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 40011U 26145.50825818 +.00000000 +00000-0 +42893-4 0 00004
2 40011 97.5460 331.4270 0024351 24.1679 336.0675 14.88063607 06
| Epoch (UTC): | 25 May 2026 12:11:53 |
| Eccentricity: | 0.0024351 |
| inclination: | 97.5460° |
| perigee height: | 587 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 331.4270° |
| argument of perigee: | 24.1679° |
| revolutions per day: | 14.88063607 |
| mean anomaly at epoch: | 336.0675° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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