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 00285U 62015 A 76144.99603793 .03716849 +00000-0 +00000-0 0 03821
2 00285 053.7584 107.0630 0004322 173.6423 186.4641 16.31702762759874
| Epoch (UTC): | 23 May 1976 23:54:17 |
| Eccentricity: | 0.0004322 |
| inclination: | 53.7584° |
| perigee height: | 185 km |
| apogee height: | 191 km |
| right ascension of ascending node: | 107.0630° |
| argument of perigee: | 173.6423° |
| revolutions per day: | 16.31702762 |
| mean anomaly at epoch: | 186.4641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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