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 36605U 10030A 23147.85624503 .00001212 00000-0 60915-4 0 9995
2 36605 97.4456 155.5285 0001736 91.8388 268.3046 15.19143535717160
Epoch (UTC): | 27 May 2023 20:32:59 |
Eccentricity: | 0.0001736 |
inclination: | 97.4456° |
perigee height: | 507 km |
apogee height: | 509 km |
right ascension of ascending node: | 155.5285° |
argument of perigee: | 91.8388° |
revolutions per day: | 15.19143535 |
mean anomaly at epoch: | 268.3046° |
orbit number at epoch: | 71716 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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