deg
ZDOT = -5779
408524 TA = 48
12743
MA = 48
06807
Ha = 225
951 n
mi
Hp = 222
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9406175
41 X = 2792984
90
Y = 19717734
65 feet Y = 6041612
29 meter
Z = 4457325
64 Z = 1372340
49
XDOT = -12798
400125 XDOT = -3908
057140
YDOT = 10406
417069 feet/sec YDOT = 3128
213428 meter/sec
ZDOT = -18961
314055 ZDOT = -5798
375565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10690695
50 X = 3258523
99
Y = -19038377
14 feet Y = -5802897
35 meter
Z = 4514662
00 Z = 1376068
98
XDOT = 14426
107004 XDOT = 4397
077415
YDOT = 3569
904567 feet/sec YDOT = 1088
106912 meter/sec
ZDOT = -19042
334798 ZDOT = -5804
103647
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
53492241
00016717 00000-0 10270-3 0 9036
2 25544 51
6460 254
6416 0006851 302
7259 57
3231 15
50489935 17749
Satellite: ISS
Catalog Number: 25544
Epoch time: 14209
53492241 = yrday
fracday
Element set: 903
Inclination: 51
6460 deg
RA of node: 254
6416 deg
Eccentricity:
0006851
Arg of perigee: 302
7259 deg
Mean anomaly: 57
3231 deg
Mean motion: 15
50489935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1774
Checksum: 309
Coasting Arc #5 (Orbit 1788)
---------------------------------------
Vector Time (GMT): 2014/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3063262
21 A = 6799695
30 meter
Y = -5998164
50 meter E =
0011908
Z = -876004
99 I = 51
32631
XDOT = 3953
556056 Wp = 4
20262
YDOT = -2878
659604 meter/sec RA = 248
92216 deg
ZDOT = 5902
446465 TA = 346
28817
MA = 346
32049
Ha = 226
133 n
mi
Hp = 222
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10050072
87 X = -2991706
42
Y = -19679017
39 feet Y = -6032019
76 meter
Z = -2874032
11 Z = -890711
91
XDOT = 12970
984436 XDOT = 3956
780405
YDOT = -9444
421273 feet/sec YDOT = -2834
430471 meter/sec
ZDOT = 19364
981842 ZDOT = 5921
659701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9943810
34 X = -3030873
39
Y = 19723880
81 feet Y = 6011838
87 meter
Z = -2935457
74 Z = -894727
52
XDOT = -13773
124470 XDOT = -4198
048338
YDOT = -4057
492078 feet/sec YDOT = -1236
723586 meter/sec
ZDOT = 19446
996116 ZDOT = 5927
444416
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
50173331
00016717 00000-0 10270-3 0 9042
2 25544 51
6456 249
8484 0006860 306
9020 53
1502 15
50453650 17893
Satellite: ISS
Catalog Number: 25544
Epoch time: 14210
50173331 = yrday
fracday
Element set: 904
Inclination: 51
6456 deg
RA of node: 249
8484 deg
Eccentricity:
0006860
Arg of perigee: 306
9020 deg
Mean anomaly: 53
1502 deg
Mean motion: 15
50453650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1789
Checksum: 289
Coasting Arc #6 (Orbit 1804)
---------------------------------------
Vector Time (GMT): 2014/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3242781
33 A = 6799850
59 meter
Y = 5962213
95 meter E =
0005969
Z = 368158
26 I = 51
33938
XDOT = -4053
438040 Wp = 130
66982
YDOT = 2576
744875 meter/sec RA = 243
94596 deg
ZDOT = -5966
429209 TA = 45
35263
MA = 45
30398
Ha = 226
298 n
mi
Hp = 222
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10639046
37 X = 3174081
11
Y = 19561069
39 feet Y = 5998092
69 meter
Z = 1207868
32 Z = 383744
15
XDOT = -13298
681232 XDOT = -4052
968013
YDOT = 8453
887386 feet/sec YDOT = 2531
419379 meter/sec
ZDOT = -19574
898981 ZDOT = -5986
118761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9146436
46 X = 2787833
83
Y = -20297924
63 feet Y = -6186807
43 meter
Z = 1273045
40 Z = 388024
24
XDOT = 13219
896259 XDOT = 4029
