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 57713U 26145.40987154 +.00000000 +00000-0 +15828-4 0 00000
2 57713 43.0018 44.8179 0000846 263.9561 96.1194 15.27578485 06
| Epoch (UTC): | 25 May 2026 09:50:12 |
| Eccentricity: | 0.0000846 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 44.8179° |
| argument of perigee: | 263.9561° |
| revolutions per day: | 15.27578485 |
| mean anomaly at epoch: | 96.1194° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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