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 47311U 21002C 24112.58294100 .09167436 99880-5 88771-3 0 9999
2 47311 60.6450 276.5573 0006279 285.8230 74.2218 16.37785734182462
| Epoch (UTC): | 21 April 2024 13:59:26 |
| Eccentricity: | 0.0006279 |
| inclination: | 60.6450° |
| perigee height: | 167 km |
| apogee height: | 176 km |
| right ascension of ascending node: | 276.5573° |
| argument of perigee: | 285.8230° |
| revolutions per day: | 16.37785734 |
| mean anomaly at epoch: | 74.2218° |
| orbit number at epoch: | 18246 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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