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 23150.52764597 .00001461 00000-0 57475-3 0 9992
2 20 33.3529 302.3313 1658932 224.2557 121.2964 11.57578110355313
| Epoch (UTC): | 30 May 2023 12:39:48 |
| Eccentricity: | 0.1658932 |
| inclination: | 33.3529° |
| perigee height: | 507 km |
| apogee height: | 3246 km |
| right ascension of ascending node: | 302.3313° |
| argument of perigee: | 224.2557° |
| revolutions per day: | 11.57578110 |
| mean anomaly at epoch: | 121.2964° |
| orbit number at epoch: | 35531 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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