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 40012U 14033C 23079.75664635 .00003193 00000-0 45733-3 0 9992
2 40012 97.6671 258.2193 0055700 344.5086 15.4417 14.76184498470726
Epoch (UTC): | 20 March 2023 18:09:34 |
Eccentricity: | 0.0055700 |
inclination: | 97.6671° |
perigee height: | 602 km |
apogee height: | 680 km |
right ascension of ascending node: | 258.2193° |
argument of perigee: | 344.5086° |
revolutions per day: | 14.76184498 |
mean anomaly at epoch: | 15.4417° |
orbit number at epoch: | 47072 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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