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 65849U 26145.54680939 +.00000000 +00000-0 +66940-3 0 00005
2 65849 53.1568 91.8387 0001034 78.3556 281.7560 15.30205933 00
| Epoch (UTC): | 25 May 2026 13:07:24 |
| Eccentricity: | 0.0001034 |
| inclination: | 53.1568° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 91.8387° |
| argument of perigee: | 78.3556° |
| revolutions per day: | 15.30205933 |
| mean anomaly at epoch: | 281.7560° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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