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 62055U 26145.59641374 +.00000000 +00000-0 +38360-3 0 00001
2 62055 42.9987 181.4626 0001796 260.8861 99.1787 15.27614179 05
| Epoch (UTC): | 25 May 2026 14:18:50 |
| Eccentricity: | 0.0001796 |
| inclination: | 42.9987° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 181.4626° |
| argument of perigee: | 260.8861° |
| revolutions per day: | 15.27614179 |
| mean anomaly at epoch: | 99.1787° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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