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 00016U 58002A 24315.00810551 .00000645 00000-0 87845-3 0 9997
2 00016 34.2607 194.4870 2023336 173.6019 189.5128 10.49481018627533
Epoch (UTC): | 10 November 2024 00:11:40 |
Eccentricity: | 0.2023336 |
inclination: | 34.2607° |
perigee height: | 651 km |
apogee height: | 4217 km |
right ascension of ascending node: | 194.4870° |
argument of perigee: | 173.6019° |
revolutions per day: | 10.49481018 |
mean anomaly at epoch: | 189.5128° |
orbit number at epoch: | 62753 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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