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 23030.26974266 -.00000120 00000-0 -33563-3 0 9998
2 00050 47.2334 31.6145 0114320 297.1919 61.7257 12.20126122787042
| Epoch (UTC): | 30 January 2023 06:28:25 |
| Eccentricity: | 0.0114320 |
| inclination: | 47.2334° |
| perigee height: | 1501 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 31.6145° |
| argument of perigee: | 297.1919° |
| revolutions per day: | 12.20126122 |
| mean anomaly at epoch: | 61.7257° |
| orbit number at epoch: | 78704 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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