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 40071U 14037C 22178.46512144 .00000615 00000-0 85171-4 0 9992
2 40071 98.4085 47.7015 0007183 289.4644 70.5787 14.81883409430825
Epoch (UTC): | 27 June 2022 11:09:46 |
Eccentricity: | 0.0007183 |
inclination: | 98.4085° |
perigee height: | 618 km |
apogee height: | 628 km |
right ascension of ascending node: | 47.7015° |
argument of perigee: | 289.4644° |
revolutions per day: | 14.81883409 |
mean anomaly at epoch: | 70.5787° |
orbit number at epoch: | 43082 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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