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 20303U 89085B 22227.84858420 .00013194 00000-0 32628-3 0 9994
2 20303 35.6384 69.9466 0077700 25.9132 334.5460 15.36545454789597
| Epoch (UTC): | 15 August 2022 20:21:57 |
| Eccentricity: | 0.0077700 |
| inclination: | 35.6384° |
| perigee height: | 403 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 69.9466° |
| argument of perigee: | 25.9132° |
| revolutions per day: | 15.36545454 |
| mean anomaly at epoch: | 334.5460° |
| orbit number at epoch: | 78959 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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