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 66708U 26145.46887366 +.00000000 +00000-0 +27432-3 0 00007
2 66708 97.4183 219.5357 0002143 84.2597 275.8883 15.20310835 07
| Epoch (UTC): | 25 May 2026 11:15:10 |
| Eccentricity: | 0.0002143 |
| inclination: | 97.4183° |
| perigee height: | 503 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 219.5357° |
| argument of perigee: | 84.2597° |
| revolutions per day: | 15.20310835 |
| mean anomaly at epoch: | 275.8883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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