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 23154.75630606 .00008348 00000-0 33685-3 0 9996
2 18421 82.4968 280.2601 0011670 256.6722 103.3214 15.24585686948914
Epoch (UTC): | 03 June 2023 18:09:04 |
Eccentricity: | 0.0011670 |
inclination: | 82.4968° |
perigee height: | 484 km |
apogee height: | 500 km |
right ascension of ascending node: | 280.2601° |
argument of perigee: | 256.6722° |
revolutions per day: | 15.24585686 |
mean anomaly at epoch: | 103.3214° |
orbit number at epoch: | 94891 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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