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 64756U 26145.56683112 +.00000000 +00000-0 +26613-3 0 00002
2 64756 53.1575 245.5484 0001896 304.2608 55.8214 15.31703087 05
| Epoch (UTC): | 25 May 2026 13:36:14 |
| Eccentricity: | 0.0001896 |
| inclination: | 53.1575° |
| perigee height: | 469 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 245.5484° |
| argument of perigee: | 304.2608° |
| revolutions per day: | 15.31703087 |
| mean anomaly at epoch: | 55.8214° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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