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 23036.04387058 .00013488 00000-0 15917-3 0 9995
2 48274 41.4747 241.6216 0002550 152.9447 341.1069 15.61090001101166
Epoch (UTC): | 05 February 2023 01:03:10 |
Eccentricity: | 0.0002550 |
inclination: | 41.4747° |
perigee height: | 383 km |
apogee height: | 386 km |
right ascension of ascending node: | 241.6216° |
argument of perigee: | 152.9447° |
revolutions per day: | 15.61090001 |
mean anomaly at epoch: | 341.1069° |
orbit number at epoch: | 10116 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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