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 23152.86905862 .00000139 00000-0 45722-4 0 9993
2 00876 65.0612 5.8538 0145295 332.0283 27.3061 14.64216125125873
Epoch (UTC): | 01 June 2023 20:51:26 |
Eccentricity: | 0.0145295 |
inclination: | 65.0612° |
perigee height: | 577 km |
apogee height: | 782 km |
right ascension of ascending node: | 5.8538° |
argument of perigee: | 332.0283° |
revolutions per day: | 14.64216125 |
mean anomaly at epoch: | 27.3061° |
orbit number at epoch: | 12587 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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