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 22009U 92037A 23273.82243862 -.00000229 00000-0 00000+0 0 9999
2 22009 13.5688 16.5185 0006617 41.8154 12.6452 0.98812222 15342
Epoch (UTC): | 30 September 2023 19:44:18 |
Eccentricity: | 0.0006617 |
inclination: | 13.5688° |
perigee height: | 36172 km |
apogee height: | 36228 km |
right ascension of ascending node: | 16.5185° |
argument of perigee: | 41.8154° |
revolutions per day: | 0.98812222 |
mean anomaly at epoch: | 12.6452° |
orbit number at epoch: | 1534 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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