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 48274U 21035A 24286.46516466 .00040465 00000-0 40807-3 0 9997
2 48274 41.4661 87.7595 0003814 189.2439 170.8332 15.64592714197445
Epoch (UTC): | 12 October 2024 11:09:50 |
Eccentricity: | 0.0003814 |
inclination: | 41.4661° |
perigee height: | 372 km |
apogee height: | 377 km |
right ascension of ascending node: | 87.7595° |
argument of perigee: | 189.2439° |
revolutions per day: | 15.64592714 |
mean anomaly at epoch: | 170.8332° |
orbit number at epoch: | 19744 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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