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 40057U 14034E 22220.46388722 .00000916 00000-0 13070-3 0 9996
2 40057 98.3684 35.0976 0011091 157.5242 202.6470 14.79294629437169
Epoch (UTC): | 08 August 2022 11:07:59 |
Eccentricity: | 0.0011091 |
inclination: | 98.3684° |
perigee height: | 624 km |
apogee height: | 639 km |
right ascension of ascending node: | 35.0976° |
argument of perigee: | 157.5242° |
revolutions per day: | 14.79294629 |
mean anomaly at epoch: | 202.6470° |
orbit number at epoch: | 43716 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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