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 45746U 26145.26177898 +.00000000 +00000-0 +44021-3 0 00009
2 45746 53.0195 131.3295 0003737 59.1697 300.9682 15.57986244 01
| Epoch (UTC): | 25 May 2026 06:16:57 |
| Eccentricity: | 0.0003737 |
| inclination: | 53.0195° |
| perigee height: | 391 km |
| apogee height: | 396 km |
| right ascension of ascending node: | 131.3295° |
| argument of perigee: | 59.1697° |
| revolutions per day: | 15.57986244 |
| mean anomaly at epoch: | 300.9682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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