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 57261U 26145.17328578 +.00000000 +00000-0 +14246-4 0 00004
2 57261 43.0031 318.6947 0001753 270.3397 89.7254 15.27576211 01
| Epoch (UTC): | 25 May 2026 04:09:31 |
| Eccentricity: | 0.0001753 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 318.6947° |
| argument of perigee: | 270.3397° |
| revolutions per day: | 15.27576211 |
| mean anomaly at epoch: | 89.7254° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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