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 23036.38853132 .00000082 00000-0 11639-3 0 9990
2 00005 34.2452 141.5331 1845578 6.1248 355.8941 10.85057509309843
| Epoch (UTC): | 05 February 2023 09:19:29 |
| Eccentricity: | 0.1845578 |
| inclination: | 34.2452° |
| perigee height: | 650 km |
| apogee height: | 3831 km |
| right ascension of ascending node: | 141.5331° |
| argument of perigee: | 6.1248° |
| revolutions per day: | 10.85057509 |
| mean anomaly at epoch: | 355.8941° |
| orbit number at epoch: | 30984 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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