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 13354U 82069B 23159.50781469 .00000159 00000-0 13873-3 0 9991
2 13354 82.9579 157.6813 0053213 119.7093 240.9377 13.79029880 58140
Epoch (UTC): | 08 June 2023 12:11:15 |
Eccentricity: | 0.0053213 |
inclination: | 82.9579° |
perigee height: | 928 km |
apogee height: | 1006 km |
right ascension of ascending node: | 157.6813° |
argument of perigee: | 119.7093° |
revolutions per day: | 13.79029880 |
mean anomaly at epoch: | 240.9377° |
orbit number at epoch: | 5814 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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