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 00445U 62059 A 65295.78699703 .00001558 +00000-0 +00000-0 0 9990
2 00445 018.0402 259.6239 5606421 254.7222 039.4907 04.62410654050216
| Epoch (UTC): | 22 October 1965 18:53:16 |
| Eccentricity: | 0.5606421 |
| inclination: | 18.0402° |
| perigee height: | 308 km |
| apogee height: | 17373 km |
| right ascension of ascending node: | 259.6239° |
| argument of perigee: | 254.7222° |
| revolutions per day: | 4.62410654 |
| mean anomaly at epoch: | 39.4907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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