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 40315U 14075A 23333.75959912 .00000031 00000-0 00000+0 0 9994
2 40315 63.6304 222.6509 0018373 206.1555 153.8342 2.13101272 70023
Epoch (UTC): | 29 November 2023 18:13:49 |
Eccentricity: | 0.0018373 |
inclination: | 63.6304° |
perigee height: | 19083 km |
apogee height: | 19176 km |
right ascension of ascending node: | 222.6509° |
argument of perigee: | 206.1555° |
revolutions per day: | 2.13101272 |
mean anomaly at epoch: | 153.8342° |
orbit number at epoch: | 7002 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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