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 24809U 26069.40072760 +.00000000 +00000-0 +13039-3 0 00004
2 24809 26.2985 71.6106 0661999 246.9292 106.0107 13.31019140 00
| Epoch (UTC): | 10 March 2026 09:37:02 |
| Eccentricity: | 0.0661999 |
| inclination: | 26.2985° |
| perigee height: | 645 km |
| apogee height: | 1641 km |
| right ascension of ascending node: | 71.6106° |
| argument of perigee: | 246.9292° |
| revolutions per day: | 13.31019140 |
| mean anomaly at epoch: | 106.0107° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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