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 25140.56971465 -.00000015 00000-0 65896-3 0 9999
2 00050 47.2326 300.3852 0113210 284.5926 74.2332 12.20155682889767
| Epoch (UTC): | 20 May 2025 13:40:23 |
| Eccentricity: | 0.0113210 |
| inclination: | 47.2326° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 300.3852° |
| argument of perigee: | 284.5926° |
| revolutions per day: | 12.20155682 |
| mean anomaly at epoch: | 74.2332° |
| orbit number at epoch: | 88976 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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