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 32790U 08021H 22226.46824758 .00001270 00000-0 13960-3 0 9992
2 32790 97.6723 194.1778 0014637 51.7319 308.5213 14.89266788775078
Epoch (UTC): | 14 August 2022 11:14:16 |
Eccentricity: | 0.0014637 |
inclination: | 97.6723° |
perigee height: | 590 km |
apogee height: | 610 km |
right ascension of ascending node: | 194.1778° |
argument of perigee: | 51.7319° |
revolutions per day: | 14.89266788 |
mean anomaly at epoch: | 308.5213° |
orbit number at epoch: | 77507 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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