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 00020U 59007A 23038.24657239 .00003916 00000-0 16120-2 0 9998
2 00020 33.3487 343.3601 1660120 347.0736 9.1822 11.56693152342277
Epoch (UTC): | 07 February 2023 05:55:03 |
Eccentricity: | 0.1660120 |
inclination: | 33.3487° |
perigee height: | 510 km |
apogee height: | 3252 km |
right ascension of ascending node: | 343.3601° |
argument of perigee: | 347.0736° |
revolutions per day: | 11.56693152 |
mean anomaly at epoch: | 9.1822° |
orbit number at epoch: | 34227 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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