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 06315U 72100 A 73233.52190223 .03953391 +02833-2 +00000-0 0 9998
2 06315 096.9243 190.6721 0048803 307.9215 051.7623 16.36712646038317
| Epoch (UTC): | 21 August 1973 12:31:32 |
| Eccentricity: | 0.0048803 |
| inclination: | 96.9243° |
| perigee height: | 142 km |
| apogee height: | 206 km |
| right ascension of ascending node: | 190.6721° |
| argument of perigee: | 307.9215° |
| revolutions per day: | 16.36712646 |
| mean anomaly at epoch: | 51.7623° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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