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 26053.70239095 +.00000000 +00000-0 +84386-4 0 00004
2 24920 69.9516 272.6006 0019177 72.5767 287.7450 14.27889694 08
| Epoch (UTC): | 22 February 2026 16:51:26 |
| Eccentricity: | 0.0019177 |
| inclination: | 69.9516° |
| perigee height: | 785 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 272.6006° |
| argument of perigee: | 72.5767° |
| revolutions per day: | 14.27889694 |
| mean anomaly at epoch: | 287.7450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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