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 40025U 14033R 24284.13775317 .00022710 00000-0 16856-2 0 9996
2 40025 98.0544 248.9937 0013223 144.2478 215.9634 15.02990214560639
Epoch (UTC): | 10 October 2024 03:18:21 |
Eccentricity: | 0.0013223 |
inclination: | 98.0544° |
perigee height: | 548 km |
apogee height: | 567 km |
right ascension of ascending node: | 248.9937° |
argument of perigee: | 144.2478° |
revolutions per day: | 15.02990214 |
mean anomaly at epoch: | 215.9634° |
orbit number at epoch: | 56063 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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