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 47825U 26145.54385284 +.00000000 +00000-0 -65598-4 0 00004
2 47825 53.1612 245.3839 0002363 89.5444 270.5828 15.31676288 07
| Epoch (UTC): | 25 May 2026 13:03:08 |
| Eccentricity: | 0.0002363 |
| inclination: | 53.1612° |
| perigee height: | 469 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 245.3839° |
| argument of perigee: | 89.5444° |
| revolutions per day: | 15.31676288 |
| mean anomaly at epoch: | 270.5828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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