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 51715U 26145.57528770 +.00000000 +00000-0 -22434-5 0 00002
2 51715 53.2106 343.9777 0001455 89.8900 270.2259 15.08839514 08
| Epoch (UTC): | 25 May 2026 13:48:24 |
| Eccentricity: | 0.0001455 |
| inclination: | 53.2106° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 343.9777° |
| argument of perigee: | 89.8900° |
| revolutions per day: | 15.08839514 |
| mean anomaly at epoch: | 270.2259° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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