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 66851U 26145.04199155 +.00000000 +00000-0 +52480-3 0 00003
2 66851 43.0030 272.1868 0001724 50.6094 309.4910 15.27587104 06
| Epoch (UTC): | 25 May 2026 01:00:28 |
| Eccentricity: | 0.0001724 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 272.1868° |
| argument of perigee: | 50.6094° |
| revolutions per day: | 15.27587104 |
| mean anomaly at epoch: | 309.4910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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