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 24285U 26071.30599830 +.00000000 +00000-0 +58428-3 0 00007
2 24285 82.9447 96.0313 1738698 310.8972 35.3668 11.82157623 08
| Epoch (UTC): | 12 March 2026 07:20:38 |
| Eccentricity: | 0.1738698 |
| inclination: | 82.9447° |
| perigee height: | 346 km |
| apogee height: | 3177 km |
| right ascension of ascending node: | 96.0313° |
| argument of perigee: | 310.8972° |
| revolutions per day: | 11.82157623 |
| mean anomaly at epoch: | 35.3668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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