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 14680U 84010B 25348.91131243 .00000080 00000-0 65397-4 0 9990
2 14680 82.9569 261.2039 0038352 16.4497 54.5825 13.76708287102679
| Epoch (UTC): | 14 December 2025 21:52:17 |
| Eccentricity: | 0.0038352 |
| inclination: | 82.9569° |
| perigee height: | 947 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 261.2039° |
| argument of perigee: | 16.4497° |
| revolutions per day: | 13.76708287 |
| mean anomaly at epoch: | 54.5825° |
| orbit number at epoch: | 10267 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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