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 06155U 72065B 24311.90150179 .00005829 00000-0 83583-3 0 9994
2 06155 35.0026 280.2653 0036110 230.8045 128.9445 14.75515224769117
Epoch (UTC): | 06 November 2024 21:38:09 |
Eccentricity: | 0.0036110 |
inclination: | 35.0026° |
perigee height: | 618 km |
apogee height: | 669 km |
right ascension of ascending node: | 280.2653° |
argument of perigee: | 230.8045° |
revolutions per day: | 14.75515224 |
mean anomaly at epoch: | 128.9445° |
orbit number at epoch: | 76911 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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