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 40941U 26145.56769501 +.00000000 +00000-0 +00000-0 0 00008
2 40941 0.0509 80.6538 0002291 330.2197 315.6506 1.00271528 05
| Epoch (UTC): | 25 May 2026 13:37:28 |
| Eccentricity: | 0.0002291 |
| inclination: | 0.0509° |
| perigee height: | 35777 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 80.6538° |
| argument of perigee: | 330.2197° |
| revolutions per day: | 1.00271528 |
| mean anomaly at epoch: | 315.6506° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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