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 65382U 26145.61519845 +.00000000 +00000-0 +12547-3 0 00006
2 65382 97.4477 16.9481 0002023 84.8271 275.3187 15.05655768 01
| Epoch (UTC): | 25 May 2026 14:45:53 |
| Eccentricity: | 0.0002023 |
| inclination: | 97.4477° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 16.9481° |
| argument of perigee: | 84.8271° |
| revolutions per day: | 15.05655768 |
| mean anomaly at epoch: | 275.3187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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