[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 30th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 637 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
186/07:13:02
000 0
0 0
0 0
0
N/A 0
0 0
0 219
7
000/00:00:00
000 0
0 0
0 211
5
191/02:58:39
097 3
2 3
9 3
9
N/A -2
1 -0
4 219
5
000/00:11:54
194 0
5 0
0 214
1
Coasting Arc #1 (Orbit 2995)
---------------------------------------
Vector Time (GMT): 2015/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5935891
77 A = 6781055
87 meter
Y = 361170
26 meter E =
0015451
Z = 3243889
45 I = 51
78897
XDOT = -2939
307229 Wp = 94
17482
YDOT = -5238
830024 meter/sec RA = 21
94884 deg
ZDOT = -4776
799030 TA = 48
27540
MA = 48
14335
Ha = 219
936 n
mi
Hp = 211
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19474710
53 X = -5955246
92
Y = 1184941
80 feet Y = 294682
57 meter
Z = 10642681
92 Z = 3215007
01
XDOT = -9643
396420 XDOT = -2857
302976
YDOT = -17187
762546 feet/sec YDOT = -5271
240118 meter/sec
ZDOT = -15671
912829 ZDOT = -4790
879179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3361668
72 X = 1024636
63
Y = 19287244
91 feet Y = 5878752
25 meter
Z = 10518387
86 Z = 3206004
62
XDOT = -14609
042129 XDOT = -4452
836041
YDOT = 11158
876214 feet/sec YDOT = 3401
225470 meter/sec
ZDOT = -15731
360026 ZDOT = -4794
918536
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15180
53879358
00016717 00000-0 10270-3 0 9000
2 25544 51
6430 22
3529 0002649 100
2328 259
9124 15
55473383 29963
Satellite: ISS
Catalog Number: 25544
Epoch time: 15180
53879358 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 22
3529 deg
Eccentricity:
0002649
Arg of perigee: 100
2328 deg
Mean anomaly: 259
9124 deg
Mean motion: 15
55473383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2996
Checksum: 317
Coasting Arc #2 (Orbit 3010)
---------------------------------------
Vector Time (GMT): 2015/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6586747
06 A = 6784821
36 meter
Y = 911848
16 meter E =
0010239
Z = -1333851
76 I = 51
76983
XDOT = 488
084098 Wp = 51
81847
YDOT = 4953
336193 meter/sec RA = 16
97384 deg
ZDOT = 5832
971536 TA = 293
68204
MA = 293
78946
Ha = 219
961 n
mi
Hp = 211
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21610062
55 X = 6582540
36
Y = 2991627
82 feet Y = 985482
15 meter
Z = -4376154
06 Z = -1301864
74
XDOT = 1601
325781 XDOT = 404
324080
YDOT = 16251
102994 feet/sec YDOT = 4958
325085 meter/sec
ZDOT = 19137
045723 ZDOT = 5835
139832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 179558
63 X = 54729
47
Y = -21842524
47 feet Y = -6657601
46 meter
Z = -4238779
10 Z = -1291979
87
XDOT = 14334
220027 XDOT = 4369
070264
YDOT = -3573
501053 feet/sec YDOT = -1089
203121 meter/sec
ZDOT = 19145
318384 ZDOT = 5835
493043
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15181
50251358
00016717 00000-0 10270-3 0 9013
2 25544 51
6413 17
5380 0002755 106
5586 253
5870 15
55434506 30119
Satellite: ISS
Catalog Number: 25544
Epoch time: 15181
50251358 = yrday
fracday
Element set: 901
Inclination: 51
6413 deg
RA of node: 17
5380 deg
Eccentricity:
0002755
Arg of perigee: 106
5586 deg
Mean anomaly: 253
5870 deg
Mean motion: 15
55434506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3011
Checksum: 286
Coasting Arc #3 (Orbit 3026)
---------------------------------------
Vector Time (GMT): 2015/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6411429
39 A = 6785104
87 meter
Y = -2040062
49 meter E =
0012502
Z = -839229
32 I = 51
74050
