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 41836U 26149.57266647 +.00000000 +00000-0 +00000-0 0 00000
2 41836 0.0160 90.0283 0001372 24.2921 119.7118 1.00269386 09
| Epoch (UTC): | 29 May 2026 13:44:38 |
| Eccentricity: | 0.0001372 |
| inclination: | 0.0160° |
| perigee height: | 35781 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 90.0283° |
| argument of perigee: | 24.2921° |
| revolutions per day: | 1.00269386 |
| mean anomaly at epoch: | 119.7118° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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