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 65925U 26145.44370062 +.00000000 +00000-0 +33834-3 0 00008
2 65925 53.1577 168.8658 0001151 86.3078 273.8054 15.30202657 09
| Epoch (UTC): | 25 May 2026 10:38:55 |
| Eccentricity: | 0.0001151 |
| inclination: | 53.1577° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 168.8658° |
| argument of perigee: | 86.3078° |
| revolutions per day: | 15.30202657 |
| mean anomaly at epoch: | 273.8054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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