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 65881U 26145.45254924 +.00000000 +00000-0 +85245-3 0 00001
2 65881 53.1584 297.2390 0001963 81.3691 278.7533 15.34418704 07
| Epoch (UTC): | 25 May 2026 10:51:40 |
| Eccentricity: | 0.0001963 |
| inclination: | 53.1584° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 297.2390° |
| argument of perigee: | 81.3691° |
| revolutions per day: | 15.34418704 |
| mean anomaly at epoch: | 278.7533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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