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 64576U 26145.56955847 +.00000000 +00000-0 +14108-3 0 00005
2 64576 97.7700 260.0874 0002306 72.6910 287.4561 14.91877097 09
| Epoch (UTC): | 25 May 2026 13:40:09 |
| Eccentricity: | 0.0002306 |
| inclination: | 97.7700° |
| perigee height: | 590 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 260.0874° |
| argument of perigee: | 72.6910° |
| revolutions per day: | 14.91877097 |
| mean anomaly at epoch: | 287.4561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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