424380
YDOT = 4712
324054 feet/sec YDOT = 1436
316372 meter/sec
ZDOT = -19658
883792 ZDOT = -5992
027780
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
53299198
00016717 00000-0 10270-3 0 9057
2 25544 51
6457 244
7353 0006785 311
0444 49
0120 15
50493137 18059
Satellite: ISS
Catalog Number: 25544
Epoch time: 14211
53299198 = yrday
fracday
Element set: 905
Inclination: 51
6457 deg
RA of node: 244
7353 deg
Eccentricity:
0006785
Arg of perigee: 311
0444 deg
Mean anomaly: 49
0120 deg
Mean motion: 15
50493137 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1805
Checksum: 300
Coasting Arc #7 (Orbit 1820)
---------------------------------------
Vector Time (GMT): 2014/212/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3410210
27 A = 6799967
17 meter
Y = -5871043
98 meter E =
0013944
Z = 130222
11 I = 51
35404
XDOT = 4199
951877 Wp = 17
38325
YDOT = -2303
385247 meter/sec RA = 238
97100 deg
ZDOT = 5985
836197 TA = 344
02366
MA = 344
06759
Ha = 226
478 n
mi
Hp = 221
974
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11188353
89 X = -3344938
02
Y = -19261955
32 feet Y = -5908814
19 meter
Z = 427237
88 Z = 113814
56
XDOT = 13779
369675 XDOT = 4196
319832
YDOT = -7557
038211 feet/sec YDOT = -2256
438971 meter/sec
ZDOT = 19638
570199 ZDOT = 6006
229880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8214686
60 X = -2503836
47
Y = 20706885
03 feet Y = 6311458
56 meter
Z = 358544
80 Z = 109284
45
XDOT = -12872
726251 XDOT = -3923
606961
YDOT = -5458
700210 feet/sec YDOT = -1663
811824 meter/sec
ZDOT = 19725
499197 ZDOT = 6012
332155
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
56424633
00016717 00000-0 10270-3 0 9066
2 25544 51
6457 239
6225 0006858 315
6366 44
4235 15
50476032 18213
Satellite: ISS
Catalog Number: 25544
Epoch time: 14212
56424633 = yrday
fracday
Element set: 906
Inclination: 51
6457 deg
RA of node: 239
6225 deg
Eccentricity:
0006858
Arg of perigee: 315
6366 deg
Mean anomaly: 44
4235 deg
Mean motion: 15
50476032 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1821
Checksum: 303
Coasting Arc #8 (Orbit 1835)
---------------------------------------
Vector Time (GMT): 2014/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3548558
51 A = 6799742
86 meter
Y = 5762096
02 meter E =
0003934
Z = -646202
41 I = 51
37016
XDOT = -4385
712771 Wp = 140
18816
YDOT = 2037
526640 meter/sec RA = 233
99680 deg
ZDOT = -5938
481087 TA = 46
80114
MA = 46
76828
Ha = 226
616 n
mi
Hp = 221
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11642252
32 X = 3487000
70
Y = 18904514
49 feet Y = 5801434
09 meter
Z = -2120086
65 Z = -629113
73
XDOT = -14388
821426 XDOT = -4379
323968
YDOT = 6684
798689 feet/sec YDOT = 1988
518469 meter/sec
ZDOT = -19483
205666 ZDOT = -5959
770534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7286595
08 X = 2220954
18
Y = -20979198
45 feet Y = -6394459
69 meter
Z = -2048472
45 Z = -624374
40
XDOT = 12664
653812 XDOT = 3860
186482
YDOT = 6302
343843 feet/sec YDOT = 1920
954403 meter/sec
ZDOT = -19573
895757 ZDOT = -5966
123427
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
53104085
00016717 00000-0 10270-3 0 9071
2 25544 51
6455 234
8290 0006773 318
9802 41
0839 15
50494928 18360
Satellite: ISS
Catalog Number: 25544
Epoch time: 14213
53104085 = yrday
fracday
Element set: 907
Inclination: 51
6455 deg
RA of node: 234
8290 deg
Eccentricity:
0006773
Arg of perigee: 318
9802 deg
Mean anomaly: 41
0839 deg
Mean motion: 15
