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 48269U 21034B 24358.17004504 .00022132 00000-0 14564-2 0 9994
2 48269 97.6407 61.2427 0003237 356.9128 3.2079 15.07558892198880
Epoch (UTC): | 23 December 2024 04:04:51 |
Eccentricity: | 0.0003237 |
inclination: | 97.6407° |
perigee height: | 541 km |
apogee height: | 546 km |
right ascension of ascending node: | 61.2427° |
argument of perigee: | 356.9128° |
revolutions per day: | 15.07558892 |
mean anomaly at epoch: | 3.2079° |
orbit number at epoch: | 19888 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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