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 14523U 83116 A 83342.89663719 .00532068 +89735-5 +40999-3 0 9998
2 14523 057.0194 158.4908 0005879 313.0670 046.9720 16.14386633001647
| Epoch (UTC): | 08 December 1983 21:31:09 |
| Eccentricity: | 0.0005879 |
| inclination: | 57.0194° |
| perigee height: | 231 km |
| apogee height: | 239 km |
| right ascension of ascending node: | 158.4908° |
| argument of perigee: | 313.0670° |
| revolutions per day: | 16.14386633 |
| mean anomaly at epoch: | 46.9720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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