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 66718U 26145.46004524 +.00000000 +00000-0 +26578-3 0 00005
2 66718 97.4224 219.3371 0006010 97.3320 262.8598 15.19269519 03
| Epoch (UTC): | 25 May 2026 11:02:27 |
| Eccentricity: | 0.0006010 |
| inclination: | 97.4224° |
| perigee height: | 504 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 219.3371° |
| argument of perigee: | 97.3320° |
| revolutions per day: | 15.19269519 |
| mean anomaly at epoch: | 262.8598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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