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 41382U 26145.49953831 +.00000000 +00000-0 +00000-0 0 00001
2 41382 0.0657 34.7616 0002446 21.8896 301.0747 1.00272819 07
| Epoch (UTC): | 25 May 2026 11:59:20 |
| Eccentricity: | 0.0002446 |
| inclination: | 0.0657° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 34.7616° |
| argument of perigee: | 21.8896° |
| revolutions per day: | 1.00272819 |
| mean anomaly at epoch: | 301.0747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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