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 24316.57366550 .00050476 00000-0 61819-3 0 9999
2 48274 41.4621 264.1120 0008528 318.0667 41.9518 15.59483539202155
Epoch (UTC): | 11 November 2024 13:46:04 |
Eccentricity: | 0.0008528 |
inclination: | 41.4621° |
perigee height: | 383 km |
apogee height: | 395 km |
right ascension of ascending node: | 264.1120° |
argument of perigee: | 318.0667° |
revolutions per day: | 15.59483539 |
mean anomaly at epoch: | 41.9518° |
orbit number at epoch: | 20215 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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