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 23336.59146610 .00021304 00000-0 22902-3 0 9993
2 48274 41.4691 210.3820 0007926 261.8811 98.1129 15.63201345148169
Epoch (UTC): | 02 December 2023 14:11:42 |
Eccentricity: | 0.0007926 |
inclination: | 41.4691° |
perigee height: | 373 km |
apogee height: | 384 km |
right ascension of ascending node: | 210.3820° |
argument of perigee: | 261.8811° |
revolutions per day: | 15.63201345 |
mean anomaly at epoch: | 98.1129° |
orbit number at epoch: | 14816 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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