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 55806U 26145.42903295 +.00000000 +00000-0 +10369-3 0 00001
2 55806 87.9151 309.5141 0000976 85.5505 274.5739 13.19725873 03
| Epoch (UTC): | 25 May 2026 10:17:48 |
| Eccentricity: | 0.0000976 |
| inclination: | 87.9151° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5141° |
| argument of perigee: | 85.5505° |
| revolutions per day: | 13.19725873 |
| mean anomaly at epoch: | 274.5739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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