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 26038.30809632 +.00000000 +00000-0 +80709-4 0 00007
2 27386 98.3679 352.6390 0001284 91.2246 31.0287 14.39025487 01
| Epoch (UTC): | 07 February 2026 07:23:39 |
| Eccentricity: | 0.0001284 |
| inclination: | 98.3679° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 352.6390° |
| argument of perigee: | 91.2246° |
| revolutions per day: | 14.39025487 |
| mean anomaly at epoch: | 31.0287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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