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 40271U 26145.42232669 +.00000000 +00000-0 +00000-0 0 00009
2 40271 0.0273 47.3487 0001030 337.6504 275.0005 1.00272912 06
| Epoch (UTC): | 25 May 2026 10:08:09 |
| Eccentricity: | 0.0001030 |
| inclination: | 0.0273° |
| perigee height: | 35782 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 47.3487° |
| argument of perigee: | 337.6504° |
| revolutions per day: | 1.00272912 |
| mean anomaly at epoch: | 275.0005° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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