XDOT = 2150
686598 Wp = 133
43941
YDOT = -4338
401462 meter/sec RA = 12
00557 deg
ZDOT = -5948
306594 TA = 55
63003
MA = 55
51184
Ha = 219
847 n
mi
Hp = 211
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21034873
34 X = -6384063
78
Y = -6693118
41 feet Y = -2111606
16 meter
Z = -2753377
03 Z = -870308
47
XDOT = 7056
058393 XDOT = 2227
934281
YDOT = -14233
600597 feet/sec YDOT = -4313
918279 meter/sec
ZDOT = -19515
441582 ZDOT = -5937
672048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3556894
35 X = -1084141
40
Y = 21768344
49 feet Y = 6634991
40 meter
Z = -2886606
34 Z = -879837
61
XDOT = -13542
976468 XDOT = -4127
899228
YDOT = -4768
042648 feet/sec YDOT = -1453
299399 meter/sec
ZDOT = -19468
780968 ZDOT = -5934
084439
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15182
53047218
00016717 00000-0 10270-3 0 9026
2 25544 51
6413 12
4029 0002777 108
0408 252
1048 15
55468856 30271
Satellite: ISS
Catalog Number: 25544
Epoch time: 15182
53047218 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 12
4029 deg
Eccentricity:
0002777
Arg of perigee: 108
0408 deg
Mean anomaly: 252
1048 deg
Mean motion: 15
55468856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3027
Checksum: 291
Coasting Arc #4 (Orbit 3042)
---------------------------------------
Vector Time (GMT): 2015/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5417346
50 A = 6781905
57 meter
Y = 2922053
79 meter E =
0015702
Z = 2832593
86 I = 51
69794
XDOT = -4557
417379 Wp = 86
38347
YDOT = 3490
376856 meter/sec RA = 7
02849 deg
ZDOT = 5092
114099 TA = 305
80594
MA = 305
95177
Ha = 219
774 n
mi
Hp = 211
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17773446
52 X = 5370509
22
Y = 9586790
65 feet Y = 2982371
82 meter
Z = 9293286
95 Z = 2858796
68
XDOT = -14952
156756 XDOT = -4620
844229
YDOT = 11451
367638 feet/sec YDOT = 3439
057472 meter/sec
ZDOT = 16706
411085 ZDOT = 5069
821701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6575405
30 X = 2004183
54
Y = -19038657
01 feet Y = -5802982
66 meter
Z = 9405356
08 Z = 2866752
53
XDOT = 12363
666423 XDOT = 3768
445526
YDOT = 12512
918587 feet/sec YDOT = 3813
937585 meter/sec
ZDOT = 16609
793834 ZDOT = 5062
665161
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15183
55842249
00016717 00000-0 10270-3 0 9037
2 25544 51
6405 7
2666 0002791 116
2522 243
8918 15
55483409 30437
Satellite: ISS
Catalog Number: 25544
Epoch time: 15183
55842249 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 7
2666 deg
Eccentricity:
0002791
Arg of perigee: 116
2522 deg
Mean anomaly: 243
8918 deg
Mean motion: 15
55483409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3043
Checksum: 308
Coasting Arc #5 (Orbit 3057)
---------------------------------------
Vector Time (GMT): 2015/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3686694
53 A = 6777078
07 meter
Y = -3614836
05 meter E =
0011370
Z = -4400623
52 I = 51
65034
XDOT = 6425
757067 Wp = 79
78387
YDOT = -2446
625537 meter/sec RA = 2
03562 deg
ZDOT = -3378
997121 TA = 156
02092
MA = 155
96793
Ha = 219
853 n
mi
Hp = 211
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12095454
51 X = -3624622
28
Y = -11859698
32 feet Y = -3655715
45 meter
Z = -14437741
22 Z = -4418382
23
XDOT = 21081
880142 XDOT = 6469
051926
YDOT = -8026
986671 feet/sec YDOT = -2374
526008 meter/sec
ZDOT = -11085
948560 ZDOT = -3347
677608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9509923
71 X = -2898624
75
Y = 13940047
62 feet Y = 4248926
52 meter
