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 66881U 26145.40376985 +.00000000 +00000-0 +56801-3 0 00005
2 66881 53.1613 27.5353 0001592 102.8280 257.2899 15.30206127 02
| Epoch (UTC): | 25 May 2026 09:41:25 |
| Eccentricity: | 0.0001592 |
| inclination: | 53.1613° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 27.5353° |
| argument of perigee: | 102.8280° |
| revolutions per day: | 15.30206127 |
| mean anomaly at epoch: | 257.2899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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