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 26106.11768304 +.00000000 +00000-0 +53947-4 0 00004
2 24305 82.9338 126.1583 0031478 65.9741 294.4703 13.74078511 06
| Epoch (UTC): | 16 April 2026 02:49:27 |
| Eccentricity: | 0.0031478 |
| inclination: | 82.9338° |
| perigee height: | 962 km |
| apogee height: | 1008 km |
| right ascension of ascending node: | 126.1583° |
| argument of perigee: | 65.9741° |
| revolutions per day: | 13.74078511 |
| mean anomaly at epoch: | 294.4703° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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