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 11060U 78096A 25348.93390986 .00000186 00000-0 10842-3 0 9990
2 11060 98.4706 13.1929 0011317 60.1914 300.0387 14.19292561652614
| Epoch (UTC): | 14 December 2025 22:24:49 |
| Eccentricity: | 0.0011317 |
| inclination: | 98.4706° |
| perigee height: | 819 km |
| apogee height: | 836 km |
| right ascension of ascending node: | 13.1929° |
| argument of perigee: | 60.1914° |
| revolutions per day: | 14.19292561 |
| mean anomaly at epoch: | 300.0387° |
| orbit number at epoch: | 65261 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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