View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 12054U 80089A 14046.92356602 .10642788 78504-5 35630-3 0 9990
2 12054 064.9024 045.5536 0015341 327.6303 033.4497 16.43050581730424
Epoch (UTC): | 15 February 2014 22:09:56 |
Eccentricity: | 0.0015341 |
inclination: | 64.9024° |
perigee height: | 147 km |
apogee height: | 168 km |
right ascension of ascending node: | 45.5536° |
argument of perigee: | 327.6303° |
revolutions per day: | 16.43050581 |
mean anomaly at epoch: | 33.4497° |
orbit number at epoch: | 73042 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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