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 52483U 26145.48970250 +.00000000 +00000-0 -26121-4 0 00005
2 52483 53.2133 64.3501 0001627 84.2182 275.8996 15.08828341 07
| Epoch (UTC): | 25 May 2026 11:45:10 |
| Eccentricity: | 0.0001627 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 64.3501° |
| argument of perigee: | 84.2182° |
| revolutions per day: | 15.08828341 |
| mean anomaly at epoch: | 275.8996° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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