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 33499U 09002H 24262.50672023 .00003998 00000-0 54159-3 0 9996
2 33499 98.1278 165.1939 0008227 178.1346 181.9897 14.79506832841919
Epoch (UTC): | 18 September 2024 12:09:40 |
Eccentricity: | 0.0008227 |
inclination: | 98.1278° |
perigee height: | 625 km |
apogee height: | 636 km |
right ascension of ascending node: | 165.1939° |
argument of perigee: | 178.1346° |
revolutions per day: | 14.79506832 |
mean anomaly at epoch: | 181.9897° |
orbit number at epoch: | 84191 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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