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 57717U 26145.40600757 +.00000000 +00000-0 +14179-3 0 00002
2 57717 43.0021 44.7919 0001370 264.7199 95.3497 15.27586771 08
| Epoch (UTC): | 25 May 2026 09:44:39 |
| Eccentricity: | 0.0001370 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 44.7919° |
| argument of perigee: | 264.7199° |
| revolutions per day: | 15.27586771 |
| mean anomaly at epoch: | 95.3497° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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