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 52286U 26145.34156829 +.00000000 +00000-0 +47645-4 0 00002
2 52286 53.2127 115.0165 0001290 57.8219 302.2898 15.08828114 08
| Epoch (UTC): | 25 May 2026 08:11:51 |
| Eccentricity: | 0.0001290 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 115.0165° |
| argument of perigee: | 57.8219° |
| revolutions per day: | 15.08828114 |
| mean anomaly at epoch: | 302.2898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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