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 58243U 26145.45182266 +.00000000 +00000-0 +13308-4 0 00006
2 58243 43.0017 211.7803 0001426 288.4309 71.6388 15.27582113 06
| Epoch (UTC): | 25 May 2026 10:50:37 |
| Eccentricity: | 0.0001426 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.7803° |
| argument of perigee: | 288.4309° |
| revolutions per day: | 15.27582113 |
| mean anomaly at epoch: | 71.6388° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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