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 18313U 87068B 24278.50325140 .00000111 00000-0 85744-4 0 9993
2 18313 82.5550 74.3215 0010421 23.3125 336.8505 13.84261037876173
Epoch (UTC): | 04 October 2024 12:04:40 |
Eccentricity: | 0.0010421 |
inclination: | 82.5550° |
perigee height: | 941 km |
apogee height: | 956 km |
right ascension of ascending node: | 74.3215° |
argument of perigee: | 23.3125° |
revolutions per day: | 13.84261037 |
mean anomaly at epoch: | 336.8505° |
orbit number at epoch: | 87617 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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