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 53263U 26145.43771013 +.00000000 +00000-0 +53765-4 0 00006
2 53263 53.2116 209.5880 0000756 82.1886 277.9192 15.08834429 03
| Epoch (UTC): | 25 May 2026 10:30:18 |
| Eccentricity: | 0.0000756 |
| inclination: | 53.2116° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 209.5880° |
| argument of perigee: | 82.1886° |
| revolutions per day: | 15.08834429 |
| mean anomaly at epoch: | 277.9192° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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