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 26050.53329634 +.00000000 +00000-0 +16299-3 0 00003
2 23908 63.3205 139.3866 0845658 47.6427 319.3124 13.45830958 04
| Epoch (UTC): | 19 February 2026 12:47:56 |
| Eccentricity: | 0.0845658 |
| inclination: | 63.3205° |
| perigee height: | 456 km |
| apogee height: | 1719 km |
| right ascension of ascending node: | 139.3866° |
| argument of perigee: | 47.6427° |
| revolutions per day: | 13.45830958 |
| mean anomaly at epoch: | 319.3124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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