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 66063U 26145.54890275 +.00000000 +00000-0 +23738-3 0 00008
2 66063 53.1596 248.6387 0000875 106.0661 254.0436 15.30201446 00
| Epoch (UTC): | 25 May 2026 13:10:25 |
| Eccentricity: | 0.0000875 |
| inclination: | 53.1596° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.6387° |
| argument of perigee: | 106.0661° |
| revolutions per day: | 15.30201446 |
| mean anomaly at epoch: | 254.0436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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