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 24285U 26025.68249956 +.00000000 +00000-0 +57780-3 0 00008
2 24285 82.9498 121.2659 1743477 45.9817 327.2294 11.81507474 03
| Epoch (UTC): | 25 January 2026 16:22:47 |
| Eccentricity: | 0.1743477 |
| inclination: | 82.9498° |
| perigee height: | 345 km |
| apogee height: | 3184 km |
| right ascension of ascending node: | 121.2659° |
| argument of perigee: | 45.9817° |
| revolutions per day: | 11.81507474 |
| mean anomaly at epoch: | 327.2294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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