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 09481U 26088.15902137 +.00000000 +00000-0 +11792-4 0 00001
2 09481 81.2150 122.6017 0023663 133.5325 226.7817 14.10344566 09
| Epoch (UTC): | 29 March 2026 03:48:59 |
| Eccentricity: | 0.0023663 |
| inclination: | 81.2150° |
| perigee height: | 841 km |
| apogee height: | 875 km |
| right ascension of ascending node: | 122.6017° |
| argument of perigee: | 133.5325° |
| revolutions per day: | 14.10344566 |
| mean anomaly at epoch: | 226.7817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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