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 65505U 26145.36574042 +.00000000 +00000-0 +90929-3 0 00005
2 65505 53.1597 273.8405 0000582 94.9460 265.1610 15.34426283 08
| Epoch (UTC): | 25 May 2026 08:46:39 |
| Eccentricity: | 0.0000582 |
| inclination: | 53.1597° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 273.8405° |
| argument of perigee: | 94.9460° |
| revolutions per day: | 15.34426283 |
| mean anomaly at epoch: | 265.1610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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