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 42807U 17039E 24357.97961761 .00000017 00000-0 -98598-6 0 9992
2 42807 86.3985 219.7663 0001927 85.5658 274.5758 14.34217377392384
Epoch (UTC): | 22 December 2024 23:30:38 |
Eccentricity: | 0.0001927 |
inclination: | 86.3985° |
perigee height: | 776 km |
apogee height: | 779 km |
right ascension of ascending node: | 219.7663° |
argument of perigee: | 85.5658° |
revolutions per day: | 14.34217377 |
mean anomaly at epoch: | 274.5758° |
orbit number at epoch: | 39238 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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