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 52265U 26145.34433866 +.00000000 +00000-0 +14876-3 0 00007
2 52265 53.2139 125.0050 0001120 72.6082 287.5033 15.08842835 09
| Epoch (UTC): | 25 May 2026 08:15:50 |
| Eccentricity: | 0.0001120 |
| inclination: | 53.2139° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 125.0050° |
| argument of perigee: | 72.6082° |
| revolutions per day: | 15.08842835 |
| mean anomaly at epoch: | 287.5033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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