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 40348U 26144.77218601 +.00000000 +00000-0 +00000-0 0 00001
2 40348 0.0437 329.9798 0002735 91.9997 298.0474 5.00115328 02
| Epoch (UTC): | 24 May 2026 18:31:56 |
| Eccentricity: | 0.0002735 |
| inclination: | 0.0437° |
| perigee height: | 8062 km |
| apogee height: | 8070 km |
| right ascension of ascending node: | 329.9798° |
| argument of perigee: | 91.9997° |
| revolutions per day: | 5.00115328 |
| mean anomaly at epoch: | 298.0474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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