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 20U 59007A 23333.15107731 .00001019 00000-0 41621-3 0 9990
2 20 33.3454 9.4075 1656422 116.4516 261.5297 11.57975414376485
| Epoch (UTC): | 29 November 2023 03:37:33 |
| Eccentricity: | 0.1656422 |
| inclination: | 33.3454° |
| perigee height: | 507 km |
| apogee height: | 3241 km |
| right ascension of ascending node: | 9.4075° |
| argument of perigee: | 116.4516° |
| revolutions per day: | 11.57975414 |
| mean anomaly at epoch: | 261.5297° |
| orbit number at epoch: | 37648 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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