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 53275U 26145.53064586 +.00000000 +00000-0 +29629-4 0 00002
2 53275 53.2109 199.1668 0001051 71.1324 288.9782 15.08833686 01
| Epoch (UTC): | 25 May 2026 12:44:07 |
| Eccentricity: | 0.0001051 |
| inclination: | 53.2109° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 199.1668° |
| argument of perigee: | 71.1324° |
| revolutions per day: | 15.08833686 |
| mean anomaly at epoch: | 288.9782° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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