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 66186U 26145.58152829 +.00000000 +00000-0 +11704-3 0 00004
2 66186 53.1571 248.2873 0000878 56.8169 303.2916 15.30194516 02
| Epoch (UTC): | 25 May 2026 13:57:24 |
| Eccentricity: | 0.0000878 |
| inclination: | 53.1571° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.2873° |
| argument of perigee: | 56.8169° |
| revolutions per day: | 15.30194516 |
| mean anomaly at epoch: | 303.2916° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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