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 23268.18168943 .00033862 00000-0 36607-3 0 9994
2 48274 41.4729 267.4724 0008055 106.0453 254.1274 15.62861577137467
Epoch (UTC): | 25 September 2023 04:21:37 |
Eccentricity: | 0.0008055 |
inclination: | 41.4729° |
perigee height: | 374 km |
apogee height: | 385 km |
right ascension of ascending node: | 267.4724° |
argument of perigee: | 106.0453° |
revolutions per day: | 15.62861577 |
mean anomaly at epoch: | 254.1274° |
orbit number at epoch: | 13746 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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