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 23266.65029092 .00001048 00000-0 42893-3 0 9997
2 20 33.3406 247.2193 1656393 122.3465 254.8320 11.57829584368772
| Epoch (UTC): | 23 September 2023 15:36:25 |
| Eccentricity: | 0.1656393 |
| inclination: | 33.3406° |
| perigee height: | 508 km |
| apogee height: | 3242 km |
| right ascension of ascending node: | 247.2193° |
| argument of perigee: | 122.3465° |
| revolutions per day: | 11.57829584 |
| mean anomaly at epoch: | 254.8320° |
| orbit number at epoch: | 36877 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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