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 55818U 26145.40376700 +.00000000 +00000-0 +22801-3 0 00001
2 55818 87.9150 309.5168 0002045 113.7493 246.3854 13.19726326 02
| Epoch (UTC): | 25 May 2026 09:41:25 |
| Eccentricity: | 0.0002045 |
| inclination: | 87.9150° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5168° |
| argument of perigee: | 113.7493° |
| revolutions per day: | 13.19726326 |
| mean anomaly at epoch: | 246.3854° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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