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 14059U 26065.36383800 +.00000000 +00000-0 +13695-3 0 00009
2 14059 82.9709 217.7007 0041538 322.1817 37.6425 13.79124129 01
| Epoch (UTC): | 06 March 2026 08:43:55 |
| Eccentricity: | 0.0041538 |
| inclination: | 82.9709° |
| perigee height: | 936 km |
| apogee height: | 998 km |
| right ascension of ascending node: | 217.7007° |
| argument of perigee: | 322.1817° |
| revolutions per day: | 13.79124129 |
| mean anomaly at epoch: | 37.6425° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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