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 66109U 26145.62164875 +.00000000 +00000-0 +44190-3 0 00003
2 66109 53.1581 106.4950 0001652 95.4399 264.6790 15.30200105 06
| Epoch (UTC): | 25 May 2026 14:55:10 |
| Eccentricity: | 0.0001652 |
| inclination: | 53.1581° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 106.4950° |
| argument of perigee: | 95.4399° |
| revolutions per day: | 15.30200105 |
| mean anomaly at epoch: | 264.6790° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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