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 20580U 90037B 24306.82966797 .00017229 00000-0 75161-3 0 9997
2 20580 28.4662 141.1368 0002843 90.2894 269.8025 15.20723624697981
Epoch (UTC): | 01 November 2024 19:54:43 |
Eccentricity: | 0.0002843 |
inclination: | 28.4662° |
perigee height: | 502 km |
apogee height: | 505 km |
right ascension of ascending node: | 141.1368° |
argument of perigee: | 90.2894° |
revolutions per day: | 15.20723624 |
mean anomaly at epoch: | 269.8025° |
orbit number at epoch: | 69798 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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