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 24298U 96051B 23159.39161765 -.00000025 00000-0 12865-4 0 9998
2 24298 70.8266 139.8205 0017504 190.1535 169.9234 14.12516344379694
Epoch (UTC): | 08 June 2023 09:23:55 |
Eccentricity: | 0.0017504 |
inclination: | 70.8266° |
perigee height: | 838 km |
apogee height: | 863 km |
right ascension of ascending node: | 139.8205° |
argument of perigee: | 190.1535° |
revolutions per day: | 14.12516344 |
mean anomaly at epoch: | 169.9234° |
orbit number at epoch: | 37969 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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