50494928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1836
Checksum: 315
Coasting Arc #9 (Orbit 1851)
---------------------------------------
Vector Time (GMT): 2014/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3658907
51 A = 6799356
50 meter
Y = -5604248
86 meter E =
0014806
Z = 1142593
08 I = 51
38797
XDOT = 4612
325326 Wp = 29
89873
YDOT = -1814
467202 meter/sec RA = 229
02413 deg
ZDOT = 5850
069213 TA = 342
53807
MA = 342
58893
Ha = 226
764 n
mi
Hp = 221
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12004289
73 X = -3601517
89
Y = -18386643
23 feet Y = -5644844
23 meter
Z = 3748664
95 Z = 1124958
14
XDOT = 15132
300938 XDOT = 4603
854771
YDOT = -5952
976384 feet/sec YDOT = -1762
936569 meter/sec
ZDOT = 19193
140461 ZDOT = 5872
454498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6288683
68 X = -1916790
79
Y = 21051678
83 feet Y = 6416551
71 meter
Z = 3674695
38 Z = 1120047
15
XDOT = -12696
497773 XDOT = -3869
892521
YDOT = -7171
497238 feet/sec YDOT = -2185
872358 meter/sec
ZDOT = 19288
450320 ZDOT = 5879
119658
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
56228363
00016717 00000-0 10270-3 0 9082
2 25544 51
6455 229
7164 0006884 323
2576 36
8102 15
50505673 18526
Satellite: ISS
Catalog Number: 25544
Epoch time: 14214
56228363 = yrday
fracday
Element set: 908
Inclination: 51
6455 deg
RA of node: 229
7164 deg
Eccentricity:
0006884
Arg of perigee: 323
2576 deg
Mean anomaly: 36
8102 deg
Mean motion: 15
50505673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1852
Checksum: 312
Coasting Arc #10 (Orbit 1866)
---------------------------------------
Vector Time (GMT): 2014/215/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3731358
78 A = 6798769
69 meter
Y = 5439209
56 meter E =
0001204
Z = -1647364
35 I = 51
40653
XDOT = -4863
022750 Wp = 115
38655
YDOT = 1613
900158 meter/sec RA = 224
05189 deg
ZDOT = -5690
034013 TA = 82
67373
MA = 82
66005
Ha = 226
918 n
mi
Hp = 221
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12241990
74 X = 3678261
29
Y = 17845175
73 feet Y = 5480639
15 meter
Z = -5404738
69 Z = -1629366
95
XDOT = -15954
799050 XDOT = -4853
068119
YDOT = 5294
948025 feet/sec YDOT = 1559
574420 meter/sec
ZDOT = -18668
090593 ZDOT = -5713
633565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5354578
06 X = 1632075
39
Y = -20987044
27 feet Y = -6396851
09 meter
Z = -5329193
29 Z = -1624338
11
XDOT = 12878
512661 XDOT = 3925
370659
YDOT = 8048
450882 feet/sec YDOT = 2453
167829 meter/sec
ZDOT = -18768
529387 ZDOT = -5720
647757
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
52906885
00016717 00000-0 10270-3 0 9092
2 25544 51
6449 224
9228 0006846 326
8000 33
2720 15
50503390 18673
Satellite: ISS
Catalog Number: 25544
Epoch time: 14215
52906885 = yrday
fracday
Element set: 909
Inclination: 51
6449 deg
RA of node: 224
9228 deg
Eccentricity:
0006846
Arg of perigee: 326
8000 deg
Mean anomaly: 33
2720 deg
Mean motion: 15
50503390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1867
Checksum: 309
Coasting Arc #11 (Orbit 1882)
---------------------------------------
Vector Time (GMT): 2014/216/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3762189
53 A = 6797934
69 meter
Y = -5236719
10 meter E =
0014460
Z = 2123127
76 I = 51
42675
XDOT = 5145
405047 Wp = 41
69682
YDOT = -1465
000055 meter/sec RA = 219
08128 deg
ZDOT = 5493
226805 TA = 341
88334
MA = 341
93481
Ha = 227
025 n
mi
Hp = 221
200
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12343141
