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 00564U 63009 A 66327.40661636 .41117245 +2821402 +00000-0 0 02142
2 00564 057.6437 347.3897 0027256 125.5060 234.7807 16.38971129203644
| Epoch (UTC): | 23 November 1966 09:45:31 |
| Eccentricity: | 0.0027256 |
| inclination: | 57.6437° |
| perigee height: | 151 km |
| apogee height: | 186 km |
| right ascension of ascending node: | 347.3897° |
| argument of perigee: | 125.5060° |
| revolutions per day: | 16.38971129 |
| mean anomaly at epoch: | 234.7807° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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