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 00031U 60003 B 67275.67017494 .01669365 +00000-0 +00000-0 0 9994
2 00031 051.2007 317.7772 0014942 349.5805 010.4801 16.23394966418285
| Epoch (UTC): | 02 October 1967 16:05:03 |
| Eccentricity: | 0.0014942 |
| inclination: | 51.2007° |
| perigee height: | 200 km |
| apogee height: | 220 km |
| right ascension of ascending node: | 317.7772° |
| argument of perigee: | 349.5805° |
| revolutions per day: | 16.23394966 |
| mean anomaly at epoch: | 10.4801° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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