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 41419U 00055KY 24356.24446296 .00025776 00000-0 81841-2 0 9997
2 41419 98.8577 92.5059 0017841 260.8698 99.0471 14.39812932455809
Epoch (UTC): | 21 December 2024 05:52:01 |
Eccentricity: | 0.0017841 |
inclination: | 98.8577° |
perigee height: | 746 km |
apogee height: | 772 km |
right ascension of ascending node: | 92.5059° |
argument of perigee: | 260.8698° |
revolutions per day: | 14.39812932 |
mean anomaly at epoch: | 99.0471° |
orbit number at epoch: | 45580 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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