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 27386U 26160.62343707 +.00000000 +00000-0 +40431-4 0 00002
2 27386 98.3831 112.1107 0001330 90.2317 87.7528 14.39063093 07
| Epoch (UTC): | 09 June 2026 14:57:44 |
| Eccentricity: | 0.0001330 |
| inclination: | 98.3831° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 112.1107° |
| argument of perigee: | 90.2317° |
| revolutions per day: | 14.39063093 |
| mean anomaly at epoch: | 87.7528° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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