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 66061U 26145.56039753 +.00000000 +00000-0 +27318-3 0 00002
2 66061 53.1590 248.0047 0001174 84.2679 275.8456 15.30199058 06
| Epoch (UTC): | 25 May 2026 13:26:58 |
| Eccentricity: | 0.0001174 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.0047° |
| argument of perigee: | 84.2679° |
| revolutions per day: | 15.30199058 |
| mean anomaly at epoch: | 275.8456° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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