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 00022U 59009A 24316.60182489 .00020347 00000-0 10294-2 0 9995
2 00022 50.2773 65.7024 0104662 324.5708 34.8324 15.12258963711670
Epoch (UTC): | 11 November 2024 14:26:37 |
Eccentricity: | 0.0104662 |
inclination: | 50.2773° |
perigee height: | 457 km |
apogee height: | 601 km |
right ascension of ascending node: | 65.7024° |
argument of perigee: | 324.5708° |
revolutions per day: | 15.12258963 |
mean anomaly at epoch: | 34.8324° |
orbit number at epoch: | 71167 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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