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 57255U 26144.92972600 +.00000000 +00000-0 +44302-4 0 00006
2 57255 43.0017 308.9997 0001440 270.6584 89.4103 15.27579852 03
| Epoch (UTC): | 24 May 2026 22:18:48 |
| Eccentricity: | 0.0001440 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 308.9997° |
| argument of perigee: | 270.6584° |
| revolutions per day: | 15.27579852 |
| mean anomaly at epoch: | 89.4103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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