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 53267U 26145.42300918 +.00000000 +00000-0 +24340-3 0 00007
2 53267 53.2122 209.6538 0001327 100.1278 259.9864 15.08820252 01
| Epoch (UTC): | 25 May 2026 10:09:07 |
| Eccentricity: | 0.0001327 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 209.6538° |
| argument of perigee: | 100.1278° |
| revolutions per day: | 15.08820252 |
| mean anomaly at epoch: | 259.9864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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