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 15925U 85063 A 85218.11470760 .00061759 +00000-0 +24499-3 0 00219
2 15925 049.4572 115.8978 0020275 304.3274 055.5206 15.85838267001101
| Epoch (UTC): | 06 August 1985 02:45:10 |
| Eccentricity: | 0.0020275 |
| inclination: | 49.4572° |
| perigee height: | 300 km |
| apogee height: | 327 km |
| right ascension of ascending node: | 115.8978° |
| argument of perigee: | 304.3274° |
| revolutions per day: | 15.85838267 |
| mean anomaly at epoch: | 55.5206° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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