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 23500U 95007 A 95076.58333332 .00001170 +00000-0 +52914-5 0 00422
2 23500 028.4687 338.2517 0019711 114.2604 038.4444 15.73105509002413
| Epoch (UTC): | 17 March 1995 13:59:59 |
| Eccentricity: | 0.0019711 |
| inclination: | 28.4687° |
| perigee height: | 337 km |
| apogee height: | 363 km |
| right ascension of ascending node: | 338.2517° |
| argument of perigee: | 114.2604° |
| revolutions per day: | 15.73105509 |
| mean anomaly at epoch: | 38.4444° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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