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 57341U 26145.56178816 +.00000000 +00000-0 +35956-4 0 00005
2 57341 43.0024 181.6280 0001878 282.9279 77.1363 15.27577253 05
| Epoch (UTC): | 25 May 2026 13:28:58 |
| Eccentricity: | 0.0001878 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 181.6280° |
| argument of perigee: | 282.9279° |
| revolutions per day: | 15.27577253 |
| mean anomaly at epoch: | 77.1363° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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