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 25197.85956160 .00000509 00000-0 61340-4 0 9990
2 28230 89.8360 56.7981 0003374 81.4098 278.7509 14.82519077602655
Epoch (UTC): | 16 July 2025 20:37:46 |
Eccentricity: | 0.0003374 |
inclination: | 89.8360° |
perigee height: | 619 km |
apogee height: | 624 km |
right ascension of ascending node: | 56.7981° |
argument of perigee: | 81.4098° |
revolutions per day: | 14.82519077 |
mean anomaly at epoch: | 278.7509° |
orbit number at epoch: | 60265 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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