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 24817U 26087.91534663 +.00000000 +00000-0 +13313-2 0 00008
2 24817 81.6863 74.2009 0359247 318.3506 64.4636 14.19714500 05
| Epoch (UTC): | 28 March 2026 21:58:05 |
| Eccentricity: | 0.0359247 |
| inclination: | 81.6863° |
| perigee height: | 568 km |
| apogee height: | 1085 km |
| right ascension of ascending node: | 74.2009° |
| argument of perigee: | 318.3506° |
| revolutions per day: | 14.19714500 |
| mean anomaly at epoch: | 64.4636° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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