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 40908U 26145.62758149 +.00000000 +00000-0 +29861-3 0 00003
2 40908 97.4678 181.6224 0006162 351.8472 8.2678 15.50596405 04
| Epoch (UTC): | 25 May 2026 15:03:43 |
| Eccentricity: | 0.0006162 |
| inclination: | 97.4678° |
| perigee height: | 411 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 181.6224° |
| argument of perigee: | 351.8472° |
| revolutions per day: | 15.50596405 |
| mean anomaly at epoch: | 8.2678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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