49 X = -3713665
14
Y = -17180836
95 feet Y = -5278519
07 meter
Z = 6965642
24 Z = 2104969
40
XDOT = 16881
250153 XDOT = 5134
720404
YDOT = -4806
430628 feet/sec YDOT = -1407
520692 meter/sec
ZDOT = 18022
397655 ZDOT = 5518
196341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4425663
55 X = -1348942
25
Y = 20712424
98 feet Y = 6313147
13 meter
Z = 6889370
48 Z = 2099880
12
XDOT = -13303
813037 XDOT = -4055
002214
YDOT = -8884
748471 feet/sec YDOT = -2708
071334 meter/sec
ZDOT = 18128
637764 ZDOT = 5525
608790
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
56029997
00016717 00000-0 10270-3 0 9109
2 25544 51
6446 219
8103 0006953 330
3041 29
7715 15
50535652 18837
Satellite: ISS
Catalog Number: 25544
Epoch time: 14216
56029997 = yrday
fracday
Element set: 910
Inclination: 51
6446 deg
RA of node: 219
8103 deg
Eccentricity:
0006953
Arg of perigee: 330
3041 deg
Mean anomaly: 29
7715 deg
Mean motion: 15
50535652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1883
Checksum: 310
Coasting Arc #12 (Orbit 1897)
---------------------------------------
Vector Time (GMT): 2014/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3751589
26 A = 6797043
40 meter
Y = 5040835
35 meter E =
0003261
Z = -2597113
10 I = 51
44756
XDOT = -5430
837911 Wp = 18
86128
YDOT = 1349
777578 meter/sec RA = 214
11070 deg
ZDOT = -5223
957622 TA = 190
37626
MA = 190
38299
Ha = 227
210 n
mi
Hp = 221
035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12308363
71 X = 3707558
51
Y = 16538173
73 feet Y = 5082541
95 meter
Z = -8520712
26 Z = -2578995
27
XDOT = -17817
709683 XDOT = -5420
151660
YDOT = 4428
404127 feet/sec YDOT = 1289
106400 meter/sec
ZDOT = -17138
968577 ZDOT = -5250
313690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3616723
73 X = 1102377
39
Y = -20327766
55 feet Y = -6195903
24 meter
Z = -8444569
95 Z = -2573904
92
XDOT = 13856
276084 XDOT = 4223
392950
YDOT = 9633
388108 feet/sec YDOT = 2936
256695 meter/sec
ZDOT = -17251
088938 ZDOT = -5258
131908
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
52707554
00016717 00000-0 10270-3 0 9119
2 25544 51
6437 215
0164 0006975 334
6658 25
4150 15
50519725 18982
Satellite: ISS
Catalog Number: 25544
Epoch time: 14217
52707554 = yrday
fracday
Element set: 911
Inclination: 51
6437 deg
RA of node: 215
0164 deg
Eccentricity:
0006975
Arg of perigee: 334
6658 deg
Mean anomaly: 25
4150 deg
Mean motion: 15
50519725 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1898
Checksum: 315
Coasting Arc #13 (Orbit 1913)
---------------------------------------
Vector Time (GMT): 2014/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3689421
30 A = 6795891
17 meter
Y = -4822495
38 meter E =
0013046
Z = 3033307
33 I = 51
46996
XDOT = 5736
879160 Wp = 52
30539
YDOT = -1288
821561 meter/sec RA = 209
14184 deg
ZDOT = 4922
044539 TA = 342
53402
MA = 342
57885
Ha = 227
285 n
mi
Hp = 220
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12104400
61 X = -3649955
54
Y = -15821835
24 feet Y = -4863532
35 meter
Z = 9951795
69 Z = 3015480
42
XDOT = 18821
782020 XDOT = 5726
955195
YDOT = -4228
417196 feet/sec YDOT = -1224
723813 meter/sec
ZDOT = 16148
440090 ZDOT = 4949
889063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2887895
23 X = -880230
46
Y = 19748247
65 feet Y = 6019265
88 meter
Z = 9876841
48 Z = 3010461
28
XDOT = -14626
306481 XDOT = -4458
098215
YDOT = -10285
661050 feet/sec YDOT = -3135
069488 meter/sec
ZDOT = 16266
885346 ZDOT = 4958
146653
