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 66104U 26145.58335647 +.00000000 +00000-0 -44933-3 0 00006
2 66104 53.1601 106.7062 0001080 91.3432 44.0459 15.34391233 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001080 |
| inclination: | 53.1601° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 106.7062° |
| argument of perigee: | 91.3432° |
| revolutions per day: | 15.34391233 |
| mean anomaly at epoch: | 44.0459° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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