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 58416U 26145.56929729 +.00000000 +00000-0 +19146-3 0 00008
2 58416 43.0026 338.3738 0001372 261.9524 98.1172 15.27587320 06
| Epoch (UTC): | 25 May 2026 13:39:47 |
| Eccentricity: | 0.0001372 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.3738° |
| argument of perigee: | 261.9524° |
| revolutions per day: | 15.27587320 |
| mean anomaly at epoch: | 98.1172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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