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 23151.83264809 .00015643 00000-0 27811-3 0 9993
2 25544 51.6408 49.6121 0005631 38.6332 76.1391 15.50338694399258
Epoch (UTC): | 31 May 2023 19:59:00 |
Eccentricity: | 0.0005631 |
inclination: | 51.6408° |
perigee height: | 412 km |
apogee height: | 419 km |
right ascension of ascending node: | 49.6121° |
argument of perigee: | 38.6332° |
revolutions per day: | 15.50338694 |
mean anomaly at epoch: | 76.1391° |
orbit number at epoch: | 39925 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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