[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 6th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17276 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 219 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
077/23:46:39
058 -2
3 2
3 2
3
N/A 0
0 0
0 222
1
000/00:05:14
116 0
3 -0
0 211
1
Coasting Arc #1 (Orbit 1205)
---------------------------------------
Vector Time (GMT): 2015/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5115501
80 A = 6783296
18 meter
Y = 3274652
95 meter E =
0021200
Z = 3002802
89 I = 51
34356
XDOT = -818
195134 Wp = 87
75212
YDOT = 5825
690628 meter/sec RA = 235
91958 deg
ZDOT = -4928
259899 TA = 57
67038
MA = 57
46527
Ha = 222
854 n
mi
Hp = 210
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16783142
38 X = 5063917
34
Y = 10743612
03 feet Y = 3331569
87 meter
Z = 9851715
52 Z = 3027526
90
XDOT = -2684
367239 XDOT = -859
339221
YDOT = 19113
158227 feet/sec YDOT = 5816
310215 meter/sec
ZDOT = -16168
831690 ZDOT = -4932
335328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12866569
94 X = 3921730
52
Y = 15148113
93 feet Y = 4617145
13 meter
Z = 9956976
89 Z = 3034886
55
XDOT = -6931
053730 XDOT = -2112
585177
YDOT = 16593
219833 feet/sec YDOT = 5057
613405 meter/sec
ZDOT = -16187
201174 ZDOT = -4933
858918
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 15065
53842474
00016717 00000-0 10270-3 0 9001
2 25544 51
6406 236
7450 0008501 73
9692 286
2397 15
54860138 12068
Satellite: ISS
Catalog Number: 25544
Epoch time: 15065
53842474 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 236
7450 deg
Eccentricity:
0008501
Arg of perigee: 73
9692 deg
Mean anomaly: 286
2397 deg
Mean motion: 15
54860138 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1206
Checksum: 313
Coasting Arc #2 (Orbit 1220)
---------------------------------------
Vector Time (GMT): 2015/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4930466
32 A = 6786396
06 meter
Y = -4487268
66 meter E =
0016523
Z = -1249698
62 I = 51
37362
XDOT = 2479
595630 Wp = 57
92159
YDOT = -4328
223955 meter/sec RA = 230
92003 deg
ZDOT = 5823
661629 TA = 288
43740
MA = 288
61694
Ha = 222
899 n
mi
Hp = 210
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16176070
61 X = -4873851
66
Y = -14722010
06 feet Y = -4542088
00 meter
Z = -4100061
10 Z = -1273511
45
XDOT = 8135
156267 XDOT = 2499
521633
YDOT = -14200
209825 feet/sec YDOT = -4300
383169 meter/sec
ZDOT = 19106
501406 ZDOT = 5835
755998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11483771
00 X = -3500253
40
Y = -18592630
73 feet Y = -5667033
85 meter
Z = -4201241
18 Z = -1280538
31
XDOT = 10250
393022 XDOT = 3124
319793
YDOT = -10613
206505 feet/sec YDOT = -3234
905343 meter/sec
ZDOT = 19158
937447 ZDOT = 5839
644134
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 15066
50249056
00016717 00000-0 10270-3 0 9017
2 25544 51
6415 231
9332 0008657 78
2026 282
0098 15
54896476 12218
Satellite: ISS
Catalog Number: 25544
Epoch time: 15066
50249056 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 231
9332 deg
Eccentricity:
0008657
Arg of perigee: 78
2026 deg
Mean anomaly: 282
0098 deg
Mean motion: 15
54896476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1221
Checksum: 309
Coasting Arc #3 (Orbit 1236)
---------------------------------------
Vector Time (GMT): 2015/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4237575
39 A = 6786657
78 meter
Y = 5243272
90 meter E =
0016609
Z = -754554
69 I = 51
39579
XDOT = -4153
394030 Wp = 113
41102
