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 65079U 26145.38493686 +.00000000 +00000-0 +93726-3 0 00005
2 65079 53.1605 27.5295 0001614 95.1299 264.9888 15.34410569 09
| Epoch (UTC): | 25 May 2026 09:14:18 |
| Eccentricity: | 0.0001614 |
| inclination: | 53.1605° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 27.5295° |
| argument of perigee: | 95.1299° |
| revolutions per day: | 15.34410569 |
| mean anomaly at epoch: | 264.9888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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