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 30959U 99025BAZ 24355.46652462 .00008036 00000-0 30350-2 0 9995
2 30959 99.6900 255.0281 0055509 147.1907 213.2738 14.30744126552647
Epoch (UTC): | 20 December 2024 11:11:47 |
Eccentricity: | 0.0055509 |
inclination: | 99.6900° |
perigee height: | 749 km |
apogee height: | 829 km |
right ascension of ascending node: | 255.0281° |
argument of perigee: | 147.1907° |
revolutions per day: | 14.30744126 |
mean anomaly at epoch: | 213.2738° |
orbit number at epoch: | 55264 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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