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 65251U 26145.12862588 +.00000000 +00000-0 +13202-3 0 00001
2 65251 97.4462 187.9958 0001268 103.2746 256.8622 15.05657215 08
| Epoch (UTC): | 25 May 2026 03:05:13 |
| Eccentricity: | 0.0001268 |
| inclination: | 97.4462° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 187.9958° |
| argument of perigee: | 103.2746° |
| revolutions per day: | 15.05657215 |
| mean anomaly at epoch: | 256.8622° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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