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 65961U 26145.31875198 +.00000000 +00000-0 +33381-3 0 00001
2 65961 51.9023 11.8322 0000866 104.8516 255.2542 14.79937945 04
| Epoch (UTC): | 25 May 2026 07:39:00 |
| Eccentricity: | 0.0000866 |
| inclination: | 51.9023° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 11.8322° |
| argument of perigee: | 104.8516° |
| revolutions per day: | 14.79937945 |
| mean anomaly at epoch: | 255.2542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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