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 66782U 26145.46945640 +.00000000 +00000-0 +49543-3 0 00006
2 66782 97.5245 217.1950 0007322 161.2143 198.9352 15.00044507 03
| Epoch (UTC): | 25 May 2026 11:16:01 |
| Eccentricity: | 0.0007322 |
| inclination: | 97.5245° |
| perigee height: | 562 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 217.1950° |
| argument of perigee: | 161.2143° |
| revolutions per day: | 15.00044507 |
| mean anomaly at epoch: | 198.9352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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