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 40267U 26145.61161280 +.00000000 +00000-0 +00000-0 0 00005
2 40267 0.0454 97.0262 0001027 351.0861 155.9126 1.00270499 05
| Epoch (UTC): | 25 May 2026 14:40:43 |
| Eccentricity: | 0.0001027 |
| inclination: | 0.0454° |
| perigee height: | 35783 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 97.0262° |
| argument of perigee: | 351.0861° |
| revolutions per day: | 1.00270499 |
| mean anomaly at epoch: | 155.9126° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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