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 26146.16893858 +.00000000 +00000-0 +00000-0 0 00007
2 40887 4.2905 42.1175 0060015 3.7334 333.7137 1.00272725 04
| Epoch (UTC): | 26 May 2026 04:03:16 |
| Eccentricity: | 0.0060015 |
| inclination: | 4.2905° |
| perigee height: | 35533 km |
| apogee height: | 36039 km |
| right ascension of ascending node: | 42.1175° |
| argument of perigee: | 3.7334° |
| revolutions per day: | 1.00272725 |
| mean anomaly at epoch: | 333.7137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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