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 23150.46875379 -.00000009 00000-0 21549-4 0 9991
2 24298 70.8264 158.6451 0018103 201.9871 158.0474 14.12515799378433
Epoch (UTC): | 30 May 2023 11:15:00 |
Eccentricity: | 0.0018103 |
inclination: | 70.8264° |
perigee height: | 837 km |
apogee height: | 864 km |
right ascension of ascending node: | 158.6451° |
argument of perigee: | 201.9871° |
revolutions per day: | 14.12515799 |
mean anomaly at epoch: | 158.0474° |
orbit number at epoch: | 37843 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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