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 30822U 99025AVG 23091.87013773 .00000963 00000-0 56234-3 0 9992
2 30822 98.8428 131.0318 0076104 193.2737 340.5346 14.09344012828059
Epoch (UTC): | 01 April 2023 20:52:59 |
Eccentricity: | 0.0076104 |
inclination: | 98.8428° |
perigee height: | 806 km |
apogee height: | 917 km |
right ascension of ascending node: | 131.0318° |
argument of perigee: | 193.2737° |
revolutions per day: | 14.09344012 |
mean anomaly at epoch: | 340.5346° |
orbit number at epoch: | 82805 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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