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 24315.76548565 .00023745 00000-0 19722-2 0 9995
2 40074 98.3502 255.2069 0002577 334.8595 25.2500 14.98748224560690
Epoch (UTC): | 10 November 2024 18:22:17 |
Eccentricity: | 0.0002577 |
inclination: | 98.3502° |
perigee height: | 569 km |
apogee height: | 572 km |
right ascension of ascending node: | 255.2069° |
argument of perigee: | 334.8595° |
revolutions per day: | 14.98748224 |
mean anomaly at epoch: | 25.2500° |
orbit number at epoch: | 56069 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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