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 32953U 08025A 22229.46500017 .00000024 00000-0 10000-3 0 9997
2 32953 82.5046 146.0054 0019833 124.0256 236.2705 12.43112531645916
Epoch (UTC): | 17 August 2022 11:09:36 |
Eccentricity: | 0.0019833 |
inclination: | 82.5046° |
perigee height: | 1478 km |
apogee height: | 1509 km |
right ascension of ascending node: | 146.0054° |
argument of perigee: | 124.0256° |
revolutions per day: | 12.43112531 |
mean anomaly at epoch: | 236.2705° |
orbit number at epoch: | 64591 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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