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 00876U 64053A 22142.91450242 .00000287 00000-0 72249-4 0 9992
2 00876 65.0627 30.6664 0124715 129.9341 231.2799 14.63898987 70983
Epoch (UTC): | 22 May 2022 21:56:53 |
Eccentricity: | 0.0124715 |
inclination: | 65.0627° |
perigee height: | 592 km |
apogee height: | 768 km |
right ascension of ascending node: | 30.6664° |
argument of perigee: | 129.9341° |
revolutions per day: | 14.63898987 |
mean anomaly at epoch: | 231.2799° |
orbit number at epoch: | 7098 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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