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 64922U 26145.55909117 +.00000000 +00000-0 +70034-3 0 00008
2 64922 53.1614 348.5577 0001319 85.3846 274.7305 15.30212445 07
| Epoch (UTC): | 25 May 2026 13:25:05 |
| Eccentricity: | 0.0001319 |
| inclination: | 53.1614° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 348.5577° |
| argument of perigee: | 85.3846° |
| revolutions per day: | 15.30212445 |
| mean anomaly at epoch: | 274.7305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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