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 66879U 26145.41010169 +.00000000 +00000-0 +55931-3 0 00005
2 66879 53.1602 27.5766 0001338 95.7397 264.3757 15.30201704 00
| Epoch (UTC): | 25 May 2026 09:50:32 |
| Eccentricity: | 0.0001338 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 27.5766° |
| argument of perigee: | 95.7397° |
| revolutions per day: | 15.30201704 |
| mean anomaly at epoch: | 264.3757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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