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 28654U 05018A 22229.32655271 .00000149 00000-0 10435-3 0 9997
2 28654 98.9457 299.7054 0014834 156.0117 204.1749 14.12765125888663
Epoch (UTC): | 17 August 2022 07:50:14 |
Eccentricity: | 0.0014834 |
inclination: | 98.9457° |
perigee height: | 839 km |
apogee height: | 860 km |
right ascension of ascending node: | 299.7054° |
argument of perigee: | 156.0117° |
revolutions per day: | 14.12765125 |
mean anomaly at epoch: | 204.1749° |
orbit number at epoch: | 88866 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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