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 52263U 26145.35536544 +.00000000 +00000-0 +49385-4 0 00007
2 52263 53.2121 124.9534 0001088 58.5283 301.5815 15.08839617 01
| Epoch (UTC): | 25 May 2026 08:31:43 |
| Eccentricity: | 0.0001088 |
| inclination: | 53.2121° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 124.9534° |
| argument of perigee: | 58.5283° |
| revolutions per day: | 15.08839617 |
| mean anomaly at epoch: | 301.5815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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