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 28230U 04014A 23331.97421392 .00001971 00000-0 25748-3 0 9990
2 28230 89.8263 69.5691 0003056 77.2490 282.9075 14.80200226 57114
Epoch (UTC): | 27 November 2023 23:22:52 |
Eccentricity: | 0.0003056 |
inclination: | 89.8263° |
perigee height: | 626 km |
apogee height: | 631 km |
right ascension of ascending node: | 69.5691° |
argument of perigee: | 77.2490° |
revolutions per day: | 14.80200226 |
mean anomaly at epoch: | 282.9075° |
orbit number at epoch: | 5711 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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