Z = -14513347
60 Z = -4423668
35
XDOT = -10683
318401 XDOT = -3256
275449
YDOT = -18670
708115 feet/sec YDOT = -5690
831834 meter/sec
ZDOT = -10950
732820 ZDOT = -3337
783364
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15184
52212009
00016717 00000-0 10270-3 0 9041
2 25544 51
6406 2
4521 0002946 115
9535 244
1922 15
55490073 30587
Satellite: ISS
Catalog Number: 25544
Epoch time: 15184
52212009 = yrday
fracday
Element set: 904
Inclination: 51
6406 deg
RA of node: 2
4521 deg
Eccentricity:
0002946
Arg of perigee: 115
9535 deg
Mean anomaly: 244
1922 deg
Mean motion: 15
55490073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3058
Checksum: 282
Coasting Arc #6 (Orbit 3073)
---------------------------------------
Vector Time (GMT): 2015/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 877726
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1486886
09 A = 6773885
89 meter
Y = 4057968
97 meter E =
0006697
Z = 5211697
52 I = 51
60723
XDOT = -7481
673171 Wp = 120
99047
YDOT = 1285
030264 meter/sec RA = 357
02497 deg
ZDOT = 1129
494076 TA = 318
16124
MA = 318
21241
Ha = 219
860 n
mi
Hp = 211
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4878235
20 X = 1416082
31
Y = 13313546
47 feet Y = 4074199
84 meter
Z = 17098745
14 Z = 5218748
88
XDOT = -24546
171821 XDOT = -7500
973210
YDOT = 4215
978558 feet/sec YDOT = 1201
257259 meter/sec
ZDOT = 3705
689226 ZDOT = 1093
103375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12117137
17 X = 3693303
41
Y = -7294804
22 feet Y = -2223456
33 meter
Z = 17128210
71 Z = 5220678
62
XDOT = 8434
060693 XDOT = 2570
701699
YDOT = 22376
608429 feet/sec YDOT = 6820
390249 meter/sec
ZDOT = 3548
915361 ZDOT = 1081
709402
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15185
55005663
00016717 00000-0 10270-3 0 9052
2 25544 51
6405 357
3160 0002924 119
4744 240
6702 15
55450564 30740
Satellite: ISS
Catalog Number: 25544
Epoch time: 15185
55005663 = yrday
fracday
Element set: 905
Inclination: 51
6405 deg
RA of node: 357
3160 deg
Eccentricity:
0002924
Arg of perigee: 119
4744 deg
Mean anomaly: 240
6702 deg
Mean motion: 15
55450564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3074
Checksum: 296
Coasting Arc #7 (Orbit 3085)
---------------------------------------
Vector Time (GMT): 2015/186/07:13:02
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3198187
47 A = 6775213
35 meter
Y = -3490711
16 meter E =
0013842
Z = -4859376
26 I = 51
59153
XDOT = 6714
895093 Wp = 79
87214
YDOT = -2765
825439 meter/sec RA = 353
03727 deg
ZDOT = -2436
110123 TA = 166
20168
MA = 166
16381
Ha = 219
677 n
mi
Hp = 211
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10492741
03 X = -3135311
14
Y = -11452464
42 feet Y = -3526123
37 meter
Z = -15942835
50 Z = -4874759
80
XDOT = 22030
495712 XDOT = 6757
157680
YDOT = -9074
230443 feet/sec YDOT = -2690
498553 meter/sec
ZDOT = -7992
487280 ZDOT = -2403
388571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14757657
17 X = -4498133
91
Y = -4623621
92 feet Y = -1409279
96 meter
Z = -16008255
20 Z = -4879316
19
XDOT = 14119
089362 XDOT = 4303
498438
YDOT = -17922
275628 feet/sec YDOT = -5462
709612 meter/sec
ZDOT = -7851
185370 ZDOT = -2393
041301
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15186
32100086
00016717 00000-0 10270-3 0 9064
2 25544 51
6450 353
4690 0002569 118
1558 241
9856 15
55515529 30869
Satellite: ISS
Catalog Number: 25544
Epoch time: 15186
32100086 = yrday
fracday
Element set: 906
Inclination: 51
6450 deg
