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 05814U 72005 A 72088.79709948 .00000000 +00000-0 +00000-0 0 9990
2 05814 090.0000 092.6592 9417350 307.6323 000.6135 00.19286108000230
| Epoch (UTC): | 28 March 1972 19:07:49 |
| Eccentricity: | 0.9417350 |
| inclination: | 90.0000° |
| perigee height: | 995 km |
| apogee height: | 239332 km |
| right ascension of ascending node: | 92.6592° |
| argument of perigee: | 307.6323° |
| revolutions per day: | 0.19286108 |
| mean anomaly at epoch: | 0.6135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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