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 14760U 84019B 23275.34254917 .00000572 00000-0 20376-3 0 9999
2 14760 74.0428 225.3029 0028928 241.7539 118.0693 14.36271813 73440
Epoch (UTC): | 02 October 2023 08:13:16 |
Eccentricity: | 0.0028928 |
inclination: | 74.0428° |
perigee height: | 750 km |
apogee height: | 791 km |
right ascension of ascending node: | 225.3029° |
argument of perigee: | 241.7539° |
revolutions per day: | 14.36271813 |
mean anomaly at epoch: | 118.0693° |
orbit number at epoch: | 7344 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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