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 58245U 26145.44797249 +.00000000 +00000-0 +10107-3 0 00003
2 58245 43.0050 211.7410 0002069 274.7460 85.3155 15.27576921 03
| Epoch (UTC): | 25 May 2026 10:45:04 |
| Eccentricity: | 0.0002069 |
| inclination: | 43.0050° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.7410° |
| argument of perigee: | 274.7460° |
| revolutions per day: | 15.27576921 |
| mean anomaly at epoch: | 85.3155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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