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 00214U 61034 B 62029.12065150 .02930741 +00000-0 +00000-0 0 9996
2 00214 081.1405 036.8318 0000000 325.8600 034.1399 16.24799335007501
| Epoch (UTC): | 29 January 1962 02:53:44 |
| Eccentricity: | 0.0000000 |
| inclination: | 81.1405° |
| perigee height: | 206 km |
| apogee height: | 206 km |
| right ascension of ascending node: | 36.8318° |
| argument of perigee: | 325.8600° |
| revolutions per day: | 16.24799335 |
| mean anomaly at epoch: | 34.1399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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