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 52663U 26145.44508519 +.00000000 +00000-0 -74562-4 0 00008
2 52663 53.2112 169.5537 0001437 49.2921 310.8196 15.08823333 00
| Epoch (UTC): | 25 May 2026 10:40:55 |
| Eccentricity: | 0.0001437 |
| inclination: | 53.2112° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 169.5537° |
| argument of perigee: | 49.2921° |
| revolutions per day: | 15.08823333 |
| mean anomaly at epoch: | 310.8196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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