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 61727U 26145.28395346 +.00000000 +00000-0 +16695-4 0 00005
2 61727 53.1606 105.5543 0001345 88.7504 271.3651 15.30189226 06
| Epoch (UTC): | 25 May 2026 06:48:53 |
| Eccentricity: | 0.0001345 |
| inclination: | 53.1606° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 105.5543° |
| argument of perigee: | 88.7504° |
| revolutions per day: | 15.30189226 |
| mean anomaly at epoch: | 271.3651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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