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 23334.11776230 .00023658 00000-0 42181-3 0 9995
2 25544 51.6413 226.6872 0000944 358.5140 150.7066 15.49963452427521
Epoch (UTC): | 30 November 2023 02:49:34 |
Eccentricity: | 0.0000944 |
inclination: | 51.6413° |
perigee height: | 416 km |
apogee height: | 417 km |
right ascension of ascending node: | 226.6872° |
argument of perigee: | 358.5140° |
revolutions per day: | 15.49963452 |
mean anomaly at epoch: | 150.7066° |
orbit number at epoch: | 42752 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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