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 65497U 26145.63681500 +.00000000 +00000-0 +10124-2 0 00001
2 65497 53.1588 272.6940 0001182 84.2941 275.8196 15.34377512 09
| Epoch (UTC): | 25 May 2026 15:17:00 |
| Eccentricity: | 0.0001182 |
| inclination: | 53.1588° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 272.6940° |
| argument of perigee: | 84.2941° |
| revolutions per day: | 15.34377512 |
| mean anomaly at epoch: | 275.8196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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