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 00020U 59007A 23338.41078063 .00000977 00000-0 39383-3 0 9993
2 00020 33.3453 350.5959 1656435 144.4630 227.8508 11.57987415377066
| Epoch (UTC): | 04 December 2023 09:51:31 |
| Eccentricity: | 0.1656435 |
| inclination: | 33.3453° |
| perigee height: | 507 km |
| apogee height: | 3241 km |
| right ascension of ascending node: | 350.5959° |
| argument of perigee: | 144.4630° |
| revolutions per day: | 11.57987415 |
| mean anomaly at epoch: | 227.8508° |
| orbit number at epoch: | 37706 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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