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 05317U 71058 A 79347.17202652 .01945177 +00000-0 +96167-4 0 9999
2 05317 051.0598 328.0487 0006626 235.3867 124.4027 16.23884333469428
| Epoch (UTC): | 13 December 1979 04:07:43 |
| Eccentricity: | 0.0006626 |
| inclination: | 51.0598° |
| perigee height: | 204 km |
| apogee height: | 213 km |
| right ascension of ascending node: | 328.0487° |
| argument of perigee: | 235.3867° |
| revolutions per day: | 16.23884333 |
| mean anomaly at epoch: | 124.4027° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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