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 24827U 97028A 24287.55860310 -.00000081 00000-0 -38344-3 0 9996
2 24827 63.3084 151.8250 1076836 61.6259 321.8861 11.07978008106794
| Epoch (UTC): | 13 October 2024 13:24:23 |
| Eccentricity: | 0.1076836 |
| inclination: | 63.3084° |
| perigee height: | 1206 km |
| apogee height: | 3036 km |
| right ascension of ascending node: | 151.8250° |
| argument of perigee: | 61.6259° |
| revolutions per day: | 11.07978008 |
| mean anomaly at epoch: | 321.8861° |
| orbit number at epoch: | 10679 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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