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 18421U 87088A 23159.41617552 .00008811 00000-0 35473-3 0 9991
2 18421 82.4969 275.5933 0011857 238.7960 121.2116 15.24663973949403
Epoch (UTC): | 08 June 2023 09:59:17 |
Eccentricity: | 0.0011857 |
inclination: | 82.4969° |
perigee height: | 483 km |
apogee height: | 500 km |
right ascension of ascending node: | 275.5933° |
argument of perigee: | 238.7960° |
revolutions per day: | 15.24663973 |
mean anomaly at epoch: | 121.2116° |
orbit number at epoch: | 94940 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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