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 31420U 99025BTG 23027.52643566 .00002301 00000-0 74426-3 0 9998
2 31420 97.5006 43.8251 0149618 300.2235 215.4618 14.33681098825180
Epoch (UTC): | 27 January 2023 12:38:04 |
Eccentricity: | 0.0149618 |
inclination: | 97.5006° |
perigee height: | 672 km |
apogee height: | 886 km |
right ascension of ascending node: | 43.8251° |
argument of perigee: | 300.2235° |
revolutions per day: | 14.33681098 |
mean anomaly at epoch: | 215.4618° |
orbit number at epoch: | 82518 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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