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 data is extracted from the following two-line orbital elements,
1 11166U 78121B 25188.48902296 .00000063 00000-0 25784-4 0 9997
2 11166 81.2383 178.8477 0066265 163.9064 196.4236 14.14196024399495
| Epoch (UTC): | 07 July 2025 11:44:11 |
| Eccentricity: | 0.0066265 |
| inclination: | 81.2383° |
| perigee height: | 797 km |
| apogee height: | 893 km |
| right ascension of ascending node: | 178.8477° |
| argument of perigee: | 163.9064° |
| revolutions per day: | 14.14196024 |
| mean anomaly at epoch: | 196.4236° |
| orbit number at epoch: | 39949 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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