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 16382U 82055W 23333.45308581 .00008637 00000-0 32972-2 0 9997
2 16382 65.7444 343.1848 0026676 349.9622 179.8077 14.30970369956398
| Epoch (UTC): | 29 November 2023 10:52:26 |
| Eccentricity: | 0.0026676 |
| inclination: | 65.7444° |
| perigee height: | 769 km |
| apogee height: | 807 km |
| right ascension of ascending node: | 343.1848° |
| argument of perigee: | 349.9622° |
| revolutions per day: | 14.30970369 |
| mean anomaly at epoch: | 179.8077° |
| orbit number at epoch: | 95639 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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