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 23086.81484137 .00047087 00000-0 10187-2 0 9999
2 43937 97.0992 115.4766 0014915 204.2296 155.8254 15.44215094233451
Epoch (UTC): | 27 March 2023 19:33:22 |
Eccentricity: | 0.0014915 |
inclination: | 97.0992° |
perigee height: | 423 km |
apogee height: | 444 km |
right ascension of ascending node: | 115.4766° |
argument of perigee: | 204.2296° |
revolutions per day: | 15.44215094 |
mean anomaly at epoch: | 155.8254° |
orbit number at epoch: | 23345 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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