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 23150.73362500 .00014222 00000-0 25397-3 0 9997
2 25544 51.6419 55.0557 0005274 37.8489 59.0538 15.50299462399084
Epoch (UTC): | 30 May 2023 17:36:25 |
Eccentricity: | 0.0005274 |
inclination: | 51.6419° |
perigee height: | 412 km |
apogee height: | 419 km |
right ascension of ascending node: | 55.0557° |
argument of perigee: | 37.8489° |
revolutions per day: | 15.50299462 |
mean anomaly at epoch: | 59.0538° |
orbit number at epoch: | 39908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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