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 12677U 81076A 23083.56230075 -.00000348 00000-0 00000-0 0 9995
2 12677 10.5037 313.6782 0006845 298.0259 272.8033 0.99556989120478
Epoch (UTC): | 24 March 2023 13:29:42 |
Eccentricity: | 0.0006845 |
inclination: | 10.5037° |
perigee height: | 35959 km |
apogee height: | 36017 km |
right ascension of ascending node: | 313.6782° |
argument of perigee: | 298.0259° |
revolutions per day: | 0.99556989 |
mean anomaly at epoch: | 272.8033° |
orbit number at epoch: | 12047 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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