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 31090U 99025BGL 24357.54120549 .00026914 00000-0 16469-2 0 9999
2 31090 99.0222 28.8435 0096356 237.7364 121.4495 15.06338707954509
Epoch (UTC): | 22 December 2024 12:59:20 |
Eccentricity: | 0.0096356 |
inclination: | 99.0222° |
perigee height: | 480 km |
apogee height: | 614 km |
right ascension of ascending node: | 28.8435° |
argument of perigee: | 237.7364° |
revolutions per day: | 15.06338707 |
mean anomaly at epoch: | 121.4495° |
orbit number at epoch: | 95450 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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