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 40908U 15049K 25119.17669847 .00015998 00000-0 43133-3 0 9995
2 40908 97.5086 138.5476 0007688 317.2417 42.8229 15.37865097531867
Epoch (UTC): | 29 April 2025 04:14:26 |
Eccentricity: | 0.0007688 |
inclination: | 97.5086° |
perigee height: | 447 km |
apogee height: | 457 km |
right ascension of ascending node: | 138.5476° |
argument of perigee: | 317.2417° |
revolutions per day: | 15.37865097 |
mean anomaly at epoch: | 42.8229° |
orbit number at epoch: | 53186 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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