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 66227U 26145.52029022 +.00000000 +00000-0 +77151-3 0 00000
2 66227 53.1586 232.9643 0001029 81.7580 278.3537 15.30196069 08
| Epoch (UTC): | 25 May 2026 12:29:13 |
| Eccentricity: | 0.0001029 |
| inclination: | 53.1586° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 232.9643° |
| argument of perigee: | 81.7580° |
| revolutions per day: | 15.30196069 |
| mean anomaly at epoch: | 278.3537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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