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 39462U 13072A 26005.24431153 0.00000000 00000-0 00000-0 0 06
2 39462 122.9991 239.5418 0004000 230.1093 129.8907 13.41439400 08
| Epoch (UTC): | 05 January 2026 05:51:48 |
| Eccentricity: | 0.0004000 |
| inclination: | 122.9991° |
| perigee height: | 1101 km |
| apogee height: | 1107 km |
| right ascension of ascending node: | 239.5418° |
| argument of perigee: | 230.1093° |
| revolutions per day: | 13.41439400 |
| mean anomaly at epoch: | 129.8907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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