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 23152.45910146 .00008533 00000-0 34474-3 0 9994
2 18421 82.4959 282.5609 0011592 266.1294 93.8618 15.24548036948346
Epoch (UTC): | 01 June 2023 11:01:06 |
Eccentricity: | 0.0011592 |
inclination: | 82.4959° |
perigee height: | 484 km |
apogee height: | 500 km |
right ascension of ascending node: | 282.5609° |
argument of perigee: | 266.1294° |
revolutions per day: | 15.24548036 |
mean anomaly at epoch: | 93.8618° |
orbit number at epoch: | 94834 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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