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 00297U 62020 A 63121.29008793 .03537089 +00000-0 +00000-0 0 00782
2 00297 048.9589 079.3998 0096415 071.2055 289.8379 16.24541103049953
| Epoch (UTC): | 01 May 1963 06:57:43 |
| Eccentricity: | 0.0096415 |
| inclination: | 48.9589° |
| perigee height: | 144 km |
| apogee height: | 271 km |
| right ascension of ascending node: | 79.3998° |
| argument of perigee: | 71.2055° |
| revolutions per day: | 16.24541103 |
| mean anomaly at epoch: | 289.8379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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