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 23030.58693324 .00000118 00000-0 15096-3 0 9992
2 00005 34.2482 159.4173 1845893 339.9941 13.6615 10.85056306309217
| Epoch (UTC): | 30 January 2023 14:05:11 |
| Eccentricity: | 0.1845893 |
| inclination: | 34.2482° |
| perigee height: | 649 km |
| apogee height: | 3831 km |
| right ascension of ascending node: | 159.4173° |
| argument of perigee: | 339.9941° |
| revolutions per day: | 10.85056306 |
| mean anomaly at epoch: | 13.6615° |
| orbit number at epoch: | 30921 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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