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 57264U 26145.47082343 +.00000000 +00000-0 +32951-4 0 00000
2 57264 43.0016 306.1770 0001113 272.3360 87.7364 15.27567978 05
| Epoch (UTC): | 25 May 2026 11:17:59 |
| Eccentricity: | 0.0001113 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 306.1770° |
| argument of perigee: | 272.3360° |
| revolutions per day: | 15.27567978 |
| mean anomaly at epoch: | 87.7364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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