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 23083.51421492 .00000082 00000-0 17340-3 0 9999
2 12458 89.8734 104.5267 0013443 332.2458 182.3543 13.23096180 20650
Epoch (UTC): | 24 March 2023 12:20:28 |
Eccentricity: | 0.0013443 |
inclination: | 89.8734° |
perigee height: | 1163 km |
apogee height: | 1183 km |
right ascension of ascending node: | 104.5267° |
argument of perigee: | 332.2458° |
revolutions per day: | 13.23096180 |
mean anomaly at epoch: | 182.3543° |
orbit number at epoch: | 2065 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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