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 51866U 26145.40230824 +.00000000 +00000-0 -29360-4 0 00005
2 51866 53.2128 24.6000 0001061 113.1810 246.9294 15.08836181 01
| Epoch (UTC): | 25 May 2026 09:39:19 |
| Eccentricity: | 0.0001061 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 24.6000° |
| argument of perigee: | 113.1810° |
| revolutions per day: | 15.08836181 |
| mean anomaly at epoch: | 246.9294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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