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 21660U 26159.56863705 +.00000000 +00000-0 -50583+0 0 00002
2 21660 86.7087 262.2380 1398753 18.6071 1.4357 8.77380436 01
| Epoch (UTC): | 08 June 2026 13:38:50 |
| Eccentricity: | 0.1398753 |
| inclination: | 86.7087° |
| perigee height: | 2163 km |
| apogee height: | 4941 km |
| right ascension of ascending node: | 262.2380° |
| argument of perigee: | 18.6071° |
| revolutions per day: | 8.77380436 |
| mean anomaly at epoch: | 1.4357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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