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 52865U 26145.42759865 +.00000000 +00000-0 +45295-3 0 00001
2 52865 53.2135 39.6304 0001447 95.3881 264.7276 15.08812305 09
| Epoch (UTC): | 25 May 2026 10:15:44 |
| Eccentricity: | 0.0001447 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 39.6304° |
| argument of perigee: | 95.3881° |
| revolutions per day: | 15.08812305 |
| mean anomaly at epoch: | 264.7276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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