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 00045U 60007A 24306.85612356 .00002250 00000-0 56685-3 0 9995
2 00045 66.6931 126.0484 0257331 232.4501 125.2974 14.35062259295020
Epoch (UTC): | 01 November 2024 20:32:49 |
Eccentricity: | 0.0257331 |
inclination: | 66.6931° |
perigee height: | 591 km |
apogee height: | 959 km |
right ascension of ascending node: | 126.0484° |
argument of perigee: | 232.4501° |
revolutions per day: | 14.35062259 |
mean anomaly at epoch: | 125.2974° |
orbit number at epoch: | 29502 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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