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 40895U 26145.08188917 +.00000000 +00000-0 +00000-0 0 00009
2 40895 0.0168 288.4386 0000385 18.4396 311.2750 1.00271485 06
| Epoch (UTC): | 25 May 2026 01:57:55 |
| Eccentricity: | 0.0000385 |
| inclination: | 0.0168° |
| perigee height: | 35785 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 288.4386° |
| argument of perigee: | 18.4396° |
| revolutions per day: | 1.00271485 |
| mean anomaly at epoch: | 311.2750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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