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 23038.52096184 .00002734 00000-0 35370-4 0 9995
2 48274 41.4740 226.5445 0003512 184.1310 209.5129 15.61163069101552
Epoch (UTC): | 07 February 2023 12:30:11 |
Eccentricity: | 0.0003512 |
inclination: | 41.4740° |
perigee height: | 382 km |
apogee height: | 386 km |
right ascension of ascending node: | 226.5445° |
argument of perigee: | 184.1310° |
revolutions per day: | 15.61163069 |
mean anomaly at epoch: | 209.5129° |
orbit number at epoch: | 10155 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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