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 45731U 26145.58335647 +.00000000 +00000-0 +45240-3 0 00000
2 45731 53.0447 210.7364 0001449 66.9717 288.3922 15.64554210 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001449 |
| inclination: | 53.0447° |
| perigee height: | 374 km |
| apogee height: | 376 km |
| right ascension of ascending node: | 210.7364° |
| argument of perigee: | 66.9717° |
| revolutions per day: | 15.64554210 |
| mean anomaly at epoch: | 288.3922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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