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 25861U 99039B 23147.83157583 .00000489 00000-0 73001-4 0 9995
2 25861 98.1395 184.8956 0014255 308.0932 51.8992 14.79322239286532
Epoch (UTC): | 27 May 2023 19:57:28 |
Eccentricity: | 0.0014255 |
inclination: | 98.1395° |
perigee height: | 621 km |
apogee height: | 641 km |
right ascension of ascending node: | 184.8956° |
argument of perigee: | 308.0932° |
revolutions per day: | 14.79322239 |
mean anomaly at epoch: | 51.8992° |
orbit number at epoch: | 28653 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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