RA of node: 353
4690 deg
Eccentricity:
0002569
Arg of perigee: 118
1558 deg
Mean anomaly: 241
9856 deg
Mean motion: 15
55515529 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3086
Checksum: 317
Coasting Arc #8 (Orbit 3101)
---------------------------------------
Vector Time (GMT): 2015/187/07:13:02
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 925667
69 A = 6773276
86 meter
Y = 4106719
04 meter E =
0004787
Z = 5302190
77 I = 51
55389
XDOT = -7499
813976 Wp = 106
29738
YDOT = 1628
998805 meter/sec RA = 348
01965 deg
ZDOT = 46
269902 TA = 343
25367
MA = 343
26947
Ha = 219
619 n
mi
Hp = 211
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3036967
50 X = 853920
88
Y = 13473487
66 feet Y = 4116668
91 meter
Z = 17395639
01 Z = 5306513
47
XDOT = -24605
688896 XDOT = -7517
697189
YDOT = 5344
484268 feet/sec YDOT = 1545
030977 meter/sec
ZDOT = 151
804140 ZDOT = 9
794442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9513987
70 X = 2899863
45
Y = 9981235
43 feet Y = 3042280
56 meter
Z = 17413364
85 Z = 5307593
61
XDOT = -17497
682120 XDOT = -5333
293510
YDOT = 16680
252231 feet/sec YDOT = 5084
140880 meter/sec
ZDOT = -5
392225 ZDOT = -1
643550
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15187
34892167
00016717 00000-0 10270-3 0 9076
2 25544 51
6453 348
3341 0002584 122
5028 237
6376 15
55525501 31025
Satellite: ISS
Catalog Number: 25544
Epoch time: 15187
34892167 = yrday
fracday
Element set: 907
Inclination: 51
6453 deg
RA of node: 348
3341 deg
Eccentricity:
0002584
Arg of perigee: 122
5028 deg
Mean anomaly: 237
6376 deg
Mean motion: 15
55525501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3102
Checksum: 305
Coasting Arc #9 (Orbit 3116)
---------------------------------------
Vector Time (GMT): 2015/188/07:13:02
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1414393
81 A = 6775172
35 meter
Y = -4491358
62 meter E =
0014230
Z = -4884738
80 I = 51
52860
XDOT = 7282
852475 Wp = 109
94068
YDOT = -268
601703 meter/sec RA = 342
99867 deg
ZDOT = 2356
591811 TA = 183
19513
MA = 183
20422
Ha = 219
570 n
mi
Hp = 211
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4640399
64 X = 1488240
12
Y = -14735428
54 feet Y = -4475128
73 meter
Z = -16026045
92 Z = -4877688
94
XDOT = 23893
872951 XDOT = 7273
867449
YDOT = -881
239183 feet/sec YDOT = -187
210461 meter/sec
ZDOT = 7731
600431 ZDOT = 2391
948286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3882142
24 X = -1183276
95
Y = -14986524
85 feet Y = -4567892
78 meter
Z = -15994791
51 Z = -4875212
45
XDOT = 18576
836359 XDOT = 5662
219722
YDOT = -13223
310620 feet/sec YDOT = -4030
465077 meter/sec
ZDOT = 7883
690090 ZDOT = 2402
948739
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15188
31259021
00016717 00000-0 10270-3 0 9081
2 25544 51
6446 343
5194 0002446 125
5745 234
5637 15
55536222 31170
Satellite: ISS
Catalog Number: 25544
Epoch time: 15188
31259021 = yrday
fracday
Element set: 908
Inclination: 51
6446 deg
RA of node: 343
5194 deg
Eccentricity:
0002446
Arg of perigee: 125
5745 deg
Mean anomaly: 234
5637 deg
Mean motion: 15
55536222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3117
Checksum: 305
Coasting Arc #10 (Orbit 3132)
---------------------------------------
Vector Time (GMT): 2015/189/07:13:02
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3504389
86 A = 6779609
41 meter
Y = 4523753
33 meter E =
0013833
Z = 3623187
36 I = 51
51381
XDOT = -6173
838043 Wp = 92
25221
YDOT = -1261
892076 meter/sec RA = 337
