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 24920U 26103.85906373 +.00000000 +00000-0 +66186-4 0 00004
2 24920 69.9526 159.3190 0021800 358.2649 1.8393 14.27917759 08
| Epoch (UTC): | 13 April 2026 20:37:03 |
| Eccentricity: | 0.0021800 |
| inclination: | 69.9526° |
| perigee height: | 783 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 159.3190° |
| argument of perigee: | 358.2649° |
| revolutions per day: | 14.27917759 |
| mean anomaly at epoch: | 1.8393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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