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 26041.50453292 +.00000000 +00000-0 +62908-4 0 00001
2 27386 98.3681 355.7573 0001327 89.6348 22.1463 14.39026608 06
| Epoch (UTC): | 10 February 2026 12:06:31 |
| Eccentricity: | 0.0001327 |
| inclination: | 98.3681° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 355.7573° |
| argument of perigee: | 89.6348° |
| revolutions per day: | 14.39026608 |
| mean anomaly at epoch: | 22.1463° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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