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 25344.17588976 -.00000051 00000-0 32594-3 0 9992
2 50 47.2331 28.4047 0113782 171.9527 188.3119 12.20161831914624
| Epoch (UTC): | 10 December 2025 04:13:16 |
| Eccentricity: | 0.0113782 |
| inclination: | 47.2331° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 28.4047° |
| argument of perigee: | 171.9527° |
| revolutions per day: | 12.20161831 |
| mean anomaly at epoch: | 188.3119° |
| orbit number at epoch: | 91462 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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