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 24291U 96050A 99316.43340756 .08700477 91082-5 36724-3 0 9991
2 24291 062.7425 281.8741 0024277 304.0609 201.2962 16.40583712176914
| Epoch (UTC): | 12 November 1999 10:24:06 |
| Eccentricity: | 0.0024277 |
| inclination: | 62.7425° |
| perigee height: | 148 km |
| apogee height: | 180 km |
| right ascension of ascending node: | 281.8741° |
| argument of perigee: | 304.0609° |
| revolutions per day: | 16.40583712 |
| mean anomaly at epoch: | 201.2962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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