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 12458U 81044A 19054.79656697 .00000014 00000-0 13036-4 0 9993
2 12458 89.9328 118.1674 0016466 110.4338 18.2461 13.22994713823671
Epoch (UTC): | 23 February 2019 19:07:03 |
Eccentricity: | 0.0016466 |
inclination: | 89.9328° |
perigee height: | 1161 km |
apogee height: | 1186 km |
right ascension of ascending node: | 118.1674° |
argument of perigee: | 110.4338° |
revolutions per day: | 13.22994713 |
mean anomaly at epoch: | 18.2461° |
orbit number at epoch: | 82367 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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