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 61436U 24140ZD 24357.93123269 .00002980 00000-0 14543-2 0 9995
2 61436 88.9515 334.8037 0060685 130.8542 229.7929 14.16842335 17447
Epoch (UTC): | 22 December 2024 22:20:58 |
Eccentricity: | 0.0060685 |
inclination: | 88.9515° |
perigee height: | 792 km |
apogee height: | 880 km |
right ascension of ascending node: | 334.8037° |
argument of perigee: | 130.8542° |
revolutions per day: | 14.16842335 |
mean anomaly at epoch: | 229.7929° |
orbit number at epoch: | 1744 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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