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 40269U 26145.44018183 +.00000000 +00000-0 +00000-0 0 00001
2 40269 6.4602 89.3589 0022497 359.9440 35.2137 1.00272932 08
| Epoch (UTC): | 25 May 2026 10:33:51 |
| Eccentricity: | 0.0022497 |
| inclination: | 6.4602° |
| perigee height: | 35691 km |
| apogee height: | 35881 km |
| right ascension of ascending node: | 89.3589° |
| argument of perigee: | 359.9440° |
| revolutions per day: | 1.00272932 |
| mean anomaly at epoch: | 35.2137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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