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 00008U 58004 B 60095.16166626 .02607090 +00000-0 +00000-0 0 02334
2 00008 065.0599 163.5585 0088318 135.6760 224.6847 16.28328133100004
| Epoch (UTC): | 04 April 1960 03:52:47 |
| Eccentricity: | 0.0088318 |
| inclination: | 65.0599° |
| perigee height: | 139 km |
| apogee height: | 255 km |
| right ascension of ascending node: | 163.5585° |
| argument of perigee: | 135.6760° |
| revolutions per day: | 16.28328133 |
| mean anomaly at epoch: | 224.6847° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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