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 51716U 26145.58169155 +.00000000 +00000-0 +44379-5 0 00003
2 51716 53.2128 343.9393 0001284 94.7691 265.3448 15.08832928 06
| Epoch (UTC): | 25 May 2026 13:57:38 |
| Eccentricity: | 0.0001284 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 343.9393° |
| argument of perigee: | 94.7691° |
| revolutions per day: | 15.08832928 |
| mean anomaly at epoch: | 265.3448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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