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 data is extracted from the following two-line orbital elements,
1 02389U 66070A 25340.88542375 .00013473 00000-0 62583-3 0 9992
2 02389 81.3265 139.9887 1035402 294.7245 54.9601 13.39619117573160
| Epoch (UTC): | 06 December 2025 21:15:00 |
| Eccentricity: | 0.1035402 |
| inclination: | 81.3265° |
| perigee height: | 335 km |
| apogee height: | 1886 km |
| right ascension of ascending node: | 139.9887° |
| argument of perigee: | 294.7245° |
| revolutions per day: | 13.39619117 |
| mean anomaly at epoch: | 54.9601° |
| orbit number at epoch: | 57316 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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