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 65931U 26145.33523139 +.00000000 +00000-0 +57571-3 0 00002
2 65931 53.1594 169.6114 0001176 86.4344 273.6791 15.30207870 03
| Epoch (UTC): | 25 May 2026 08:02:43 |
| Eccentricity: | 0.0001176 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.6114° |
| argument of perigee: | 86.4344° |
| revolutions per day: | 15.30207870 |
| mean anomaly at epoch: | 273.6791° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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