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 51895U 26145.37285882 +.00000000 +00000-0 +82152-4 0 00004
2 51895 53.2136 14.8754 0001547 129.8068 230.3061 15.08840231 07
| Epoch (UTC): | 25 May 2026 08:56:55 |
| Eccentricity: | 0.0001547 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 14.8754° |
| argument of perigee: | 129.8068° |
| revolutions per day: | 15.08840231 |
| mean anomaly at epoch: | 230.3061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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