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 40025U 14033R 23332.86653120 .00009624 00000-0 85945-3 0 9991
2 40025 98.0171 282.9517 0012440 105.0323 255.2275 14.96091613512745
| Epoch (UTC): | 28 November 2023 20:47:48 |
| Eccentricity: | 0.0012440 |
| inclination: | 98.0171° |
| perigee height: | 570 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 282.9517° |
| argument of perigee: | 105.0323° |
| revolutions per day: | 14.96091613 |
| mean anomaly at epoch: | 255.2275° |
| orbit number at epoch: | 51274 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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