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 24315.42384232 .00014382 00000-0 17617-2 0 9993
2 40012 97.7178 112.2536 0050237 186.5954 173.4605 14.82360001559485
Epoch (UTC): | 10 November 2024 10:10:19 |
Eccentricity: | 0.0050237 |
inclination: | 97.7178° |
perigee height: | 587 km |
apogee height: | 657 km |
right ascension of ascending node: | 112.2536° |
argument of perigee: | 186.5954° |
revolutions per day: | 14.82360001 |
mean anomaly at epoch: | 173.4605° |
orbit number at epoch: | 55948 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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