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 65739U 26145.50800694 +.00000000 +00000-0 +31425-3 0 00001
2 65739 53.1611 336.1622 0001257 88.4452 271.6692 15.30187456 01
| Epoch (UTC): | 25 May 2026 12:11:31 |
| Eccentricity: | 0.0001257 |
| inclination: | 53.1611° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 336.1622° |
| argument of perigee: | 88.4452° |
| revolutions per day: | 15.30187456 |
| mean anomaly at epoch: | 271.6692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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