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 14218
55829492
00016717 00000-0 10270-3 0 9120
2 25544 51
6433 209
9037 0007055 337
3165 22
7673 15
50560905 19147
Satellite: ISS
Catalog Number: 25544
Epoch time: 14218
55829492 = yrday
fracday
Element set: 912
Inclination: 51
6433 deg
RA of node: 209
9037 deg
Eccentricity:
0007055
Arg of perigee: 337
3165 deg
Mean anomaly: 22
7673 deg
Mean motion: 15
50560905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1914
Checksum: 311
Coasting Arc #14 (Orbit 1928)
---------------------------------------
Vector Time (GMT): 2014/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3588800
11 A = 6794807
91 meter
Y = 4626060
24 meter E =
0007367
Z = -3457468
28 I = 51
49329
XDOT = -6021
447877 Wp = 22
19196
YDOT = 1266
818669 meter/sec RA = 204
17267 deg
ZDOT = -4551
690288 TA = 198
33387
MA = 198
36044
Ha = 227
481 n
mi
Hp = 220
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11774278
58 X = 3553598
76
Y = 15177362
98 feet Y = 4665995
87 meter
Z = -11343399
86 Z = -3440119
88
XDOT = -19755
406419 XDOT = -6013
055857
YDOT = 4156
229228 feet/sec YDOT = 1199
530119 meter/sec
ZDOT = -14933
367085 ZDOT = -4580
920791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2320456
69 X = 707275
20
Y = -19111554
81 feet Y = -5825201
91 meter
Z = -11270432
86 Z = -3435227
94
XDOT = 15466
804358 XDOT = 4714
281968
YDOT = 10764
528485 feet/sec YDOT = 3281
028282 meter/sec
ZDOT = -15057
711065 ZDOT = -4589
590333
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 14219
52506006
00016717 00000-0 10270-3 0 9132
2 25544 51
6428 205
1095 0007119 342
3827 17
7076 15
50539808 19290
Satellite: ISS
Catalog Number: 25544
Epoch time: 14219
52506006 = yrday
fracday
Element set: 913
Inclination: 51
6428 deg
RA of node: 205
1095 deg
Eccentricity:
0007119
Arg of perigee: 342
3827 deg
Mean anomaly: 17
7076 deg
Mean motion: 15
50539808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1929
Checksum: 306
Coasting Arc #15 (Orbit 1944)
---------------------------------------
Vector Time (GMT): 2014/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3431280
24 A = 6793505
82 meter
Y = -4423837
80 meter E =
0010845
Z = 3835449
71 I = 51
51806
XDOT = 6315
068113 Wp = 60
36825
YDOT = -1295
254149 meter/sec RA = 199
20552 deg
ZDOT = 4152
053549 TA = 345
85007
MA = 345
88043
Ha = 227
539 n
mi
Hp = 220
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11257481
10 X = -3400187
89
Y = -14513903
53 feet Y = -4462034
91 meter
Z = 12583496
43 Z = 3818856
66
XDOT = 20718
727406 XDOT = 6308
913618
YDOT = -4249
521485 feet/sec YDOT = -1224
669580 meter/sec
ZDOT = 13622
222930 ZDOT = 4182
715701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1897856
05 X = -578466
52
Y = 18317596
23 feet Y = 5583203
33 meter
Z = 12513691
27 Z = 3814173
10
XDOT = -16474
994230 XDOT = -5021
578241
YDOT = -11110
200687 feet/sec YDOT = -3386
389169 meter/sec
ZDOT = 13752
669393 ZDOT = 4191
813631
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 14220
55626751
00016717 00000-0 10270-3 0 9148
2 25544 51
6427 199
9966 0007167 344
4880 15
6050 15
50582278 19457
Satellite: ISS
Catalog Number: 25544
Epoch time: 14220
55626751 = yrday
fracday
Element set: 914
Inclination: 51
6427 deg
RA of node: 199
9966 deg
Eccentricity:
0007167
Arg of perigee: 344
4880 deg
Mean anomaly: 15
6050 deg
Mean motion: 15
50582278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1945
Checksum: 329
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