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 5U 58002B 23339.88082696 .00000401 00000-0 49489-3 0 9999
2 5 34.2588 286.1208 1842820 292.4934 49.1200 10.85128437342905
| Epoch (UTC): | 05 December 2023 21:08:23 |
| Eccentricity: | 0.1842820 |
| inclination: | 34.2588° |
| perigee height: | 652 km |
| apogee height: | 3828 km |
| right ascension of ascending node: | 286.1208° |
| argument of perigee: | 292.4934° |
| revolutions per day: | 10.85128437 |
| mean anomaly at epoch: | 49.1200° |
| orbit number at epoch: | 34290 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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