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 66685U 26145.14497572 +.00000000 +00000-0 +48511-3 0 00003
2 66685 97.4220 219.4414 0006403 95.6513 264.5454 15.22232556 07
| Epoch (UTC): | 25 May 2026 03:28:45 |
| Eccentricity: | 0.0006403 |
| inclination: | 97.4220° |
| perigee height: | 495 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 219.4414° |
| argument of perigee: | 95.6513° |
| revolutions per day: | 15.22232556 |
| mean anomaly at epoch: | 264.5454° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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