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 3951U 69046B 71120.18240740 -.00000433 00000-0 10000-3 0 9995
2 3951 32.9470 146.6540 6908899 208.7530 240.4898 0.46230172 3345
| Epoch (UTC): | 30 April 1971 04:22:39 |
| Eccentricity: | 0.6908899 |
| inclination: | 32.9470° |
| perigee height: | 15460 km |
| apogee height: | 113083 km |
| right ascension of ascending node: | 146.6540° |
| argument of perigee: | 208.7530° |
| revolutions per day: | 0.46230172 |
| mean anomaly at epoch: | 240.4898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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