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 52852U 26145.41656175 +.00000000 +00000-0 +51119-3 0 00008
2 52852 53.2127 39.6800 0001308 101.8711 258.2428 15.08797261 08
| Epoch (UTC): | 25 May 2026 09:59:50 |
| Eccentricity: | 0.0001308 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 39.6800° |
| argument of perigee: | 101.8711° |
| revolutions per day: | 15.08797261 |
| mean anomaly at epoch: | 258.2428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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