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 58459U 26145.53865580 +.00000000 +00000-0 +49633-4 0 00001
2 58459 43.0009 327.9303 0001225 269.4831 90.5881 15.27576562 06
| Epoch (UTC): | 25 May 2026 12:55:39 |
| Eccentricity: | 0.0001225 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.9303° |
| argument of perigee: | 269.4831° |
| revolutions per day: | 15.27576562 |
| mean anomaly at epoch: | 90.5881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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