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 39928U 94029AGB 24357.02125107 .00038019 00000-0 35549-2 0 9993
2 39928 81.0119 92.8427 0149901 61.2371 300.3804 14.85741048555150
| Epoch (UTC): | 22 December 2024 00:30:36 |
| Eccentricity: | 0.0149901 |
| inclination: | 81.0119° |
| perigee height: | 506 km |
| apogee height: | 716 km |
| right ascension of ascending node: | 92.8427° |
| argument of perigee: | 61.2371° |
| revolutions per day: | 14.85741048 |
| mean anomaly at epoch: | 300.3804° |
| orbit number at epoch: | 55515 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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