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 18123U 87053A 23274.12816291 .00000405 00000-0 21451-3 0 9991
2 18123 98.7275 98.5683 0013568 124.7202 235.5254 14.19108684876622
Epoch (UTC): | 01 October 2023 03:04:33 |
Eccentricity: | 0.0013568 |
inclination: | 98.7275° |
perigee height: | 818 km |
apogee height: | 838 km |
right ascension of ascending node: | 98.5683° |
argument of perigee: | 124.7202° |
revolutions per day: | 14.19108684 |
mean anomaly at epoch: | 235.5254° |
orbit number at epoch: | 87662 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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