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 65885U 26145.32974501 +.00000000 +00000-0 +11629-2 0 00005
2 65885 53.1588 14.2741 0001232 78.0872 282.0268 15.34404885 03
| Epoch (UTC): | 25 May 2026 07:54:49 |
| Eccentricity: | 0.0001232 |
| inclination: | 53.1588° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 14.2741° |
| argument of perigee: | 78.0872° |
| revolutions per day: | 15.34404885 |
| mean anomaly at epoch: | 282.0268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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