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 57228U 26144.88473948 +.00000000 +00000-0 +19407-4 0 00000
2 57228 43.0056 319.9709 0001642 261.6194 98.4471 15.27578455 06
| Epoch (UTC): | 24 May 2026 21:14:01 |
| Eccentricity: | 0.0001642 |
| inclination: | 43.0056° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 319.9709° |
| argument of perigee: | 261.6194° |
| revolutions per day: | 15.27578455 |
| mean anomaly at epoch: | 98.4471° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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