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 23038.86966288 -.00000038 00000-0 44753-3 0 9997
2 00050 47.2342 4.9240 0114261 322.8288 36.4632 12.20126105788092
| Epoch (UTC): | 07 February 2023 20:52:18 |
| Eccentricity: | 0.0114261 |
| inclination: | 47.2342° |
| perigee height: | 1501 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 4.9240° |
| argument of perigee: | 322.8288° |
| revolutions per day: | 12.20126105 |
| mean anomaly at epoch: | 36.4632° |
| orbit number at epoch: | 78809 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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