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 64566U 26145.58048199 +.00000000 +00000-0 +18215-3 0 00002
2 64566 97.7701 259.9638 0002558 53.8392 306.3064 14.93505204 07
| Epoch (UTC): | 25 May 2026 13:55:53 |
| Eccentricity: | 0.0002558 |
| inclination: | 97.7701° |
| perigee height: | 585 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 259.9638° |
| argument of perigee: | 53.8392° |
| revolutions per day: | 14.93505204 |
| mean anomaly at epoch: | 306.3064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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