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 11963U 80073B 22147.54291684 .00000281 00000-0 14914-3 0 9996
2 11963 81.2748 174.4202 0074365 8.9407 351.3068 14.09757705144623
| Epoch (UTC): | 27 May 2022 13:01:48 |
| Eccentricity: | 0.0074365 |
| inclination: | 81.2748° |
| perigee height: | 806 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 174.4202° |
| argument of perigee: | 8.9407° |
| revolutions per day: | 14.09757705 |
| mean anomaly at epoch: | 351.3068° |
| orbit number at epoch: | 14462 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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