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 25343.19309561 -.00000035 00000-0 47646-3 0 9990
2 50 47.2331 31.4552 0113783 169.0165 191.3144 12.20161816914508
| Epoch (UTC): | 09 December 2025 04:38:03 |
| Eccentricity: | 0.0113783 |
| inclination: | 47.2331° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 31.4552° |
| argument of perigee: | 169.0165° |
| revolutions per day: | 12.20161816 |
| mean anomaly at epoch: | 191.3144° |
| orbit number at epoch: | 91450 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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