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 is defined by the following mean 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° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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