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 14549U 83121 A 83353.11901967 .00148846 -30177-5 +10157-3 0 9996
2 14549 082.3080 208.1807 0033052 067.3112 293.1685 16.15214355000787
| Epoch (UTC): | 19 December 1983 02:51:23 |
| Eccentricity: | 0.0033052 |
| inclination: | 82.3080° |
| perigee height: | 211 km |
| apogee height: | 254 km |
| right ascension of ascending node: | 208.1807° |
| argument of perigee: | 67.3112° |
| revolutions per day: | 16.15214355 |
| mean anomaly at epoch: | 293.1685° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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