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 52854U 26145.40551227 +.00000000 +00000-0 +89910-4 0 00002
2 52854 53.2135 39.7276 0001499 89.7041 270.4123 15.08830629 02
| Epoch (UTC): | 25 May 2026 09:43:56 |
| Eccentricity: | 0.0001499 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 39.7276° |
| argument of perigee: | 89.7041° |
| revolutions per day: | 15.08830629 |
| mean anomaly at epoch: | 270.4123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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