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 05879U 72014 A 80005.25645854 .01931614 +11524-5 +19107-2 0 9998
2 05879 097.4568 228.7558 0004204 087.4386 272.7364 16.11269803433461
| Epoch (UTC): | 05 January 1980 06:09:18 |
| Eccentricity: | 0.0004204 |
| inclination: | 97.4568° |
| perigee height: | 240 km |
| apogee height: | 246 km |
| right ascension of ascending node: | 228.7558° |
| argument of perigee: | 87.4386° |
| revolutions per day: | 16.11269803 |
| mean anomaly at epoch: | 272.7364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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