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 51886U 26145.34341652 +.00000000 +00000-0 +41640-3 0 00005
2 51886 53.2146 15.0077 0001327 99.3760 260.7382 15.08808035 04
| Epoch (UTC): | 25 May 2026 08:14:31 |
| Eccentricity: | 0.0001327 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 15.0077° |
| argument of perigee: | 99.3760° |
| revolutions per day: | 15.08808035 |
| mean anomaly at epoch: | 260.7382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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