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 66618U 26145.25715682 +.00000000 +00000-0 +40080-3 0 00009
2 66618 53.1604 143.9815 0000732 74.3814 285.7267 15.30203550 09
| Epoch (UTC): | 25 May 2026 06:10:18 |
| Eccentricity: | 0.0000732 |
| inclination: | 53.1604° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 143.9815° |
| argument of perigee: | 74.3814° |
| revolutions per day: | 15.30203550 |
| mean anomaly at epoch: | 285.7267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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