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 57964U 26144.67367986 +.00000000 +00000-0 +80588-4 0 00006
2 57964 43.0027 267.1959 0001210 261.4749 98.5965 15.27583069 03
| Epoch (UTC): | 24 May 2026 16:10:05 |
| Eccentricity: | 0.0001210 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 267.1959° |
| argument of perigee: | 261.4749° |
| revolutions per day: | 15.27583069 |
| mean anomaly at epoch: | 98.5965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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