YDOT = 2518
963935 meter/sec RA = 225
92818 deg
ZDOT = -5932
005544 TA = 74
77194
MA = 74
58835
Ha = 222
847 n
mi
Hp = 210
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13902806
41 X = 4182294
26
Y = 17202338
89 feet Y = 5290351
02 meter
Z = -2475573
14 Z = -734104
55
XDOT = -13626
620832 XDOT = -4152
437671
YDOT = 8264
317372 feet/sec YDOT = 2472
522414 meter/sec
ZDOT = -19461
960447 ZDOT = -5952
179882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9005861
69 X = 2744986
64
Y = 20211991
72 feet Y = 6160615
08 meter
Z = -2388890
46 Z = -728133
81
XDOT = -13704
357094 XDOT = -4177
088042
YDOT = 3840
131322 feet/sec YDOT = 1170
472027 meter/sec
ZDOT = -19548
684255 ZDOT = -5958
438961
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 15067
53080143
00016717 00000-0 10270-3 0 9022
2 25544 51
6415 226
8001 0008671 80
1120 280
1011 15
54968936 12379
Satellite: ISS
Catalog Number: 25544
Epoch time: 15067
53080143 = yrday
fracday
Element set: 902
Inclination: 51
6415 deg
RA of node: 226
8001 deg
Eccentricity:
0008671
Arg of perigee: 80
1120 deg
Mean anomaly: 280
1011 deg
Mean motion: 15
54968936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1237
Checksum: 275
Coasting Arc #4 (Orbit 1252)
---------------------------------------
Vector Time (GMT): 2015/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3100854
14 A = 6784019
86 meter
Y = -5433888
28 meter E =
0022208
Z = 2598332
68 I = 51
41046
XDOT = 5584
864287 Wp = 80
26677
YDOT = -673
168199 meter/sec RA = 220
93420 deg
ZDOT = 5222
756827 TA = 309
11969
MA = 309
31692
Ha = 222
823 n
mi
Hp = 210
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10173405
96 X = -3052482
35
Y = -17827717
45 feet Y = -5468293
22 meter
Z = 8524713
51 Z = 2583387
64
XDOT = 18323
045560 XDOT = 5566
606594
YDOT = -2208
557082 feet/sec YDOT = -610
815939 meter/sec
ZDOT = 17135
028960 ZDOT = 5249
842694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5619573
72 X = -1712846
07
Y = -19769117
59 feet Y = -6025627
04 meter
Z = 8461608
57 Z = 2579098
29
XDOT = 16766
366331 XDOT = 5110
388458
YDOT = 2666
522040 feet/sec YDOT = 812
755918 meter/sec
ZDOT = 17251
044143 ZDOT = 5258
118255
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 15068
55908864
00016717 00000-0 10270-3 0 9035
2 25544 51
6422 221
6676 0008625 85
4430 274
7709 15
54985649 12530
Satellite: ISS
Catalog Number: 25544
Epoch time: 15068
55908864 = yrday
fracday
Element set: 903
Inclination: 51
6422 deg
RA of node: 221
6676 deg
Eccentricity:
0008625
Arg of perigee: 85
4430 deg
Mean anomaly: 274
7709 deg
Mean motion: 15
54985649 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1253
Checksum: 339
Coasting Arc #5 (Orbit 1267)
---------------------------------------
Vector Time (GMT): 2015/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1489961
89 A = 6779509
99 meter
Y = 5164853
69 meter E =
0016086
Z = -4146763
63 I = 51
42088
XDOT = -6591
726448 Wp = 80
19916
YDOT = -1092
986506 meter/sec RA = 215
93015 deg
ZDOT = -3739
518653 TA = 151
18310
MA = 151
09415
Ha = 222
788 n
mi
Hp = 210
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4888326
42 X = 1452239
95
Y = 16945058
03 feet Y = 5181303
96 meter
Z = -13604867
55 Z = -4139617
99
XDOT = -21626
399106 XDOT = -6560
849335
YDOT = -3585
913735 feet/sec YDOT = -1166
527338 meter/sec
ZDOT = -12268
761985 ZDOT = -3771
464808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1038915
69 X = 316661
50
Y = 17628406
16 feet Y = 5373138
20 meter
Z = -13575091
09 Z = -4137687
