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 46810U 26145.41606409 +.00000000 +00000-0 +18382-3 0 00005
2 46810 34.9977 188.2018 0010608 324.3392 35.6609 15.07007452 09
| Epoch (UTC): | 25 May 2026 09:59:07 |
| Eccentricity: | 0.0010608 |
| inclination: | 34.9977° |
| perigee height: | 538 km |
| apogee height: | 553 km |
| right ascension of ascending node: | 188.2018° |
| argument of perigee: | 324.3392° |
| revolutions per day: | 15.07007452 |
| mean anomaly at epoch: | 35.6609° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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