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 26044.82586472 +.00000000 +00000-0 +56679-4 0 00004
2 27386 98.3686 358.9977 0001343 88.0018 299.9675 14.39027861 00
| Epoch (UTC): | 13 February 2026 19:49:14 |
| Eccentricity: | 0.0001343 |
| inclination: | 98.3686° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 358.9977° |
| argument of perigee: | 88.0018° |
| revolutions per day: | 14.39027861 |
| mean anomaly at epoch: | 299.9675° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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