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 23227U 26151.15876337 +.00000000 +00000-0 +00000-0 0 00004
2 23227 12.3339 30.4682 0006957 22.0704 323.8306 0.98694768 06
| Epoch (UTC): | 31 May 2026 03:48:37 |
| Eccentricity: | 0.0006957 |
| inclination: | 12.3339° |
| perigee height: | 36205 km |
| apogee height: | 36264 km |
| right ascension of ascending node: | 30.4682° |
| argument of perigee: | 22.0704° |
| revolutions per day: | 0.98694768 |
| mean anomaly at epoch: | 323.8306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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