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 66680U 26145.62693264 +.00000000 +00000-0 +26910-3 0 00006
2 66680 97.4210 219.3917 0007546 82.2325 277.9766 15.18913864 07
| Epoch (UTC): | 25 May 2026 15:02:46 |
| Eccentricity: | 0.0007546 |
| inclination: | 97.4210° |
| perigee height: | 504 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 219.3917° |
| argument of perigee: | 82.2325° |
| revolutions per day: | 15.18913864 |
| mean anomaly at epoch: | 277.9766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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