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 00055U 60011 A 60232.67329979 .00000000 +00000-0 +00000-0 0 9993
2 00055 064.8999 133.4774 0000029 074.8933 285.1068 15.88175450000050
| Epoch (UTC): | 19 August 1960 16:09:33 |
| Eccentricity: | 0.0000029 |
| inclination: | 64.8999° |
| perigee height: | 307 km |
| apogee height: | 307 km |
| right ascension of ascending node: | 133.4774° |
| argument of perigee: | 74.8933° |
| revolutions per day: | 15.88175450 |
| mean anomaly at epoch: | 285.1068° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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