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 12698U 81053AS 24357.84185863 .00011109 00000-0 44261-2 0 9998
2 12698 82.9035 134.4993 0014926 228.1622 131.8290 14.28432689214247
Epoch (UTC): | 22 December 2024 20:12:16 |
Eccentricity: | 0.0014926 |
inclination: | 82.9035° |
perigee height: | 786 km |
apogee height: | 807 km |
right ascension of ascending node: | 134.4993° |
argument of perigee: | 228.1622° |
revolutions per day: | 14.28432689 |
mean anomaly at epoch: | 131.8290° |
orbit number at epoch: | 21424 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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