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 12586U 81065B 22229.20030581 .00001939 00000-0 11527-3 0 9999
2 12586 97.6871 223.9705 0017428 202.2457 157.8019 15.12389355241408
Epoch (UTC): | 17 August 2022 04:48:26 |
Eccentricity: | 0.0017428 |
inclination: | 97.6871° |
perigee height: | 517 km |
apogee height: | 541 km |
right ascension of ascending node: | 223.9705° |
argument of perigee: | 202.2457° |
revolutions per day: | 15.12389355 |
mean anomaly at epoch: | 157.8019° |
orbit number at epoch: | 24140 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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