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 66112U 26145.61637189 +.00000000 +00000-0 +61510-3 0 00004
2 66112 53.1591 106.4632 0001361 91.5792 268.5364 15.30200087 08
| Epoch (UTC): | 25 May 2026 14:47:34 |
| Eccentricity: | 0.0001361 |
| inclination: | 53.1591° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 106.4632° |
| argument of perigee: | 91.5792° |
| revolutions per day: | 15.30200087 |
| mean anomaly at epoch: | 268.5364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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