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 58495U 26145.58595675 +.00000000 +00000-0 +34938-4 0 00003
2 58495 43.0048 349.6177 0001168 264.8519 95.2199 15.27590433 04
| Epoch (UTC): | 25 May 2026 14:03:46 |
| Eccentricity: | 0.0001168 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 349.6177° |
| argument of perigee: | 264.8519° |
| revolutions per day: | 15.27590433 |
| mean anomaly at epoch: | 95.2199° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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