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 29093U 06015B 22143.84468016 .00029966 00000-0 38889-3 0 9995
2 29093 97.6050 1.7446 0038719 274.0021 85.6809 15.57871597895821
| Epoch (UTC): | 23 May 2022 20:16:20 |
| Eccentricity: | 0.0038719 |
| inclination: | 97.6050° |
| perigee height: | 367 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 1.7446° |
| argument of perigee: | 274.0021° |
| revolutions per day: | 15.57871597 |
| mean anomaly at epoch: | 85.6809° |
| orbit number at epoch: | 89582 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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