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 12091U 80099A 24280.78712656 .00000182 00000-0 17564-3 0 9994
2 12091 82.9367 101.8944 0033292 348.8473 22.1675 13.74638586197790
| Epoch (UTC): | 06 October 2024 18:53:27 |
| Eccentricity: | 0.0033292 |
| inclination: | 82.9367° |
| perigee height: | 958 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 101.8944° |
| argument of perigee: | 348.8473° |
| revolutions per day: | 13.74638586 |
| mean anomaly at epoch: | 22.1675° |
| orbit number at epoch: | 19779 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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