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 13663U 82033 AD 82350.39213515 .19051854 +06697-5 +06815-3 0 9991
2 13663 051.5951 340.8255 0001477 222.7553 137.5672 16.38387871038115
| Epoch (UTC): | 16 December 1982 09:24:40 |
| Eccentricity: | 0.0001477 |
| inclination: | 51.5951° |
| perigee height: | 169 km |
| apogee height: | 171 km |
| right ascension of ascending node: | 340.8255° |
| argument of perigee: | 222.7553° |
| revolutions per day: | 16.38387871 |
| mean anomaly at epoch: | 137.5672° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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