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 24308.80219352 .00040806 00000-0 69068-3 0 9997
2 25544 51.6388 343.7865 0008969 132.8605 227.3139 15.51108030480201
Epoch (UTC): | 03 November 2024 19:15:09 |
Eccentricity: | 0.0008969 |
inclination: | 51.6388° |
perigee height: | 407 km |
apogee height: | 419 km |
right ascension of ascending node: | 343.7865° |
argument of perigee: | 132.8605° |
revolutions per day: | 15.51108030 |
mean anomaly at epoch: | 227.3139° |
orbit number at epoch: | 48020 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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