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 2142U 66031A 23273.52374533 .00000252 00000-0 95688-4 0 9993
2 2142 35.0469 343.7337 0006468 86.8680 273.2747 14.34105737 9183
Epoch (UTC): | 30 September 2023 12:34:11 |
Eccentricity: | 0.0006468 |
inclination: | 35.0469° |
perigee height: | 773 km |
apogee height: | 782 km |
right ascension of ascending node: | 343.7337° |
argument of perigee: | 86.8680° |
revolutions per day: | 14.34105737 |
mean anomaly at epoch: | 273.2747° |
orbit number at epoch: | 918 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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