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 66757U 26145.14774786 +.00000000 +00000-0 +25038-3 0 00007
2 66757 97.4218 219.2898 0002695 67.0406 293.1113 15.20215452 05
| Epoch (UTC): | 25 May 2026 03:32:45 |
| Eccentricity: | 0.0002695 |
| inclination: | 97.4218° |
| perigee height: | 503 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 219.2898° |
| argument of perigee: | 67.0406° |
| revolutions per day: | 15.20215452 |
| mean anomaly at epoch: | 293.1113° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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