77
XDOT = -18905
159672 XDOT = -5762
292668
YDOT = -8414
140926 feet/sec YDOT = -2564
630154 meter/sec
ZDOT = -12405
311086 ZDOT = -3781
138819
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 15069
52308461
00016717 00000-0 10270-3 0 9041
2 25544 51
6429 216
8560 0008683 87
8604 272
3544 15
55013202 12683
Satellite: ISS
Catalog Number: 25544
Epoch time: 15069
52308461 = yrday
fracday
Element set: 904
Inclination: 51
6429 deg
RA of node: 216
8560 deg
Eccentricity:
0008683
Arg of perigee: 87
8604 deg
Mean anomaly: 272
3544 deg
Mean motion: 15
55013202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1268
Checksum: 308
Coasting Arc #6 (Orbit 1283)
---------------------------------------
Vector Time (GMT): 2015/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 379789
11 A = 6775661
68 meter
Y = -4476513
68 meter E =
0013359
Z = 5061773
79 I = 51
43485
XDOT = 7018
453310 Wp = 104
49662
YDOT = 2579
054765 meter/sec RA = 210
91317 deg
ZDOT = 1747
106107 TA = 328
54617
MA = 328
62599
Ha = 222
622 n
mi
Hp = 210
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1246027
26 X = 405230
13
Y = -14686724
66 feet Y = -4472123
78 meter
Z = 16606869
39 Z = 5063681
05
XDOT = 23026
421620 XDOT = 6980
605301
YDOT = 8461
465764 feet/sec YDOT = 2657
328274 meter/sec
ZDOT = 5731
975416 ZDOT = 1781
108129
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4169790
46 X = 1270952
13
Y = -14126960
58 feet Y = -4305897
58 meter
Z = 16615727
74 Z = 5064473
81
XDOT = 19697
030262 XDOT = 6003
654824
YDOT = 12753
938620 feet/sec YDOT = 3887
400492 meter/sec
ZDOT = 5877
106262 ZDOT = 1791
341989
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 15070
55132073
00016717 00000-0 10270-3 0 9051
2 25544 51
6430 211
7227 0008525 91
4400 268
7730 15
55071178 12849
Satellite: ISS
Catalog Number: 25544
Epoch time: 15070
55132073 = yrday
fracday
Element set: 905
Inclination: 51
6430 deg
RA of node: 211
7227 deg
Eccentricity:
0008525
Arg of perigee: 91
4400 deg
Mean anomaly: 268
7730 deg
Mean motion: 15
55071178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1284
Checksum: 284
Coasting Arc #7 (Orbit 1298)
---------------------------------------
Vector Time (GMT): 2015/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890325
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2381085
52 A = 6774608
41 meter
Y = 3528761
18 meter E =
0023449
Z = -5290470
34 I = 51
45978
XDOT = -6673
012607 Wp = 94
41459
YDOT = -3708
378363 meter/sec RA = 205
89138 deg
ZDOT = 530
094455 TA = 180
66468
MA = 180
66780
Ha = 222
645 n
mi
Hp = 209
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7811960
37 X = -2394668
92
Y = 11577300
47 feet Y = 3502057
82 meter
Z = -17357186
15 Z = -5302070
53
XDOT = -21893
085982 XDOT = -6633
623686
YDOT = -12166
595680 feet/sec YDOT = -3782
780053 meter/sec
ZDOT = 1739
155036 ZDOT = 497
774389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9772031
70 X = -2978515
26
Y = 9890539
62 feet Y = 3014636
48 meter
Z = -17407387
64 Z = -5305771
75
XDOT = -18453
616788 XDOT = -5624
662397
YDOT = -15415
610130 feet/sec YDOT = -4698
677968 meter/sec
ZDOT = 1601
381983 ZDOT = 488
101228
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 15071
51526981
00016717 00000-0 10270-3 0 9064
2 25544 51
6435 206
9119 0008690 94
4184 265
7963 15
55102226 12995
Satellite: ISS
Catalog Number: 25544
Epoch time: 15071
51526981 = yrday
fracday
Element set: 906
Inclination: 51
6435 deg
RA of node: 206
9119 deg
Eccentricity:
0008690
Arg of perigee: 94
