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 26905U 01040A 21107.84974737 0.00000000 00000-0 00000-0 0 00
2 26905 63.4042 52.6191 0498700 1.7704 358.2296 13.40794220 01
Epoch (UTC): | 17 April 2021 20:23:38 |
Eccentricity: | 0.0498700 |
inclination: | 63.4042° |
perigee height: | 733 km |
apogee height: | 1479 km |
right ascension of ascending node: | 52.6191° |
argument of perigee: | 1.7704° |
revolutions per day: | 13.40794220 |
mean anomaly at epoch: | 358.2296° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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