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 66516U 26145.43472693 +.00000000 +00000-0 +59060-3 0 00006
2 66516 42.9983 204.2632 0001195 280.3898 79.6818 15.27592915 09
| Epoch (UTC): | 25 May 2026 10:26:00 |
| Eccentricity: | 0.0001195 |
| inclination: | 42.9983° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.2632° |
| argument of perigee: | 280.3898° |
| revolutions per day: | 15.27592915 |
| mean anomaly at epoch: | 79.6818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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