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 21873U 92006A 23080.38313303 .00000003 00000-0 00000-0 0 9998
2 21873 14.4438 11.3784 0004833 356.8516 201.9125 0.99037306 13464
Epoch (UTC): | 21 March 2023 09:11:42 |
Eccentricity: | 0.0004833 |
inclination: | 14.4438° |
perigee height: | 36115 km |
apogee height: | 36156 km |
right ascension of ascending node: | 11.3784° |
argument of perigee: | 356.8516° |
revolutions per day: | 0.99037306 |
mean anomaly at epoch: | 201.9125° |
orbit number at epoch: | 1346 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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