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 65857U 26145.15001737 +.00000000 +00000-0 +10529-2 0 00005
2 65857 53.1603 298.9151 0000749 66.7622 293.3460 15.34416261 05
| Epoch (UTC): | 25 May 2026 03:36:01 |
| Eccentricity: | 0.0000749 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 298.9151° |
| argument of perigee: | 66.7622° |
| revolutions per day: | 15.34416261 |
| mean anomaly at epoch: | 293.3460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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