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 51647U 26145.41267507 +.00000000 +00000-0 -13429-2 0 00008
2 51647 87.8849 40.8056 0001858 93.0249 267.1091 13.10370387 00
| Epoch (UTC): | 25 May 2026 09:54:15 |
| Eccentricity: | 0.0001858 |
| inclination: | 87.8849° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8056° |
| argument of perigee: | 93.0249° |
| revolutions per day: | 13.10370387 |
| mean anomaly at epoch: | 267.1091° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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