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 57093U 26144.94716520 +.00000000 +00000-0 +18244-3 0 00000
2 57093 43.0020 25.3976 0001361 237.7436 122.3284 15.27595396 04
| Epoch (UTC): | 24 May 2026 22:43:55 |
| Eccentricity: | 0.0001361 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 25.3976° |
| argument of perigee: | 237.7436° |
| revolutions per day: | 15.27595396 |
| mean anomaly at epoch: | 122.3284° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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