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 30814U 99025AUY 24311.48993609 .00045465 00000-0 12613-1 0 9998
2 30814 99.0610 248.7842 0044718 4.1024 61.6917 14.45705283919124
Epoch (UTC): | 06 November 2024 11:45:30 |
Eccentricity: | 0.0044718 |
inclination: | 99.0610° |
perigee height: | 708 km |
apogee height: | 771 km |
right ascension of ascending node: | 248.7842° |
argument of perigee: | 4.1024° |
revolutions per day: | 14.45705283 |
mean anomaly at epoch: | 61.6917° |
orbit number at epoch: | 91912 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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