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 36089U 09061B 24281.46430758 .00002312 00000-0 56808-3 0 9994
2 36089 98.3739 246.7597 0080380 131.1925 229.6237 14.51338888788449
Epoch (UTC): | 07 October 2024 11:08:36 |
Eccentricity: | 0.0080380 |
inclination: | 98.3739° |
perigee height: | 664 km |
apogee height: | 778 km |
right ascension of ascending node: | 246.7597° |
argument of perigee: | 131.1925° |
revolutions per day: | 14.51338888 |
mean anomaly at epoch: | 229.6237° |
orbit number at epoch: | 78844 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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