4184 deg
Mean anomaly: 265
7963 deg
Mean motion: 15
55102226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1299
Checksum: 323
Coasting Arc #8 (Orbit 1314)
---------------------------------------
Vector Time (GMT): 2015/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890325
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4233387
92 A = 6776978
95 meter
Y = -2393689
58 meter E =
0015655
Z = 4707367
33 I = 51
49666
XDOT = 5600
326633 Wp = 81
60957
YDOT = 4476
682621 meter/sec RA = 200
87140 deg
ZDOT = -2749
981786 TA = 35
67611
MA = 35
57158
Ha = 222
556 n
mi
Hp = 209
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13889067
96 X = 4236973
56
Y = -7853312
28 feet Y = -2346328
57 meter
Z = 15444118
53 Z = 4727941
15
XDOT = 18373
775043 XDOT = 5563
209403
YDOT = 14687
278941 feet/sec YDOT = 4539
101328 meter/sec
ZDOT = -9022
249954 ZDOT = -2722
867199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14947793
31 X = 4556087
40
Y = -5329577
63 feet Y = -1624455
26 meter
Z = 15532565
69 Z = 4734326
02
XDOT = 15201
854889 XDOT = 4633
525370
YDOT = 16582
484575 feet/sec YDOT = 5054
341298 meter/sec
ZDOT = -8906
862152 ZDOT = -2714
811584
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 15072
54345661
00016717 00000-0 10270-3 0 9073
2 25544 51
6435 201
7777 0008725 97
9136 262
3008 15
55093045 13152
Satellite: ISS
Catalog Number: 25544
Epoch time: 15072
54345661 = yrday
fracday
Element set: 907
Inclination: 51
6435 deg
RA of node: 201
7777 deg
Eccentricity:
0008725
Arg of perigee: 97
9136 deg
Mean anomaly: 262
3008 deg
Mean motion: 15
55093045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1315
Checksum: 309
Coasting Arc #9 (Orbit 1329)
---------------------------------------
Vector Time (GMT): 2015/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890325
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5704535
71 A = 6781177
19 meter
Y = 1239116
69 meter E =
0013566
Z = -3464273
79 I = 51
54162
XDOT = -3807
958429 Wp = 98
20881
YDOT = -4841
159429 meter/sec RA = 195
86641 deg
ZDOT = 4552
268212 TA = 221
11891
MA = 221
22122
Ha = 222
476 n
mi
Hp = 209
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18715668
35 X = -5701139
82
Y = 4065343
47 feet Y = 1175343
51 meter
Z = -11365727
66 Z = -3491976
97
XDOT = -12493
301932 XDOT = -3775
653473
YDOT = -15883
068993 feet/sec YDOT = -4883
561454 meter/sec
ZDOT = 14935
263163 ZDOT = 4533
848946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19050375
72 X = -5806554
52
Y = 1082463
76 feet Y = 329934
96 meter
Z = -11484532
28 Z = -3500485
44
XDOT = -9855
126182 XDOT = -3003
842460
YDOT = -16274
240848 feet/sec YDOT = -4960
388610 meter/sec
ZDOT = 14857
143960 ZDOT = 4528
457479
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 15073
50735478
00016717 00000-0 10270-3 0 9080
2 25544 51
6440 196
9658 0008514 100
1926 260
0188 15
55145850 13304
Satellite: ISS
Catalog Number: 25544
Epoch time: 15073
50735478 = yrday
fracday
Element set: 908
Inclination: 51
6440 deg
RA of node: 196
9658 deg
Eccentricity:
0008514
Arg of perigee: 100
1926 deg
Mean anomaly: 260
0188 deg
Mean motion: 15
55145850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1330
Checksum: 308
Coasting Arc #10 (Orbit 1345)
---------------------------------------
Vector Time (GMT): 2015/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890325
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6573997
00 A = 6785047
69 meter
Y = -59542
07 meter E =
0022425
Z = 1638087
80 I = 51
58570
