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 51215U 82092BAR 23150.79397329 .00172428 00000-0 10966-2 0 9993
2 51215 82.5617 272.7068 0008418 234.0946 125.9538 15.75907217 78918
Epoch (UTC): | 30 May 2023 19:03:19 |
Eccentricity: | 0.0008418 |
inclination: | 82.5617° |
perigee height: | 336 km |
apogee height: | 348 km |
right ascension of ascending node: | 272.7068° |
argument of perigee: | 234.0946° |
revolutions per day: | 15.75907217 |
mean anomaly at epoch: | 125.9538° |
orbit number at epoch: | 7891 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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