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 00020U 59007A 24317.88190845 .00002231 00000-0 89191-3 0 9992
2 00020 33.3428 196.8712 1645727 181.5554 177.9379 11.60122616417036
Epoch (UTC): | 12 November 2024 21:09:56 |
Eccentricity: | 0.1645727 |
inclination: | 33.3428° |
perigee height: | 508 km |
apogee height: | 3221 km |
right ascension of ascending node: | 196.8712° |
argument of perigee: | 181.5554° |
revolutions per day: | 11.60122616 |
mean anomaly at epoch: | 177.9379° |
orbit number at epoch: | 41703 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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