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 62831U 26145.54898076 +.00000000 +00000-0 +13334-2 0 00004
2 62831 43.0011 203.1557 0002992 247.7519 112.3031 15.70842907 05
| Epoch (UTC): | 25 May 2026 13:10:31 |
| Eccentricity: | 0.0002992 |
| inclination: | 43.0011° |
| perigee height: | 354 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 203.1557° |
| argument of perigee: | 247.7519° |
| revolutions per day: | 15.70842907 |
| mean anomaly at epoch: | 112.3031° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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