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 52882U 26145.37695404 +.00000000 +00000-0 +90528-5 0 00003
2 52882 53.2117 29.4310 0001073 97.5311 262.5803 15.08826429 03
| Epoch (UTC): | 25 May 2026 09:02:48 |
| Eccentricity: | 0.0001073 |
| inclination: | 53.2117° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 29.4310° |
| argument of perigee: | 97.5311° |
| revolutions per day: | 15.08826429 |
| mean anomaly at epoch: | 262.5803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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