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 25397U 98043D 25164.83653104 .00000074 00000-0 52201-4 0 9993
2 25397 98.9702 144.0443 0001398 149.7393 210.3866 14.24316336399112
Epoch (UTC): | 13 June 2025 20:04:36 |
Eccentricity: | 0.0001398 |
inclination: | 98.9702° |
perigee height: | 810 km |
apogee height: | 812 km |
right ascension of ascending node: | 144.0443° |
argument of perigee: | 149.7393° |
revolutions per day: | 14.24316336 |
mean anomaly at epoch: | 210.3866° |
orbit number at epoch: | 39911 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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