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 26052U 26140.18392916 +.00000000 +00000-0 +00000-0 0 00000
2 26052 11.8626 32.6686 0005665 19.8461 340.5270 0.99108016 08
| Epoch (UTC): | 20 May 2026 04:24:51 |
| Eccentricity: | 0.0005665 |
| inclination: | 11.8626° |
| perigee height: | 36092 km |
| apogee height: | 36140 km |
| right ascension of ascending node: | 32.6686° |
| argument of perigee: | 19.8461° |
| revolutions per day: | 0.99108016 |
| mean anomaly at epoch: | 340.5270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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