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 55807U 26145.38488582 +.00000000 +00000-0 +31391-3 0 00002
2 55807 87.8932 294.2794 0001178 105.7962 254.3298 13.14502199 06
| Epoch (UTC): | 25 May 2026 09:14:14 |
| Eccentricity: | 0.0001178 |
| inclination: | 87.8932° |
| perigee height: | 1205 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2794° |
| argument of perigee: | 105.7962° |
| revolutions per day: | 13.14502199 |
| mean anomaly at epoch: | 254.3298° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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