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 22009U 92037A 23079.91087219 .00000028 00000-0 00000-0 0 9992
2 22009 13.4441 17.8356 0010447 22.3454 171.1334 0.98808749 13443
| Epoch (UTC): | 20 March 2023 21:51:39 |
| Eccentricity: | 0.0010447 |
| inclination: | 13.4441° |
| perigee height: | 36157 km |
| apogee height: | 36246 km |
| right ascension of ascending node: | 17.8356° |
| argument of perigee: | 22.3454° |
| revolutions per day: | 0.98808749 |
| mean anomaly at epoch: | 171.1334° |
| orbit number at epoch: | 1344 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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