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 07531U 74089C 22228.75617080 -.00000055 00000-0 -54232-4 0 9996
2 07531 101.9084 208.3625 0011028 298.5577 237.5728 12.53478070184804
Epoch (UTC): | 16 August 2022 18:08:53 |
Eccentricity: | 0.0011028 |
inclination: | 101.9084° |
perigee height: | 1441 km |
apogee height: | 1458 km |
right ascension of ascending node: | 208.3625° |
argument of perigee: | 298.5577° |
revolutions per day: | 12.53478070 |
mean anomaly at epoch: | 237.5728° |
orbit number at epoch: | 18480 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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