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 43803U 18099AX 23335.79893709 .00012290 00000-0 90631-3 0 9999
2 43803 97.5475 34.1920 0009898 258.7659 101.2454 15.03398225272851
Epoch (UTC): | 01 December 2023 19:10:28 |
Eccentricity: | 0.0009898 |
inclination: | 97.5475° |
perigee height: | 549 km |
apogee height: | 563 km |
right ascension of ascending node: | 34.1920° |
argument of perigee: | 258.7659° |
revolutions per day: | 15.03398225 |
mean anomaly at epoch: | 101.2454° |
orbit number at epoch: | 27285 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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