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 66855U 26145.34706950 +.00000000 +00000-0 +67823-3 0 00004
2 66855 42.9988 270.1696 0001344 243.3334 116.7380 15.27600470 05
| Epoch (UTC): | 25 May 2026 08:19:46 |
| Eccentricity: | 0.0001344 |
| inclination: | 42.9988° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.1696° |
| argument of perigee: | 243.3334° |
| revolutions per day: | 15.27600470 |
| mean anomaly at epoch: | 116.7380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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