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 53966U 26145.54535605 +.00000000 +00000-0 +33236-4 0 00004
2 53966 53.2152 239.1779 0001283 87.9981 272.1158 15.08837660 03
| Epoch (UTC): | 25 May 2026 13:05:18 |
| Eccentricity: | 0.0001283 |
| inclination: | 53.2152° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 239.1779° |
| argument of perigee: | 87.9981° |
| revolutions per day: | 15.08837660 |
| mean anomaly at epoch: | 272.1158° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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