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 27431U 26160.13087008 +.00000000 +00000-0 +63809-4 0 00002
2 27431 98.9520 210.4977 0014303 265.2722 94.6815 14.10223565 01
| Epoch (UTC): | 09 June 2026 03:08:27 |
| Eccentricity: | 0.0014303 |
| inclination: | 98.9520° |
| perigee height: | 848 km |
| apogee height: | 869 km |
| right ascension of ascending node: | 210.4977° |
| argument of perigee: | 265.2722° |
| revolutions per day: | 14.10223565 |
| mean anomaly at epoch: | 94.6815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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