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 41339U 16012C 24358.08673577 .00009304 00000-0 53081-3 0 9991
2 41339 31.0061 251.4797 0010986 338.2861 21.7311 15.11413088486143
Epoch (UTC): | 23 December 2024 02:04:53 |
Eccentricity: | 0.0010986 |
inclination: | 31.0061° |
perigee height: | 524 km |
apogee height: | 539 km |
right ascension of ascending node: | 251.4797° |
argument of perigee: | 338.2861° |
revolutions per day: | 15.11413088 |
mean anomaly at epoch: | 21.7311° |
orbit number at epoch: | 48614 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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