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 55825U 26145.39915709 +.00000000 +00000-0 +79449-3 0 00005
2 55825 87.8934 294.2703 0001662 88.1057 272.0263 13.14501828 02
| Epoch (UTC): | 25 May 2026 09:34:47 |
| Eccentricity: | 0.0001662 |
| inclination: | 87.8934° |
| perigee height: | 1205 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2703° |
| argument of perigee: | 88.1057° |
| revolutions per day: | 13.14501828 |
| mean anomaly at epoch: | 272.0263° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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