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 66854U 26145.35736615 +.00000000 +00000-0 +11680-2 0 00004
2 66854 42.9984 270.2574 0001057 276.5358 83.5373 15.27614181 08
| Epoch (UTC): | 25 May 2026 08:34:36 |
| Eccentricity: | 0.0001057 |
| inclination: | 42.9984° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.2574° |
| argument of perigee: | 276.5358° |
| revolutions per day: | 15.27614181 |
| mean anomaly at epoch: | 83.5373° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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