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 40350U 26144.21221237 +.00000000 +00000-0 +00000-0 0 00002
2 40350 0.0557 356.8794 0002547 62.1963 300.9485 5.00115963 07
| Epoch (UTC): | 24 May 2026 05:05:35 |
| Eccentricity: | 0.0002547 |
| inclination: | 0.0557° |
| perigee height: | 8062 km |
| apogee height: | 8070 km |
| right ascension of ascending node: | 356.8794° |
| argument of perigee: | 62.1963° |
| revolutions per day: | 5.00115963 |
| mean anomaly at epoch: | 300.9485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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