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 04382U 26133.50066765 +.00000000 +00000-0 +15817-3 0 00005
2 04382 68.4226 132.6227 1030683 11.3906 350.8652 13.14360986 01
| Epoch (UTC): | 13 May 2026 12:00:57 |
| Eccentricity: | 0.1030683 |
| inclination: | 68.4226° |
| perigee height: | 425 km |
| apogee height: | 1988 km |
| right ascension of ascending node: | 132.6227° |
| argument of perigee: | 11.3906° |
| revolutions per day: | 13.14360986 |
| mean anomaly at epoch: | 350.8652° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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