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 45711U 26145.58866734 +.00000000 +00000-0 +46114-3 0 00005
2 45711 53.0448 5.3244 0007027 70.8529 289.3246 15.67011893 04
| Epoch (UTC): | 25 May 2026 14:07:40 |
| Eccentricity: | 0.0007027 |
| inclination: | 53.0448° |
| perigee height: | 363 km |
| apogee height: | 372 km |
| right ascension of ascending node: | 5.3244° |
| argument of perigee: | 70.8529° |
| revolutions per day: | 15.67011893 |
| mean anomaly at epoch: | 289.3246° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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