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 58965U 26145.40989081 +.00000000 +00000-0 +28806-4 0 00001
2 58965 53.1612 300.0362 0001139 95.5245 264.5886 15.30191512 08
| Epoch (UTC): | 25 May 2026 09:50:14 |
| Eccentricity: | 0.0001139 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 300.0362° |
| argument of perigee: | 95.5245° |
| revolutions per day: | 15.30191512 |
| mean anomaly at epoch: | 264.5886° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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