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 66777U 26145.64587897 +.00000000 +00000-0 +40809-3 0 00002
2 66777 97.4262 220.2473 0000636 353.8423 6.2806 15.22266030 07
| Epoch (UTC): | 25 May 2026 15:30:03 |
| Eccentricity: | 0.0000636 |
| inclination: | 97.4262° |
| perigee height: | 499 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 220.2473° |
| argument of perigee: | 353.8423° |
| revolutions per day: | 15.22266030 |
| mean anomaly at epoch: | 6.2806° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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