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 20U 59007A 24257.52124848 .00006385 00000-0 25469-2 0 9997
2 20 33.3514 53.4558 1648740 219.0694 127.8669 11.59714287410058
| Epoch (UTC): | 13 September 2024 12:30:35 |
| Eccentricity: | 0.1648740 |
| inclination: | 33.3514° |
| perigee height: | 507 km |
| apogee height: | 3226 km |
| right ascension of ascending node: | 53.4558° |
| argument of perigee: | 219.0694° |
| revolutions per day: | 11.59714287 |
| mean anomaly at epoch: | 127.8669° |
| orbit number at epoch: | 41005 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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