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 41166U 26150.46935185 +.00000000 +00000-0 +47379-3 0 00009
2 41166 14.9815 221.6276 0004458 327.4656 32.5394 15.49135916 08
| Epoch (UTC): | 30 May 2026 11:15:52 |
| Eccentricity: | 0.0004458 |
| inclination: | 14.9815° |
| perigee height: | 416 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 221.6276° |
| argument of perigee: | 327.4656° |
| revolutions per day: | 15.49135916 |
| mean anomaly at epoch: | 32.5394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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