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 39484U 13076B 23084.16003623 .00000009 00000-0 -93927-5 0 9998
2 39484 82.4927 185.0921 0022580 146.4712 213.7802 12.42881015419560
Epoch (UTC): | 25 March 2023 03:50:27 |
Eccentricity: | 0.0022580 |
inclination: | 82.4927° |
perigee height: | 1476 km |
apogee height: | 1512 km |
right ascension of ascending node: | 185.0921° |
argument of perigee: | 146.4712° |
revolutions per day: | 12.42881015 |
mean anomaly at epoch: | 213.7802° |
orbit number at epoch: | 41956 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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