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 18583U 87097A 23270.77215089 -.00000013 00000-0 00000-0 0 9994
2 18583 12.9731 344.2387 0024731 245.9408 112.8319 0.98385011 14948
Epoch (UTC): | 27 September 2023 18:31:53 |
Eccentricity: | 0.0024731 |
inclination: | 12.9731° |
perigee height: | 36218 km |
apogee height: | 36429 km |
right ascension of ascending node: | 344.2387° |
argument of perigee: | 245.9408° |
revolutions per day: | 0.98385011 |
mean anomaly at epoch: | 112.8319° |
orbit number at epoch: | 1494 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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