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 24317.83629836 .00003146 00000-0 39806-3 0 9999
2 28230 89.8344 61.9092 0002268 107.3366 252.8107 14.81655131566214
Epoch (UTC): | 12 November 2024 20:04:16 |
Eccentricity: | 0.0002268 |
inclination: | 89.8344° |
perigee height: | 622 km |
apogee height: | 625 km |
right ascension of ascending node: | 61.9092° |
argument of perigee: | 107.3366° |
revolutions per day: | 14.81655131 |
mean anomaly at epoch: | 252.8107° |
orbit number at epoch: | 56621 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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