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 00365U 62037 A 62226.04669118 .00573069 +00000-0 +00000-0 0 9995
2 00365 064.9972 110.2319 0035705 089.4962 270.9128 16.32289505000288
| Epoch (UTC): | 14 August 1962 01:07:14 |
| Eccentricity: | 0.0035705 |
| inclination: | 64.9972° |
| perigee height: | 163 km |
| apogee height: | 210 km |
| right ascension of ascending node: | 110.2319° |
| argument of perigee: | 89.4962° |
| revolutions per day: | 16.32289505 |
| mean anomaly at epoch: | 270.9128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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