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 18421U 87088A 24284.56387176 .00032856 00000-0 79295-3 0 9999
2 18421 82.4888 139.7781 0008106 318.5646 41.4984 15.41011260 24399
Epoch (UTC): | 10 October 2024 13:31:58 |
Eccentricity: | 0.0008106 |
inclination: | 82.4888° |
perigee height: | 437 km |
apogee height: | 448 km |
right ascension of ascending node: | 139.7781° |
argument of perigee: | 318.5646° |
revolutions per day: | 15.41011260 |
mean anomaly at epoch: | 41.4984° |
orbit number at epoch: | 2439 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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