98846 deg
ZDOT = -4381
935727 TA = 44
63645
MA = 44
52517
Ha = 219
504 n
mi
Hp = 211
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11497342
07 X = -3572315
07
Y = 14841710
40 feet Y = 4484184
93 meter
Z = 11887097
65 Z = 3605999
13
XDOT = -20255
374157 XDOT = -6137
982755
YDOT = -4140
065867 feet/sec YDOT = -1330
731231 meter/sec
ZDOT = -14376
429550 ZDOT = -4411
839821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1508317
14 X = -459735
06
Y = 18760706
15 feet Y = 5718263
23 meter
Z = 11812248
60 Z = 3600373
37
XDOT = -17752
203335 XDOT = -5410
871577
YDOT = 7734
304244 feet/sec YDOT = 2357
415934 meter/sec
ZDOT = -14504
746950 ZDOT = -4421
046870
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 15189
34049477
00016717 00000-0 10270-3 0 9098
2 25544 51
6448 338
3846 0002305 126
8671 233
2694 15
55577289 31339
Satellite: ISS
Catalog Number: 25544
Epoch time: 15189
34049477 = yrday
fracday
Element set: 909
Inclination: 51
6448 deg
RA of node: 338
3846 deg
Eccentricity:
0002305
Arg of perigee: 126
8671 deg
Mean anomaly: 233
2694 deg
Mean motion: 15
55577289 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3133
Checksum: 341
Coasting Arc #11 (Orbit 3147)
---------------------------------------
Vector Time (GMT): 2015/190/07:13:02
000
Vector Time (MET): N/A
Weight (LBS) : 892160
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5048577
63 A = 6783928
99 meter
Y = -4164171
45 meter E =
0007709
Z = -1781666
23 I = 51
49750
XDOT = 4330
359593 Wp = 54
98189
YDOT = 2840
529617 meter/sec RA = 332
99130 deg
ZDOT = 5653
328026 TA = 285
40518
MA = 285
49033
Ha = 219
486 n
mi
Hp = 211
833
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16563574
89 X = 5103421
80
Y = -13661979
82 feet Y = -4107408
17 meter
Z = -5845361
66 Z = -1757008
40
XDOT = 14207
216511 XDOT = 4270
812622
YDOT = 9319
322889 feet/sec YDOT = 2888
621190 meter/sec
ZDOT = 18547
664126 ZDOT = 5674
219562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6002802
63 X = 1829654
24
Y = -20644761
90 feet Y = -6292523
43 meter
Z = -5738477
61 Z = -1749087
98
XDOT = 15385
823683 XDOT = 4689
599059
YDOT = -686
539430 feet/sec YDOT = -209
257218 meter/sec
ZDOT = 18636
897187 ZDOT = 5680
526262
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 15190
30414948
00016717 00000-0 10270-3 0 9107
2 25544 51
6435 333
5696 0002278 132
2061 227
9286 15
55538414 31488
Satellite: ISS
Catalog Number: 25544
Epoch time: 15190
30414948 = yrday
fracday
Element set: 910
Inclination: 51
6435 deg
RA of node: 333
5696 deg
Eccentricity:
0002278
Arg of perigee: 132
2061 deg
Mean anomaly: 227
9286 deg
Mean motion: 15
55538414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3148
Checksum: 309
Coasting Arc #12 (Orbit 3160)
---------------------------------------
Vector Time (GMT): 2015/191/03:04:36
194
Vector Time (MET): N/A
Weight (LBS) : 891730
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 731516
83 A = 6777971
24 meter
Y = -4828577
17 meter E =
0010200
Z = -4710028
22 I = 51
44799
XDOT = 6956
829914 Wp = 118
66922
YDOT = -1637
254354 meter/sec RA = 328
84152 deg
ZDOT = 2758
685924 TA = 178
74910
MA = 178
74654
Ha = 219
542 n
mi
Hp = 214
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2399989
59 X = 808336
26
Y = -15841788
62 feet Y = -4819966
96 meter
Z = -15452848
49 Z = -4706288
48
XDOT = 22824
245126 XDOT = 6961
220409
YDOT = -5371
569403 feet/sec YDOT = -1559
434205 meter/sec
ZDOT = 9050
806836 ZDOT = 2792
491303
