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 00305U 62022 B 62169.78192530 .02385371 +00000-0 +00000-0 0 9998
2 00305 074.2700 290.4607 0138170 091.8937 147.4274 16.27003507002704
| Epoch (UTC): | 18 June 1962 18:45:58 |
| Eccentricity: | 0.0138170 |
| inclination: | 74.2700° |
| perigee height: | 110 km |
| apogee height: | 291 km |
| right ascension of ascending node: | 290.4607° |
| argument of perigee: | 91.8937° |
| revolutions per day: | 16.27003507 |
| mean anomaly at epoch: | 147.4274° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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