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 22300U 92095 A 93010.41127156 .00380216 +85000-5 +51951-3 00254
2 22300 062.8060 204.7624 0108547 111.4285 250.2119 15.95206248001871
| Epoch (UTC): | 10 January 1993 09:52:13 |
| Eccentricity: | 0.0108547 |
| inclination: | 62.8060° |
| perigee height: | 215 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 204.7624° |
| argument of perigee: | 111.4285° |
| revolutions per day: | 15.95206248 |
| mean anomaly at epoch: | 250.2119° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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