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 40887U 26138.89871228 +.00000000 +00000-0 +00000-0 0 00005
2 40887 4.2765 42.0594 0059774 3.1248 229.9222 1.00271855 04
| Epoch (UTC): | 18 May 2026 21:34:08 |
| Eccentricity: | 0.0059774 |
| inclination: | 4.2765° |
| perigee height: | 35535 km |
| apogee height: | 36039 km |
| right ascension of ascending node: | 42.0594° |
| argument of perigee: | 3.1248° |
| revolutions per day: | 1.00271855 |
| mean anomaly at epoch: | 229.9222° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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