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 00115U 60002D 24261.29284232 .00021219 00000-0 21217-2 0 9992
2 00115 48.1646 345.0050 0031457 274.9605 84.7719 14.90931385422678
Epoch (UTC): | 17 September 2024 07:01:41 |
Eccentricity: | 0.0031457 |
inclination: | 48.1646° |
perigee height: | 573 km |
apogee height: | 617 km |
right ascension of ascending node: | 345.0050° |
argument of perigee: | 274.9605° |
revolutions per day: | 14.90931385 |
mean anomaly at epoch: | 84.7719° |
orbit number at epoch: | 42267 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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