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 25200.11241545 -.00000117 00000-0 -28428-3 0 9990
2 50 47.2306 115.5692 0113066 101.9607 259.3883 12.20156893897491
| Epoch (UTC): | 19 July 2025 02:41:52 |
| Eccentricity: | 0.0113066 |
| inclination: | 47.2306° |
| perigee height: | 1502 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 115.5692° |
| argument of perigee: | 101.9607° |
| revolutions per day: | 12.20156893 |
| mean anomaly at epoch: | 259.3883° |
| orbit number at epoch: | 89749 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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