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 31797U 26140.61583258 +.00000000 +00000-0 +43755-3 0 00008
2 31797 98.1018 241.7348 0012259 200.4784 159.5973 15.46453515 07
| Epoch (UTC): | 20 May 2026 14:46:47 |
| Eccentricity: | 0.0012259 |
| inclination: | 98.1018° |
| perigee height: | 419 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 241.7348° |
| argument of perigee: | 200.4784° |
| revolutions per day: | 15.46453515 |
| mean anomaly at epoch: | 159.5973° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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