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 18958U 26039.58546411 +.00000000 +00000-0 +18741-3 0 00002
2 18958 82.5121 279.7072 0003186 321.2174 38.8831 15.17733025 09
| Epoch (UTC): | 08 February 2026 14:03:04 |
| Eccentricity: | 0.0003186 |
| inclination: | 82.5121° |
| perigee height: | 510 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 279.7072° |
| argument of perigee: | 321.2174° |
| revolutions per day: | 15.17733025 |
| mean anomaly at epoch: | 38.8831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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