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 52482U 26145.08121273 +.00000000 +00000-0 -14679-3 0 00007
2 52482 53.2124 66.1850 0001425 97.5879 262.5275 15.08843613 01
| Epoch (UTC): | 25 May 2026 01:56:56 |
| Eccentricity: | 0.0001425 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 66.1850° |
| argument of perigee: | 97.5879° |
| revolutions per day: | 15.08843613 |
| mean anomaly at epoch: | 262.5275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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