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 53807U 22111AL 23336.41032216 .00015732 00000-0 67052-3 0 9997
2 53807 53.2377 22.7206 0010204 201.9921 158.0641 15.23093264 68062
Epoch (UTC): | 02 December 2023 09:50:51 |
Eccentricity: | 0.0010204 |
inclination: | 53.2377° |
perigee height: | 489 km |
apogee height: | 503 km |
right ascension of ascending node: | 22.7206° |
argument of perigee: | 201.9921° |
revolutions per day: | 15.23093264 |
mean anomaly at epoch: | 158.0641° |
orbit number at epoch: | 6806 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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