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 41334U 16010A 23086.81212528 0.00000100 00000-0 17903-3 0 08
2 41334 123.0067 152.2528 0003592 133.0872 226.9361 13.41446917 03
Epoch (UTC): | 27 March 2023 19:29:27 |
Eccentricity: | 0.0003592 |
inclination: | 123.0067° |
perigee height: | 1101 km |
apogee height: | 1106 km |
right ascension of ascending node: | 152.2528° |
argument of perigee: | 133.0872° |
revolutions per day: | 13.41446917 |
mean anomaly at epoch: | 226.9361° |
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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