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 65928U 26145.48274515 +.00000000 +00000-0 +44662-3 0 00002
2 65928 53.1579 169.1118 0001125 85.8463 274.2666 15.30207714 05
| Epoch (UTC): | 25 May 2026 11:35:09 |
| Eccentricity: | 0.0001125 |
| inclination: | 53.1579° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.1118° |
| argument of perigee: | 85.8463° |
| revolutions per day: | 15.30207714 |
| mean anomaly at epoch: | 274.2666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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