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 64291U 26145.29916946 +.00000000 +00000-0 +22234-3 0 00005
2 64291 70.0021 1.3141 0002348 274.7031 85.3860 14.98337011 02
| Epoch (UTC): | 25 May 2026 07:10:48 |
| Eccentricity: | 0.0002348 |
| inclination: | 70.0021° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 1.3141° |
| argument of perigee: | 274.7031° |
| revolutions per day: | 14.98337011 |
| mean anomaly at epoch: | 85.3860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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