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 66116U 26145.43972176 +.00000000 +00000-0 +39156-3 0 00007
2 66116 53.1604 42.9618 0001314 87.1376 272.9775 15.30210391 06
| Epoch (UTC): | 25 May 2026 10:33:11 |
| Eccentricity: | 0.0001314 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 42.9618° |
| argument of perigee: | 87.1376° |
| revolutions per day: | 15.30210391 |
| mean anomaly at epoch: | 272.9775° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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