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 24278U 96046B 25117.64875470 .00000032 00000-0 65390-4 0 9997
2 24278 98.5802 17.1843 0350935 93.8100 270.3232 13.53245167416969
| Epoch (UTC): | 27 April 2025 15:34:12 |
| Eccentricity: | 0.0350935 |
| inclination: | 98.5802° |
| perigee height: | 799 km |
| apogee height: | 1321 km |
| right ascension of ascending node: | 17.1843° |
| argument of perigee: | 93.8100° |
| revolutions per day: | 13.53245167 |
| mean anomaly at epoch: | 270.3232° |
| orbit number at epoch: | 41696 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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