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 40912U 15049P 22136.19425141 .00011953 00000-0 47556-3 0 9995
2 40912 97.4386 147.7644 0014867 60.5752 357.9586 15.25319446368830
Epoch (UTC): | 16 May 2022 04:39:43 |
Eccentricity: | 0.0014867 |
inclination: | 97.4386° |
perigee height: | 479 km |
apogee height: | 500 km |
right ascension of ascending node: | 147.7644° |
argument of perigee: | 60.5752° |
revolutions per day: | 15.25319446 |
mean anomaly at epoch: | 357.9586° |
orbit number at epoch: | 36883 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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