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 14780U 84021A 25342.74414563 .00005584 00000-0 39432-3 0 9991
2 14780 98.0740 248.6955 0071519 36.4544 324.1519 15.03289544762762
| Epoch (UTC): | 08 December 2025 17:51:34 |
| Eccentricity: | 0.0071519 |
| inclination: | 98.0740° |
| perigee height: | 507 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 248.6955° |
| argument of perigee: | 36.4544° |
| revolutions per day: | 15.03289544 |
| mean anomaly at epoch: | 324.1519° |
| orbit number at epoch: | 76276 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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