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 55826U 26145.38139193 +.00000000 +00000-0 -12158-2 0 00004
2 55826 87.9164 279.0215 0002091 119.0197 241.1146 13.20772200 02
| Epoch (UTC): | 25 May 2026 09:09:12 |
| Eccentricity: | 0.0002091 |
| inclination: | 87.9164° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 279.0215° |
| argument of perigee: | 119.0197° |
| revolutions per day: | 13.20772200 |
| mean anomaly at epoch: | 241.1146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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