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 27566U 26150.53235170 +.00000000 +00000-0 +00000-0 0 00009
2 27566 10.0556 43.1844 0011661 250.4892 296.4452 0.98865138 04
| Epoch (UTC): | 30 May 2026 12:46:35 |
| Eccentricity: | 0.0011661 |
| inclination: | 10.0556° |
| perigee height: | 36136 km |
| apogee height: | 36235 km |
| right ascension of ascending node: | 43.1844° |
| argument of perigee: | 250.4892° |
| revolutions per day: | 0.98865138 |
| mean anomaly at epoch: | 296.4452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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