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 58418U 26145.23595123 +.00000000 +00000-0 +44189-3 0 00006
2 58418 43.0022 340.1813 0000997 262.1682 97.9057 15.27574591 04
| Epoch (UTC): | 25 May 2026 05:39:46 |
| Eccentricity: | 0.0000997 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 340.1813° |
| argument of perigee: | 262.1682° |
| revolutions per day: | 15.27574591 |
| mean anomaly at epoch: | 97.9057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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