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 26042.09077525 +.00000000 +00000-0 +17208-3 0 00004
2 18958 82.5122 277.2289 0003024 310.3088 49.7881 15.17751572 00
| Epoch (UTC): | 11 February 2026 02:10:42 |
| Eccentricity: | 0.0003024 |
| inclination: | 82.5122° |
| perigee height: | 511 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 277.2289° |
| argument of perigee: | 310.3088° |
| revolutions per day: | 15.17751572 |
| mean anomaly at epoch: | 49.7881° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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