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 23332.77390321 .00003218 00000-0 45583-3 0 9996
2 33499 98.1543 227.0702 0010039 62.6407 297.5823 14.77737525798365
Epoch (UTC): | 28 November 2023 18:34:25 |
Eccentricity: | 0.0010039 |
inclination: | 98.1543° |
perigee height: | 629 km |
apogee height: | 643 km |
right ascension of ascending node: | 227.0702° |
argument of perigee: | 62.6407° |
revolutions per day: | 14.77737525 |
mean anomaly at epoch: | 297.5823° |
orbit number at epoch: | 79836 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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