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 40333U 26144.56598985 +.00000000 +00000-0 +00000-0 0 00008
2 40333 0.0100 1.8500 0000249 205.2209 139.6088 1.00272307 02
| Epoch (UTC): | 24 May 2026 13:35:01 |
| Eccentricity: | 0.0000249 |
| inclination: | 0.0100° |
| perigee height: | 35785 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 1.8500° |
| argument of perigee: | 205.2209° |
| revolutions per day: | 1.00272307 |
| mean anomaly at epoch: | 139.6088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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