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 66980U 26145.51399248 +.00000000 +00000-0 +62954-3 0 00000
2 66980 43.0004 309.8546 0001743 265.8564 94.2089 15.27591851 04
| Epoch (UTC): | 25 May 2026 12:20:08 |
| Eccentricity: | 0.0001743 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.8546° |
| argument of perigee: | 265.8564° |
| revolutions per day: | 15.27591851 |
| mean anomaly at epoch: | 94.2089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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