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 14781U 84021B 23338.70528850 .00002217 00000-0 26138-3 0 9995
2 14781 97.6808 309.3171 0008462 12.8099 347.3331 14.85709279119450
Epoch (UTC): | 04 December 2023 16:55:36 |
Eccentricity: | 0.0008462 |
inclination: | 97.6808° |
perigee height: | 605 km |
apogee height: | 617 km |
right ascension of ascending node: | 309.3171° |
argument of perigee: | 12.8099° |
revolutions per day: | 14.85709279 |
mean anomaly at epoch: | 347.3331° |
orbit number at epoch: | 11945 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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