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 24091U 94029EN 24357.79480089 .00007215 00000-0 54331-3 0 9990
2 24091 81.9947 216.4693 0068472 206.6952 283.2526 15.00473290548910
| Epoch (UTC): | 22 December 2024 19:04:30 |
| Eccentricity: | 0.0068472 |
| inclination: | 81.9947° |
| perigee height: | 518 km |
| apogee height: | 613 km |
| right ascension of ascending node: | 216.4693° |
| argument of perigee: | 206.6952° |
| revolutions per day: | 15.00473290 |
| mean anomaly at epoch: | 283.2526° |
| orbit number at epoch: | 54891 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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