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 24305U 26106.77303541 +.00000000 +00000-0 +49617-4 0 00003
2 24305 82.9338 125.6731 0031460 64.2200 296.2196 13.74078557 04
| Epoch (UTC): | 16 April 2026 18:33:10 |
| Eccentricity: | 0.0031460 |
| inclination: | 82.9338° |
| perigee height: | 962 km |
| apogee height: | 1008 km |
| right ascension of ascending node: | 125.6731° |
| argument of perigee: | 64.2200° |
| revolutions per day: | 13.74078557 |
| mean anomaly at epoch: | 296.2196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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