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 51725U 26145.55592578 +.00000000 +00000-0 +22487-4 0 00004
2 51725 53.2135 344.0526 0001388 89.2438 270.8713 15.08842249 00
| Epoch (UTC): | 25 May 2026 13:20:31 |
| Eccentricity: | 0.0001388 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 344.0526° |
| argument of perigee: | 89.2438° |
| revolutions per day: | 15.08842249 |
| mean anomaly at epoch: | 270.8713° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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