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 00269U 62009 A 63229.96168589 .02320186 +00000-0 +00000-0 0 01105
2 00269 048.8589 171.1884 0056512 050.1316 310.3546 16.29526092074089
| Epoch (UTC): | 17 August 1963 23:04:49 |
| Eccentricity: | 0.0056512 |
| inclination: | 48.8589° |
| perigee height: | 157 km |
| apogee height: | 231 km |
| right ascension of ascending node: | 171.1884° |
| argument of perigee: | 50.1316° |
| revolutions per day: | 16.29526092 |
| mean anomaly at epoch: | 310.3546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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