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 40717U 26145.62150438 +.00000000 +00000-0 -12178-5 0 00004
2 40717 97.6600 14.9751 0006373 122.3526 237.8308 14.85702068 08
| Epoch (UTC): | 25 May 2026 14:54:57 |
| Eccentricity: | 0.0006373 |
| inclination: | 97.6600° |
| perigee height: | 607 km |
| apogee height: | 616 km |
| right ascension of ascending node: | 14.9751° |
| argument of perigee: | 122.3526° |
| revolutions per day: | 14.85702068 |
| mean anomaly at epoch: | 237.8308° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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