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 65509U 26145.64941429 +.00000000 +00000-0 +64886-3 0 00000
2 65509 53.1578 272.7716 0002452 105.4234 254.7040 15.34414088 00
| Epoch (UTC): | 25 May 2026 15:35:09 |
| Eccentricity: | 0.0002452 |
| inclination: | 53.1578° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 272.7716° |
| argument of perigee: | 105.4234° |
| revolutions per day: | 15.34414088 |
| mean anomaly at epoch: | 254.7040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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