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 44909U 19096E 23332.79508716 .00000039 00000-0 10819-3 0 9991
2 44909 82.5227 238.5554 0217671 161.8394 199.0640 12.79724077183212
Epoch (UTC): | 28 November 2023 19:04:55 |
Eccentricity: | 0.0217671 |
inclination: | 82.5227° |
perigee height: | 1174 km |
apogee height: | 1510 km |
right ascension of ascending node: | 238.5554° |
argument of perigee: | 161.8394° |
revolutions per day: | 12.79724077 |
mean anomaly at epoch: | 199.0640° |
orbit number at epoch: | 18321 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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