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 40910U 15049M 22176.48958691 .00008785 00000-0 37417-3 0 9994
2 40910 97.4722 183.5040 0011400 315.0263 197.5171 15.23152285374407
Epoch (UTC): | 25 June 2022 11:45:00 |
Eccentricity: | 0.0011400 |
inclination: | 97.4722° |
perigee height: | 488 km |
apogee height: | 504 km |
right ascension of ascending node: | 183.5040° |
argument of perigee: | 315.0263° |
revolutions per day: | 15.23152285 |
mean anomaly at epoch: | 197.5171° |
orbit number at epoch: | 37440 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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