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 00005U 58002B 24255.40363772 .00001625 00000-0 20580-2 0 9991
2 00005 34.2431 141.2923 1843319 116.0069 264.1639 10.85627216373291
| Epoch (UTC): | 11 September 2024 09:41:14 |
| Eccentricity: | 0.1843319 |
| inclination: | 34.2431° |
| perigee height: | 649 km |
| apogee height: | 3825 km |
| right ascension of ascending node: | 141.2923° |
| argument of perigee: | 116.0069° |
| revolutions per day: | 10.85627216 |
| mean anomaly at epoch: | 264.1639° |
| orbit number at epoch: | 37329 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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