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 42130U 81053QS 24351.77052963 .00006646 00000-0 32489-2 0 9991
2 42130 82.8591 169.7222 0020332 134.4268 225.8580 14.17710376568873
Epoch (UTC): | 16 December 2024 18:29:33 |
Eccentricity: | 0.0020332 |
inclination: | 82.8591° |
perigee height: | 818 km |
apogee height: | 848 km |
right ascension of ascending node: | 169.7222° |
argument of perigee: | 134.4268° |
revolutions per day: | 14.17710376 |
mean anomaly at epoch: | 225.8580° |
orbit number at epoch: | 56887 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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