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 08361U 75099 A 92071.07774538 .00015818 +00000-0 +73340-3 0 9991
2 08361 081.2474 226.3477 0051474 040.4607 320.0056 15.18745483137440
| Epoch (UTC): | 11 March 1992 01:51:57 |
| Eccentricity: | 0.0051474 |
| inclination: | 81.2474° |
| perigee height: | 474 km |
| apogee height: | 545 km |
| right ascension of ascending node: | 226.3477° |
| argument of perigee: | 40.4607° |
| revolutions per day: | 15.18745483 |
| mean anomaly at epoch: | 320.0056° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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