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 24263.68175955 .00001124 00000-0 14133-2 0 9995
2 00005 34.2435 115.7461 1843206 153.3160 217.5526 10.85648047374191
| Epoch (UTC): | 19 September 2024 16:21:44 |
| Eccentricity: | 0.1843206 |
| inclination: | 34.2435° |
| perigee height: | 649 km |
| apogee height: | 3825 km |
| right ascension of ascending node: | 115.7461° |
| argument of perigee: | 153.3160° |
| revolutions per day: | 10.85648047 |
| mean anomaly at epoch: | 217.5526° |
| orbit number at epoch: | 37419 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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