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 23150.91291839 -.00000082 00000-0 28126-4 0 9997
2 00050 47.2340 17.1700 0113553 297.1026 61.8218 12.20129348801779
| Epoch (UTC): | 30 May 2023 21:54:36 |
| Eccentricity: | 0.0113553 |
| inclination: | 47.2340° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 17.1700° |
| argument of perigee: | 297.1026° |
| revolutions per day: | 12.20129348 |
| mean anomaly at epoch: | 61.8218° |
| orbit number at epoch: | 80177 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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