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 26038.13500639 +.00000000 +00000-0 +25527-3 0 00004
2 18958 82.5122 281.1418 0003270 326.7584 33.3443 15.17722537 05
| Epoch (UTC): | 07 February 2026 03:14:24 |
| Eccentricity: | 0.0003270 |
| inclination: | 82.5122° |
| perigee height: | 510 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 281.1418° |
| argument of perigee: | 326.7584° |
| revolutions per day: | 15.17722537 |
| mean anomaly at epoch: | 33.3443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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