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9409590
51 X = 2868043
19
Y = -12988820
18 feet Y = -3958992
39 meter
Z = -15435766
90 Z = -4704821
75
XDOT = 21779
770371 XDOT = 6638
474009
YDOT = 4848
121050 feet/sec YDOT = 1477
707296 meter/sec
ZDOT = 9196
490077 ZDOT = 2803
090175
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 15191
13931335
00016717 00000-0 10270-3 0 9114
2 25544 51
6442 329
3963 0001891 222
7559 137
3447 15
54810554 31618
Satellite: ISS
Catalog Number: 25544
Epoch time: 15191
13931335 = yrday
fracday
Element set: 911
Inclination: 51
6442 deg
RA of node: 329
3963 deg
Eccentricity:
0001891
Arg of perigee: 222
7559 deg
Mean anomaly: 137
3447 deg
Mean motion: 15
54810554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3161
Checksum: 306
Coasting Arc #13 (Orbit 3176)
---------------------------------------
Vector Time (GMT): 2015/192/03:04:36
194
Vector Time (MET): N/A
Weight (LBS) : 891730
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2452253
13 A = 6782180
74 meter
Y = 5255294
95 meter E =
0010959
Z = 3506200
87 I = 51
43499
XDOT = -6216
902763 Wp = 94
82969
YDOT = 105
399399 meter/sec RA = 323
83337 deg
ZDOT = -4494
882351 TA = 43
74082
MA = 43
65404
Ha = 219
545 n
mi
Hp = 214
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8045449
90 X = -2527868
61
Y = 17241781
33 feet Y = 5227449
11 meter
Z = 11503283
70 Z = 3494105
20
XDOT = -20396
662609 XDOT = -6195
784915
YDOT = 345
798552 feet/sec YDOT = 35
996445 meter/sec
ZDOT = -14746
989339 ZDOT = -4525
031479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14850269
88 X = -4526362
26
Y = 11945560
60 feet Y = 3641006
87 meter
Z = 11450191
69 Z = 3490018
43
XDOT = -17531
387647 XDOT = -5343
566955
YDOT = -7499
174822 feet/sec YDOT = -2285
748486 meter/sec
ZDOT = -14876
631524 ZDOT = -4534
397289
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 15192
16769209
00016717 00000-0 10270-3 0 9128
2 25544 51
6439 324
2645 0001863 225
7134 134
3866 15
54808634 31771
Satellite: ISS
Catalog Number: 25544
Epoch time: 15192
16769209 = yrday
fracday
Element set: 912
Inclination: 51
6439 deg
RA of node: 324
2645 deg
Eccentricity:
0001863
Arg of perigee: 225
7134 deg
Mean anomaly: 134
3866 deg
Mean motion: 15
54808634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3177
Checksum: 323
Coasting Arc #14 (Orbit 3191)
---------------------------------------
Vector Time (GMT): 2015/193/03:04:36
194
Vector Time (MET): N/A
Weight (LBS) : 891730
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3812787
56 A = 6785833
21 meter
Y = -5296183
16 meter E =
0005464
Z = -1852287
09 I = 51
42322
XDOT = 4962
534365 Wp = 33
45638
YDOT = 1612
413128 meter/sec RA = 318
83559 deg
ZDOT = 5617
058634 TA = 306
10080
MA = 306
15137
Ha = 219
397 n
mi
Hp = 214
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12509145
55 X = 3880725
05
Y = -17375928
99 feet Y = -5253166
00 meter
Z = -6077057
37 Z = -1833600
98
XDOT = 16281
280724 XDOT = 4916
849712
YDOT = 5290
069317 feet/sec YDOT = 1667
651363 meter/sec
ZDOT = 18428
670059 ZDOT = 5641
054773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18713503
26 X = 5703875
79
Y = -10449378
61 feet Y = -3184970
60 meter
Z = -5995626
67 Z = -1827467
01
XDOT = 11653
117376 XDOT = 3551
870176
YDOT = 10259
913427 feet/sec YDOT = 3127
221613 meter/sec
ZDOT = 18531
503045 ZDOT = 5648
402128
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 15193
13178903
00016717 00000-0 10270-3 0 9132
2 25544 51
6446 319
4526 0001891 232
