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 23908U 26042.28558007 +.00000000 +00000-0 +17190-3 0 00005
2 23908 63.3205 160.9493 0845119 47.5161 319.4204 13.45813845 02
| Epoch (UTC): | 11 February 2026 06:51:14 |
| Eccentricity: | 0.0845119 |
| inclination: | 63.3205° |
| perigee height: | 457 km |
| apogee height: | 1719 km |
| right ascension of ascending node: | 160.9493° |
| argument of perigee: | 47.5161° |
| revolutions per day: | 13.45813845 |
| mean anomaly at epoch: | 319.4204° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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