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 24282.20332642 .00043740 00000-0 54209-2 0 9998
2 40012 97.7165 80.2230 0050217 296.6824 62.9253 14.81606213554565
Epoch (UTC): | 08 October 2024 04:52:47 |
Eccentricity: | 0.0050217 |
inclination: | 97.7165° |
perigee height: | 589 km |
apogee height: | 659 km |
right ascension of ascending node: | 80.2230° |
argument of perigee: | 296.6824° |
revolutions per day: | 14.81606213 |
mean anomaly at epoch: | 62.9253° |
orbit number at epoch: | 55456 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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