9180 127
1800 15
54842441 31924
Satellite: ISS
Catalog Number: 25544
Epoch time: 15193
13178903 = yrday
fracday
Element set: 913
Inclination: 51
6446 deg
RA of node: 319
4526 deg
Eccentricity:
0001891
Arg of perigee: 232
9180 deg
Mean anomaly: 127
1800 deg
Mean motion: 15
54842441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3192
Checksum: 300
Coasting Arc #15 (Orbit 3207)
---------------------------------------
Vector Time (GMT): 2015/194/03:04:36
194
Vector Time (MET): N/A
Weight (LBS) : 891730
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4742546
97 A = 6787337
33 meter
Y = 4845916
74 meter E =
0011718
Z = -79601
02 I = 51
40500
XDOT = -3374
524365 Wp = 144
50581
YDOT = -3393
561524 meter/sec RA = 313
84547 deg
ZDOT = -5994
533125 TA = 36
35479
MA = 36
27525
Ha = 219
365 n
mi
Hp = 214
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15559537
30 X = -4795996
03
Y = 15898676
96 feet Y = 4792583
63 meter
Z = -261158
19 Z = -102768
44
XDOT = -11071
274162 XDOT = -3307
206983
YDOT = -11133
732034 feet/sec YDOT = -3430
920549 meter/sec
ZDOT = -19667
103428 ZDOT = -6010
762684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20679502
72 X = -6303112
43
Y = 8195281
08 feet Y = 2497921
67 meter
Z = -361758
42 Z = -110263
97
XDOT = -4871
876964 XDOT = -1484
948099
YDOT = -13117
207614 feet/sec YDOT = -3998
124881 meter/sec
ZDOT = -19736
181624 ZDOT = -6015
588159
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 15194
16015319
00016717 00000-0 10270-3 0 9148
2 25544 51
6449 314
3205 0001948 235
4965 124
6004 15
54812493 32087
Satellite: ISS
Catalog Number: 25544
Epoch time: 15194
16015319 = yrday
fracday
Element set: 914
Inclination: 51
6449 deg
RA of node: 314
3205 deg
Eccentricity:
0001948
Arg of perigee: 235
4965 deg
Mean anomaly: 124
6004 deg
Mean motion: 15
54812493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3208
Checksum: 299
Coasting Arc #16 (Orbit 3223)
---------------------------------------
Vector Time (GMT): 2015/195/03:04:36
194
Vector Time (MET): N/A
Weight (LBS) : 891730
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5175339
15 A = 6785546
25 meter
Y = -3909031
94 meter E =
0012134
Z = 1975336
28 I = 51
37817
XDOT = 1660
040945 Wp = 68
34937
YDOT = 5018
488724 meter/sec RA = 308
85284 deg
ZDOT = 5558
778679 TA = 313
54622
MA = 313
64694
Ha = 219
257 n
mi
Hp = 214
115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16979459
16 X = 5209070
91
Y = -12824907
94 feet Y = -3850969
54 meter
Z = 6480762
07 Z = 2000558
24
XDOT = 5446
328561 XDOT = 1576
797477
YDOT = 16464
858018 feet/sec YDOT = 5036
586274 meter/sec
ZDOT = 18237
462858 ZDOT = 5566
641163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20603761
90 X = 6280026
63
Y = -5180489
97 feet Y = -1579013
34 meter
Z = 6589999
47 Z = 2008631
84
XDOT = -1910
625121 XDOT = -582
358537
YDOT = 15737
263287 feet/sec YDOT = 4796
717850 meter/sec
ZDOT = 18270
241570 ZDOT = 5568
769631
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 15195
18850903
00016717 00000-0 10270-3 0 9158
2 25544 51
6450 309
1881 0001812 247
1530 112
9432 15
54842247 32242
Satellite: ISS
Catalog Number: 25544
Epoch time: 15195
18850903 = yrday
fracday
Element set: 915
Inclination: 51
6450 deg
RA of node: 309
1881 deg
Eccentricity:
0001812
Arg of perigee: 247
1530 deg
Mean anomaly: 112
9432 deg
Mean motion: 15
54842247 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3224
Checksum: 294
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