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 66674U 26145.61877772 +.00000000 +00000-0 +17252-3 0 00005
2 66674 97.4174 219.1642 0008101 86.1321 274.0839 15.17993975 08
| Epoch (UTC): | 25 May 2026 14:51:02 |
| Eccentricity: | 0.0008101 |
| inclination: | 97.4174° |
| perigee height: | 506 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 219.1642° |
| argument of perigee: | 86.1321° |
| revolutions per day: | 15.17993975 |
| mean anomaly at epoch: | 274.0839° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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