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 39417U 13066B 23079.53489111 .00004314 00000-0 50900-3 0 9992
2 39417 97.6754 44.4100 0054389 217.4446 142.2975 14.84165358504042
Epoch (UTC): | 20 March 2023 12:50:14 |
Eccentricity: | 0.0054389 |
inclination: | 97.6754° |
perigee height: | 578 km |
apogee height: | 654 km |
right ascension of ascending node: | 44.4100° |
argument of perigee: | 217.4446° |
revolutions per day: | 14.84165358 |
mean anomaly at epoch: | 142.2975° |
orbit number at epoch: | 50404 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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