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 57849U 26145.66668980 +.00000000 +00000-0 -37380-4 0 00009
2 57849 53.1593 286.6115 0001225 66.9104 271.3750 15.31692415 08
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001225 |
| inclination: | 53.1593° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 286.6115° |
| argument of perigee: | 66.9104° |
| revolutions per day: | 15.31692415 |
| mean anomaly at epoch: | 271.3750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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