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 31863U 07032B 23150.40367727 .00000542 00000-0 50983-3 0 9999
2 31863 45.9105 214.7721 4957435 167.9400 210.7357 5.53015976319565
Epoch (UTC): | 30 May 2023 09:41:17 |
Eccentricity: | 0.4957435 |
inclination: | 45.9105° |
perigee height: | 433 km |
apogee height: | 13825 km |
right ascension of ascending node: | 214.7721° |
argument of perigee: | 167.9400° |
revolutions per day: | 5.53015976 |
mean anomaly at epoch: | 210.7357° |
orbit number at epoch: | 31956 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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