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 23657U 26069.42587308 +.00000000 +00000-0 +18055-3 0 00008
2 23657 82.5242 136.1055 0017131 296.8951 63.0519 14.94369475 08
| Epoch (UTC): | 10 March 2026 10:13:15 |
| Eccentricity: | 0.0017131 |
| inclination: | 82.5242° |
| perigee height: | 572 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 136.1055° |
| argument of perigee: | 296.8951° |
| revolutions per day: | 14.94369475 |
| mean anomaly at epoch: | 63.0519° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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