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 00050U 60009B 25198.88390219 -.00000103 00000-0 -15212-3 0 9995
2 00050 47.2304 119.3823 0113043 98.2928 263.0697 12.20156916896889
| Epoch (UTC): | 17 July 2025 21:12:49 |
| Eccentricity: | 0.0113043 |
| inclination: | 47.2304° |
| perigee height: | 1502 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 119.3823° |
| argument of perigee: | 98.2928° |
| revolutions per day: | 12.20156916 |
| mean anomaly at epoch: | 263.0697° |
| orbit number at epoch: | 89688 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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