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 53805U 26145.58634272 +.00000000 +00000-0 +79317-4 0 00000
2 53805 53.2117 264.0426 0000997 101.4213 258.6891 15.08835699 06
| Epoch (UTC): | 25 May 2026 14:04:20 |
| Eccentricity: | 0.0000997 |
| inclination: | 53.2117° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 264.0426° |
| argument of perigee: | 101.4213° |
| revolutions per day: | 15.08835699 |
| mean anomaly at epoch: | 258.6891° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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