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 24357.73533308 .00000038 00000-0 72885-4 0 9996
2 24278 98.5886 267.7139 0350787 60.0112 303.5358 13.53226779399939
| Epoch (UTC): | 22 December 2024 17:38:52 |
| Eccentricity: | 0.0350787 |
| inclination: | 98.5886° |
| perigee height: | 799 km |
| apogee height: | 1321 km |
| right ascension of ascending node: | 267.7139° |
| argument of perigee: | 60.0112° |
| revolutions per day: | 13.53226779 |
| mean anomaly at epoch: | 303.5358° |
| orbit number at epoch: | 39993 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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