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 00266U 62008 A 62141.87528190 .02135369 +00000-0 +00000-0 0 9993
2 00266 048.9855 317.5610 0119598 042.4543 141.8598 16.04632966010227
| Epoch (UTC): | 21 May 1962 21:00:24 |
| Eccentricity: | 0.0119598 |
| inclination: | 48.9855° |
| perigee height: | 182 km |
| apogee height: | 341 km |
| right ascension of ascending node: | 317.5610° |
| argument of perigee: | 42.4543° |
| revolutions per day: | 16.04632966 |
| mean anomaly at epoch: | 141.8598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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