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 00011U 26046.82743911 +.00000000 +00000-0 +29126-3 0 00001
2 00011 32.8631 184.3825 1446325 86.2953 290.1285 11.90231349 06
| Epoch (UTC): | 15 February 2026 19:51:30 |
| Eccentricity: | 0.1446325 |
| inclination: | 32.8631° |
| perigee height: | 553 km |
| apogee height: | 2897 km |
| right ascension of ascending node: | 184.3825° |
| argument of perigee: | 86.2953° |
| revolutions per day: | 11.90231349 |
| mean anomaly at epoch: | 290.1285° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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