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 00771U 64015 A 67320.00871375 .02032692 +00000-0 +00000-0 0 03123
2 00771 051.5941 189.3694 0059823 147.4196 213.0435 16.14040010194527
| Epoch (UTC): | 16 November 1967 00:12:32 |
| Eccentricity: | 0.0059823 |
| inclination: | 51.5941° |
| perigee height: | 196 km |
| apogee height: | 275 km |
| right ascension of ascending node: | 189.3694° |
| argument of perigee: | 147.4196° |
| revolutions per day: | 16.14040010 |
| mean anomaly at epoch: | 213.0435° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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