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 25544U 98067A 23152.28957880 .00028823 00000-0 50433-3 0 9991
2 25544 51.6411 47.3482 0005092 38.3010 108.4298 15.50372472399323
Epoch (UTC): | 01 June 2023 06:56:59 |
Eccentricity: | 0.0005092 |
inclination: | 51.6411° |
perigee height: | 412 km |
apogee height: | 419 km |
right ascension of ascending node: | 47.3482° |
argument of perigee: | 38.3010° |
revolutions per day: | 15.50372472 |
mean anomaly at epoch: | 108.4298° |
orbit number at epoch: | 39932 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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