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 65780U 26145.49576531 +.00000000 +00000-0 +34432-3 0 00006
2 65780 51.8968 65.8960 0000856 95.4202 264.6858 14.79939837 09
| Epoch (UTC): | 25 May 2026 11:53:54 |
| Eccentricity: | 0.0000856 |
| inclination: | 51.8968° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 65.8960° |
| argument of perigee: | 95.4202° |
| revolutions per day: | 14.79939837 |
| mean anomaly at epoch: | 264.6858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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