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 64928U 26144.99341985 +.00000000 +00000-0 +91474-3 0 00005
2 64928 53.1584 351.4224 0000693 60.1344 299.9725 15.30207932 09
| Epoch (UTC): | 24 May 2026 23:50:31 |
| Eccentricity: | 0.0000693 |
| inclination: | 53.1584° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 351.4224° |
| argument of perigee: | 60.1344° |
| revolutions per day: | 15.30207932 |
| mean anomaly at epoch: | 299.9725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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