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 66787U 26145.44732596 +.00000000 +00000-0 +43038-3 0 00006
2 66787 97.5244 217.0782 0013884 217.2499 142.7763 14.99915390 02
| Epoch (UTC): | 25 May 2026 10:44:08 |
| Eccentricity: | 0.0013884 |
| inclination: | 97.5244° |
| perigee height: | 558 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 217.0782° |
| argument of perigee: | 217.2499° |
| revolutions per day: | 14.99915390 |
| mean anomaly at epoch: | 142.7763° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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