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 65080U 26145.38704196 +.00000000 +00000-0 +82124-3 0 00008
2 65080 53.1604 27.5412 0001411 93.2557 266.8607 15.34407812 09
| Epoch (UTC): | 25 May 2026 09:17:20 |
| Eccentricity: | 0.0001411 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 27.5412° |
| argument of perigee: | 93.2557° |
| revolutions per day: | 15.34407812 |
| mean anomaly at epoch: | 266.8607° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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