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 40892U 26145.54311935 +.00000000 +00000-0 +00000-0 0 00005
2 40892 0.2666 84.9581 0005960 344.5117 164.1513 1.00270228 08
| Epoch (UTC): | 25 May 2026 13:02:05 |
| Eccentricity: | 0.0005960 |
| inclination: | 0.2666° |
| perigee height: | 35762 km |
| apogee height: | 35812 km |
| right ascension of ascending node: | 84.9581° |
| argument of perigee: | 344.5117° |
| revolutions per day: | 1.00270228 |
| mean anomaly at epoch: | 164.1513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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