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 00601U 63021 B 63198.26285399 .08013236 +51875-1 +00000-0 0 00104
2 00601 069.8602 108.0309 0070306 101.6907 259.1304 16.27635082004908
| Epoch (UTC): | 17 July 1963 06:18:30 |
| Eccentricity: | 0.0070306 |
| inclination: | 69.8602° |
| perigee height: | 153 km |
| apogee height: | 245 km |
| right ascension of ascending node: | 108.0309° |
| argument of perigee: | 101.6907° |
| revolutions per day: | 16.27635082 |
| mean anomaly at epoch: | 259.1304° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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