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 25138.19457287 -.00000014 00000-0 66842-3 0 9997
2 50 47.2328 307.7574 0113221 277.5234 81.2706 12.20155354889924
| Epoch (UTC): | 18 May 2025 04:40:11 |
| Eccentricity: | 0.0113221 |
| inclination: | 47.2328° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 307.7574° |
| argument of perigee: | 277.5234° |
| revolutions per day: | 12.20155354 |
| mean anomaly at epoch: | 81.2706° |
| orbit number at epoch: | 88992 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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