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 31012U 99025BDE 24358.18218861 .00000837 00000-0 34764-3 0 9994
2 31012 98.9481 242.6462 0082425 198.5422 313.5704 14.27368946927074
Epoch (UTC): | 23 December 2024 04:22:21 |
Eccentricity: | 0.0082425 |
inclination: | 98.9481° |
perigee height: | 741 km |
apogee height: | 860 km |
right ascension of ascending node: | 242.6462° |
argument of perigee: | 198.5422° |
revolutions per day: | 14.27368946 |
mean anomaly at epoch: | 313.5704° |
orbit number at epoch: | 92707 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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