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 is defined by the following mean orbital elements,
1 14051U 26075.63624258 +.00000000 +00000-0 +36961-3 0 00008
2 14051 25.3343 56.6423 0984765 239.2457 110.7434 13.34419688 07
| Epoch (UTC): | 16 March 2026 15:16:11 |
| Eccentricity: | 0.0984765 |
| inclination: | 25.3343° |
| perigee height: | 391 km |
| apogee height: | 1870 km |
| right ascension of ascending node: | 56.6423° |
| argument of perigee: | 239.2457° |
| revolutions per day: | 13.34419688 |
| mean anomaly at epoch: | 110.7434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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