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 40069U 14037A 23085.45179936 -.00000024 00000-0 78287-5 0 9990
2 40069 98.4260 95.2618 0005137 211.9389 148.1484 14.20758948451907
Epoch (UTC): | 26 March 2023 10:50:35 |
Eccentricity: | 0.0005137 |
inclination: | 98.4260° |
perigee height: | 819 km |
apogee height: | 826 km |
right ascension of ascending node: | 95.2618° |
argument of perigee: | 211.9389° |
revolutions per day: | 14.20758948 |
mean anomaly at epoch: | 148.1484° |
orbit number at epoch: | 45190 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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