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 55824U 26145.38813347 +.00000000 +00000-0 +27438-3 0 00009
2 55824 87.9161 279.0304 0002191 88.1632 271.9752 13.20770964 06
| Epoch (UTC): | 25 May 2026 09:18:54 |
| Eccentricity: | 0.0002191 |
| inclination: | 87.9161° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 279.0304° |
| argument of perigee: | 88.1632° |
| revolutions per day: | 13.20770964 |
| mean anomaly at epoch: | 271.9752° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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