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 65845U 26145.25723848 +.00000000 +00000-0 +88393-3 0 00002
2 65845 53.1606 92.1673 0001211 91.5504 268.5637 15.34402439 00
| Epoch (UTC): | 25 May 2026 06:10:25 |
| Eccentricity: | 0.0001211 |
| inclination: | 53.1606° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 92.1673° |
| argument of perigee: | 91.5504° |
| revolutions per day: | 15.34402439 |
| mean anomaly at epoch: | 268.5637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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