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 65805U 26145.35707755 +.00000000 +00000-0 +13704-3 0 00002
2 65805 97.4509 8.1055 0002085 85.7254 274.4212 15.05656324 04
| Epoch (UTC): | 25 May 2026 08:34:11 |
| Eccentricity: | 0.0002085 |
| inclination: | 97.4509° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 8.1055° |
| argument of perigee: | 85.7254° |
| revolutions per day: | 15.05656324 |
| mean anomaly at epoch: | 274.4212° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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