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 58483U 26145.55176255 +.00000000 +00000-0 +12334-2 0 00000
2 58483 42.9988 185.7007 0002594 10.1839 349.9066 15.30164727 03
| Epoch (UTC): | 25 May 2026 13:14:32 |
| Eccentricity: | 0.0002594 |
| inclination: | 42.9988° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 185.7007° |
| argument of perigee: | 10.1839° |
| revolutions per day: | 15.30164727 |
| mean anomaly at epoch: | 349.9066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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