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 40074U 14037F 24260.77141647 .00017806 00000-0 15759-2 0 9992
2 40074 98.3438 196.4716 0006721 115.0335 245.1583 14.96331793552466
Epoch (UTC): | 16 September 2024 18:30:50 |
Eccentricity: | 0.0006721 |
inclination: | 98.3438° |
perigee height: | 573 km |
apogee height: | 583 km |
right ascension of ascending node: | 196.4716° |
argument of perigee: | 115.0335° |
revolutions per day: | 14.96331793 |
mean anomaly at epoch: | 245.1583° |
orbit number at epoch: | 55246 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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