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 43145U 18005A 23140.96047659 0.00000000 00000-0 00000-0 0 00
2 43145 106.0225 0.2272 0002644 28.0468 331.9532 13.48009236 04
Epoch (UTC): | 20 May 2023 23:03:05 |
Eccentricity: | 0.0002644 |
inclination: | 106.0225° |
perigee height: | 1077 km |
apogee height: | 1081 km |
right ascension of ascending node: | 0.2272° |
argument of perigee: | 28.0468° |
revolutions per day: | 13.48009236 |
mean anomaly at epoch: | 331.9532° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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