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 38771U 12049A 23277.77042022 .00000262 00000-0 13943-3 0 9990
2 38771 98.6666 335.2512 0001226 92.9861 15.4107 14.21505178573115
Epoch (UTC): | 04 October 2023 18:29:24 |
Eccentricity: | 0.0001226 |
inclination: | 98.6666° |
perigee height: | 819 km |
apogee height: | 821 km |
right ascension of ascending node: | 335.2512° |
argument of perigee: | 92.9861° |
revolutions per day: | 14.21505178 |
mean anomaly at epoch: | 15.4107° |
orbit number at epoch: | 57311 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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