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 3950U 69046A 70228.76458333 -.00000733 00000-0 10000-3 0 9998
2 3950 33.9870 151.3720 6739400 198.9070 286.9198 0.46154007 1057
| Epoch (UTC): | 16 August 1970 18:21:00 |
| Eccentricity: | 0.6739400 |
| inclination: | 33.9870° |
| perigee height: | 16683 km |
| apogee height: | 112016 km |
| right ascension of ascending node: | 151.3720° |
| argument of perigee: | 198.9070° |
| revolutions per day: | 0.46154007 |
| mean anomaly at epoch: | 286.9198° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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