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 39440U 13066AA 23341.43310830 .00002400 00000-0 30222-3 0 9999
2 39440 97.7929 284.8698 0072613 181.8472 178.2484 14.81087013539789
| Epoch (UTC): | 07 December 2023 10:23:40 |
| Eccentricity: | 0.0072613 |
| inclination: | 97.7929° |
| perigee height: | 575 km |
| apogee height: | 677 km |
| right ascension of ascending node: | 284.8698° |
| argument of perigee: | 181.8472° |
| revolutions per day: | 14.81087013 |
| mean anomaly at epoch: | 178.2484° |
| orbit number at epoch: | 53978 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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