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 26100.55091963 +.00000000 +00000-0 +70138-4 0 00002
2 14059 82.9754 191.5709 0041654 220.3606 139.4460 13.79130668 08
| Epoch (UTC): | 10 April 2026 13:13:19 |
| Eccentricity: | 0.0041654 |
| inclination: | 82.9754° |
| perigee height: | 936 km |
| apogee height: | 998 km |
| right ascension of ascending node: | 191.5709° |
| argument of perigee: | 220.3606° |
| revolutions per day: | 13.79130668 |
| mean anomaly at epoch: | 139.4460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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