XDOT = 1482
668475 Wp = 111
90381
YDOT = 4901
831024 meter/sec RA = 190
87704 deg
ZDOT = -5717
533299 TA = 50
12327
MA = 49
92628
Ha = 222
403 n
mi
Hp = 209
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21568231
62 X = 6566217
08
Y = -195348
01 feet Y = 13929
31 meter
Z = 5374303
82 Z = 1670003
78
XDOT = 4864
397883 XDOT = 1455
518194
YDOT = 16082
122782 feet/sec YDOT = 4918
258830 meter/sec
ZDOT = -18758
311347 ZDOT = -5710
397279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21348292
44 X = 6506959
54
Y = 2826552
88 feet Y = 861533
32 meter
Z = 5510982
33 Z = 1679747
41
XDOT = 2885
304825 XDOT = 879
440911
YDOT = 15063
617406 feet/sec YDOT = 4591
390586 meter/sec
ZDOT = -18728
504479 ZDOT = -5708
448165
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 15074
53548851
00016717 00000-0 10270-3 0 9092
2 25544 51
6441 191
8318 0008587 104
3260 255
8847 15
55192217 13469
Satellite: ISS
Catalog Number: 25544
Epoch time: 15074
53548851 = yrday
fracday
Element set: 909
Inclination: 51
6441 deg
RA of node: 191
8318 deg
Eccentricity:
0008587
Arg of perigee: 104
3260 deg
Mean anomaly: 255
8847 deg
Mean motion: 15
55192217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1346
Checksum: 325
Coasting Arc #11 (Orbit 1361)
---------------------------------------
Vector Time (GMT): 2015/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890325
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6695839
38 A = 6786058
15 meter
Y = -1000184
49 meter E =
0018787
Z = 387321
31 I = 51
62158
XDOT = 1057
060145 Wp = 71
87095
YDOT = -4664
472187 meter/sec RA = 185
89877 deg
ZDOT = 5995
638652 TA = 292
30732
MA = 292
50639
Ha = 222
341 n
mi
Hp = 209
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21967976
98 X = -6686038
87
Y = -3281445
17 feet Y = -1075006
89 meter
Z = 1270739
22 Z = 354818
55
XDOT = 3468
045094 XDOT = 1080
016610
YDOT = -15303
386440 feet/sec YDOT = -4652
522440 meter/sec
ZDOT = 19670
730486 ZDOT = 6000
829847
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21404102
87 X = -6523970
55
Y = -5963080
34 feet Y = -1817546
89 meter
Z = 1131691
89 Z = 344939
69
XDOT = 4767
636914 XDOT = 1453
175731
YDOT = -13212
546781 feet/sec YDOT = -4027
184259 meter/sec
ZDOT = 19693
673498 ZDOT = 6002
631682
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 15075
56359493
00016717 00000-0 10270-3 0 9100
2 25544 51
6450 186
6983 0008564 106
4537 253
7558 15
55237578 13628
Satellite: ISS
Catalog Number: 25544
Epoch time: 15075
56359493 = yrday
fracday
Element set: 910
Inclination: 51
6450 deg
RA of node: 186
6983 deg
Eccentricity:
0008564
Arg of perigee: 106
4537 deg
Mean anomaly: 253
7558 deg
Mean motion: 15
55237578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1362
Checksum: 342
Coasting Arc #12 (Orbit 1376)
---------------------------------------
Vector Time (GMT): 2015/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890325
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6000281
68 A = 6783533
06 meter
Y = 2021872
65 meter E =
0013837
Z = -2432938
61 I = 51
64529
XDOT = -3564
474253 Wp = 119
74157
YDOT = 4176
478491 meter/sec RA = 180
92071 deg
ZDOT = -5349
669959 TA = 87
47710
MA = 87
31870
Ha = 222
286 n
mi
Hp = 209
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19685963
53 X = 5989044
82
Y = 6633440
45 feet Y = 2088908
58 meter
Z = -7982082
05 Z = -2403818
35
XDOT = -11694
469334 XDOT = -3584
925354
YDOT = 13702
357253 feet/sec YDOT = 4136
503181 meter/sec
ZDOT = -17551
410626 ZDOT = -5367
