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 47440U 21006AD 23083.10311622 .00035242 00000-0 14944-2 0 9990
2 47440 97.3986 141.9982 0009728 31.0134 329.1675 15.22992345119720
Epoch (UTC): | 24 March 2023 02:28:29 |
Eccentricity: | 0.0009728 |
inclination: | 97.3986° |
perigee height: | 490 km |
apogee height: | 503 km |
right ascension of ascending node: | 141.9982° |
argument of perigee: | 31.0134° |
revolutions per day: | 15.22992345 |
mean anomaly at epoch: | 329.1675° |
orbit number at epoch: | 11972 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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