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 45461U 26145.61910595 +.00000000 +00000-0 +19227-3 0 00001
2 45461 34.9953 348.0249 0002437 353.2812 6.7863 15.02595561 04
| Epoch (UTC): | 25 May 2026 14:51:30 |
| Eccentricity: | 0.0002437 |
| inclination: | 34.9953° |
| perigee height: | 557 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 348.0249° |
| argument of perigee: | 353.2812° |
| revolutions per day: | 15.02595561 |
| mean anomaly at epoch: | 6.7863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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