035456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18921219
30 X = 5767187
64
Y = 8688955
99 feet Y = 2648393
79 meter
Z = -7857660
60 Z = -2395014
95
XDOT = -12337
355387 XDOT = -3760
425922
YDOT = 11015
020408 feet/sec YDOT = 3357
378220 meter/sec
ZDOT = -17626
423463 ZDOT = -5372
533871
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 15076
52742012
00016717 00000-0 10270-3 0 9111
2 25544 51
6452 181
8855 0008525 110
1778 250
0293 15
55283338 13778
Satellite: ISS
Catalog Number: 25544
Epoch time: 15076
52742012 = yrday
fracday
Element set: 911
Inclination: 51
6452 deg
RA of node: 181
8855 deg
Eccentricity:
0008525
Arg of perigee: 110
1778 deg
Mean anomaly: 250
0293 deg
Mean motion: 15
55283338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1377
Checksum: 303
Coasting Arc #13 (Orbit 1392)
---------------------------------------
Vector Time (GMT): 2015/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890325
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4597390
86 A = 6778909
66 meter
Y = -2884117
94 meter E =
0019204
Z = 4050246
54 I = 51
66262
XDOT = 5628
269882 Wp = 107
20380
YDOT = -3482
628314 meter/sec RA = 175
93210 deg
ZDOT = 3887
892733 TA = 302
48269
MA = 302
66818
Ha = 222
198 n
mi
Hp = 209
835
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15083303
34 X = -4584472
63
Y = -9462329
21 feet Y = -2935456
14 meter
Z = 13288210
45 Z = 4027945
38
XDOT = 18465
452370 XDOT = 5647
909447
YDOT = -11425
945913 feet/sec YDOT = -3419
578939 meter/sec
ZDOT = 12755
553585 ZDOT = 3915
281663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14265461
89 X = -4348112
78
Y = -10772954
23 feet Y = -3283596
45 meter
Z = 13193115
81 Z = 4021261
70
XDOT = 18542
081109 XDOT = 5651
626322
YDOT = -8703
794101 feet/sec YDOT = -2652
916442 meter/sec
ZDOT = 12873
403155 ZDOT = 3923
813282
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 15077
55547366
00016717 00000-0 10270-3 0 9121
2 25544 51
6458 176
7518 0008500 113
4154 246
7894 15
55348543 13937
Satellite: ISS
Catalog Number: 25544
Epoch time: 15077
55547366 = yrday
fracday
Element set: 912
Inclination: 51
6458 deg
RA of node: 176
7518 deg
Eccentricity:
0008500
Arg of perigee: 113
4154 deg
Mean anomaly: 246
7894 deg
Mean motion: 15
55348543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1393
Checksum: 332
Coasting Arc #14 (Orbit 1399)
---------------------------------------
Vector Time (GMT): 2015/077/23:49:16
116
Vector Time (MET): N/A
Weight (LBS) : 890095
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1800360
90 A = 6776364
48 meter
Y = 4202514
30 meter E =
0019388
Z = -5019450
00 I = 51
66492
XDOT = -7348
605679 Wp = 108
25744
YDOT = -751
675313 meter/sec RA = 173
43483 deg
ZDOT = 2006
882705 TA = 181
26638
MA = 181
27129
Ha = 222
090 n
mi
Hp = 211
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5906695
88 X = -1822838
25
Y = 13787776
59 feet Y = 4182255
03 meter
Z = -16468011
81 Z = -5028250
96
XDOT = -24109
598684 XDOT = -7349
402690
YDOT = -2466
126355 feet/sec YDOT = -833
856364 meter/sec
ZDOT = 6584
260844 ZDOT = 1971
183162
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7507138
56 X = 2288175
83
Y = -12937180
28 feet Y = -3943252
55 meter
Z = -16506346
94 Z = -5031134
55
XDOT = 22698
317290 XDOT = 6918
447110
YDOT = 4967
372075 feet/sec YDOT = 1514
055009 meter/sec
ZDOT = 6431
443785 ZDOT = 1960
304066
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 15078
00524141
00016717 00000-0 10270-3 0 9139
2 25544 51
6451 174
