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 40039U 14033AF 23336.75957169 .00003585 00000-0 38656-3 0 9995
2 40039 97.8989 258.7794 0014724 121.3673 238.8987 14.88973656512292
Epoch (UTC): | 02 December 2023 18:13:46 |
Eccentricity: | 0.0014724 |
inclination: | 97.8989° |
perigee height: | 591 km |
apogee height: | 611 km |
right ascension of ascending node: | 258.7794° |
argument of perigee: | 121.3673° |
revolutions per day: | 14.88973656 |
mean anomaly at epoch: | 238.8987° |
orbit number at epoch: | 51229 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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