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 01002U 65008C 24308.44949754 .00000012 00000-0 41318-3 0 9998
2 01002 32.1489 4.1359 0014863 300.5716 59.3314 9.88354178157740
Epoch (UTC): | 03 November 2024 10:47:16 |
Eccentricity: | 0.0014863 |
inclination: | 32.1489° |
perigee height: | 2780 km |
apogee height: | 2807 km |
right ascension of ascending node: | 4.1359° |
argument of perigee: | 300.5716° |
revolutions per day: | 9.88354178 |
mean anomaly at epoch: | 59.3314° |
orbit number at epoch: | 15774 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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