5084 0006567 114
1504 246
0336 15
54907944 14000
Satellite: ISS
Catalog Number: 25544
Epoch time: 15078
00524141 = yrday
fracday
Element set: 913
Inclination: 51
6451 deg
RA of node: 174
5084 deg
Eccentricity:
0006567
Arg of perigee: 114
1504 deg
Mean anomaly: 246
0336 deg
Mean motion: 15
54907944 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1400
Checksum: 283
Coasting Arc #15 (Orbit 1415)
---------------------------------------
Vector Time (GMT): 2015/078/23:49:16
116
Vector Time (MET): N/A
Weight (LBS) : 890095
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3726468
94 A = 6780061
24 meter
Y = -3990040
78 meter E =
0016423
Z = 4005357
38 I = 51
70882
XDOT = 6299
675667 Wp = 93
30951
YDOT = 1899
250883 meter/sec RA = 168
43867 deg
ZDOT = -3956
006405 TA = 37
78238
MA = 37
66720
Ha = 221
958 n
mi
Hp = 211
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12225947
97 X = 3751353
15
Y = -13090684
97 feet Y = -3948229
16 meter
Z = 13140936
29 Z = 4023520
84
XDOT = 20668
227253 XDOT = 6297
186275
YDOT = 6231
138068 feet/sec YDOT = 1969
683390 meter/sec
ZDOT = -12979
023638 ZDOT = -3925
410355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13508585
41 X = -4117416
83
Y = 11674368
55 feet Y = 3558347
53 meter
Z = 13219352
58 Z = 4029258
67
XDOT = -19087
550558 XDOT = -5817
885410
YDOT = -7489
760457 feet/sec YDOT = -2282
878987 meter/sec
ZDOT = -12848
231343 ZDOT = -3916
140913
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 15079
03354362
00016717 00000-0 10270-3 0 9140
2 25544 51
6449 169
3766 0006597 117
4443 242
7382 15
54941310 14163
Satellite: ISS
Catalog Number: 25544
Epoch time: 15079
03354362 = yrday
fracday
Element set: 914
Inclination: 51
6449 deg
RA of node: 169
3766 deg
Eccentricity:
0006597
Arg of perigee: 117
4443 deg
Mean anomaly: 242
7382 deg
Mean motion: 15
54941310 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1416
Checksum: 317
Coasting Arc #16 (Orbit 1430)
---------------------------------------
Vector Time (GMT): 2015/079/23:49:16
116
Vector Time (MET): N/A
Weight (LBS) : 890095
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5216737
51 A = 6784152
72 meter
Y = 3575153
41 meter E =
0009654
Z = -2463538
44 I = 51
75434
XDOT = -4586
994602 Wp = 89
53017
YDOT = -3027
095590 meter/sec RA = 163
45716 deg
ZDOT = 5338
477711 TA = 242
94256
MA = 243
04111
Ha = 221
866 n
mi
Hp = 211
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17115280
53 X = -5244361
06
Y = 11729505
95 feet Y = 3516661
58 meter
Z = -8082475
18 Z = -2488948
00
XDOT = -15049
194887 XDOT = -4578
736290
YDOT = -9931
415977 feet/sec YDOT = -3078
343293 meter/sec
ZDOT = 17514
690653 ZDOT = 5316
215572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18079406
37 X = 5510603
06
Y = -10093001
21 feet Y = -3076346
77 meter
Z = -8191882
22 Z = -2496885
70
XDOT = 13436
021758 XDOT = 4095
299432
YDOT = 9976
822988 feet/sec YDOT = 3040
935647 meter/sec
ZDOT = 17419
766319 ZDOT = 5309
544774
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 15079
99755252
00016717 00000-0 10270-3 0 9159
2 25544 51
6454 164
5647 0006528 120
6635 239
5162 15
54997853 14317
Satellite: ISS
Catalog Number: 25544
Epoch time: 15079
99755252 = yrday
fracday
Element set: 915
Inclination: 51
6454 deg
RA of node: 164
5647 deg
Eccentricity:
0006528
Arg of perigee: 120
6635 deg
Mean anomaly: 239
5162 deg
Mean motion: 15
54997853 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1431
Checksum: 340
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