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 26931U 01043C 23085.93206402 .00000561 00000-0 24498-3 0 9995
2 26931 67.0518 49.2037 0006992 282.7548 77.2772 14.30866717121815
Epoch (UTC): | 26 March 2023 22:22:10 |
Eccentricity: | 0.0006992 |
inclination: | 67.0518° |
perigee height: | 784 km |
apogee height: | 794 km |
right ascension of ascending node: | 49.2037° |
argument of perigee: | 282.7548° |
revolutions per day: | 14.30866717 |
mean anomaly at epoch: | 77.2772° |
orbit number at epoch: | 12181 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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