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 52610U 26145.39263346 +.00000000 +00000-0 -19246-4 0 00008
2 52610 53.2128 299.7852 0001217 94.4660 265.6471 15.08832248 01
| Epoch (UTC): | 25 May 2026 09:25:23 |
| Eccentricity: | 0.0001217 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 299.7852° |
| argument of perigee: | 94.4660° |
| revolutions per day: | 15.08832248 |
| mean anomaly at epoch: | 265.6471° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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