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 45062U 26145.63759536 +.00000000 +00000-0 +45150-3 0 00000
2 45062 53.0415 230.0301 0002087 310.0157 50.0677 15.72406445 03
| Epoch (UTC): | 25 May 2026 15:18:08 |
| Eccentricity: | 0.0002087 |
| inclination: | 53.0415° |
| perigee height: | 351 km |
| apogee height: | 353 km |
| right ascension of ascending node: | 230.0301° |
| argument of perigee: | 310.0157° |
| revolutions per day: | 15.72406445 |
| mean anomaly at epoch: | 50.0677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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