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 57229U 26145.46180096 +.00000000 +00000-0 +90490-5 0 00007
2 57229 43.0055 317.4238 0001997 278.9005 81.1621 15.27575846 08
| Epoch (UTC): | 25 May 2026 11:04:59 |
| Eccentricity: | 0.0001997 |
| inclination: | 43.0055° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 317.4238° |
| argument of perigee: | 278.9005° |
| revolutions per day: | 15.27575846 |
| mean anomaly at epoch: | 81.1621° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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