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 23267.07042684 .00000127 00000-0 15563-3 0 9994
2 5 34.2511 150.5140 1845672 324.6715 24.4202 10.85085269335009
| Epoch (UTC): | 24 September 2023 01:41:24 |
| Eccentricity: | 0.1845672 |
| inclination: | 34.2511° |
| perigee height: | 649 km |
| apogee height: | 3831 km |
| right ascension of ascending node: | 150.5140° |
| argument of perigee: | 324.6715° |
| revolutions per day: | 10.85085269 |
| mean anomaly at epoch: | 24.4202° |
| orbit number at epoch: | 33500 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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