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 00363U 62036 A 62226.04441590 .00777458 +00000-0 +00000-0 0 00049
2 00363 064.9574 112.3949 0031811 091.5844 268.7947 16.34937053000445
| Epoch (UTC): | 14 August 1962 01:03:57 |
| Eccentricity: | 0.0031811 |
| inclination: | 64.9574° |
| perigee height: | 158 km |
| apogee height: | 200 km |
| right ascension of ascending node: | 112.3949° |
| argument of perigee: | 91.5844° |
| revolutions per day: | 16.34937053 |
| mean anomaly at epoch: | 268.7947° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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