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 12298U 81013B 25190.84046236 .00000035 00000-0 20072-4 0 9998
2 12298 82.9505 303.1665 0028364 292.2594 181.7237 13.76884069230144
Epoch (UTC): | 09 July 2025 20:10:15 |
Eccentricity: | 0.0028364 |
inclination: | 82.9505° |
perigee height: | 954 km |
apogee height: | 996 km |
right ascension of ascending node: | 303.1665° |
argument of perigee: | 292.2594° |
revolutions per day: | 13.76884069 |
mean anomaly at epoch: | 181.7237° |
orbit number at epoch: | 23014 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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