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 35221U 99025DQD 22222.38865215 .00003258 00000-0 12277-2 0 9995
2 35221 98.4196 20.0326 0072609 272.5572 86.7301 14.30622508473515
Epoch (UTC): | 10 August 2022 09:19:39 |
Eccentricity: | 0.0072609 |
inclination: | 98.4196° |
perigee height: | 737 km |
apogee height: | 841 km |
right ascension of ascending node: | 20.0326° |
argument of perigee: | 272.5572° |
revolutions per day: | 14.30622508 |
mean anomaly at epoch: | 86.7301° |
orbit number at epoch: | 47351 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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