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 31113U 26150.45497404 +.00000000 +00000-0 +58323-4 0 00008
2 31113 98.3487 132.9887 0012249 252.7542 107.2301 14.31022107 08
| Epoch (UTC): | 30 May 2026 10:55:09 |
| Eccentricity: | 0.0012249 |
| inclination: | 98.3487° |
| perigee height: | 780 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 132.9887° |
| argument of perigee: | 252.7542° |
| revolutions per day: | 14.31022107 |
| mean anomaly at epoch: | 107.2301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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