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 115U 60002D 25083.44623854 .00008703 00000-0 81670-3 0 9992
2 115 48.1622 147.1306 0027342 33.3983 326.8652 14.94271206471944
Epoch (UTC): | 24 March 2025 10:42:35 |
Eccentricity: | 0.0027342 |
inclination: | 48.1622° |
perigee height: | 565 km |
apogee height: | 603 km |
right ascension of ascending node: | 147.1306° |
argument of perigee: | 33.3983° |
revolutions per day: | 14.94271206 |
mean anomaly at epoch: | 326.8652° |
orbit number at epoch: | 47194 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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