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 24827U 26106.97572329 +.00000000 +00000-0 -26934-3 0 00003
2 24827 63.3068 308.5407 1090457 68.9485 92.1180 11.07981116 00
| Epoch (UTC): | 16 April 2026 23:25:02 |
| Eccentricity: | 0.1090457 |
| inclination: | 63.3068° |
| perigee height: | 1194 km |
| apogee height: | 3048 km |
| right ascension of ascending node: | 308.5407° |
| argument of perigee: | 68.9485° |
| revolutions per day: | 11.07981116 |
| mean anomaly at epoch: | 92.1180° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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