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 23340.39367355 .00000716 00000-0 28621-3 0 9992
2 20 33.3456 343.5031 1656424 155.0247 214.0628 11.57990240377322
| Epoch (UTC): | 06 December 2023 09:26:53 |
| Eccentricity: | 0.1656424 |
| inclination: | 33.3456° |
| perigee height: | 507 km |
| apogee height: | 3241 km |
| right ascension of ascending node: | 343.5031° |
| argument of perigee: | 155.0247° |
| revolutions per day: | 11.57990240 |
| mean anomaly at epoch: | 214.0628° |
| orbit number at epoch: | 37732 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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