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 64925U 26145.30416356 +.00000000 +00000-0 +77844-3 0 00008
2 64925 53.1609 349.8067 0001208 104.5457 255.5678 15.30202522 06
| Epoch (UTC): | 25 May 2026 07:17:59 |
| Eccentricity: | 0.0001208 |
| inclination: | 53.1609° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 349.8067° |
| argument of perigee: | 104.5457° |
| revolutions per day: | 15.30202522 |
| mean anomaly at epoch: | 255.5678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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