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 43937U 19003F 23153.85291197 .00048824 00000-0 82453-3 0 9996
2 43937 97.0862 181.2512 0009694 334.6816 25.3960 15.51428932243823
Epoch (UTC): | 02 June 2023 20:28:11 |
Eccentricity: | 0.0009694 |
inclination: | 97.0862° |
perigee height: | 406 km |
apogee height: | 419 km |
right ascension of ascending node: | 181.2512° |
argument of perigee: | 334.6816° |
revolutions per day: | 15.51428932 |
mean anomaly at epoch: | 25.3960° |
orbit number at epoch: | 24382 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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