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 26037.73942514 +.00000000 +00000-0 +26987-3 0 00002
2 18958 82.5123 281.5330 0003294 328.8673 31.2365 15.17718553 04
| Epoch (UTC): | 06 February 2026 17:44:46 |
| Eccentricity: | 0.0003294 |
| inclination: | 82.5123° |
| perigee height: | 510 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 281.5330° |
| argument of perigee: | 328.8673° |
| revolutions per day: | 15.17718553 |
| mean anomaly at epoch: | 31.2365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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