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 23037.88681283 -.00000045 00000-0 38006-3 0 9999
2 00050 47.2341 7.9743 0114273 319.8989 39.3409 12.20126010787974
| Epoch (UTC): | 06 February 2023 21:17:00 |
| Eccentricity: | 0.0114273 |
| inclination: | 47.2341° |
| perigee height: | 1501 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 7.9743° |
| argument of perigee: | 319.8989° |
| revolutions per day: | 12.20126010 |
| mean anomaly at epoch: | 39.3409° |
| orbit number at epoch: | 78797 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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