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 00433U 62052 A 62276.56409039 .02123437 +00000-0 +00000-0 0 9996
2 00433 032.5500 058.6365 0098501 074.3803 143.5476 16.19408693000016
| Epoch (UTC): | 03 October 1962 13:32:17 |
| Eccentricity: | 0.0098501 |
| inclination: | 32.5500° |
| perigee height: | 156 km |
| apogee height: | 286 km |
| right ascension of ascending node: | 58.6365° |
| argument of perigee: | 74.3803° |
| revolutions per day: | 16.19408693 |
| mean anomaly at epoch: | 143.5476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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