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 08332U 75092 A 82272.60525535 .08073712 +15666-4 +12986-2 0 9995
2 08332 037.1316 332.8469 0002468 237.4844 122.6834 16.32559126385570
| Epoch (UTC): | 29 September 1982 14:31:34 |
| Eccentricity: | 0.0002468 |
| inclination: | 37.1316° |
| perigee height: | 184 km |
| apogee height: | 187 km |
| right ascension of ascending node: | 332.8469° |
| argument of perigee: | 237.4844° |
| revolutions per day: | 16.32559126 |
| mean anomaly at epoch: | 122.6834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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