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 26039.71732326 +.00000000 +00000-0 +18875-3 0 00007
2 18958 82.5121 279.5769 0003195 320.9595 39.1408 15.17734313 08
| Epoch (UTC): | 08 February 2026 17:12:56 |
| Eccentricity: | 0.0003195 |
| inclination: | 82.5121° |
| perigee height: | 510 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 279.5769° |
| argument of perigee: | 320.9595° |
| revolutions per day: | 15.17734313 |
| mean anomaly at epoch: | 39.1408° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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