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 23157.38161352 .00008252 00000-0 33252-3 0 9999
2 18421 82.4973 277.6309 0011801 246.7029 113.2967 15.24629348949090
Epoch (UTC): | 06 June 2023 09:09:31 |
Eccentricity: | 0.0011801 |
inclination: | 82.4973° |
perigee height: | 484 km |
apogee height: | 500 km |
right ascension of ascending node: | 277.6309° |
argument of perigee: | 246.7029° |
revolutions per day: | 15.24629348 |
mean anomaly at epoch: | 113.2967° |
orbit number at epoch: | 94909 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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