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 65763U 26145.59617778 +.00000000 +00000-0 +72429-3 0 00005
2 65763 51.8579 349.4332 0006395 222.6091 137.4402 15.41930631 01
| Epoch (UTC): | 25 May 2026 14:18:29 |
| Eccentricity: | 0.0006395 |
| inclination: | 51.8579° |
| perigee height: | 436 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 349.4332° |
| argument of perigee: | 222.6091° |
| revolutions per day: | 15.41930631 |
| mean anomaly at epoch: | 137.4402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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