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 25544U 98067A 23079.87218834 .00015558 00000-0 28656-3 0 9996
2 25544 51.6406 46.0718 0006135 111.8377 340.8929 15.49330280388091
Epoch (UTC): | 20 March 2023 20:55:57 |
Eccentricity: | 0.0006135 |
inclination: | 51.6406° |
perigee height: | 414 km |
apogee height: | 423 km |
right ascension of ascending node: | 46.0718° |
argument of perigee: | 111.8377° |
revolutions per day: | 15.49330280 |
mean anomaly at epoch: | 340.8929° |
orbit number at epoch: | 38809 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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