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 61906U 26145.64391169 +.00000000 +00000-0 +56858-3 0 00007
2 61906 97.4165 226.1599 0010495 115.8659 244.3669 15.36927852 06
| Epoch (UTC): | 25 May 2026 15:27:13 |
| Eccentricity: | 0.0010495 |
| inclination: | 97.4165° |
| perigee height: | 448 km |
| apogee height: | 462 km |
| right ascension of ascending node: | 226.1599° |
| argument of perigee: | 115.8659° |
| revolutions per day: | 15.36927852 |
| mean anomaly at epoch: | 244.3669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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