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 23334.44455680 .00001215 00000-0 49437-3 0 9993
2 20 33.3453 4.7816 1656414 123.3388 253.6836 11.57979379376632
| Epoch (UTC): | 30 November 2023 10:40:09 |
| Eccentricity: | 0.1656414 |
| inclination: | 33.3453° |
| perigee height: | 507 km |
| apogee height: | 3241 km |
| right ascension of ascending node: | 4.7816° |
| argument of perigee: | 123.3388° |
| revolutions per day: | 11.57979379 |
| mean anomaly at epoch: | 253.6836° |
| orbit number at epoch: | 37663 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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