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 58080U 26145.30968691 +.00000000 +00000-0 +26643-4 0 00009
2 58080 43.0030 5.1953 0001399 275.0137 85.0554 15.27576338 07
| Epoch (UTC): | 25 May 2026 07:25:56 |
| Eccentricity: | 0.0001399 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 5.1953° |
| argument of perigee: | 275.0137° |
| revolutions per day: | 15.27576338 |
| mean anomaly at epoch: | 85.0554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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