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 25191.46059132 .00000019 00000-0 30908-5 0 9997
2 11166 81.2385 175.9340 0066389 155.5300 204.9050 14.14196177399916
| Epoch (UTC): | 10 July 2025 11:03:15 |
| Eccentricity: | 0.0066389 |
| inclination: | 81.2385° |
| perigee height: | 797 km |
| apogee height: | 893 km |
| right ascension of ascending node: | 175.9340° |
| argument of perigee: | 155.5300° |
| revolutions per day: | 14.14196177 |
| mean anomaly at epoch: | 204.9050° |
| orbit number at epoch: | 39991 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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