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 62331U 26145.58305602 +.00000000 +00000-0 +10828-3 0 00007
2 62331 86.5001 350.8917 0001494 84.3558 275.7746 13.24407391 03
| Epoch (UTC): | 25 May 2026 13:59:36 |
| Eccentricity: | 0.0001494 |
| inclination: | 86.5001° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 350.8917° |
| argument of perigee: | 84.3558° |
| revolutions per day: | 13.24407391 |
| mean anomaly at epoch: | 275.7746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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