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 18123U 87053A 25162.86285387 .00000031 00000-0 35305-4 0 9995
2 18123 98.7304 349.1365 0013116 142.4972 217.7122 14.19455623964292
Epoch (UTC): | 11 June 2025 20:42:30 |
Eccentricity: | 0.0013116 |
inclination: | 98.7304° |
perigee height: | 818 km |
apogee height: | 836 km |
right ascension of ascending node: | 349.1365° |
argument of perigee: | 142.4972° |
revolutions per day: | 14.19455623 |
mean anomaly at epoch: | 217.7122° |
orbit number at epoch: | 96429 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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