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 52866U 26145.43494983 +.00000000 +00000-0 -27955-4 0 00005
2 52866 53.2128 39.5976 0001358 77.6924 282.4221 15.08846282 06
| Epoch (UTC): | 25 May 2026 10:26:19 |
| Eccentricity: | 0.0001358 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 39.5976° |
| argument of perigee: | 77.6924° |
| revolutions per day: | 15.08846282 |
| mean anomaly at epoch: | 282.4221° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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