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 55798U 26145.35786345 +.00000000 +00000-0 +53872-3 0 00004
2 55798 87.9165 279.0233 0002406 80.2189 279.9216 13.20771288 03
| Epoch (UTC): | 25 May 2026 08:35:19 |
| Eccentricity: | 0.0002406 |
| inclination: | 87.9165° |
| perigee height: | 1180 km |
| apogee height: | 1184 km |
| right ascension of ascending node: | 279.0233° |
| argument of perigee: | 80.2189° |
| revolutions per day: | 13.20771288 |
| mean anomaly at epoch: | 279.9216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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