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 50U 60009B 24255.54171533 -.00000061 00000-0 21718-3 0 9997
2 50 47.2349 359.5451 0113705 256.3215 102.4892 12.20144722859563
| Epoch (UTC): | 11 September 2024 13:00:04 |
| Eccentricity: | 0.0113705 |
| inclination: | 47.2349° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 359.5451° |
| argument of perigee: | 256.3215° |
| revolutions per day: | 12.20144722 |
| mean anomaly at epoch: | 102.4892° |
| orbit number at epoch: | 85956 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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