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 40664U 26144.85515777 +.00000000 +00000-0 +00000-0 0 00005
2 40664 0.0393 113.1161 0002053 322.6663 35.7225 1.00270108 02
| Epoch (UTC): | 24 May 2026 20:31:25 |
| Eccentricity: | 0.0002053 |
| inclination: | 0.0393° |
| perigee height: | 35778 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 113.1161° |
| argument of perigee: | 322.6663° |
| revolutions per day: | 1.00270108 |
| mean anomaly at epoch: | 35.7225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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