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 04256U 69082B 25344.78959804 .00000214 00000-0 18420-3 0 9995
2 04256 70.0105 9.7227 0022067 306.1046 53.8018 13.99129795864116
| Epoch (UTC): | 10 December 2025 18:57:01 |
| Eccentricity: | 0.0022067 |
| inclination: | 70.0105° |
| perigee height: | 881 km |
| apogee height: | 913 km |
| right ascension of ascending node: | 9.7227° |
| argument of perigee: | 306.1046° |
| revolutions per day: | 13.99129795 |
| mean anomaly at epoch: | 53.8018° |
| orbit number at epoch: | 86411 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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