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 66113U 26145.32567507 +.00000000 +00000-0 +61354-3 0 00005
2 66113 53.1575 108.2071 0001253 102.4864 257.6277 15.30213842 05
| Epoch (UTC): | 25 May 2026 07:48:58 |
| Eccentricity: | 0.0001253 |
| inclination: | 53.1575° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.2071° |
| argument of perigee: | 102.4864° |
| revolutions per day: | 15.30213842 |
| mean anomaly at epoch: | 257.6277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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