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 23034.62170047 .00012966 00000-0 15341-3 0 9996
2 48274 41.4748 250.2796 0002341 138.2092 273.0189 15.61049212100946
Epoch (UTC): | 03 February 2023 14:55:14 |
Eccentricity: | 0.0002341 |
inclination: | 41.4748° |
perigee height: | 383 km |
apogee height: | 386 km |
right ascension of ascending node: | 250.2796° |
argument of perigee: | 138.2092° |
revolutions per day: | 15.61049212 |
mean anomaly at epoch: | 273.0189° |
orbit number at epoch: | 10094 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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