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 23150.11467181 -.00000015 00000-0 18266-4 0 9990
2 24298 70.8264 159.3922 0018124 202.4406 157.5923 14.12515765378646
Epoch (UTC): | 30 May 2023 02:45:07 |
Eccentricity: | 0.0018124 |
inclination: | 70.8264° |
perigee height: | 837 km |
apogee height: | 864 km |
right ascension of ascending node: | 159.3922° |
argument of perigee: | 202.4406° |
revolutions per day: | 14.12515765 |
mean anomaly at epoch: | 157.5923° |
orbit number at epoch: | 37864 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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