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 40903U 15049E 23112.43632650 .18814400 25108-5 15498-3 0 9990
2 40903 97.0819 181.5568 0011783 175.5276 309.8044 16.51931608427640
Epoch (UTC): | 22 April 2023 10:28:18 |
Eccentricity: | 0.0011783 |
inclination: | 97.0819° |
perigee height: | 126 km |
apogee height: | 142 km |
right ascension of ascending node: | 181.5568° |
argument of perigee: | 175.5276° |
revolutions per day: | 16.51931608 |
mean anomaly at epoch: | 309.8044° |
orbit number at epoch: | 42764 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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